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IBIS MAGIC GS-700 FLIGHT MANUAL

1. 02 Date 20 Oct 2011 103 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 WING FLAP SYSTEM FLAP CONTROLS Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 104 144 yy AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC 05 700 SEATS The seating arrangement consists of two separate adjustable seats for the pilot and passenger The pilot s and passenger s seats are available in one design three way adjustable Three way seats may be moved forward or aft to adjust the seat back pull forward on the knob under the center of the seat and apply pressure to the back To return the seat back to the upright position pull forward on the exposed portion of the seat back frame Both seat backs will also fold full forward Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 105 144 PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC 05 700 mmm pid y ux AIRCRAFT S A PILOT AND PASSANGER SEATS SEAT BELT BUCKLE SHOULDER HARNESS ADJUSTABLE LINK Position link just below shoulder level pull link and harness downward to connectto seat belt SEAT BELT SHOULDER HARNESS ADJUSTABLE LINK Position link just below shoulder level pull link and harness downward to connectto seat belt buckle Figure 7 4 seat Belts and Shoulder Harnesses SEAT BELTS AND
2. 9 Gallons CAPACITY EACH LONG RANGE TANKS each WING 9 Gallons NOTE Due to cross feeding between fuel tanks the tanks should be re topped after each refueling to assure maximum capacity Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 140 144 g A AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 LANDING GEAR NOSE WHEEL TIRE PRESSURE 1 7 bar 25 PSI MAIN WHEEL TIRE PRESSURE 1 7 bar 25 PSI NOSE GEAR SHOCK STRUT Note Do not over inflate The Ibis tires should be properly inflated at all times Maintaining the proper inflation will minimize tread wear and aid in ground control of the aircraft When inflating visually check both sides of the tires for bulges cracking of the side wall and cuts WARNING Tire size is important on your IBIS MAGIC GS 700 Use only the specified tire Other sizes will not fit into the wheel and damage the mechanism and aircraft structure BRAKES Hydraulic disk brakes system pilot side with independent master cylinders Dual articulating hydraulic pilot breaks The brakes are independent systems on each of the main gear wheels The fluid reservoir for each is located on the top of the each pedal The toe brakes should depress approximately 1 2 inch before any pressure is generated on the brake when properly serviced Lines should be checked for leaks and chaffing due to rubbing on the tire or the air fram
3. Bs SE AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 TIME FUEL AND DISTANCE TO CLIMB MAXIMUM RATE OF CLIMB Conditions Flaps Up Full Throttle 30 MAP Standard Temperature NOTES 1 Add 0 6 gallon of fuel for engine start taxi and takeoff allowance 2 Propeller adjusted above 500 ft for maximum RPM 3 Increase time fuel and distance by 10 for each 10 degrees above standard temperature 4 Distances shown are based on zero wind DISTANCE MILES 2 2000 0 86 3 3000 1 04 5 4000 1 13 7 5000 1 30 9 6000 1 48 12 7000 1 78 14 8000 1 90 17 9000 2 19 21 10000 2 45 25 11000 2 8 29 12000 3 16 34 Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 81 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 CRUISE PERFORMANCE Conditions 1320 Pounds Recommended prior to takeoff from fields above 50 ft elevations the propeller should be adjusted to give optimum cruise speeds PRESSURE 20 Below ALTITUDE St ndard FT temperature KTS GPH TIME 8000 4800 72 88 5 0 3 3 333 6 9 697 10000 4800 72 90 5 0 3 3 342 6 9 717 8000 4900 73 89 51 3 2 380 6 7 690 10000 4900 73 91 51 3 2 336 6 7 704 8000 5000 75 93 5 3 3 11 333 6 5 696 10000 5000 75 96 5 3 3 11 345 6
4. ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS IF ALTERNATOR INSTALLED Malfunctions in the electrical power supply system can be detected by periodic monitoring of the ammeter and low voltage warning light however the cause of these malfunctions is usually difficult to determine A broken alternator drive belt or wiring is most likely the cause of alternator failures although other factors could cause the problem A damaged or improperly adjusted alternator control unit can also cause malfunctions Problems of this nature constitute an electrical emergency and should be dealt with immediately Electrical power malfunctions usually fall into two categories excessive rate of charge and insufficient rate of charge The paragraphs below describe the recommended remedy for each situation EXCESSIVE RATE OF CHARGE After engine starting and heavy electrical usage at low engine speeds such as extended taxiing the battery condition will be low enough to accept above normal charging during the initial part of a flight However after thirty minutes of cruising Original Issue Date 14January 2011 Revision No 02 Date 20 Oct 2011 Page 47 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 flight the ammeter if installed should be indicating less than two needle widths of charging current If the charging rate were to remain above this value on a long flight the battery would overheat and evaporate the
5. IBIS CUSTOMER CARE PROGRAM Specific benefits and provisions of the IBIS WARRANTY plus other important benefits for you are contained in your CUSTOMER CARE PROGRAM book supplied with your airplane You will want to thoroughly review your Customer Care Program book and keep it in your airplane at all times Coupons attached to the Program book entitle you to an initial inspection and either a Progressive Care Operation No 1 or the first 100 hour inspection If you take delivery from your Dealer the initial inspection will have been performed before delivery of the airplane to you If you pick up your airplane at the factory plan to take it to your Dealer reasonably soon after you take delivery so the Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 132 144 g A AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 initial inspection may be performed allowing the Dealer to make any minor adjustments which may be necessary You will also want to return to your Dealer either at 50 hours for your first Progressive Care Operation or at 100 hours for your first 100 hour inspection depending on which program you choose to establish for your airplane While these important inspections will be performed for you by any IBIS Dealer in most cases you will prefer to have the Dealer from whom you purchased the airplane accomplish this work PILOT CONDUCTED PREVENTIVE MAINTENANCE A certified pilot
6. 3 Fire Extinguisher ACTIVATE if available 4 Land the airplane as soon as possible to inspect for damage WING FIRE 1 Navigation Light Switch if installed OFF 2 Strobe Light Switch if installed OFF 3 Pilot Heat Switch if installed OFF NOTE Perform a side slip to keep the flames away from the fuel tank and cabin and land as soon as possible with flaps retracted Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 40 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 INADVERTENT ICING ENCOUNTER 1 Turn pitot heat switch ON if installed 2 Turn back or change altitude to obtain an outside air temperature that is less conducive to icing 3 Open the throttle to increase engine speed and minimize ice buildup on propeller blades 4 Watch for signs of carburetor air filter ice An unexpected loss in engine speed could be caused by carburetor ice or air intake filter ice 5 Plan a landing at the nearest airport With an extremely rapid ice build up select a suitable off airport landing site 6 With an ice accumulation of 1 4 inch or more on the wing leading edges be prepared for significantly higher stall speed 7 Leave wing flaps retracted With a severe ice build up on the horizontal tail the change in wing wake airflow direction caused by wing flap extension could result in a loss
7. NOTE If disorientation precludes a visual determination of the direction of rotation the symbolic airplane in the turn coordinator IF INSTALLED may be referred to for this information Variations in basic airplane rigging or in weight and balance due to installed equipment or cockpit occupancy can cause differences in behavior particularly in extended spins These differences are normal and will result in variations in the spin characteristics and in the recovery lengths for spins of more than 3 turns However the above recovery procedure should always be used and will result in the most expeditious recovery from any spin Intentional spins with flaps extended are prohibited since the high speeds which may occur during recovery are potentially damaging to flap wing structure LANDING Normal landing approaches can be made with power on or power off Speeds of 52 to 60 Kts with flaps up and 48 to 56 Kts with flaps down Surface winds and air turbulence are usually the primary factors in determining the most comfortable approach speeds Actual touchdown should be made with power off and on the Wheels first The nose wheel should be lowered smoothly to the runway as speed is diminished Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 67 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage SHORT FIELD LANDING For a short field landing in smooth air condi
8. SECURING AIRPLANE 1 Parking Brake SET 2 Radios Electrical Equipment OFF CREDI T CUT OFF pull full out 4 Ignition Switch OFF 5 Master Switch OFF 6 7 INSTALL 8 Fuel Shut Off Valve CLOSE AMPLIFIED PROCEDURES STARTING ENGINE During engine starting close the throttle If the engine is warm no choke will be required In extremely cold temperatures it may be necessary to continue pooling while cranking the engine and after it starts until it is running smoothly The carburetor is not equipped with an accelerator pump and therefore pumping the throttle does not enrich the mixture for starting Weak intermittent firing followed by puffs of black smoke from the exhaust stack indicate over priming or flooding Excess fuel can be cleared from the combustion chambers by the following procedures throttle full open and crank the engine through several revolutions with the starter Repeat the starting procedure without any additional throttle If the engine is under primed most likely in cold weather with a cold engine it will not fire at all and additional throttle will be necessary As soon as the cylinders begin to fire close the throttle slightly to keep it running After starting if the oil gage does not begin to show pressure within
9. 2 EMPENNAGE 1 Rudder Gust Lock REMOVE If installed 2 Tail Tie Down DISCONNECTS 3 Control Surfaces CHECK freedom of movement and security 3 RIGHT WING Trailing Edge 15 m CHECK freedom of movement and security 2 Aileron and flaps Control CHECK surfaces 4 RIGHT WING 1 Wing DISCONNECT 2 Main Wheel Tire CHECK for proper inflation 3 Before first flight of the day and after each refueling use sampler cup and drain small quantity of fuel from fuel tank sump quick drain valve to check for water sediment and proper fuel grade If installed 4 Strut and jury strut 5 Fuel Tank Vent Cover Remove If installed 6 Fuel CHECK VISUALLY for desired level 7 Fuel Filler Cap SECURE 5 NOSE 1 Engine Oil Level CHECK do not operate with less than three quarts For extended flight 2 Before first flight of the day and after each refueling pull out strainer drain knob for about four seconds to clear fuel strainer of possible water and sediment Check strainer drain closed If water is observed the fuel system may contain additional water and further draining of the system at the strainer Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 20
10. AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Landing 4 67 Short Field Landing 4 68 Crosswind Landing 4 68 Balked Landing 4 68 Cold Weather Operation 4 68 Noise Abatement 4 70 Gr gmal issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 51 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage INTRODUCTION Section 4 provides noted checklist and amplified procedures for the conduct of normal operation SPEEDS FOR NORMAL OPERATION Unless otherwise noted the following speeds are based on a maximum weight of 1320 Lb and may be used for any lesser weight Takeoff Normal Climb que eae es 57 52Kts Short Field Takeoff Flaps 10 Speed at 50 47 52Kts Climb Flaps Up Normal T 57 60Kts Best Rate of Climb Sea 57Kts Best Rate of Climb 10 000 53Kts Best Angle of Climb Sea Level thru 10 000 Feet 48Kts Landing Approach Normal Approach Flaps 52 57Kts Normal Approach Flaps 30 48 57Kts Short Field Approach Flaps 30 47Kts Balked Landing Maximum Power Flaps BU ORE Pepe 48Kts Ma
11. MARKING Kts VALUE OR SIGNIFICANCE RANGE White Arc 30 57 Full Flap Operating Range Lower limit is the maximum weight Vso in landing configuration Upper limit is maximum sed permisible with flaps extended Green Arc 57 87 Normal Operating Range Lower limit is maximum weight Vs at most forward C G with flaps retracted Upper limit is maximum structural crusing sed Yellow Arc 87 104 Operation must be conducted with caution and only in smooth air Red Line 113 Maximum speed for all operations POWER PLANT LIMITATIONS Figure 2 2 Airspeed Indicator Markings Engine Manufacturer ROTAX Engine Model Type 912 UL 80HP 912 ULS 100HP Engine Operating Limits for Takeoff and continuous Operations Maximum Power 100 BHP Maximum Engine RPM 5800 RPM Maximum Oil Temperature 130 C 266 Oil Pressure Minimum Maximum Propeller Manufacturer 1 5bar Model Patriotic 0 3 blade Propeller Diameter Maximum 72 inch Minimum 70 inches IVO PROP Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 29 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage POWER PLANT INSTRUMENT MARKINGS RED LINE GREEN ARC RED LINE INSTRUMENT MINIMUM NORMAL MAXIMUM LIMIT OPERATING LIMIT Tachometer 5200 RPM 5500 RPM Oil Temperature 90C 110 C 194 F 130C 266 F 230 F Oil Pressure 1 5 bar
12. Page 35 144 Inadvertent Icing Encounter Lading With a Flat Main Tire Electrical Power supply System Malfunctions Over Voltage Light Eliminates Ammeter Shows Discharge optional AMPLIFIED PROCEDURES Engine Failure Forced Landings Landing without Elevator Control Fires Emergency Operation in Could Vacuum System Failure Executing a 180 Turn in Clouds Emergency Descent through Clouds Recovery from A Spiral Dive Flight in icing Conditions Spins Rough Engine Operation or Loss of Power Carburetor Icing Spark Plug Fouling Magneto Malfunction Low Oil Pressure Electrical Power Supply System Malfunctions Excessive Rate of Charge Insufficient Rate of Charge Original Issue Date 14 January 2011 Revision No 02 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC 05 700 3 41 3 41 3 41 3 41 3 42 3 42 3 43 3 43 3 44 3 44 3 44 3 45 3 45 3 45 3 46 3 46 3 46 3 46 3 47 3 47 3 47 3 47 3 48 Date 20 Oct 2011 Page 36 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage INTRODUCTION Section 3 provides checklist and amplified Procedures for coping with emergencies that may occur Emergencies caused by airplane or engine malfunctions are extremely rare if proper preflight inspections and maintenance are practiced Enrooted weather emergencies can be minimized or eliminated by careful flight planning and good judgment when un
13. This will leave a fuel reserve of 16 5 8 61 7 89 Gallons Once the flight is underway ground speed checks will provide a more accurate basis for estimating the time enrooted and the corresponding fuel required completing the trip with ample reserve LANDING A procedure similar to takeoff should be used for estimating the landing distance at the destination airport Figure 5 8 presents landing distances for various airport altitude and temperature combinations are using the short field technique The distances corresponding to 2000 feet and 86 F 30 are as follows Ground rolls 559 Feet Total distance to clear a 50 feet obstacle 928 Feet A correction for the effect of wind may be made based on Note 2 of the landing chart using the same procedure as outlined for takeoff Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 75 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 AIRSPEED CALIBRATION CONDITIONS Power required for level flight or maximum rated RPM dive FLAPS UP 40 50 60 70 80 90 100 110 120 130 140 5 46 53 60 60 78 88 97 107 117 127 136 KCAS FLAPS 10 40 50 60 70 80 o P KIAS 44 52 61 70 80 P P KCAS FLAPS 30 40 50 60 70 80 o mec Cm KIAS 43 51 61 71 82 KCAS Figure 5 1 Airspeed Calibration NOTE KIAS knots indicated air speed shown on the air speed indicator an
14. corresponding fuel consumption for various altitudes can be determined by using your IBIS information on data in Section 5 NOTE Cruising should be done at 7096 to 75 power until a total of 50 hours has accumulated or oil consumption has stabilized This is to ensure proper seating of the rings and is applicable to new engines and engines in service following cylinder replacement or top overhaul of one or more oylinders Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 63 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 The data in Section 5 shows the increased range and improved fuel economy that is obtainable when operating at lower power settings The use of lower power settings and the selection of cruise altitude on the basis of the most favorable wind conditions are significant factors that should be considered on every trip to reduce fuel consumption 75 POWER 7096 POWER ALTITUDE kts kts Sea Level 82 8000 Feet 84 10000 Feet 87 Standard conditions Zero Wind Figure 4 3 Cruise Performance Table The Cruise Performance Table figure 4 3 shows the true airspeed knot during cruise for various altitudes and percent powers This table should be used as a guide along with the available winds aloft information to determine the most favorable altitude and power setting for a given trip To achieve the recommended fuel
15. 18 C and lower weather the use of an external preheated is recommended whenever possible to reduce wear and abuse to the engine and electrical system Cold weather starting procedures are as follows With Preheat 1 with ignition switch OFF and throttle closed pull the choke as the propeller is being turned over by hand Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 68 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage NOTE Use choke for best result Release ignition switch to BOTH when engine starts Pull choke knob full on after engine has started Leave on until engine is running smoothly 1 Propeller CLEAR 2 Master Switch ON 3 Choke E PULL ON 4 Throttle FULL AFT POSITION 5 Ignition Switoht scene START 6 7 8 Oil Pressure CHECK 9 FULL AFT POSITION Without Preheat 1 Pull Choke Full forward position while the propeller is being turned by hand with the throttle closed 2 Propeller CLEAR 3 Master Switch ON 4 Propeller HIGH RPM A 2 iio EIER IN IDLE POSITION 6 Ignition Switch START 7 Release ignition switch to BOTH when engine sta
16. Fuel and Distance To Climb Figure 5 7 Cruise Performance Figure 5 8 Landing Distance Original Issue Date 14 January 2011 Revision No 02 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Magie Page 5 72 5 72 5 72 5 72 5 73 5 74 5 75 5 76 5 77 5 78 5 79 5 80 5 81 5 82 5 83 Date 20 Oct 2011 Page 71 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage INTRODUCTION Performance data charts on the following pages are presented so that you may know what to expect from the airplane under various conditions and also to facilitate the planning of flights in detail and with reasonable accuracy The data in the charts has been computed from actual flight tests with the airplane and engine in good condition and using average piloting techniques Some indeterminate variables such as mixture leaning if installed technique fuel metering characteristics engine and propeller condition and air turbulence may account for variations of 10 or more in range and endurance Therefore it is important to utilize all available information to estimate the fuel required for the particular flight USE OF PERFORMANCE CHARTS Performance data is presented in tabular or graphical form to illustrate the effect of different variables Sufficiently detailed information is provided in the tables so that conservative values can be selected and used to determine the particula
17. Glide FORCED LANDINGS If all attempts to restart the engine fail and a forced landing is imminent select suitable field and prepare for the landing as discussed under the Emergency Landing without Engine Power checklist Before attempting an off airport landing with engine power available one should fly over the landing area at a safe but low altitude to inspect the terrain for obstructions and surface conditions proceeding as discussed under the Precautionary Landing with Engine Power checklist Prepare for ditching by securing or jettisoning heavy objects located in the baggage area and collect folded coats for protection of occupants face at touchdown Transmit Mayday message on 121 5 MHz giving location and intentions LANDING WITH OUT ELEVATOR CONTROL Trim for horizontal flight with airspeed of approximately 52 Kts and flaps lowered to 20 by using throttle and elevator trim controls Then do not change the elevator trim control setting control the glide angle by adjusting power exclusively At flare out the nose down moment resulting from power reduction is an adverse factor and the airplane may hit on the nose wheel Consequently at flare out the trim control should be set at the full nose up position and the power adjusted so that the Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 43 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Magie airplan
18. Heavy seas INTO THE WIND 4 Light Winds Heavy Swells PARALLEL TO SWELLS 5 Wing flaps ooo oret 30 6 ESTABLISH 300 FT MIN DESCENT 48 Kts 7 Cabin Doors UNLATCH 8 Touchdown LEVEL ATTITUDE AT 300 FT MIN DESCENT 9 CUSHION at touchdown with folded coat 10 EVACUATE through cabin doors If necessary open windows and flood cabin to equalize pressure so doors can be opened 11 Life vests and raft INFLATE FIRES DURING START ON GROUND o decane ce rona CONTINUE to get a start which would suck the flames and accumulated fuel through the carburetor and into the engines If engine starts 1 1700 RPM for a few minutes 2 ENON esenee SHUTDOWN and inspect for damage If engine fail to start 1 Cranking CONTINUE in an effort to obtain a start 2 Fire Extinguisher OBTAIN have ground attendants obtain in not installed d ENJINS SECURE a Master Switch OFF b Ignition Switch OFF Fuel Shutoff Valve OFF 4 EXTINGUISH using fire extinguisher wool Intentionally in blanket or dirt 5 Fire INSPECT repair damage or replace damaged components or wiring before conducting another flight ENGINE FIRE E
19. Keep hands off control wheel 4 Monitor turn coordinator and make corrections by rudder alone 5 Check trend of compass card movement and make cautious corrections with rudder to stop turn 6 Upon breaking out of clouds resume normal cruising flight RECOVERY FROM A SPIRAL DIVE If a spiral is encountered proceed as follows 1 Close the throttle 2 Stop the turn by using coordinated aileron and rudder control to align the symbolic airplane in the turn coordinator if installed with the horizon reference line 3 Cautiously apply elevator back pressure to slowly reduce the airspeed to 60Kts 4 Adjust the elevator trim control to maintain at 60 Kts glide 5 Keep hands off the control wheel using rudder control to hold a straight heading 6 Clear engine occasionally but avoid using enough power to disturb the trimmed glide 7 Upon breaking out of clouds resume normal cruising flight FLIGHT IN ICING CONDITIONS Flight into icing conditions is prohibited An inadvertent encounter with these conditions can best be handled using the checklist procedures The best procedure of course is to turn back or change altitude to escape icing conditions Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 45 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage SPINS Should an inadvertent spin occur the following recovery procedure should be used 1 PLACE AILERON
20. Revision No 02 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 7 108 7 108 7 109 7 109 7 109 7 110 7 110 7 111 7 111 7 111 7 111 7 112 7 112 7 115 7 115 7 115 7 118 7 118 Date 20 Oct 2011 94 144 Circuit Breakers Fuses Ground Service Plug Receptacle Optional Lighting Systems Exterior Lighting Cabin Ventilating Pitot Static System and Instruments Airspeed Indicator Rate Of Climb Indicator Altimeter Vacuum System and Instruments Attitude Indicator Directional Indicator Original Issue Date 14 January 2011 Revision No 02 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 7 118 7 119 7 119 7 119 7 120 7 122 7 122 7 122 7 123 7 123 7 123 7 123 Date 20 Oct 2011 95 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 INTRODUCTION This section provides description and operation of the airplane and its systems Some equipment described herein is optional and may not be installed in the airplane AIRFRAME The airplane is an all metal two place high wing single engine airplane equipped with tricycle landing gear and is designed for general utility purposes The construction of the fuselage is a conventional formed sheet metal bulkhead stringer and skin design referred to as semi monocoque Ma
21. Revision No 02 Page 2 28 2 28 2 29 2 29 2 30 2 30 2 30 2 31 2 31 2 31 2 32 2 33 Date 20 Oct 2011 Page 27 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage INTRODUCTION Section 2 includes Limitations instrument markings and basic placards necessary for the safe operation of the airplane its engine standard systems and standard equipment The limitations included in this section have been approved by the manufacturer AIRSPEED LIMITATION Kts Kts IAS CAS REMARKS SPEEED Do not exceed this speed in any VNE Never Exceed Speed 113 108 operation Do not exceed this speed except AONO ee 100 95 in smooth air and then only with Cruising Speed caution VH Maximum 104 99 Maximum speed in level flight at speed max continuous power MSL Do not make full or abrupt control Maneuvering speed 74 70 movements above this speed 1320Lb S LSA Maximum Flap 57 52 Do not exceed this speed with VFE Extended speed flaps down VSO Stall speed with flaps 30 26 Minimum speed VS Stall speed No flaps 42 36 Minimum speed Figure 2 1 Airspeed Limitations Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 28 144 y 4 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC 05 700 AIRSPEED INDICATOR MARKINGS
22. SET If installed 2 Cabin CLOSED and LATCHED 3 Flight Controls ret Re FREE and CORRECT 4 Wing Flap eret e 10 5 Flight Instruments SET 6 Auxiliary Fuel ON 7 Fuel ON OFF ON 8 Elevator cerent perro etta TAKE OFF 9 TOS 3000 RPM a CHECK RPM drop should not exceed 125 on either magneto or 50 RPM differential between magnetos b Engine Instruments and Ammeter CHECK cc EIE SET 11 Flashing Beacon landing lights Navigation Lights and or Strobe Lights ON as required 12 Throttle Friction Lock ADJUST If installed Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 56 144 AIRCRAFT S A TAKEOFF NORMAL TAKEOFF Wing ux ede me naive Elevator Control Climb Speed Propeller After 2 Auxiliary Fuel Pump 5 SHORT FIELD TAKEOFF Wing Flaps Fue
23. aft cabin bulkhead Access to the baggage compartment is gained from within the airplane cabin baggage net with four tie down straps is provided for securing baggage and is attached by tying the strop to tie down rings provide in the airplane when loading airplane children should not be placed or permitted in the baggage compartment and any material that might be hazardous to the airplane or occupants should not be placed anywhere in the airplane For baggage area dimensions refer to Section 6 Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 99 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 AILERON CONTROL SYSTEM AILERON CONTROLS Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 100 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 RUDDER CONTROL SYSTEM RUDDER CONTROLS Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 101 144 yy AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC 05 700 ELEVATOR TRIM CONTROL SYSTEM TRIM CONTROLS Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 102 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 ELEVATOR CONTROL SYSTEM ELEVATOR CONTROLS 7 4 Original Issue Date 14 January 2011
24. airplane flight attitude is changed Stall speeds for various combinations of flap setting and bank angle are summarized in Section 5 SPINS Intentional spins are approved in this airplane see Section 2 Before attempting to perform spins however several Items should be carefully considered to assure a safe flight No spins should be attempted without first having received dual instruction in both spin entries and spin recoveries from a qualified instructor who is familiar with the spin characteristics of the IBIS MAGIC GS 700 The cabin should be clean and all loose equipment including the microphone should be stowed For a solo flight in which spins will be conducted the copilot s seat belt and shoulder harness should be secured Spins with baggage loadings is not approved The seat belts and shoulder harnesses should be adjusted to provide proper restraint during all anticipated flight conditions However care should be taken to Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 65 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 ensure that the pilot can easily reach the flight controls and produce maximum control travels It is recommended that where feasible entries be accomplished at high enough altitude that recoveries are completed 4000 feet Or more above ground level At least 1000 feet of altitude loss should be allowed for a 1 turn spin and recover
25. and indicates engine speed An hour meter below the center of the tachometer dial records elapsed engine time in hours and tenths Instrument markings include a normal operating range green arc of 2200 to 5800 RPM and a maximum red line of 5800 RPM NEW ENGINE BREAK IN AND OPERATION The engine underwent a run in at the factory and is ready for the full range of use It is however suggested that cruising be accomplished at 6596 to 7596 power until a Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 109 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 total of 50 hours has accumulated or oil consumption has stabilized This will ensure proper seating of the rings The airplane is delivered from the factory with oil in the engine At the first 5 hours oil must be replaced See Rotax Manual ENGINE OIL SYSTEM Oil for engine lubrication is supplied from a sump on the bottom of the engine The capacity of the engine sump is three Oil is drawn from the sump through an oil suction strainer screen into the engine driven oil pump From the pump oil is routed to a bypass valve If the oil is cold the bypass valve allows the oil to bypass the oil cooler and go directly from the pump to the oil pressure screen full flow oil filter if installed If the oil is hot the bypass valves routes the oil cooler on the front side of the left forward engine baffle Pre
26. and park areas and other noise sensitive areas should make every effort to fly not less than 2000 feet above the surface weather permitting even though flight at a lower level may be consistent with the provisions of government regulations 2 During departure from or approach to an airport climb after takeoff and descent for landing should be made so as to avoid prolonged flight at low altitude near noise sensitive areas NOTE The above recommended procedures do not apply where they would conflict with Air Traffic Control clearances or instructions or where in the pilot s judgment an altitude of less than 2000 feet is necessary for him to adequately exercise his duty to see and avoid other aircraft The certificated noise level for the Model MAGIC GS 700 at 1320 Lb maximum weight is 18 0dB A No determination has been made by the Federal Aviation Administration that the noise level of this airplane are or should be acceptable or unacceptable for operation at into or out of any airport Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 70 144 SECTION 5 TABLE CONTENTS Introduction Use of Performance Charts Sample Problem Takeoff Cruise Fuel Required Landing Figure 5 1 Airspeed Calibration Figure 5 2 Temperature Conversion Chart Figure 5 3 Stall Speeds Figure 5 4 Takeoff Distance Figure 5 5 Rate of Climb Maximum Figure 5 6 Time
27. between the main wheel centers Repeat on right side and average the measurements 5 Using weights from item 3 and measurements from item 4 the airplane weight and C G can be determined Basic Empty Weight may be determined by completing figure 6 1 Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 86 144 Bs ETA AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 WEIGTH AND BALANCE CALCULATION PROCEDURE Note Reference Datum Wing leading edge Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 87 144 04 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Magi DESCRIPTION 1 Determine weight distribution on the wheels of the empty aircraft W1 W2 y W3 2 Determine weight of the W items W4 W5 W6 W7 y W8 3 Measure distance between DATUM and Center of Gravity of the W items arm 4 Fill the table and make sure that CG is between 10 59 inch and 18 54 inch AFT of the DATUM mew vesorienion I Kg mm Kg x mm W2 W3 550 00 Piot 80 00 44 000 00 30 00 1 205 00 36 150 00 wa Reservor Fuel Tank 2GL 5 140 1 054 10 5 418 07 TOTAL GROSS WEIGHT 569 32 246 505 07 Tota Moment 246 505 07 ver Weight 569 32 sin 432 98 mm AFT from DATUM This aircraft is between permitted range Wing Chord 2602 20 1346 MM 432 98 471 1 Figure
28. data and information of general interest It also contains definitions or explanations of symbols abbreviations and terminology commonly used THREE VIEW DRAWING 44 1 12m 6 2 1 9m r Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 18 144 B zz AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 SIDE VIEW 47 5 1 21m 82 5 2 1m TOP VIEW 55 1 046m 511 1805 Sonico 28 8 55 Figure 1 1 Three View Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 19 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage DESCRIPTIVE DATA WING Wing span 8 55m 28 Wing chord 1 346 53 Wing surface 11 34m 122ff Aspect ratio 6 446 Taper ratio 0 718 Wing loading 10 82lb ft FUSELAGE Overall length 6 850m 22 6 Overall width 1 051m 41 3 Overall height 2 180m 7 27 EMPENNAGE Stabilator span 2 500m 8 2 Vertical tail span 1 279m 50 3 LANDING GEAR Wheel track 1 900m 6 27 Main gear train 5 00 5 CONTROL SURFACES TRAVEL LIMITS Ailerons Up 20 down 15 Flaps 0 42 Rudder RH 25 LH 25 Elevator Up 30 down 25 ENGINE Number of engines 1 Engine Manufacturer ROTAX Engine Model Number 912 UL 912ULS Engine Type Normally aspirated direct drive air cooled w
29. expressed in knots Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 76 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 TEMPERATURE CONVERSION CHART Temperature Degrees Celsius Temperature Degrees Fahrenheit Figure 5 2 Temperature Conversion Chart CONDITIONS Power Off NOTE KIAS values are approximate and are based on airspeed calibration data with power off Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 77 144 wem 4 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 MOST REARWARD CENTER OF GRAVITY GROSS FLAP ANGLE OF BANK WEIGHT sETTING o gt fo Je MPH IAS MPH IAS MPH IAS MPH IAS 1320 Lb 41 44 48 58 41 52 48 58 35 50 42 50 MOST FORWARD CENTER OF GRAVITY GROSS FLAP WEIGHT SETTING ANGLE OF BANK MPH IAS MPH IAS MPH IAS MPH IAS 1320 Lb 45 48 55 65 46 49 55 65 40 43 47 56 Figure 5 3 Stall Speeds Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 78 144 wm mum AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 TAKE OFF DISTANCE SHORT FIELD CONDITIONS Flaps 10 Full Throttle MAP 30 P
30. handbook Subsequent changes will be made in the form of stickers These should examine and attached to the appropriate page in the handbook immediately after receipt the handbook should not be used for operational purposes until it has been updated to a current status Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 16 144 SECTION 1 GENERAL TABLE OF CONTENTS Introduction Three View Drawing Descriptive Data Engine Propeller Fuel Maximum Certificated Weights Standard Airplane Weights Specific Loadings Symbols Abbreviations And Terminology Original Issue Date 14 January 2011 Revision No 02 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 1 20 1 20 1 21 1 21 1621 1 22 1 23 1 23 1 23 Date 20 Oct 2011 Page 17 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage INTRODUCTION The Magic GS 700 is a two seater high performance aircraft with tapered planform a tricycle gear with controllable nose wheel It presents essential features such as high wing built mainly in metal using aircraft aeronautical aluminum chromium molybdenum alloy and composites designed and developed by IBIS AIRCRAFT This handbook contains 9 sections and includes the material required to be furnished to the pilot It also contains supplemental data supplied IBIS Aircraft S A Section 1 provides basic
31. is the amount of fuel in gallons consumed per hour KPL Kilometers per Liter is the distance in kilometers which can be expected per liter of fuel consumed at a specific engine power setting and or flight configuration G G is acceleration due to gravity WEIGHT AND BALANCE TERMINOLOGY Reference Reference Datum is an imaginary vertical plane from which datum all horizontal distances are measured for balance purposes Station Station is a location along the airplane fuselage given in terms of the distance from the reference datum Arm Arm is the horizontal distance from the reference datum to the center of gravity C G of an item Moment Moment is the product of the weight of an item multiplied by its arm Moment divided by the constant 1000 is used in this handbook to simplify balance calculation by reducing the number of digits Center of Center of Gravity is the point at which an airplane or equipment would Gravity balance if suspended Its distance from the reference datum is found by C G dividing the total moment by the total weight of the airplane C G Arm Center of Gravity Arm is the arm obtained by adding the airplane s Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 25 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage Individual moments and dividing the sum by the total weight C G Limits Center of Gravity Limits are the ext
32. necessary and about other seasonal and periodic services IDENTIFICATION PLATE All correspondence regarding your airplane should include the SERIAL NUMBER The Serial Number Model Number Production Certificate Number PC and Type Certificate Number TC can be found on the Identification Plate located on the left rear of the fuselage e CUSTOMER CARE PROGRAM BOOK e PILOT S OPERATING HANDBOOK SUPPLEMENTS FOR YOUR AIRPLANE e PILOT S CHECKLISTS SALES AND SERVICE DEALER DIRECTORY The following additional publications plus many other supplies that are applicable to your airplane are available from your IBIS Dealer e SERVICE MANUALS AND PARTS CATALOGS FOR YOUR AIRPLANE Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 129 144 g A AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 ENGINE AND ACCESSORIES Your IBIS Dealer has a Customer Care Supplies Catalog covering all available Items many of which he keeps on hand He will be happy to place an order for any item which is not in stock AIRPLANE FILE There are miscellaneous data information and licenses that are a part of the airplane file The following is a checklist for that file In addition a periodic check should be made of the latest Federal Aviation Regulations to ensure that all data requirements are met A To be displayed in the airplane at all times 1 Aircraft Airworthiness Certificate FAA fo
33. of elevator effectiveness 8 Open left window and if practical scrape ice from a portion of the windshield for visibility in the landing approach 9 Perform a landing approach using a forward slip if necessary for improved visibility 10 Approach at 57 to 65 Knots PH depending upon the amount of ice accumulation 11 Perform a landing in level attitude LANDING WITH A FLAT MAIN TIRE 1 Wing Flaps iie attt ias AS DESIRED 2 Approach NORMAL 3 GOOD FIRST hold airplane off flat tire as long as Possible with aileron control ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS OVER VOLTAGE LIGHT ILLUMINATES IF INSTALLED 1 Master Switch OFF both sides 2 Master Switch ON 3 Over Voltage Light OFF Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 41 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage If over voltage light illuminates again 4 as soon as practical AMMETER SHOWS DISCHARGE 12 M OFF 2 Nonessential Electrical Equipment OFF E A as soon as practical AMPLIFIED PROCEDURES ENGINE FAILURE If an engine failure occurs during the takeoff run the most important thing to do is stop th
34. of normal operation Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 48 144 SECTION 4 CHECKLIST PROCEDURES TABLE OF CONTENTS Introduction Preflight Inspection Empennage Right Wing trailing edge Right wing Nose Left wing Left wing Leading Edge Left wing trailing Edge Before Starting engine Starting engine Before Takeoff Takeoff Normal Takeoff Short Field Takeoff Enroute Climb Cruise Before Landing Landing Original Issue Date 14 January 2011 Revision No 02 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 4 52 4 54 4 54 4 54 4 54 4 54 4 55 4 55 4 55 4 55 4 56 4 56 4 57 4 57 4 57 4 57 4 58 4 58 4 58 Date 20 Oct 2011 Page 49 144 Normal Landing Short Field Landing Balked Landing After Landing Securing Airplane Amplified procedures Starting Engine Taxiing Before Takeoff Warm Up Magneto Check Alternator Check optional Takeoff Power Check Wing flap Settings Enroute Climb Cruise Fuel Saving Procedures for Flight Training Operations Stalls Spins Original Issue Date 14 January 2011 Revision No 02 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 4 58 4 58 4 58 4 59 4 59 4 59 4 59 4 60 4 61 4 61 4 61 4 62 4 62 4 62 4 62 4 63 4 63 4 65 4 65 Date 20 Oct 2011 Page 50 144 B
35. other areas of Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 111 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 the engine by baffling and is then exhausted through an opening at the bottom aft edge of the cowling No manual cooling system control is provided PROPELLER The airplane is equipped with a three bladed electric controller pitch propeller the propeller is 70 72 inches in diameter FUEL SYSTEM The airplane may be equipped with either a standard fuel system or long range system see figure 7 6 both systems consist of two vented fuel tanks two in each wing a fuel shutoff valve fuel strainer manual choke and carburetor Refer to figure 7 5 for fuel quantity data for both systems FUEL QUANTITY DATA U S GALLONS TOTAL USABLE FUEL TOTAL TOTAL FUEL TANKS ALL FLIGHT CONDITION UNUSABLE FUEL VOLUME STANDARD 18 5 Gallons 1 5 20 9 us Gallons each wing and Reserve tank LONG RANGE 18 Gallons 0 18 9 us Gallons each wing Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 112 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 FUEL QUANTITY DATA GRAPH RESERVOIR FUEL TANK m i d CARBURETOR Qg FUEL SHUTOFF p VALVE TO ENGINE 0 THROTTLE CYLINDERS 05 CHOKE NOTE Due to cross feeding between fuel tank
36. raised tilting the jack The jack must then be lowered for a second jacking operation Do not jack both main wheels simultaneously using the individual main gear jack pads If nose gear maintenance is required the nose wheel may be raised off the ground by pressing down on a tail cone bulkhead just forward of the horizontal stabilizer and allowing the tail to rest on the tail tie down ring Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 135 144 EXT AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 NOTE Do not apply pressure on the elevator or outboard stabilizer surfaces When pushing on the tail cone always apply pressure at a bulkhead to avoid buckling the skin To assist in raising and holding the nose wheel off the ground weight down the tail by placing sand bags or suitable weight on each side of the horizontal stabilizer next to the fuselage If ground anchors are available the tail should be securely tied down NOTE Ensure that the nose will be held off the ground under all conditions by means of suitable stands or supports underweight supporting bulkheads near the nose of the airplane FLYABLE STORAGE The aircraft is to be put flyable storage airplanes placed in non operational storage for a maximum of 30 days or those which receive only intermittent operational use for the first 25 hours are considered in flyable stora
37. 0 47 1000 542 900 547 908 550 913 554 920 559 928 2000 546 906 550 913 555 921 559 928 563 935 3000 550 913 555 921 560 930 565 938 568 943 4000 554 920 558 927 563 935 568 943 573 952 5000 558 926 562 933 566 940 571 948 578 960 6000 562 933 566 940 570 946 575 953 584 970 7000 566 940 570 946 574 952 579 961 590 980 8000 570 946 575 955 580 963 585 971 595 988 Figure 5 8 Landing Distance Revision No 02 Original Issue Date 14 January 2011 Date 20 Oct 2011 Page 83 144 Bs SE AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 SECTION 6 WEIGHT amp BALANCE EQUIPMENT LIST TABLE OF CONTENTS Page Introduction 6 85 Airplane Weighing Procedures 6 85 Weight and Balance 6 87 Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 84 144 Bs SE AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 INTRODUCTION This section describes the procedure for establishing the basic empty weight and moment of the airplane Sample forms are provided for reference Procedures for calculating the weight and moment for various operations are also provided A comprehensive list of all IBIS equipment available for this airplane is including at the back of this section It should be noted that specific information regarding the weight arm moment and installed equipment l
38. 11 Page 54 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 fuel tank sumps and fuel line drain plug will be necessary 3 Propeller and Spinner CHECK for nicks and security 4 Carburetor Air Filter CHECK for restrictions by dust or other foreign matter 5 Landing Light s CHECK for condition and cleanliness If installed 6 Nose Wheel fairing and Tire CHECK for proper inflation 7 Nose Tie Down DISCONNECT 8 Static Source Opening in if stalled left side of fuselage 9 CHECK for stoppage If installed 6 LEFT WING 1 Main Wheel Tire CHECK for proper inflation 2 Before first flight of day and after each refueling use sampler cup and drain small quantity of fuel from fuel tank sump quick drain valve to check for water sediment and proper fuel grade If installed 3 Fuel Quantity CHECKS VISUALLY for desired level 4 Fuel Filler SECURES 5 Strut and Jury Strut 6 Fuel Tank Vent Cover Remove If installed 7 Wing Tie Down DISCONNECTS 7 LEFT WING Leading Edge 1 Pitot tube REMOVE and check opening for stoppage 2 Stall Warning Opening if installed CHECK for stoppage To check the system place a clean handkerchief over the v
39. 2 5 bar 7bar Water Temperature 80 C 100 C 176 F 110 C 230 F CHT 212 F 135 275 F EGT 880 1616 F 880C 1616 F Figure 2 3 Power Plant Instrument Markings SEE ROTAX MANUAL WEIGHT LIMITS Maximum Takeoff Weight 1320 Lb Maximum Landing Weight 1320 Lb Maximum Weight in Compartment 50 Lb CENTER OF GRAVITY LIMITS Center of Gravity Limits range Forward 10 59 inches aft of datum 269mm Aft 18 54 inches aft of datum 471 mm Reference Datum wing leading edge SERVICE CEILING 12000 Feet 3657 m Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 30 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage MANEUVER LIMITS This airplane is certificated in the utility category and is designed limited aerobatic flight In the acquisition of various certificates such as commercial pilot instrument pilot and flight instructor certain maneuvers are required All of these maneuvers are permitted in this airplane No aerobatic maneuvers are approved except listed below MANEUVER MAXIMUM ENTRY SPEED cm es 74 Kts Lazy Eights ea E R 74 Kts Steep 74 Kts Sn mM M Use Slow Deceleration Stalls Except Whip Use Slow Deceleration Highe
40. 30 seconds in the summertime and about twice that long in very cold weather stop engine and investigate Lack of oil pressure can cause serious engine damage Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 59 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Additional details concerning cold weather starting and operation may be found under COLD WEATHER OPERATION paragraphs in this section TAXIING When taxiing it is important that speed and use of brakes be held to a minimum and that all controls be utilized see Taxiing Diagram figure 4 2 to maintain directional control and balance Figure 4 2 Taxiing Diagram Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 60 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage Taxiing over loose gravel or cinders should be done at low engine speed to avoid abrasion and stone damage to the propeller tips The nose wheel is designed to automatically center straight ahead when the nose strut is fully extended In the event the nose strut is over inflated and the airplane is loaded to a rearward center of gravity position it may be necessary to partially compress the strut to permit steering This can be accomplished prior to taxiing by depressing the airplane nose by hand or during taxi by sharply applying brakes BEFORE TAKE
41. 4 g A AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 ENGINE CONTROLS Engine power is controlled by a throttle located on the lower center portion of the instrument panel The throttle operates in a conventional manner in the full forward position the throttle is open and in the full aft position it is closed ENGINE INSTRUMENTS Engine operation is monitored by the following instruments oil pressure gauge oil temperature gauge tachometer water temperature gauge and EGT The oil pressure gage located on the right side off subpanel is operated by oil pressure A direct pressure oil line from the engine delivers oil at engine operating pressure to the oil pressure gauge Gauge markings indicate that minimum idling pressure is 1 5 bar 22 PSI red line the normal operating range is 1 9 to 6 4 bar 27 93 PSI green arc and maximum pressure is 6 9 bar 100 PSI red line Oil temperature is indicated by a gauge located on the right side of subpanel The gage is operated by an electrical resistance type temperature sensor which receives power from the airplane electrical system Oil temperature limitations are the normal operating range green arc which is 90 C to 194 F to 230 F 110 C and the maximum red line which is 266 F 130 C The engine driven electrical tachometer is located near the upper right portion of the instrument panel The instrument is calibrated in increments of 100 RPM
42. 5 722 8000 5100 76 94 54 3 05 330 6 38 690 10000 5100 76 97 54 3 05 336 6 38 719 80000 5200 78 95 5 5 3 0 327 6 27 684 10000 5200 78 98 5 5 3 0 339 6 27 709 80000 5300 80 96 5 6 2 94 324 6 16 678 10000 5300 80 99 56 2 94 335 6 16 702 80000 5400 81 96 5 7 2 89 321 6 05 672 10000 5400 81 100 57 2 89 332 6 05 696 8000 5500 82 97 6 0 2 75 308 5 75 644 10000 5500 82 101 6 0 2 75 319 5 75 667 Figure 5 7 Cruise Performance Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 82 144 AIRCRAFT S A LANDING DISTANCE SHORT FIELD Conditions PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Flaps 30 Power Off Maximum Braking Paved Level Dry Runway Zero Wind NOTES 1 Decrease distances 10 for each 9 knots Head wind For operation with tail winds up to 10 knots Increase distances by 10 for each 2 knots 2 For operation on a dry grass runway increase distances by 45 of the ground roll figure WT SPEED PRESS 0 10 20 30 40 TO TO TO TO TO Lb AT43 ALT FT CLEAR GRND CLEAR GRND ad CLEAR GRND CLEAR KTS RUN 50 5 RUN 50 5 RUN OBS RUN 50 5 RUN 50 OBS FT FT FT FT S L 536 890 539 895 544 903 549 911 554 920 132
43. 6 1 Sample Airplane Weighing Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 88 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 WEIGHT AND BALANCE The following information will enable you to operate your IBIS MAGIC GS 700 within the prescribed weight and center of gravity limitations To figure weight and balance use the Sample Problem Loading Graph and Center of Gravity Moment Envelope as follows Take the basic empty weight and moment from appropriate weight and balance records carried in your airplane and enter them in the column titled YOUR AIRPLANE on the Sample Loading Problem NOTE In addition to the basic empty weight and moment noted on these records the C G arm fuselage station is also shown but need not be used on the Sample Loading Problem The moment which is shown must divided by 1000 and this value used as the moment 1000 on the loading problem Use the Loading Graph to determine the moment 1000 for each additional item to be carried then list these on the loading problem NOTE Loading Graph information for the pilot passengers and baggage is based on seats positioned for average occupants and baggage loaded in the center of the baggage areas as shown on the Loading Arrangements diagram For loadings which may differ from these the Sample Loading Problem lists fuselage stations for these items to indicate their forward and aft rang
44. A AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 After the first 25 hours of operation drain engine oil sump and oil cooler and clean the oil pressure screen If an oil filter is installed change filter at this time Refill sump with straight mineral oil and use until a total of 50 hours has accumulated or oil consumption has stabilized then changes to dispersant oil On airplanes which have an oil filter the oil change interval may be extended to 100 hour intervals providing the oil filter is changed at 100 hour intervals Change engine oil at least every 6 months even though less than the recommended hours have accumulated Reduce intervals for pro longed operation in dusty areas cold climates or when short flights and long idle periods result in slugging conditions FUEL SERVICING The ibis fuel requirements are dependent on the engine installed the engine manual should be cheeked for the recommended grade In any case the fuel should be clean and water free the firewall gas collector should be checked on preflight inspection four evidence of water and the filter checked four solid foreign materials It is a practice to leave the tanks full to minimize the amount of combustible fuel air vapor present in the tanks this also helps minimize the amount of water vapor in the fuel system FUEL APPROVED FUEL GRADES 94 Grade Fuel 100 Formerly 100 130 Grade Aviation Fuel CAPACITY EACH STANDARD TANKS each WING
45. ART if propeller is stopped FORCED LANDINGS EMERGENCY LANDING WITHOUT ENGINE POWER 1 Airspeed 57 Kts flaps up 52 Kts flaps down 2 Fuel Shutoff Valve OFF Ignition Switch OFF 4 Wing Flaps AS REQUIRED 30 recommended 5 Master Switch OFF 6 UNLATCH PRIOR TO TOUCHDOWN 7 Touchdown SLIGHTLY TAIL LOW 8 APPLY HEAVILY 1 Airspeed 52 Kts 2 Wing 1 5 20 3 Selected Field FLY OVER noting terrain and obstructions then retract flaps upon reaching a safe altitude and airspeed 4 Radio and Electrical Switches OFF 5 Wing Flaps 30 on final approach 6 Airspeed 48 Kts 7 Master Switch OFF 8 UNLATCH PRIOR TO TOUCHDOWN 9 Touchdown SLIGHTLY TAIL LOW 10 Ignition Switches OFF 11 APPLY HEAVILY DITCHING INE Coo Pm TRANSMIT MAY DAY o 21 5 Mhz Giving location and intentions 2 Heavy Objects in baggage area SECURE OR JETTISON Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 38 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Magie 3 High Winds
46. Baggage s loading Tie Down Cabin Height Measurements Dok OPEHING Di ERSIOHS WIDTH WIDTH HI HEIGHT TOP BOTTOM FRONT REAR pw Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 91 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 CABIN WIDHT MEASUREMENTS TIE DOWN RINGS 4 CABIN STATIONS 00 Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 92 144 g A AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 SECTION 7 AIRPLANE amp SYSTEMS DESCRIPTIONS TABLE OF CONTENTS Page Introduction 7 96 Airframe 7 96 Flight Controls 7 97 Trim System 7 97 Instrument Panel 7 97 Ground Control 7 98 Wing Flap System 7 99 Landing Gear System 7 99 Baggage Compartment 7 99 Seats 7 105 Seat Belts And Shoulder Harnesses 7 106 Seat Belts 7 107 Shoulder Harnesses 7 107 Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 93 144 Entrance Doors And Cabin Windows Engine Engine Controls Engine Instruments New Engine Break In And Operation Engine Oil System Ignition Starter System Air Induction System Exhaust System Carburetor System Cooling System Propeller Fuel System Brake System Electrical System Master Switch Ammeter Over Voltage Sensor and Warning Light Optional Original Issue Date 14 January 2011
47. D ROOT CHORD TIP CHORD SERVICE CEILING RANGE AUTONOMY EMPTY WEIGHT MAXIMUM TAKE OFF WEIGHT Date of last Weighing Specify how weight was measured List equipment fitted to aircraft and included in empty weight FORWARD AND AFT CENTRE OF GRAVITY LIMITS FWD AFT Specify in inches mm from datum and position of datum State how or from where limits are obtained Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 8 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 COLOR AIRPLANE COLOR FUSELAGE WINGS TAIL MAXIMUM AND MINIMUM AIRSPEEDS MAXIMUM NEVER EXCEED AIRSPEED STALL SPEED LANDING CONFIGURATION MAX CRUISE FUEL SYSTEM TYPE OF FUEL NUMBER OF FUEL TANKS TOTAL FUEL CAPACITY CAPACITY OF EACH TANK SEAT BELTS AND EQUIPMENT List equipment fitted to aircraft including seat belts showing type amp manufacturer radio transponder etc ENGINE DETAILS ENGINE MANUFACTURER MODEL ENGINE SERIAL NUMBER Original Issue Date 14January 2011 Revision No 02 Date 20 Oct 2011 Page 9 144 TWO OR FOUR STROKE AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage CAPACITY IN CC RATED HORSEPOWER OIL SYSTEM PROPELLER DETAILS TYPE
48. ETEOROLOGICAL TERMINOLOGY OAT Outside Air Temperature is the free air static temperature It is expressed in either degrees Celsius formerly centigrade or degrees Fahrenheit Standard Standard Temperature is 59 F 15 C at sea level pressure Temperature altitude and decreases by 35 6 F 2 C for each 1000 feet of altitude Pressure Pressure Altitude is the altitude read from an altimeter when Altitude the altimeter s barometric scale has been set to 29 92 Inches of mercury 760 mm ENGINE POWER TERMINOLOGY BHP Brake Horsepower is the power developed by the engine RPM Revolutions per Minute is engine speed Static Static RPM is engine speed attained during a full throttle RPM engine run up when the airplane is on the ground and Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 24 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Magie stationary AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY Demon Demonstrated Crosswind Velocity is the velocity of the crosswind Started component for witch adequate control of the airplane during Crosswind takeoff and landing was actually demonstrated during certification Velocity tests The value shown is not considered to be limiting Useable Fuel Usable Fuel is the fuel available for flight planning Unusable Fuel Unusable Fuel is the quantity of fuel that cannot be safely used in flight LTH Liters per Hour
49. Grasp the forward edge of the handle and pull out To close or open the doors from inside the airplane use the recessed door handle and arm rest Both cabin doors should be checked for security prior to flight and should not be opened intentionally during flight NOTE Accidental opening of a cabin door in flight due to improper closing does not constitute a need to land the airplane The best procedure is to set up the plane in a trimmed condition at approximately 56 Kts momentarily shove the door outward slightly and forcefully close the door Exit from the airplane is accomplished by grasping the forward edge of the door handle and pulling To lock the airplane lock the right cabin door from the inside by lifting up on the lever near the aft edge of the door close the left cabin door and using the ignition key lock the door ENGINE The airplane is powered by a horizontally opposed four cylinder overhead valve air cooled carbureted engine with a dry sump oil system The engine is a ROTAX Model 912 UL or 912 ULS and is rated at 80 100 horse power at 5800 RPM Major engine accessories mounted on the front of the engine include a starter a belt driven alternator if installed and oil cooler Dual magnetos are mounted on an accessory drive pad on the rear of the engine Provisions are also made for a vacuum pump and full flow oil filter Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 108 14
50. L An attitude indicator if installed is available and gives a visual indication of flight attitude Bank attitude is presented by a pointer at the top of the indicator relative to the bank scale which has Index marks at 10 20 30 60 and 90 either side of the center mark Pitch and roll attitudes are presented by a miniature airplane in relation to the horizon bar A knob at the bottom of the instrument is provided for in flight adjustment of the miniature airplane to the horizon bar for a more accurate flight attitude indication DIRECTIONAL INDICATOR OPTIONAL A directional indicator if installed is available and displays airplane heading on a compass card in relation to a fixed simulated airplane image and index The directional indicator will process slightly over a period of time Therefore the compass card should be set in accordance with the magnetic compass just prior to takeoff and occasionally re adjusted on extended flights A knob on the lower left edge of the instrument is used to adjust the compass card to correct for any precession Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 123 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 CABIN HEATING VENTILATING AND DEFROSTING SYSTEM GRAPH ADJUSTABLE ADJUSTABLE VENTILATION VENTILATION CODE RAMAIR FLOW lt VENTILATINGAIR Original Issue Date 14 January 2011 Revision No 02 Da
51. LOADING Pounds HP FUEL CAPACITY Standard Tanks Auxiliary Tanks OIL CAPACITY ENGINE Rotax 100 bhp at 5800 rpm PROPELLER Controllable electric pitch propellers diameter Original Issue Date 14 January 2011 Revision No 02 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 921 ft 42 Kts 30 Kts 24 Kts 1320 LBS 704 LBS 616LBS 50 LBS 10 85 13 2 18GAL 18GAL 3QTS 912 5 9145 72 IN 70 IN Date 20 Oct 2011 Page 13 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 THANK YOU You have purchased a state of the art high performance general aviation aircraft your IBIS MAGIC GS700 It s performance is spectacular and it s life almost beyond measure when given reasonable care Your IBIS has been designed and instructed to give you the most in performance economy and comfort It is our desire that will find flying it either for business or pleasure a pleasant and profitable experience This Pilot s Operating Handbook has been prepared as a guide to help you get the most assure and utility from your airplane It contains information about your IBIS S equipment operating procedures and performance and suggestions for its servicing and care We urge you to read it from cover to cover and to refer to it frequently Our interest in your flying pleasure has not ceased with your purchase of an IBIS worldwide the IBIS Dealer Organi
52. MODEL PITCH AND DIAMETER X NUMBER OF BLADES REDUCTION DRIVE TYPE REDUCTION RATIO PROPELLER MANUFACTURER NAME AIRCRAFT CONSTRUCTION DETAILS WHERE AIRCRAFT WAS BUILT State Territory City MATERIALS USED IN CONSTRUCTION 1 Fuselage Frame and Covering Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 10 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Magie 2 Wing Frame and Covering 3 Other parts unless similar to the above PICTURES Please attach the following RECENT PICTURES showing Aircraft from FRONT and SIDE AIRCRAFT REGISTRATION NUMBERS ON WING AND FUSELAGE TAIL COCKPIT SHOWING INSTRUMENT PANEL including MTOW WEIGHT AND WARNING PLACARDS Please annotate pictures with the aircraft registration number and the date on which they were taken NAME AND ADDRESS OF THE PERSON COMPLETING THIS FORM Name Address Contact Numbers Phone Fax Signature Date Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 11 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Magie PERFORMANCE SPECIFICATIONS SPEED M ximum at Sea Level CRUISE 75 Power at 8 000 ft 4800 RPM 7296 Power at 8 000 ft 16 5 Gallons usable fuel 7296 Power at 8 000 ft 34 5 Gallons usable fuel Speed Max
53. N FLIGHT 1 Throttle CUT OFF 2 Fuel Shutoff Salve OFF 3 Magnetos OFF 4 Master Switch OFF Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 39 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage 5 78 Kts if fire is not extinguished increase glide speed to find an airspeed which will provide an incombustible mixture 6 Forced Landing EXECUTE as described on emergency landing without engine power ELECTRICAL FIRE IN FLIGHT 1 Master Switch OFF 2 All Other Switches except ignition switch OFF 3 Vents Cabin Air CLOSED 4 Fire Extinguisher ACTIVATE if available WARNING After discharging an extinguisher within a closed cabin ventilate the cabin If fire appears out and electrical power is necessary for continuance of flight 5 Master Switch ON 6 Circuit Breakers CHECK for faulty circuit do not reset 7 Radio Electrical Switches ON one at a time with delay after each until short circuit is localized 8 Vents Cabin OPEN when it is ascertained that fire is completely extinguished CABIN FIRE 1 Master Switch OFF 2 Vents Cabin Air CLOSED to avoid drafts
54. NG NORMAL LANDING 1 Airspeed 2 Wing Flaps 3 Airspeed 4 Touchdown 5 Landing Roll 6 SHORT FIELD LANDING 1 Airspeed 2 Wing Flaps 3 4 5 Touchdown 6 Brakes 7 Wing BALKED LANDING 1 2 Propeller 3 Wing Flaps 4 Airspeed 5 Wing Original Issue Date 14 January 2011 PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage 5000 RPM no more than 75 ADJUST ADJUST ADJUST and LOCK ON HIGH RPM FULL OPEN 52Kts 61Kts flaps UP AS DESIRED below 52 61Kts 48 56 Kts Flaps DOWN MAIN WHEELS FIRST LOWER NOSE WHEEL GENTLY MINIMUM REQUIRED 39 48 Kts flaps UP 30 Below 56 Kts MAINTAIN 48 Kts REDUCE to idle as obstacle is cleared MAIN WHEELS FIRST APPLY HEAVILY RETRACT FULL OPEN HIGH RPM RETRACT to 20 48 Kts RETRACT slowly Revision No 02 Date 20 Oct 2011 Page 58 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Magie AFTER LANDING 1 Wing 1 2 UP
55. No 02 Date 20 Oct 2011 Page 33 144 z IBIS f Magi AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 FUEL 36 GAL ON OFF 4 Near both fuel tanks filler cap standard tanks FUEL N 94 MIN OCTANE AUTOMOTIVE CAP 9 US GAL 34LITERS USABLE FUEL 94 MIN OCTANE AUTOMOTIVE CAP 9 US GAL 34LITERS USABLE 5 On the upper left instrument panel NO INTENTIONAL SPINS 6 On the upper right instrument panel SMOKING PROHIBITED 7 In the top center of the battery box CAUTION BATTERY 12 VOLTS D C i C Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 34 144 SECTION 3 EMERGENCY PROCEDURES TABLE OF CONTENTS Introduction Air speeds For Emergency Operation OPERATIONAL CHECKLIST Engine Failures Engine Failures DuringTake off run Engine Failures Immediately after Takeoff Engine Failures During Flight Forced Landings Emergency Lading without Engine Power Precautionary Landing with Engine Power Ditching Fire During Start On Ground Engine Fire In Flight Electrical Fire In Flight Cabin Fire Wing Fire Icing Original Issue Date 14 January 2011 Revision No 02 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC 05 700 3 37 3 37 3 37 3 37 3 37 3 38 3 38 3 38 3 38 3 38 3 39 3 39 3 39 3 40 3 40 3 40 3 41 Date 20 Oct 2011
56. ODEL MAGIC GS 700 aircraft Dealer Make your directory one of your cross country flight planning aids a warm welcome awaits you at every IBIS aircraft Dealer IMPORTANT NOTICE This handbook must be read carefully by the owner or operator s of your IBIS in order to be become familiar with its operation and to obtain all it has to offer in terms of both speed and reliability Herein are suggestions and recommendation to help you obtain safe performance without sacrificing economy You are encouraged to operate your machine in accordance with and within the limits identified in this Pilots Operating Handbook as well as any placards located in the airplane Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 15 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 TABLE CONTENTS SECTION GENERAL LIMITATIONS EMERGENCY PROCEDURES NORMAL PROCEDURES PERFORMANCE WEIGHT amp BALANCE EQUIPMENT LIST AIRPLANE amp SYSTEMS DESCRIPTIONS AIRPLANE HANDLING SERVICE amp MAINTENANCE SAFETY INFORMATION OOAN OA BROWN This handbook will be kept current by Service letters published by IBIS Aircraft S A These are distributed to IBIS aircraft Dealers and to those who subscribe through the Owner Follow Up System if you are not receiving subscription service You will want to keep in touch with your IBIS Aircraft Dealer for information concerning the change status of the
57. OFF WARM UP Starting warm period at 2000 r p m for approx 2 minutes continue at 2500 r p m duration depending on ambient temperature until oil temperature reaches 50 120 e Check Temperatures and pressures Throttle Response e Shortfull throttle ground test CAUTION After a full load ground test allow a short cooling run to prevent vapor formation in the cylinder heat Most of the warm up will have been conducted during taxi and additional warm up before takeoff should be restricted to the checklist procedures Since the engine is closely cow led for efficient in flight cooling precautions should be taken to avoid overheating on the ground MAGNETO CHECK The magneto check should be made at 4000 RPM as follows Move ignition switch if Installed first to R position and note RPM Next move switch back to BOTH to clear the other set of plugs Then move switch to the L position note RPM and return the switch to the BOTH position RPM drop should not exceed 125 RPM on either magneto or show greater than 50 RPM differential between magnetos If there is a doubt concerning operation of the ignition system RPM checks at higher engine speeds will usually confirm whether a deficiency exists An absence of RPM drop may be an indication of faulty grounding of one side of the ignition system or should be cause for suspicion that the magneto timing is set in advance of the setting specified Original Issue Dat
58. S BASED ON THIS HANDBOOK PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL AIRPLANE IBIS MAGIC GS 700 REV 2 20 October 2011 Original Flight Manual Airplane IBIS MAGIC GS 700 WARNING This manual MUST be present inside the cockpit at all times Should you be selling the aircraft make sure this manual is handed over to the new owner Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 4 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage Brand Model Serial number Date of manufacture Aircraft empty weight kg Fuel weight Available cargo weight Equipment included in aircraft empty weight Office Address Calle 13A 100 35 Cali Valle del Cauca Telephone 57 2 681 44 33 ext 5 Factory Vereda Paso de la Bolsa Km 2 Via la Ventura Jamundi Valle del Cauca Telephone 57 2 550 42 80 Colombia South America www ibis aircraft com Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 5 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL AIRPLANE IBIS MAGIC GS 700 Model Data Sheet number Factory serial number Registration number Date of Issue Pages signed under Approval in section Index of revisions and List of valid pages are approved by Authority Signature Stamp Original date of Appro
59. S IN NEUTRAL POSITION 2 RETARD THROTTLE TO IDLE POSITION 3 APPLY AND HOLD FULL RUDDER OPPOSITE TO THE DIRECTION OF ROTATION 4 JUST AFTER THE RUDDER REACHES THE STOP MOVE THE CONTROL WHEEL BRISKLY FORWARD FAR ENOUGH TO BREAK THE STALL 5 Full down elevator may be required at aft center of gravity loadings to assure optimum recoveries 6 HOLD THESE CONTROL INPUTS UNTIL ROTATION STOPS Premature relaxation of the control inputs may extend the recovery 7 AS ROTATION STOPS NEUTRALIZE RUDDER AND MAKE A SMOOTH RECOVERY FROM THE RESULTING DIVE NOTE If disorientation precludes a visual determination of the direction of rotation the symbolic airplane in the turn coordinator if installed may be referred to for this information For additional information on spins and spin recovery see the discussion under SPINS in Normal Procedures Section 4 ROUGH ENGINE OPERATION OR LOSS OF POWER CARBURETOR ICING A gradual loss of RPM and eventual engine roughness may result from the formation of carburetor ice The best procedure of course is to turn back or change altitude to escape icing conditions SPARK PLUG FOULING A slight engine roughness in flight may be caused by one or more spark plugs becoming fouled by carbon or lead deposits This may be verified by turning the ignition switch momentarily from BOTH to either L or R position An obvious power loss in single ignition operation is evidence of spark plug or magnet
60. SBIS ors OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL AIRPLANE MAGIC GS 700 MODEL MAGIC GS 700 SERIAL NUMBER REGISTRATION NUMBER ORIGINAL ISSUE 14 January 2009 REVISION No 2 20 OCTOBER 2011 IBIS AIRCRAFT S A COLOMBIA SOUTH AMERICA www ibis aircraft com Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 1 144 m AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Magie PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL AIRPLANE RECORD OF MANUAL REVISIONS Any revisions to the present manual must be recorded in the following table Revision No Date released Chapter Approved by 1 0 08 18 2010 All Ibis Aircraft 2 0 10 20 2011 All Ibis Aircraft Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page2 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage THIS PAGE BLANK Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 3 144 m AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 THIS HAND BOOK INCLUDES THE MATERIAL REQUIRED TO BE FURNISHED TO THE PILOT AND CONSTITUTES THE APPROVED AIRPLANE FLIGHT MANUAL OWNERS ARE ENCOURAGED TO EVALUATE THEIR OWN CHECKLISTS AND OWNER DEVELOPED MANUAL DATA FOR COMPLETENES
61. SHOULDER HARNESSES All seat positions are equipped with seat belts see figure 7 4 The pilot s and passenger s seats are also equipped with separate shoulder harnesses Integrated Revision No 02 Date 20 Oct 2011 106 144 Original Issue Date 14 January 2011 EXT AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 seat belt shoulder harnesses with inertia reels can be furnished for the pilot s and passenger s seat positions if desired SEAT BELTS The seat belts used with the pilot s The buckle half of the seat belt is inboard of each seat and has a fixed length the link half of the belt is outboard and is the adjustable part of the belt To use the seat belts for the pilot s and passenger s seats position the seat as desired and then lengthen the link half of the belt as needed by grasping the sides of the link and pulling against the belt Insert and lock the belt link into the buckle Tighten the belt to a snug fit by pulling the free end of the belt To release the seat belts grasp the top of the buckle opposite the link and pull upward SHOULDER HARNESSES Each shoulder harness is attached to a rear doorpost above the window line and is stowed behind a stowage sheath above the cabin door To stow the harness fold it and place it behind the seat The shoulder harnesses are used by fastening and adjusting the seat belt first Then lengthen the harness as required by pulling on the
62. Y Sw ignition Amp AMPERE Sw Switch V VOLTMETER Original Issue Date 14 January 2011 x VY Relay Starter A AMPEREMETER LAMP 9 2 10 UHF 10 Amp lt uod oce to Fiaps 10 Amp 4 N to Propeller ro 10 to Strobelights T M loAmp Vo d jo instruments EN to landing y taxi 4 X a lights 15 Amp L4 o 10 Boost pump SAmp Xponder 2 gt SAmp 4 Awad SAmp 4 o Q to GPS 5 Amp lt Xo 4 tim ee lAmp R Revision No 02 Date 20 Oct 2011 117 144 EXT AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 AMMETER IF INSTALLED The ammeter located on the upper right side of the instrument panel indicates the flow of current in amperes from the alternator to the battery or from the battery to the airplane electrical system When the engine is operating and the master switch is turned on the ammeter indicates the charging rate applied to the battery In the event the alternator is not functioning or the electrical load exceeds the output of the alternator the ammeter indicates the battery discharge rate OVER VOLTAGE SENSOR AND WARNING LIGHT IF INSTALLED The airplane is equipped with an automatic over voltage protection system consisting of an over voltage sensor behind the instrument panel and a red warning light labeled HIGH VOLTAGE unde
63. ated around either main landing gear by pressing down on the tail cone just forward of the vertical stabilizer to raise the nose wheel off the ground Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 98 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 WING FLAP SYSTEM The wing flaps are of the single slot type see figure 7 3 and are extended or retracted by positioning the wing flap switch lever on the instrument panel to the desired flap deflection position The switch lever is moved up or down For flap settings greater than 10 move the switch lever to the right to clear the stop and position it as desired A scale and pointer on the top of the switch lever indicates flap travel in degrees The wing flap light system circuit is protected by a 10 ampere circuit breaker LANDING GEAR SYSTEM The landing gear is of the tricycle type with a steerable nose wheel and two main wheels The landing gear may be equipped with wheel fairings Shock absorption is provided by the tubular spring steel main landing gear struts and the air oil nose gear shock strut Each main gear wheel is equipped with a hydraulically actuated disc type brake on the inboard side of each wheel When wheel fairings are installed an aerodynamic fairing covers each brake BAGGAGE COMPARTMENT The baggage compartment consists of the area from the back of the pilot and passenger s seats to the
64. ater cooled horizontally opposed carburetor equipped four cylinder engine with 912 UL A F 1211 cm 73 9 in 12 UL S 1352 cm 82 5 in Horsepower Rating and Engine Speed 80 100 rated BHP at 5800 RPM Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 20 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage PROPELLER Propeller Manufacturer PROP Number of Blades 3 Propeller Diameter Maximum 72 inches 100 BHP Minimum 70 inches 80 BHP Propeller Type Electric controllable pitch propeller FUEL Approved Fuel 94 Octane Fuel Capacity Standard Tanks Total Capacity Each Tank 9 us Gallons Reserve tank 2 us Gallons Total Capacity 20 us Gallons Total Usable 18 5 us Gallons Long Range Auxiliary Tanks Total Capacity 18 us Gallons Total Capacity Each Tank 9 us Gallons Total Usable 18 us Gallons NOTE Due to Cross feeding between fuel tanks the tanks should be re topped after each refueling to assure maximum capacity OIL Oil Grade Specification Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 21 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Magie Aviation Grade Straight Mineral Oil Use to replenish supply during first 5 hours and at the first 25 hours oil change Continue to use until a total of 50 hours has accumulated
65. ch located on the left subpanel The switch is labeled clockwise OFF R L BOTH and STARTS The engine should be operated on both magnetos BOTH position except for magneto checks The R and L positions are for checking purposes and emergency use only When the switch is rotated to the spring loaded START position with the master switch in the ON position the starter contactor is energized and the starter will crank the engine When the switch is released it will automatically return to the BOTH position AIR INDUCTION SYSTEM The engine air induction system receives ram air through an intake in the lower portion of the engine cowling The intake is covered by an air filter which removes dust and other foreign matter from the induction air Airflow passing through the filter enters an air box After passing through the air box induction air enters the inlet in the carburetor and is then ducted to the engine cylinders through intake manifold tubes EXHAUST SYSTEM Exhaust gas from each cylinder passes through riser assemblies to a muffler and tail pipe on the underside of the engine CARBURETOR The engine is equipped with two an up draft float type fixed jet carburetor mounted on the top of the engine The carburetor has throttle mechanism and manual choke control COOLING SYSTEM Ram air for engine cooling enters through two intake openings in the front of the engine cowling The cooling air is directed around the cylinders and
66. connecting link on the end of the harness and the narrow release strap Snap the connecting link firmly onto the retaining stud on the seat belt link half Then adjust to length Removing the harness is accomplished by pulling upward on the narrow release strap and removing the harness connecting link from the stud on the seat belt link In an emergency the shoulder harness may be removed by releasing the seat belt first and allowing the harness still attached to the link half of the seat belt to drop to the side of the seat Adjustment of the shoulder harness is important A properly adjusted harness will permit the occupant to lean forward enough to sit completely erect but prevent excessive forward movement and contact with objects during sudden deceleration Also the pilot will want the freedom to reach all controls easily Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 107 144 g A AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 ENTRANCE DOORS AND CABIN WINDOWS Entry to and exit from the airplane is accomplished through either of two entry doors one on each side of the cabin refer to Section 6 for cabin and cabin door dimensions The doors incorporate a recessed exterior and interior door handle a key operated door lock left door only and a door stop mechanism To open the doors from outside the airplane utilize the recessed door handle near the aft edge of each door
67. consumption figures shown in Section 5 the propeller should be adjusted slightly to obtain smooth operation Carburetor ice as evidenced by an unexplained drop in RPM to prevent carburetor ice during flight avoided flight in very heavy rain condition this prevent the possibility of engine stoppage due to excessive water ingestion Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 64 144 B AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 FUEL SAVINGS PROCEDURES FOR FLIGHT TRAINING OPERATIONS For best fuel economy during flight training operations the following procedures are recommended 1 Use 7596 power while transitioning to and from the practice area approximately 5000 RPM 2 Propeller may be adjusted during climbs above 1000 feet and for practicing such maneuvers as stalls NOTE When cruising at 7596 or less power the propeller may be adjusted This is especially applicable to cross country training flights but may also be practiced during transition flights to and from the practice area Using the above recommended procedures can provide fuel savings of up to 1396 When compared to typical training operations STALLS The stall characteristics are conventional for the flaps up and flaps down condition The stall warning horn if installed produces a steady signal 4 to 9 Kts before the actual stall is reached and remains on until the
68. d control panel Directly below these controls are the elevator trim control wheel trim position indicator microphone and circuit breakers For details concerning the instruments switches circuit breakers and controls on this panel refer in this section to the description of the systems to which these items are related GROUND CONTROL Effective ground control while taxiing is accomplished through nose wheel steering by using the rudder pedals left rudder pedal to steer left and right rudder pedal to steer right When a rudder pedal is depressed a spring loaded steering bungee which is connected to the nose gear and to the rudder bars will turn the nose wheel through an arc of approximately 8 5 each side of center By applying either left or right brake the degree of turn may be increased up to 30 side of center Moving the airplane by hand is most easily accomplished by attaching a tow bar to the nose gear strut If a tow bar is not available or pushing is required use the wing struts as push points Do not use the vertical or horizontal surfaces to move the airplane If the airplane is to be towed by vehicle never turn the nose wheel more than 30 either side of center or structural damage to the nose gear could result The minimum turning radius of the airplane using differential braking and nose wheel steering during taxi is approximately 23 feet To obtain a minimum radius turn during ground handling the airplane may be rot
69. d corrected for position and instrument error and expressed in knots Knots calibrated airspeed is equal to KTAS standard atmosphere at sea level KIAS Knots Indicated Airspeed is the speed shown on the airspeed indicator and expressed in knots KTAS Knots True Airspeed is the airspeed expressed in knots relative to undisturbed air which is KCAS corrected for altitude and temperature VA Maneuvering Speed is the maximum speed at which you may Use abrupt control travel V FE Maximum Flap Extended Speed is the highest speed Permissible with wing flaps in a prescribed extended position Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 23 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage VNO Maximum Structural Cruising Speed is speed that should Not be exceeded except in smooth air then only with caution VNE Never Exceed Speed is the speed limit that not be exceeded at any time VS Stalling Speed or the minimum steady flight speed at which the airplane is controllable VSO Stalling Speed or the minimum steady flight speed at which the airplane is controllable in the landing configuration at the most forward center of gravity VX Best Angel of Climb Speed is the speed which results in the greatest gain of altitude in a given horizontal distance VY Best Rate of Climb Speed is the speed which results in the greatest gain in altitude in a given time M
70. d the battery serviced in a low discharged condition If the battery is low in charged service to cover the plates charge to full then service to full Full is generally indicated by a service level within each cell of the battery ENGINE CARE Clean the engine with a neutral solvent While the engine is warm but not hot spray with solvent and allow setting a few minutes Follow with a spray wash and allow drying Avoid excessively high pressure which can force entry water and or solvents under seals resulting in contamination of the seal system or entry through the five walls in to the cabin Use caution and protect any electrical relays or switches your may have installed in the engine compartment as well Use solvents which do not attack rubber or plastics Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 138 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 CAUTION Particular care should be given to electrical equipment before cleaning Cleaning fluids should not be allowed to enter magnetos starter alternator and the like Protect these components before saturating the engine with sol vents All other openings should also be covered before cleaning the engine assembly Caustic cleaning solutions should be used cautiously and should always be properly neutralized after their use CAPACITY OF ENGINE SUMP 3 Quarts Do not operate on less than 3 q
71. e CLEANING AND CARE WINDSHIELD WINDOWS Windshield and Windows of polycarbonate plastic highly resistant to impacts should be cleaned with an aircraft windshield cleaner Apply the cleaner sparingly with soft cloths and rub with moderate pressure until all dirt oil scum and bug stains are removed Allow the cleaner to dry and then wipe it off with soft flannel cloths Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 141 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 If a windshield cleaner is not available the polycarbonate plastic can be cleaned with soft cloths moistened with Stoddard solvent to remove oil and grease NOTE Never use gasoline benzene alcohol acetone carbon tetrachloride fire extinguisher or anti ice fluid lacquer thinner or glass cleaner to clean the polycarbonate plastic These materials will attack the plastic and may cause it to craze Follow by carefully washing with a mild detergent and plenty of water Rinse thoroughly and then dry with a clean moist chamois Do not rub the polycarbonate plastic with a dry cloth since this builds up an electrostatic charge which attracts dust Waxing with a good commercial wax will finish the cleaning job A thin even coat of wax polished out by hand with clean soft flannel cloths will fill in minor scratches and help prevent further scratching Do not uses a canvas cover on the
72. e 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 61 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage Check the two ignition circuits at 4000 r p m approx 1700 r p m propeller e Speed drop with only one ignition circuit must no exceed 300 r p m approx 130 r p m Propeller e 120 r p m approx 50 r p m propeller max difference of speed by use of either circuit A or B NOTE The propeller speed depends on the actual reduction ratio ALTERNATOR CHECK optional Prior to flights where verification of proper alternator if installed and voltage regulator operation is essential a positive verification can be made by loading the electrical system momentarily 3 to 5 seconds with the landing light or by operating the wing flaps during the engine run up 3000 RPM The ammeter will remain within a needle width of its initial position if the alternator and voltage regulator are operating properly TAKEOFF POWER CHECK It is important to check full throttle engine operation early in the takeoff run Any sign of rough engine operation or sluggish engine acceleration is good cause for discontinuing the takeoff If this occurs you are justified in making a thorough full throttle static run up before another takeoff is attempted Full throttle run ups over loose gravel are especially harmful to propeller tips When takeoffs must be made over a gravel surface it is very important that
73. e Date 14 January 2011 Revision No 02 Date 20 Oct 2011 121 144 g A AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 PITOT STATIC SYSTEM AND INSTRUMENTS The pitot static system supplies ram air pressure to the airspeed indicator and static pressure to the airspeed indicator rate of climb indicator and altimeter The System is composed of either an unheated pitot tube mounted on the lower surf ace of the left wing and the associated plumbing necessary to connect the instruments to the sources AIRSPEED INDICATOR The airspeed indicator is calibrated miles per hour Limitation and range markings include the white are 30 to 60 miles green are 45 to 100 miles yellow are 100 to 120 miles and a red line 130 miles If a true airspeed indicator is installed it is equipped with a rotatable ring which works in conjunction with the airspeed indicator dial in a manner similar to the operation of a flight computer To operate the indicator first rotate the ring until pressure altitude is aligned with outside air temperature in degrees Fahrenheit Pressure altitude should not be confused with indicated altitude To obtain pressure altitude momentarily set the barometric scale on the altimeter to 29 92 and read pressure altitude on the altimeter Be sure to return the altimeter barometric scale to the original barometric setting after pressure altitude has been obtained Having set the ring to correct for alti
74. e airplane on the remaining runway Those extra items on the checklist will provide added safety after a failure of this type Prompt lowering of the nose to maintain airspeed and establish a glide attitude is the first response to an engine failure after takeoff In most cases the landing should be planned straight ahead with only small changes in direction to avoid obstructions Altitude and airspeed are seldom sufficient to execute a 180 gliding turn necessary to return to the runway The checklist procedures assume that adequate time exists to secure the fuel and ignition systems prior to touchdown After an engine failure in flight the best glide speed as shown in fig 3 1 should be established as quickly as possible While gliding toward suitable landing area an effort should be made to identify the cause of it failure If time permits an engine restart should be attempted as shown the checklist If the engine cannot be restarted a forced landing without power must be completed Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 42 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage SPEED 65 MPH PROPELLER WINDMILLING FLAPS UP ZERO WIND LE LL gt I 9 I 20 000 30 000 40 000 50 000 60 000 70 000 80 000 90 000 100 000 110 000 GROUND DISTANCE FT Figure 3 1 Maximum
75. e limitation baggage area limitation Additional moment calculations based on the actual weight and C G arm fuselage station of the item being loaded must be made if the position of the load is different from that shown on the Loading Graph Total the weights and moments 1000 and plot these values on the Center of Gravity Moment Envelope to determine whether the point falls within the envelope and if the loading is acceptable XC Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 89 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Figure 6 3 Baggage Loading Arrangements LOADING ARRANGEMENTS STATION C G ARM Pilot or passenger center of gravity on adjustable seats positioned for average occupant Numbers parenthese indicate Reference Datum orward and after limit of ocupant center of Wing Leading Edge gravity range MTOW Arms measured to the center of the areas 2 47 Inch 16 68 Inch Datum shown 0 03 Inch To 4 97 Inch NOTE he after baggage wall can be used as a convenient interior reference point for determining the location of baggage area uselage staion 4 29 Inch 2 2 22 2 2 22 22 22 2 Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 90 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Figure 6 4
76. e will rotate to the horizontal attitude for touchdown Close the throttle at touchdown FIRES Although engine fires are extremely rare in flight the steps of the appropriate checklist should be followed if one is encountered After completion of this procedure execute a forced landing Do not attempt to restart engine The initial indication of an electrical fire is usually the odor of burning insulation The checklist for this problem should result in elimination of the fire EMERGENCY OPERATION IN CLOUDS Vacuum System Failure if installed In the event of a vacuum system failure during flight in marginal weather the directional indicator and attitude indicator will be disabled and the pilot will have to rely on the turn coordinator if he inadvertently flies into clouds The following instructions assume that only the electrically powered turn coordinator is operative if installed and that the pilot is not completely proficient in instrument flying EXECUTING A 180 TURN IN CLOUDS Upon inadvertently entering the clouds an immediate plan should be made to turn back as follows 1 Note the time of the minute hand and observe the position of the sweep second hand on the clock 2 When the sweep second hand indicates the nearest half minute initiate a standard rate left turn holding the turn coordinator symbolic airplane wing opposite the lower left index mark for 60 seconds Then roll back to level flight by leveling the miniatu
77. electrolyte at an excessive rate Electronic components in the electrical system could be adversely affected by higher than normal voltage If a faulty voltage regulator setting is causing the overcharging To preclude these possibilities and over _ voltage sensor will automatically shut down the alternator and the over voltage warning light illuminate if de charge voltage reaches approximately 16 volts Assuming that the malfunction was only momentary an attempt should be made to reactivate the alternator system To do this turn both sides of the master switch off and then on again If the problem no longer exists normal alternator charging will resume and the warning light will go off If the light illuminates again a malfunction is confirmed In this event the flight should be terminated and or the current drain on the battery Minimized because the battery can supply the electrical system for only a limited period of time Power must be conserved for later use of the landing light and flaps during landing INSUFFICIENT RATE OF CHARGE IF ALTERNATOR INSTALLED If the ammeter indicates a continuous discharge rate in flight the alternator is not supplying power to the system and should be shut down since the alternator field circuit may be placing an unnecessary load on the system All nonessential equipment should be turned off and the flight terminated as soon as practical Section 4 provides checklist and amplified procedures for the conduct
78. em is operative AVIONICS SUPPORT EQUIPMENT The airplane may at the owner s discretion be equipped with various types of avionics support equipment such as an audio control panel and static dischargers The installation of IBIS radio equipment provides certain audio back up capabilities and transmitter selector switch functions that the pilot should be familiar with The audio amplifier in the COM radio is required for speaker and transmitter operation The amplifier is automatically selected along with the transmitter by the transmitter selector switch In the event the audio amplifier in use fails as evidenced by loss of all speaker audio and transmitting capability of the selected transmitter select the other transmitter This should re establish speaker audio and transmitter operation Since headset audio is not affected by audio amplifier operation the pilot should be aware Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 125 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 that while utilizing a headset the only indication of audio amplifier failure is loss of the selected transmitter This can be verified by switching to the speaker function The speaker phone switches determine whether the output of the receiver in use is fed to the headphones or through the audio amplifier to the speaker Place the switch for the desired receiving system either in the up pos
79. ence often found near ground level Soft or rough field takeoffs are performed with 10 wing flaps by lifting the airplane off the ground as soon as practical in a slightly tail low attitude If no obstacles are ahead the airplane should be leveled off immediately to accelerate to a higher climb speed Takeoffs into strong crosswinds normally are performed with the minimum flap setting necessary for the field length to minimize the drift angle immediately after takeoff The airplane is accelerated to a speed slightly higher than normal and then pulled off abruptly to prevent possible settling back to the runway while drifting When clear of the ground make a coordinated turn into the wind to correct for drift ENROUTE CLIMB Normal climbs are performed with flaps up and full throttle and at speeds 4 to 9 Kts higher than best rate of climb speeds for the best combination of performance visibility and engine cooling The propeller should be adjusted below 500 feet for smoother operation or to obtain maximum RPM For maximum rate of climb use the best rate of climb speeds shown in the Rate of Climb chart in Section 5 If an obstruction dictates the use of a steep climb angle the best angle of climb speed should be used with flaps up and maximum power Climbs at speeds lower than the best rate of climb speed should be of short duration to improve engine cooling CRUISE Normal cruising is performed between 70 and 75 power The engine RPM and
80. ent opening and apply suction a sound from the warning horn will confirm system operation 8 LEFT WING Trailing Edge Te _ sciret t retener CHECK freedom of movement and security 2 and flaps Control CHECK surfaces BEFORE STARTING ENGINE 1 Preflight Inspection COMPLETES 2 Seats Belts Shoulder Harnesses ADJUST and LOCK 3 Fuel Valve ON OFF ON 4 Radios Electrical Equipment OFF 5 TEST and SET Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 55 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage 6 Circuit CHECK IN 7 Electric fuel pump ON B IDLE POSITION STARTING ENGINE 1 IDLE POSITION 2 Choke pulled AS REQUIRED 3 Propeller Area CLEARS 4 Master ON 5 Magnetos ON 6 Ignition aes START release when engine starts 7 Oil IT 7 0 P CHECK 8 Throttle RO ADJUST for 1400 RPM Idle speed 9 Beacon if installed ON 10 EL E ON 11 TS CHECK BEFORE TAKEOFF 1 Parking Brake
81. er switch is a split rocker type switch if installed labeled MASTER and is ON in the up position and OFF in the down position The right half of the switch Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 115 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 labeled BAT controls all electrical power to the airplane The left half labeled ALT controls the alternator If Installed Normally both sides of the master switch should be used simultaneously however the BAT side of the switch could be turned ON separately to check equipment while on the ground The ALT side of the switch when placed in the OFF position removes the alternator from the electrical system With this switch in the OFF position the entire electrical load is placed on the battery Continued operation with the alternator switch in the OFF position will reduce battery power low enough to open the battery contactor remove power from the alternator field and prevent alternator restart Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 116 144 4 d AIRCRAFT S A Code PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 agg to Engine Alternator Sw Master REGULATOR ELECTRIC SYSTEM GRAPHIC MAGIC GS 700 ELECTRIC SYSTEM Capacitor 22000 4 4 Vs Circut Breaker 4 e Switch v Ground Magnetos CY 0 L R HO
82. essure cleaning systems and solvents They can damage parts such as propeller hubs pitot probes and static ports Cover cooling ports to the interior and avionics When the airplane is parked outside in cold climates and it is necessary to remove ice before flight care should be taken to protect the painted surfaces during ice removal with chemical liquids A 50 50 solution of isopropyl alcohol and water will satisfactorily remove ice accumulations without damaging the paint A solution with more than 5096 alcohol is harmful and should be avoided While applying the de icing solution keep it away from the windshield and cabin Windows since the alcohol will attack the polycarbonate plastic and may cause it to craze PROPELLER CARE Preflight inspection of propeller blades for nicks and wiping them occasionally with an oily cloth to clean off grass and bug stains will assure long trouble free service Small nicks on the propeller particularly near the tips and on the leading edges should be dressed out as soon as possible since these nicks produce stress concentrations and if ignored may result in cracks Never use an alkaline cleaner on the blades remove grease and dirt with carbon tetrachloride or Stoddard solvent Your propeller should be serviced according to the manufacturer s instruction Treat it with care The propeller is sensitive to leading edge damage and possible erosion shield delaminating Refer to their service bulle
83. expected weather is encountered However should an emergency arise the basic guidelines described in this section should be considered and applied as necessary to correct the problem AIRSPEEDS FOR EMERGENCY OPERATION Engine Failure after 52 Kts Maneuvering Speed rr ore rt 74 Kts Maximum Glide 0 09 56 Kts Precautionary Lading with Engine Power 48 Kts Lading Without Engine Power Wing Flaps Up e rrr e ee ey hae re e ee YR gs 52 Kts Wing 48 Kts OPERATIONAL CHECKLIST ENGINE FAILURES ENGINE FAILURE DURING TAKEOFF RUN 1 WOME oe IDLE 2 APPLY Wing Flaps RETRACT 4 Ignition Switch OFF 5 Master Switch OFF 1 Airspeed 52 Kts 2 Fuel Shutoff Valve OFF Ignition Switch OFF 4 Master Switch OFF 5 Wing Flaps As Required Original Issue Date 14January 2011 Revision No 02 Date 20 Oct 2011 Page 37 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage ENGINE FAILURE DURING FLIGHT 1 Airspeed 52 Kts 2 Fuel Shutoff Valve ON 3 Ignition Switch BOTH or ST
84. ge status Every seventh day during these periods the propeller should be rotated by hand through five revolutions This action every seven days stop the propeller at 45 90 deg this action limbers the oil and prevents any accumulation of corrosion on engine cylinder walls WARNING For maximum safety check that the ignition switch is OFF the throttle is closed and the fuel valve control is in cut off position and the airplane is secured before rotating the propeller by hand Do not stand within there are of the propeller blades while turning the propeller After 30 days the airplane should be flown for 30 minutes or a ground run up should be made just long enough to produce an oil temperature within the lower green are range Excessive ground run up should be avoided Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 136 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Engine run up also helps to eliminate excessive accumulations of water in the fuel system and other air spaces in the engine Keep fuel tanks full to minimize condensation in the tanks Keep the battery fully charged to prevent the electrolyte from freezing in cold weather If the airplane is to be stored temporarily or indefinitely refer to the Service Manual for proper storage procedures OUT OF SERVICE CARE Should you be required to place your IBIS in storage precauti
85. imum Range at 10 000 ft 16 5 Gallons usable fuel Maximum Range at 10 000 ft 34 5 Gallons usable fuel Speed 5000 RPM 7596 Power at 8 000 ft 16 5 Gallons usable fuel 7596 Power at 8 000 ft 34 5 Gallons usable fuel Speed Maximum Range at 10 000 ft 16 5 Gallons usable fuel Maximum Range at 10 000 ft 34 5 Gallons usable fuel 5500 RPM Speed 8296 Power at 8 000 ft 16 5 Gallons usable fuel 8296 Power at 8 000 ft 34 5 Gallons usable fuel Speed Maximum Range at 10 000 ft 16 5 Gallons usable fuel Maximum Range at 10 000 ft 34 5 Gallons usable fuel Speed RATE OF CLIMB AT SEA LEVEL SERVICE CEILING TAKEOFF PERFORMANCE Ground Roll Total Distance over 50ft obstacle LANDING PERFORMANCE Ground roll Original Issue Date 14 January 2011 Revision No 02 104 Kts 93 Kts 4 6 GLH 333 MILES 3 3HRS 697 MILES 6 9 HRS 88 Kts 342 MILES 3 3 HRS 717MILES 6 9 HOURS 90Kts 5 3GLH 333 MILES 3 1 HRS 696 MILES 6 5 HRS 103Kts 345 MILES 3 1 HRS 722 MILES 6 5 HRS 6 6 GLH 96 Kts 288 MILES 2 5 HRS 601 MILES 5 2 HRS 97Kts 300 MILES 2 5 HRS 627 MILES 5 22 HRS 101Kts 865 fpm 12 000 ft 509 ft 845 ft 542 ft Date 20 Oct 2011 Page 12 144 Total Distance over 50 ft obstacle STALL SPEED CAS Flaps up power off Flaps down power off Flaps with Robertson Stol System Ramp STANDARD EMPTY WEIGHT MAGIC GS 700 MAXIMUM USEFUL LOAD MAGIC GS 700 BAGGAGE ALLOWANCE WING LOADING Pounds Sq Ft POWER
86. in panel formed leading edge skin and a dorsal The rudder is constructed of a formed leading edge skin Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 96 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 containing hinge halves wrap around skin panel and ribs and formed trailing edge skin with a ground adjustable trim tab at its base The top of the rudder incorporates a leading edge extension which contains a balance weight The horizontal stabilizer is constructed of a forward spar main spar formed sheet metal ribs and stiffeners a wrap around skin panel and formed leading edge skins The horizontal stabilizer also contains Electrical elevator trim tab actuator Construction of the elevator consists of a main spar and bell crank left and right wrap around skin panels and a formed trailing edge skin on the left half of the elevator the entire trailing edge of the right half is hinged and forms the elevator trim tab The leading edge of both left and right elevator tips incorporate extensions which contain balance weights FLIGHT CONTROLS The airplane s flight control system see figure 7 1 consists of conventional aileron rudder and elevator control surfaces The control surfaces are manually operated through mechanical linkage using a control wheel for the ailerons and elevator and rudder brake pedals for the rudder TRIM SYSTEM An electrical opera
87. ist for this airplane can only be found in the appropriate weight and balance records carried in the airplane It is the responsibility of the pilot to ensure that the airplane is loaded properly AIRPLANE WEIGHING PROCEDURES 1 Preparation a Inflate tires to recommended operating pressures b Remove the fuel tank sump quick drain fittings and fuel line drain plug to drain all fuel c Remove oil sump drain plug to drain all oil d Move sliding seats to the most forward position e Raise flaps to the fully retracted position f Place all control surfaces in neutral position 2 Leveling a Place scales under each wheel 500 minimum capacity for scales b Deflate nose tire and or lower or raise the nose strut to center bubble on level see figure 6 1 3 Weighing a With the airplane level and brakes released record the weight shown on each scale Deduct the tare if any from each reading 4 Measuring Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 85 144 Bs SE AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 a Obtain measurement A by measuring horizontally along the airplane center line from a line stretched between the main wheel centers to a plumb bob dropped from the firewall b Obtain measurement B by measuring horizontally and parallel to the airplane center line from center of nose wheel axle left side to a plumb bob dropped from the line
88. ition for speaker operation or in the down position for headphones The center OFF position will remove receiver output to either headphones or the speaker STATIC DISCHARGERS OPTIONAL Installation of wick type static dischargers is recommended to improve radio Communications during flight through dust or various forms of precipitation rain snow or ice crystals Under these conditions the build up and discharge of static electricity from the trailing edges of the wings rudder elevator propeller tips and radio antennas can result in loss of usable radio signals on all Communications and navigation radio equipment Usually the ADF if installed is first to be affected and VHF communication equipment is the last to be affected Installation of static dischargers reduces interference from precipitation static but it is possible to encounter severe precipitation static conditions which might cause the loss of radio signals even with static dischargers installed Whenever possible avoid known severe precipitation areas to prevent loss of dependable radio signals If avoidance is impractical minimize airspeed and anticipate temporary loss of radio signals while in these areas Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 126 144 EXT AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 SECTION 8 AIRPLANE HANDLING SERVICE amp MAINTENANCE TABLE OF CONTENTS Page In
89. jor items of structure are the front and rear carry through spars to which the wings are attached a bulkhead and forgings for main landing gear attachment at the base of the rear door posts and a bulkhead with attaching plates at the base of the forward door posts for the lower attachment of the wing struts Four engine mount stringers are also attached to the forward door posts and extend forward to the firewall The externally braced wings containing the fuel tanks are constructed of a front and rear spar with formed sheet metal ribs doublers and stringers The entire structure is covered with aluminum skin The front spars are equipped with wing to fuselage and wing to strut attaches fit tings The aft spars are equipped with wing to fuselage attach fittings and are partial span spars Conventional hinged ailerons and single slotted flaps are attached to the trailing edge of the wings The ailerons are constructed of a forward spar containing balance weights formed sheet metal ribs and V type corrugated aluminum skin joined together at the trailing edge The flaps are constructed basically the same as the ailerons with the exception of the balance weights and the addition of a formed sheet metal leading edge section The empennage tail assembly consists of a conventional vertical stabilizer rudder horizontal stabilizer and elevator The vertical stabilizer consists of a spar formed sheet metal ribs and reinforcements A wraparound sk
90. l Brakes eene Thitottle Propeller Brakes ei PEN EXER Elevator Control Climb Wing Flaps T 52Kts ENROUTE CLIMB 1 Airspeed 2 3 2 PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC 05 700 Mage 0 10 As required RELEASE FULL OPEN HIGH RPM LIFT NOSE WHEEL at 43 Kts 57 61 Kts 30 MAP MAX Reduce Throttle 29 MAP As required OFF 109 As required ON APPLY FULL OPEN HIGH RPM RELEASE SLIGHTLY TAIL LOW 47Kts until all obstacles are cleared RETRACT slowly after reaching 57Kts FULL OPEN Adjusted 29 MAP As required If a maximum performance climb is necessary use speeds shown in the Rate of Climb chart in section 5 Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 57 144 AIRCRAFT S A CRUISE 1 Power 2 Elevator Trim 3 Propeller BEFORE LANDING Seats Belts Harnesses Auxiliary Fuel Pump Propeller Set throttle LANDI
91. l may perform any and all work on the aircraft for which he holds repairman s certificate For aircraft registered in the Unite Stated FAR 43 defines the types of servicing and maintenance that the certified pilot who owns or operates the aircraft may perform For other countries the registered of that country should be consulted to the fine the work may be performed by appropriately licensed personnel AIRPLANE INSPECTION PERIODS The airplane may require inspections by the issuance of airworthiness directives applicable to the airplane engine propeller and components It is the responsibility of the owner operator to ensure compliance with all applicable airworthiness directives and when the inspections are repetitive to take appropriate steps to prevent inadvertent noncompliance In lieu of the 100 HOURS and ANNUAL inspection requirements an airplane may be inspected in accordance with progressive inspection schedule which allows the work load to be divided into smaller operations that can be accomplished in shorter time periods The IBIS PROGRESSIVE CARE PROGRAM has been developed to provide a modern progressive inspection schedule that satisfies the complete airplane inspection requirements of both the 100 HOUR and ANNUAL inspections as applicable to IBIS airplanes The program assists the owner in his responsibility to comply with all FAA inspection requirements while ensuring timely Original Issue Date 14 January 2011 Revi
92. ll the control wheel lock and chock the wheels In severe weather and high wind conditions tie the airplane down outlined in the following paragraph Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 134 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 TIE DOWN Proper tie down procedure is the best precaution against damage to the parked airplane by gusty or strong winds To tie down the airplane securely proceed as follows 1 Chock the wheels and install the control wheel lock 2 Install a surface control lock between each aileron and flap 3 Tie sufficiently strong ropes or chains 700 pounds tensile strength to the wing and tail tie down fittings and secure each rope to a ramp tie down 4 Install a surface control lock over the fin and rudder 5 Tie a rope no chains or cables to an exposed portion of the Engine mount and secure to a ramp tie down 6 Install a Pitot tube cover JACKING When requirement exists to jack the entire airplane off the ground or when wing jack points are used in the jacking operation refer to the Service Manual for specific procedures and equipment required Individual main gear may be jacked by using the jack pad which is incorporated in the main landing gear strut step bracket When using the individual gear strut jack pad flexibility of the gear strut will cause the main wheel to slide inboard as the wheel is
93. ncreasing the rotation rate and changing the pitch attitude For the purpose of training in spins and spin recoveries a 1 to 2 turn spin is adequate and should be used Up to 2 turns the spin will progress to a fairly rapid rate of rotation and a steep attitude Application of recovery controls will produce prompt recoveries of from 1 4 to 1 2 of a turn If the spin is continued beyond the 2 to 3 turn range some change in character of the spin may be noted Rotation rates may vary and some additional sideslip may be felt Normal recoveries from such extended spins may take up to a full turn or more Regardless of how many turns the spin is held or how it is entered the following recovery technique should be used Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 66 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 1 VERIFY THAT AILERONS ARE NEUTRAL AND THROTTLE IN IDLE POSITION 2 APPLY AND HOLD FULL RUDDER OPPOSITE TO THE DIRETION OF ROTATION 3 JUST AFTER THE RUDDER REACHES THE STOP MOVE THE CONTROL WHEEL BRISKLY FORWARD FAR ENOUGH TO BREAK THE STALL Full down elevator may be required at aft center of gravity loadings to assure optimum recoveries 4 HOLD THESE CONTROL INPUTS UNTIL ROTATION STOPS Premature relaxation of the control inputs may extend the recovery 5 AS ROTATION STOPS NEUTRALIZE RUDDER AND MAKE SMOOTH RECOVERY FROM THE RESULTING DIVE
94. nd are sufficiently accurate for most Right planning purposes However a further correction for the effect of temperature may be made as noted on the climb chart The approximate effect of a non standard temperature is to increase the time fuel and distance by 10 for each IO C above standard temperature due to the lower rate of climb In this case assuming a temperature 16 C above standard the correction would be 16 C 10 16 Increase With this factor included the fuel estimate would be calculated as follows Fuel to climb standard temperature 1 48 gallons Increase due to non standard temperature 1 0 X16 0 2 gallons Corrected fuel to climb 1 5 gallons Using a similar procedure for the distance to climb results in 10 miles The resultant cruise distance is Total distance 120 Climb distance 10 Cruise distance 110 Miles With an expected 10 knot headwind the ground speed for cruise is predicted to be 99 10 89 Miles Therefore the time required for the cruise portion of the trip is 110 Miles 89 Miles 1 23 Hours Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 74 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 The fuel required for cruise is 1 23 hours x 5 3 gallons hour 6 51 gallons The total estimated fuel required is as follows Engine start taxi and takeoff 0 6 Climb 1 5 Cruise 6 51 Total fuel required 8 61 Gallons
95. o trouble proceed to the nearest airport for repairs using the BOTH position of the ignition switch unless extreme roughness dictates the use of a single ignition position Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 46 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Magie MAGNETO MALFUNCTION A sudden engine roughness or misfiring is usually evidence of magneto problems Switching from BOTH to either L or R ignition switch position will identify which magneto is malfunctioning Select different power settings to determine if continued operation on BOTH magnetos is practicable if not switch to the good magneto and proceed to the nearest airport for repairs LOW OIL PRESSURE If low oil pressure is accompanied by normal oil temperature there is a possibility the oil pressure gage or relief valve is malfunctioning A leak in the line to the gage is not necessarily cause for an immediate precautionary landing because an orifice in this line will prevent a sudden loss of oil from the engine sump However a landing at the nearest airport would be advisable to inspect the source of trouble If a total loss of oil pressure is accompanied by a rise in oil temperature there is good reason to suspect an engine failure is imminent Reduce engine power immediately and select a suitable forced landing field Use only the minimum power required to reach the desired touchdown spot
96. on and test requirements for your airplane are detailed in the Service Manual The Service Manual outlines all items which require attention at 50 Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 137 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 100 and 200 hour intervals plus those items which require servicing inspection and or testing at special intervals Since IBIS Dealers conduct all service inspection and test procedures in accordance with applicable Service Manuals it is recommended that you contact your IBIS Dealer concerning these requirements and begin scheduling your airplane for service at the recommended intervals IBIS Progressive Care ensures that these requirements are accomplished at the required intervals to comply with the 100 hour or ANNUAL inspection as previously covered Depending on various flight operations your local Government Aviation Agency may require additional service inspections or tests For these regulatory requirements owners should check with local aviation officials where the airplane is being operated For quick and ready reference quantities materials and specifications for frequently used service items are as follows BATTERY IT DEPENDS ON THE TYPE OF BATTERY The battery should be checked for electrolyte level at each 50 hours inspection and serviced as necessary with distilled water Do not overfill nor shoul
97. ons to protect it from deterioration are recommended It long term storage is required protection from the elements is the primary concern with the IBIS it may be easiest to remove the wings and store it in your garage where you have or can provide some control over temperature and humidity In any case the most susceptible element of your aircraft 5 the engine s cylinder walls and Bering surface The engine should be preserved according to the manufacturer s directions These will essentially require it to have desiccant plugs installed and replace the oil with preservative oil as well as plugging the intake and exhaust ports with a desiccant Again refer to the engine manufacturer for detailed instructions PREPARATION FOR SERVICE Following storage the aircraft preparations or flight should include the following Remove all tape openings plugs and control locks clean and thoroughly inspect the aircraft checking the gear tires control pitot and static ports install a serviced battery install spark plug and check the oil level the preservative oil used for storage should be remove and proper oil installed The fuel tanks should be checked for water accumulation and purged as required Following a short but through engine ground check the aircraft should be flow for 30 minutes maximum and given every through post Flight Inspection SERVICING In addition to the PREFLIGHT INSPECTION covered in Section 4 COMPLETE servicing inspecti
98. or oil consumption has stabilized NOTE The airplane was delivered from the factory with corrosion preventive aircraft engine oil This oil should be drained after the first 5 hours of operation The next oil change is at 25 hours of operation Recommended Viscosity Sport Campion 4T Castrol GTX APIFL Synthetic 10 W 60 SAE 20 W 50 ELF Synthetic 10 W 60 SHELL ELI PLUS 10 W 40 Oil Capacity Sump 3 0 Quarts Total 3 2 Quarts if oil filter installed Oil Temp Max 130 C 266 Min 50 C 122 F Norm 90 C 110 194 F 230 F MAXIMUM CERTIFICATED WEIGHTS Takeoff 1320 Lb Landing 1320 Lb Weight in Baggage Compartment Baggage Area 1 50 Lb The maximum weight capacity for baggage areas is 50 Lb Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 22 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage STANDARD AIRPLANE WEIGHTS Standard Empty Weight IBIS 704 Lb Maximum Useful Load IBIS 616 Lb CABIN ENTRY DIMENSIONS Detailed dimensions of the cabin interior and entry door openings are illustrate in Section 6 BAGGAGE SPACE DIMENSIONS Baggage area dimensions are illustrated in detail in Section 6 SPECIFIC LOADINGS Wing Loading 10 82 Lb 2 Power Loading 13 2Lb hp SYMBOLS ABBREVIATIONS AND TERMINOLOGY GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS KCAS Knots Calibrated Airspeed is indicated airspee
99. otal Capacity 18 us gallons Total Capacity Each Tank 9 us gallons Total Usable 18 us gallons NOTE Due to cross feeding between fuel thanks the tanks should be re topped after each refueling to assure maximum capacity NOTE Takeoffs have not been demonstrated with less than 2 gallons total fuel 1 gallon per tank Approved Fuel 94 Octane Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 32 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Magie PLACARDS The following information is displayed in the individual placards 1 In full view of the pilot The DAY entry shown on the example below will vary as the airplane equipped This airplane is approved in the utility category and must be operated in compliance with the operating limitations as stated in the form of placards markings and manuals MAXIMUMS MANEUVERING SPEED IAS GROSS WEIGHT FLIGHT LOAD FACTOR Flaps Up Flaps Down NO ACROBATIC MANEUVERS INCLUDING SPINGS ARE APPROVED LISTED FLIGHT INTO KNOW ICING CONDITIONS PROHIBITED 2 In the central rear compartment of the Baggage BAGGAGE ALLOWANCE 50 POUNDS MAXIMUM FOR ADDITIONAL LOADING INSTRUCTIONS SEE WEIGHT AND BALANCE DATA 3 Near fuel shutoff valve standard tanks FUEL 18 GAL ON OFF Near fuel shutoff valve Long Range Extra tanks Original Issue Date 14 January 2011 Revision
100. plets or particles in the atmosphere particularly at night can produce vertigo and loss of orientation Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 119 144 g A AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 The high intensity strobe lights will enhance anti collision protection However the lights should be turned off when taxiing in the vicinity of other airplanes or during night flight through clouds fog or haze The most probable cause of a light failure is a burned out bulb however in the event any of the lighting systems fail to illuminate when turned on check the appropriate circuit breaker If the circuit breaker has opened white button popped out and there is no obvious indication of a short circuit smoke or odor turn off the light switch of the affected lights reset the breaker and turn the switch on again do not reset it CABIN VENTILATING SYSTEM Full ventilation air may be obtained by utilization of Dual adjustable fresh air vents near the upper left and right corners of the Windshield Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 120 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 NOLLV ILLN3A 318visnfrav A Y a lt 2 E gt Lx gt D NOILV ILLN3A 318visnrav Figure 7 8 Cabin Heating Ventilating and defrosting System Original Issu
101. r performance figure with reasonable accuracy SAMPLE PROBLEM The following sample flight problem utilizes information from the various charts to determine the predicted performance data for a typical flight The following information is known AIRPLANE CONFIGURATION Takeoff weight 1320 Pounds Usable fuel 18 5 Gallons TAKEOFF Field pressure altitude 1000 feet Temperature 82 F 60 F above standard Wind component along runway 12 Knot Headwind Field length 500 feet Date 14 2011 Revision 02 Date 20 Oct 2011 Page 72 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 CRUISE Total distance 120 MPH Miles Pressure altitude 5500 Feet Temperature 68 F 61 F above standard Expected wind enrooted 10 knot Headwind LANDING Field pressure altitude 2000 Feet Temperature 77 25 Field length 705 Feet TAKEOFF The takeoff distance chart figure 5 4 should be consulted keeping in mind that the distances shown are based on the short field technique Conservative distances can be established by reading the chart at the next higher value of altitude and temperature For example in this particular sample problem the takeoff distance information presented for a pressure altitude of 2000 feet and a temperature of 30 should be used and in the following Ground roll 594 Feet Total distance to clear a 50 foot obstacle 986 Feet These dis
102. r speeds can be used if abrupt use of the controls is avoided Aerobatics that may impose high loads should not be attempted The important thing to bear in mind in flight maneuvers is that the airplane is clean in aerodynamic design and will build up speed quickly with the nose down Proper speed control is an essential requirement for execution of any maneuver and care should always be exercised to avoid excessive speed which in turn can impose excessive loads In the execution of all maneuvers avoid abrupt use of controls FLIGHT LOAD FACTOR LIMITS Flight Load Factors with maximum take off weight 1320 LB Flaps Up 44 0 2 0G Flaps Down 2 0 gt The design load factors are 150 of above and in all cases the structure meets exceeds loads KINDS OF OPERATION LIMITS The airplane is equipped for day VFR The reference to types of flight operations on the operations on the operating limitations placard reflects equipment installed at the time of Airworthiness Certificate issuance Flight into known icing conditions is prohibited Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 31 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage FUEL LIMITATIONS Fuel Capacity Standard Tanks Total Capacity Each Tank 9 us gallons Reserve tank 2 us gallons Total Capacity 20 us gallons Total Usable 18 5 us gallons Long Range Auxiliary Tanks T
103. r the ammeter In the event an over voltage condition occurs the over voltage sensor alternator automatically removes alternator field current and shuts down the alternator The red warning light will then turn on indicating to the pilot that the alternator is not operating and the battery is supplying all electrical power The over voltage sensor may be reset by turning the master switch off and back on again If the warning light does not illuminate normal alternator charging has resumed however if the light does illuminate again a malfunction has occurred and the flight should be terminated as soon as practical The warring light may be tested by momentarily turning off the ALT portion of the master switch and leaving the BAT portion turned on CIRCUIT BREAKERS AND FUSES Most of the electrical circuits in the airplane are protected by push to reset circuit breakers mounted under the engine controls on the instrument panel The cigar lighter If Installed is equipped with a manually reset type circuit breaker located on the back of the lighter and a fuse behind the instrument panel Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 118 144 EXT AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 GROUND SERVICE PLUG RECEPTACLE IF INSTALLED A ground service plug receptacle may be installed to permit the use of an external power source for cold weather starting and du
104. re airplane 3 Check accuracy of the turn by observing the compass heading which should be the reciprocal of the original heading 4 f necessary adjust heading primarily with skidding motions rather than rolling motions so that the compass will read more accurately 5 Maintain altitude and airspeed by cautious application of elevator control Avoid over controlling by keeping the hands off the control wheel as much as possible and steering only with rudder Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 44 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage EMERGENCY DESCENT THROUGH CLOUDS If conditions preclude reestablishment of VFR flight by a 180 turn a descent through a cloud deck to VFR conditions may be appropriate If possible obtain radio clearance for an emergency descent through clouds To guard against a spiral dive choose an easterly or westerly heading to minimize compass card swings due to changing bank angles In addition keep hands off the control wheel and steer a straight course with rudder control by monitoring the turn coordinator Occasionally check the compass heading and make minor corrections to hold an approximate course Before descending into the clouds set up a stabilized let down condition as follows 1 Reduce power to set up a 500 to 800 ft min rate of descent 2 Adjust the elevator trim for a stabilized descent at 52 Kts 3
105. reme center of gravity locations Within which the airplane must be operated at a given weight Standard Standard Empty Weight is the weight of a standard airplane Empty Weight including unusable fuel operating fluids and full engine oil Basic Empty Basic Empty Weight is the standard empty weight plus the weight Weight of Optional equipment Useful Useful load is the difference between takeoff weight and the basic Load empty weight Gross Gross loaded Weight is the loaded weight of the airplane Loaded weight Maximum Maximum Takeoff Weight is maximum the weight approved for Takeoff the start of the takeoff runs Weight Maximum Maximum Landing Weight is the maximum weight approved Landing for landing touchdown Weight Tare Tare is the weight of chocks blocks stands etc Used when weighing an airplane and is included in the scale readings Tare is deducted from the scale Reading to obtain the actual Net airplane weight Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 26 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 SECTION 2 LIMITATIONS TABLE OF CONTENTS Introduction Airspeed Limitations Airspeed Indicator Markings Power Plant limitations Power Plant Instrument Markings Weight Limits Center of Gravity Limits Maneuver Limits Flight Load Factor Limits Kinds of Operation Limits Fuel Limitations Placards Original Issue Date 14 January 2011
106. ring lengthy maintenance work on the electrical and electronic equipment The receptacle is located behind a door on the left side of the fuselage near the aft edge of the cowling Just before connecting an external power source generator type or battery cart the master switch should be turned ON This is especially important since it will enable the battery to absorb transient voltages which otherwise might damage the transistors in the electronic equipment The battery and external power circuits have been designed to completely eliminate the need to jumper across the battery contactor to close it for charging a completely dead battery An especial fused circuit in the external power system supplies the needed jumper across the contacts so that with dead battery and an external power source applied turning the master switch ON will close the battery contactor LIGHTING SYSTEMS EXTERIOR LIGHTING IF INSTALLED Conventional navigation lights are located on the wing tips and top of the rudder a single landing light is installed in the cowl nose cap and a flashing beacon is mounted on top of the vertical fin and a strobe light on each wing tip All exterior lights are controlled by rocker type switches on the lower left side of the instrument panel The switches are ON in the up position and OFF in the down position The flashing beacon should not be used when flying through clouds or overcast the flashing light reflected from water dro
107. rior to Brake Release Paved Level Dry Runway Zero Wind Notes 1 Prior to takeoff from fields above 500 feet elevation the propeller should be adjusted to give optimum RPM in a full throttle static run up 2 Decrease distances 1096 for each 9 knots of headwind For operation with tailwinds up to 10 knots increase distances by 10 for each 2 knots 3 For operation on a dry grass runway increase distances by 15 of the ground roll figure ALT Ft TOCLEAR GRND TOCLEAR GRND TOCLEAR GRND TOCLEAR GRND TO CLEAR RUN ft 50 ae ft RUN ft 50 OBS ft RUN ft 50 255 ft RUN ft 50 OBS ft RUN ft 50 OBS ft 548 Figure 5 4 Takeoff Distance 2 mE BEEN Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 79 144 wm mum AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 RATE OF CLIMB DATA MAXIMUM Conditions Flaps Up Full Throttle 30 MAP NOTE Propeller adjusted above 500 ft for maximum RPM CLIMB IRATEOFCLIMBFPM CLIMB FPM 1320 S L 2000 57 735 670 600 535 4000 56 635 570 505 445 6000 55 535 475 415 355 8000 54 440 380 320 265 10000 53 340 285 230 175 12000 52 245 190 135 85 Figure 5 5 Rate of Climb Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 80 144
108. rm 8100 2 2 Aircraft Registration Certificate FAA form 8050 3 3 Aircraft Radio Station License if transmitter installed FCC form 556 B To be carried in the airplane at all times 1 Weight and Balance and associated papers latest copy of the repair and alteration foul FAA form 337 if applicably 2 Equipment list C To be made available upon request 1 Airplane Log Book 2 Engine Log Book Most of the items listed are required by the United States Federal Aviation Regulations Since the Regulations of other nations may require other documents and data owners of airplanes not registered the United States should check with their own aviation officials to determine their individual requirements Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 130 144 EXT AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 IBIS recommends that these items plus the Pilot s Operating Handbook Pilot s Checklists Customer Care Program book and Customer Care Card be carried in the airplane at all times NON OWNER BUILT AIRCRAFT If you purchased your IBIS from the builder it then falls under rules of all other aircraft and owner pilot maintenance is significantly restricted It is then treated just as a commercially built aircraft except than is not required for annuals on any A amp P can perform annuals on an amateur built aircraft The original builder stil
109. rts 8 Pull choke knob full on after engine has started Leave on until engine is Running smoothly 9 Oil CHECK 10 GHOKG eod es ri FULL AFT POSITION NOTE If the engine does not start during the first few attempts or if engine firing diminishes in strength it is probable that the spark plugs have been frosted over Preheat must be used before another start is attempted During cold weather operations no indication will be apparent on the oil temperature gage prior to takeoff if outside air temperatures are very cold After a suitable warm up period 2 to 5 minutes at 1000 RPM accelerate the engine several times to higher engine RPM If the engine accelerates smoothly and the oil pressure remains normal and steady the airplane is ready for takeoff Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 69 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Magie NOISE ABATEMENT Increased emphasis on improving the quality of our environment requires renewed effort on the part of all pilots to minimize the effect of airplane noise on the public We as pilots can demonstrate our concern for environmental improvement by application of the following suggested procedures and thereby tend to build public support for aviation 1 Pilots operating aircraft under VFR over outdoor assemblies of persons recreational
110. s the tanks should be re topped after each refueling to assure maximum capacity FILLER CAP LEFT FUEL TANK Figure 7 5 Fuel Quantity Data Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 113 144 g A AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Fuel flows by gravity from the two wing tanks to a fuel shutoff valve With the valve in the ON position fuel flows through a strainer to the carburetor From the carburetor mixed fuel and air flows to the cylinders through intake manifold tubes Fuel system venting is essential to system operation Blockage of the venting system will result in a decreasing fuel flow and eventual engine stoppage Venting is accomplished by an interconnecting line from the right fuel tank to the left tank The left tank is vented overboard through a vent line which is equipped with a check valve and protrudes from the bottom surface of the left wing near the wing strut attach point The right fuel tank filler cap is also vented Fuel quantity is measured by two visual fuel low level indication system one in each side of the cabin The indicators cannot be relied upon for accurate readings during skids slips or unusual attitudes The amount of unusable fuel is relatively small due to the dual outlets at each tank The maximum unusable fuel quantity as determined from the most critical flight condition is about 1 5 gallons total This quantit
111. s need only be wiped off with a damp cloth Oil and grease on the control wheel and control knobs can be removed with a cloth moistened with Stoddard solvent Volatile solvents such as mentioned in paragraphs on care of the windshield must never be used since they soften and craze the plastic Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 144 144
112. sion No 02 Date 20 Oct 2011 131 144 g A AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 replacement of life limited parts and adherence to factory recommended inspection intervals and maintenance procedures IBIS PROGRESSIVE CARE The IBIS PROGRESSIVE CARE PROGRAM has been designed to help you realize maximum utilization of your airplane at a minimum cost and downtime Under this program your airplane is inspected and maintained in four operations at 50 hour intervals during a 200 hour period The operations are recycled each 200 hours and are recorded in a specially provided Aircraft Inspection Log as each operation is conducted The IBIS Aircraft S A recommends Progressive Care for airplanes that are being flown 200 hours or more per year and the 100 hour inspection for all other airplanes The procedures for the Progressive Care Program and the 100 hour inspection have been carefully worked out by the factory and are followed by the IBIS Dealer Organization The complete familiarity of IBIS Dealers with IBIS equipment and factory approved procedures provides the highest level of service possible at lower cost to IBIS owners Regardless of the inspection method selected by the owner he should keep in mind that FAR Part 43 and FAR Part 91 establishes the requirement that properly certified agencies or personnel accomplish all required FAA inspections and most of the manufacturer recommended inspections
113. ssure oil from the cooler returns to the accessory housing where it passes through the pressure strainer screen full flow oil filter if installed The filtered oil then enters a pressure relief valve which regulates engine oil pressure by allowing excessive oil to return to the sump while the balance of the pressure oil is circulated to various engine parts for lubrication Residual oil returns to the sump by gravity flow An oil filler cap oil dipstick is located at the rear of the engine on the right side The filler cap dipstick are accessible through an access door in the engine cowling The engine should not be operated on less than three quarts of oil To minimize loss of oil through the breather fill to three quarts for normal flights for engine oil grade and specifications refer to Section 8 of this handbook IGNITION STARTER SYSTEM Engine ignition is provided by two engine driven magnetos and two spark plugs in each cylinder The right magneto fires the lower right and the upper left spark plugs and the left magneto fires the lower left and upper right spark plugs Normal operation is conducted with both magnetos due to the more complete burning of the fuel air mixture with dual ignition Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 110 144 EXT AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Ignition and starter operation is controlled by a rotary type swit
114. t pilot s or right copilot s if installed set of rudder pedals which are interconnected For maximum brake life keep the brake system properly maintained and minimize brake usage during taxi operations and landings Some of the symptoms of impending brake failure are gradual decrease in braking action after brake application noisy or dragging brakes soft or spongy pedals and excessive travel and weak braking action If any of these symptoms appear the brake system is in need of immediate attention If during taxi or landing roll braking action decreases let up on the pedals and then re apply the brakes with heavy pressure If the brakes become spongy or pedal travel increases pumping the pedals should build braking pressure If one brake becomes weak or fails use the other brake sparingly while using opposite rudder as required to offset the good brake ELECTRICAL SYSTEM Electrical energy see figure 7 7 is supplied by battery with 12 volt 17 amps Hour battery located on the right forward side of the firewall Power is supplied through a single bus bar a master switch controls this power to all circuits except the engine ignition system or flight hour recorder if installed All avionics equipment should be turned off prior to starting the engine or using an external power source if installed to prevent harmful transient voltages from damaging the transistors in this equipment MASTER SWITCH OPTIONAL The mast
115. tances are well within the available takeoff field length However a correction for the effect of wind may be made based on Note 3 of the takeoff chart The correction for a 12 knot headwind is 12 Knots 9 Knots X 10 13 Decrease This results in the following distances corrected for wind Ground roll zero wind 594 Ft Decrease in ground roll 193 feet x 13 77 Ft Corrected ground roll 517 Ft Total distance to clear a 50 feet obstacle zero wind 986 Ft Decrease in total distance 352 feet x 1396 128 Ft Corrected total distance to clear 50 feet obstacle 858 Ft Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 73 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Mage CRUISE The cruising altitude should be selected based on a consideration of trip length winds aloft and the airplane s performance However the power setting selection for cruise must be determined based on several considerations Considerable fuel savings a longer range result when lower power settings are used FUEL REQUIRED The total fuel requirement for the flight may be estimated using the performance information in figures 5 6 and 5 7 For this sample problem figure 5 6 shows that a climb from 2000 Feet to 6000 Feet requires 1 48 gallon of fuel The corresponding distance during the climb is 10 nautical miles These values are for a standard temperature as shown on the climb chart a
116. te 20 Oct 2011 124 144 EXT AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 SUCTION GAUGE OPTIONAL Suction gage if installed is located on the left side of the instrument panel when the airplane is equipped with a vacuum system Suction available for operation of the attitude indicator and directional indicator is shown by this gage which is calibrated in inches of mercury The desired suction range is 4 6 to 5 4 inches of mercury A suction reading below this range may indicate a system malfunction or improper adjustment and in this case the indicators should not be considered reliable STALL WARNING SYSTEM OPTIONAL The airplane is equipped if installed with a pneumatic type stall warning system consisting of an inlet in the leading edge of the left wing an air operated horn near the upper left corner of the windshield and associated plumbing As the airplane approaches a stall the low pressure on the upper surface of the wings moves forward around the leading edge of the wings This low pressure creates a differential pressure in the stall warning system which draws air through the warning horn resulting in an audible warning at 5 to 10 knots above stall in all flight conditions The stall warning system should be checked during the preflight inspection by placing a clean handkerchief over the vent opening and applying suction A sound from the warning horn will confirm that the syst
117. ted elevator trim tab is provided Elevator trimming is accomplished through the elevator trim tab by utilizing the switch mounted trim control Down position of the trim switch will trim nose down conversely up position will trim nose up INSTRUMENT PANEL The instrument panel is designed to place the primary flight instruments directly in front of the pilot The gyro operated flight instruments are arranged one above the other slightly to the left of the control column To the left of these instruments is the airspeed indicator turn coordinator and suction gage If Installed The clock optional altimeter rate of climb indicator and navigation instruments are above and or to the right of the control column Avionics equipment is stacked approximately on the centerline of the panel with space for additional equipment on Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 97 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 the lower right side of the instrument panel right side of the panel also contains the tachometer and additional instruments such as a flight hour recorder Engine instruments positioned right side the pilot s space for control wheel The electrical switches radio ignition master switches and choke are located below de pilot s control wheel The engine controls wing flap switch are to the left of the pilot at the center of the switch an
118. terations on the airplane to ensure that airworthiness of the airplane is not violated Alterations or repairs to the airplane must be accomplished by licensed personnel NOTE Only IBIS approved parts should be used for any repairs to your IBIS Salvage parts whose history cannot be fully traced and their care in storage and handling completely defined and determined acceptable by IBIS aircraft S A are not acceptable and are considered unsafe for use GROUND HANDLING TOWING The airplane is most easily and safely maneuvered by hand with the tow bar attached to the nose wheel When towing with a vehicle do not exceed the nose gear turning angle of 30 either side of center or damage to the gear will result If the airplane is towed or pushed over a rough surface during hangaring watch that the normal cushioning action of the nose strut does not cause excessive vertical movement of the tail and the resulting contact with low hangar doors or structure A flat nose tire or deflated strut will also increase tail height CAUTION Do not exert force on the propeller or control surfaces during towing by hand use care when turning the propeller ASSUME THE MAGNETOS ARE HOT If the nose wheel must be raised apply weight on the rear fuselage forward of the horizontal stabilizer Whit the nose wheel off the ground the aircraft can be pivoted around the main gear as required PARKING When parking the airplane head into the wind insta
119. the throttle be advanced slowly This allows the airplane to start rolling before high RPM is developed and the gravel will be blown back of the propeller rather than pulled into it When unavoidable small dents appear in the propeller blades they should be immediately corrected Prior to takeoff from fields above 500 feet elevation the propeller should be adjusted to give maximum RPM in a full throttle static run up After full throttle is applied adjust the throttle friction lock if installed clockwise to prevent the throttle from creeping back from a maximum power position Similar friction lock adjustment should be made as required in other flight conditions to maintain a fixed throttle setting WING FLAP SETTINGS Normal takeoffs are accomplished with wing flaps 0 10 Using 10 wing flaps reduces the total distance over an obstacle by approximately 1096 Flap deflections Original Issue Date 14January 2011 Revision No 02 Date 20 Oct 2011 Page 62 144 B AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 greater than 10 are not approved for takeoff If 10 wing flaps are used for takeoff they should be left down until all obstacles are cleared and a safe flap retraction speed of 52 Kts is reached On short field 10 wing flaps and an obstacle clearance speed of 47 Kts should be used This speed provides the best overall climb speed to clear obstacles when taking into account turbul
120. tins for tolerances and repairs WARNING Use care when handling the propeller insure that the magnetos are off the throttle closed Then remain as clear is possible during the dressing operation Be prepared for a cylinder to fire when moving the propeller to a new position Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 143 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 INTERIOR CARE To remove dust and loose dirt from the upholstery and carpet clean the interior regularly with a vacuum cleaner Blot up any spilled liquid promptly with cleansing tissue or rags Don t pat the spot press the blotting material firmly and hold it for several seconds Continue blotting until no more liquid is taken up Scrape off sticky materials with a dull knife and then spot clean the area Oily spots may be cleaned with household spot removers used sparingly Before using any solvent read the instructions on the container and test it on an obscure place on the fabric to be cleaned Never saturate the fabric with a volatile solvent it may damage the padding and backing materials Soiled upholstery and carpet may be cleaned with foam type detergent used according to the manufacturer s instructions To minimize wetting the fabric keep the foam as dry as possible and remove it with a vacuum cleaner The plastic trim headliner instrument panel and control knob
121. tions make an approach at 47 Kts with 30 flaps using enough power to control the glide path After all approach obstacles are cleared progressively reduce power and maintain 47 Kts by lowering the nose of the airplane Touchdown should be made with power off and on the main wheels first Immediately after touchdown lower the nose wheel and apply heavy braking as required For maximum brake effectiveness retract the flaps hold full nose up elevator and apply maximum brake pressure without sliding the tires Slightly higher approach speeds should be used under turbulent air conditions CROSSWIND LANDING When landing in a strong crosswind use the minimum flap setting required for the field length Use a wing low crab or a combination method of drift correction and land in a nearly level attitude BALKED LANDING In a balked landing go around climb the wing flap setting should be reduced to 20 immediately after full power is applied Upon reaching a safe airspeed the flaps should be slowly retracted to the full up position COLD WEATHER OPERATION Prior to starting on cold mornings it is advisable to pull the propeller through several times by hand to break loose or limber the oil thus conserving battery energy NOTE When pulling the propeller through by hand treat it as if the ignition switch is turned on A loose or broken ground wire on either magneto could cause the engine to fire In extremely cold
122. troduction 8 129 Identification Plate 8 129 Airplane File 8 130 IBIS Progressive Care 8 132 IBIS Customer Care Program 8 132 Pilot Conducted Preventive Maintenance 8 133 Alterations Or Repairs 8 133 Ground Handling 8 134 Towing 8 134 Parking 8 134 Tie Down 8 135 Jacking 8 135 Flyable Storage 8 136 Servicing 8 137 Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 127 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Fuel 8 140 Landing Gear 8 141 Cleaning And Care 8 141 Windshield Windows 8 141 Painted Surfaces 8 142 Propeller Care 8 143 Interior Care 8 144 Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 128 144 EXT AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 INTRODUCTION This section contains factory recommended procedures for proper ground handling and routine care and servicing of your IBIS It also identifies certain inspection and maintenance requirements which must be followed if your airplane is to retain that new plane performance and dependability It is wise to follow a planned schedule of lubrication and preventive maintenance based on climatic and flying conditions encountered in your locality Keep in touch with your IBIS Dealer and take advantage of his knowledge and experience He knows your airplane and how to maintain it He will remind you when lubrications and oil changes are
123. tude and temperature read the true airspeed shown on the rotatable ring by the indicator pointer For best accuracy the indicated airspeed should be corrected to calibrated airspeed by referring to the Airspeed Calibration chart in Section 5 Knowing the calibrated airspeed read true airspeed on the ring opposite the calibrated airspeed RATE OF CLIMB INDICATOR The rate of climb indicator depicts airplane rate of climb or descent in feet per minute The pointer is actuated by atmospheric pressure changes resulting from changes of altitude as supplied by the static source Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 122 144 g A AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 ALTIMETER Airplane altitude is depicted by a barometric type altimeter A knob near the lower left portion of the indicator provides adjustment of the instrument s barometric scale to the current altimeter setting VACUUM SYSTEM AND INSTRUMENTS OPTIONAL An engine driven vacuum system if installed see figure 7 9 is available and provides the suction necessary to operate the attitude indicator and directional indicator The system consists of a vacuum pump mounted on the engine a vacuum relief valve and vacuum system air filter on the aft side of the firewall below the instrument panel and instruments including a suction gage on the left side of the instrument panel ATTITUDE INDICATOR OPTIONA
124. uarts To minimize loss of oil through breather fill to 3 quart level for normal flights of less than 3 hours For extended flight full to 3 quarts These quantities refer to oil dipstick level readings During oil and oil filter changes one additional part is required when the filter is changed OIL AND OIL FILTER CHANGE The airplane was the delivered from the factory with oil in the engine during the first 5 hours oil must be changed and then minimum of each 50 hours of flight time The engine oil should be drained while the engine is thoroughly warm with the aircraft in a level position The filter should be change at each oil change and the element examined for its contents Sand type material is indicative of inadequate air filtration and may warrant corrective action ranging for more frequent changes to the installation of and improved filter system Metallic particle may vary from aluminum to steel to stainless steel Following the initial break in period during which some metallic particles are normal almost any amount becomes cause for concern If subsequent change should additional metallic particles the source should be determined The type can be somewhat determined by separating by category i e magnetic or not steel or aluminum silicon sand etc Another method of determining the source is the use spectral analysis of an oil sample Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 139 144 g
125. val This aircraft is to be operated in compliance with information and limitations contained herein The original English Language edition of this manual has been approved as operating instruction according the legislations applicable and in force by the above authority Approval of translation has been done by best knowledge and judgment Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 6 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 This Data Sheet provides basic information about the IBIS Magic 05 700 airplane A Data Sheet must be completed for these aircraft and then return a copy to the company The Data Sheet stays with the aircraft and must be amended each time major changes are made to the configuration performance or characteristics of the aircraft WARNING This aircraft is not required to comply with the safety regulations for standard aircraft PERSONS FLY IN THIS AIRCRAFT AT THEIR OWN RISK AIRCRAFT TYPE AIRCRAFT TYPE MODEL SERIAL No AIRCRAFT BUILDER NAME CONTACT PHONE FAX ADDRESS AIRCRAFT DETAILS DATE OF CONSTRUCTION DATE OF FIRST FLIGHT WING SPAN WING AREA Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 7 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Magie A C LENGTH WING CHOR
126. who owns or operates an airplane not used as an air carrier is authorized by FAR Part 43 to perform limited maintenance on his airplane Refer to FAR Part 43 for a list of the specific maintenance operations which are allowed NOTE Pilots operating airplanes of other than U S registry should refer to the regulations of the country of certification for information on preventive maintenance that may be performed by pilots A Service Manual should be obtained prior to performing any preventive maintenance to ensure that proper procedures are followed Your IBIS Dealer should be contacted for further information or for required maintenance which must be accomplished by appropriately licensed personnel ALTERATIONS OR REPAIRS In the interest of safety we strongly recommended that you seek experienced consultation before making any modification to your IBIS We take pride in your IBIS as well and have your interest heart Any modifications or change that affect the airworthiness or that is considered a mayor change must be approved by the factory Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 133 144 g A AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 If you want to make any modifications contact IBIS aircraft S A for advice In any case the work must be performed by properly licensed personnel It is essential that the IBIS aircraft S A be contacted prior to any al
127. windshield unless freezing rain or sleet is anticipated since the cover may scratch the polycarbonate plastic surface PAINTED SURFACES The painted exterior surfaces of your new IBIS have a durable long lasting finish and under normal conditions require no polishing or buffing Approximately 30 days are required for the paint to cure completely in most cases the curing period will have been completed prior to delivery of the airplane In the event that polishing or buffing is required within the curing period it is recommended that the work be done by someone experienced in handling uncured paint Generally the painted surfaces can be kept bright by washing with water and mild soap followed by a rinse with water and drying with cloths or a chamois Harsh or abrasive soaps or detergents which cause corrosion or scratches should never be used Remove stubborn oil and grease with a cloth moistened with Stoddard solvent Waxing is unnecessary to keep the painted surfaces bright However if desired the airplane may be waxed with a good automotive wax A heavier coating of wax on the Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 142 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 leading edges of the wings and tail and on the engine nose and propeller spinner will help reduce the abrasion encountered in these areas CAUTION Avoid the use of high pr
128. ximum Recommended Turbulent Air Penetration Speed pog p M IH 90Kts ix A 82Kts 450 6T 78Kts Maximum Demonstrated Crosswind Velocity 12Kts Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 52 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Visually check airplane for general condition during walk around inspection In cold weather remove even small accumulations of frost ice or snow from wing tail and control surfaces Also make sure that control surfaces contain no internal accumulations of ice or debris Prior to flight check that pitot heater if installed is warm to touch with 30 seconds with battery and pitot heat switches on Figure 4 1 Preflight Inspection Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 53 144 AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 Magie CHECKLIST PROCEDURES PREFLIGHT INSPECTION 1 CABIN 2 Control Wheel Lock REMOVE If installed 3 Ignition Switch OFF 4 Master Switch OFF 5 Fuel Quantity Indicators CHECK QUANTITY Visual 6 Master OFF 7 Fuel Valve ON OFF OFF
129. y while a 6 turn spin and recovery may require somewhat more than twice that amount For example the recommended entry altitude for a 6 turn spin would be 6000 feet above ground level In any case entries should be planned so that recoveries are completed well above the minimum 1500 feet above ground level required by FAR 91 71 Another reason for using high altitudes for practicing spins is that a greater field of view is provided which will assist in maintaining pilot orientation The normal entry is made from a power off stall As the stall is approached the elevator control should be smoothly pulled to the full aft position Just prior to reaching the stall break rudder control in the desired direction of the spin rotation should be applied so that full rudder deflection is reached almost simultaneously with reaching full aft elevator A slightly greater rate of deceleration than for normal stall entries or the use of partial power at the entry will assure more consistent and positive entries to the spin Both elevator and rudder controls should be held full with the spin until the spin recovery is initiated An inadvertent relaxation of either of these controls could result in the development of a nose down spiral NOTE Careful attention should be taken to assure that the aileron control is neutral during all phases of the spin since any aileron deflection in the direction of the spin may alter the spin characteristics by i
130. y was not exceeded by any other reasonable flight condition including prolonged 30 second full rudder sideslips in the landing configuration Takeoffs have not been demonstrated with less than 2 gallons total fuel 1 gallon per tank The fuel system is equipped if installed with drain valves to provide a means for the examination of fuel in the system for contamination and grade The system should be examined before the first flight of every day and after each refueling by using the sampler cup provided to drain fuel from the wing tank sumps and by utilizing the fuel strainer drain The fuel tanks should be filled after each flight to prevent condensation When the airplane is equipped with long ranger tanks it may be serviced to a reduced fuel capacity to permit heavier cabin loadings This is accomplished by filling each tank to the bottom of the indicator on the fuel filler neck When filled to this level the tank contains 9 gallons 8 25 usable in all flight conditions Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 114 144 EXT AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL MODEL MAGIC GS 700 BRAKE SYSTEM The airplane has a single disc hydraulically actuated brake on each main landing gear wheel Each brake is connected by a hydraulic line to a master cylinder attached to each of the pilot s rudder pedals The brakes are operated by applying pressure to the top of either the lef
131. zation backed by the IBIS Customer Services Department stands ready to serve you The following services are offered by most IBIS Dealers e THE IBIS WARRANTY which provides coverage for parts and labor is available at IBIS Dealers worldwide Specific benefits and provisions of warranty plus other important benefits for you are contained in your Customer Care Program book supplied with your airplane Warranty service is available to you at authorized IBIS Dealers throughout the world upon presentation of your Customer Care Card which establishes your eligibility under the warranty FACTORY TRAINED PERSONNEL to provide you with courteous expert or service e FACTORY APPROVED SERVICE EQUIPMENT to provide you efficient and accurate workmanship ASTOCK OF GENUINE IBIS SERVICE PARTS on hand when you need them e THE LATEST AUTHORITATIVE INFORMATION FOR SERVICING IBIS AIRPLANES since IBIS Dealers have all of the Service Manuals and Parts Catalogs kept current by Service Letters and Service News Letters published by IBIS Aircraft S A We urge all IBIS aircraft owners to use the IBIS Dealer Organization to the fullest A current IBIS aircraft Dealer Directory accompanies your new airplane The Directory is revised frequently and a current copy can be obtained from your IBIS Original Issue Date 14 January 2011 Revision No 02 Date 20 Oct 2011 Page 14 144 B AIRCRAFT S A PILOT S OPERATING HANDBOOK AND FLIGHT MANUAL M

IBIS MAGIC GS-700 FLIGHT MANUAL

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