Flight Design CT-LSA Pilot Operating Handbook CT2K & CTSW LSA
Contents
1. Choke Brake Trim tab ss I S SE 12 ls 5 lt S US 3 4 amp I MO x em E E 28 HS 3 nw ies SS a S Throttle UU b aec p 1 ML Flap position indicator Ignition switch and starter 2 ignition 1 ignition 21 2 ignition 0 starter AU 01 0 01 000 Original Issue Date 28 02 2005 off Revision Date 05 10 2005 Pilot Operation Handbook Page 20 Flydat Rotax for water cooled 4 stroke engine 912 ULS EGT PTO CHT OIL TEMP 2 1 min T F d STATUS FLYdat DATA d i T EGT display PSI MEMORY EGT MAG LEFI RIGHT OIL PRESS v WARNING using t is mperative frat you read the Operator s Manual its entirety If you do not ungerstand everything in fe do not use fis instrumen Display panel Description Unit Resolution RPM iei cose rite NMIN I NN Operation hours DOS 0 1 op Exhaust gas temperature AS F 1 or 10 HO Exhaust gas temperature MS F 1 or 10 Cylinder head temperature 2 1 5 rn Oil temperature i a ai a pi cere 1 Bo EE Oll pressure2. 15 4242 Eoad lero ee PE 15 4 6 Prohibited maneuvers 16 5 Weight and Balance Information esse 21 54 Installed equipment 21 5 2 Center of gravity CG range and 26 p Performante scooter a alu ast O ata at O Eta aa ala 27 6 1 Takeoff and landing distances 27 6 25 dale OEGI TID ad cune uen o dece CU Ulud LSE DUM 27 ia dot bd tox pui pdt Re oa A pui pnt coi 27 DA RPM oir erat iet 27 6 5 Fuel consumption sedentes penc teg euet acad a Ses Cus ou 27 7 Emergency Procedures ame ce oa sree at a add sete 28 B 30 9 1 lt lt 30 8 2 Engine 222 aa ca ai aaa aa aa aa aaa a aaa aa LE 31 oa APEI IC de atlet dat dai dt dt 32 8 4 Nornnaltakeolfusesi oet loa apa e a aie ial oa e preste lit 32 8 5 Best angle of climb Speed V de cit ee dud ai ba 33 62555 5 Gic paenitet CATH E Du R 33 Ou ADpIOSED GI ENTRE
3. 33 8 8 Normal landin eere tec rene ene eee ca eene ees ener ev et 33 8 9 Short field takeoff and landing procedures 34 8 10 Balked landing procedures ccce cocco crecen eec eee cae 34 8 11 Information on stalls spins and any other useful pilot information 34 9 Aircraft Ground Handling and 35 9 1 Servicing fuel oil and CoolBEllL ee 35 9 2 Towing and tie down instructions 35 10 Required Placards and 36 10 1 Airspeed indicator range 36 10 2 Operating limitations on instrument panel 36 10 3 Passenger Warning 5 e eee oaia tore D ex ek pud 36 Original Date 28 02 2005 AU 010 01000 Revision Dato 05102006 10 4 NO INTENTIONAL SPINS Gne 36 10 5 Miscellaneous placards and 36 11 Supplementary Information 37 11 1 Familiarization flight 37 12 PROVISIONS LATERI Ra te 37 Origina
4. 5 8 psi ERU Y RE cio dcum 0 15 bar 2 2 psi NOTE Exceeding the max admissible fuel pressure will override the float valve of the carburetor The delivery pressure of an additional backing pump e g electric standby pump must not exceed 0 3 bar 4 4 psi in order not to override the float valve Original 1 Date 28 02 2005 AU 010 01000 Revision Date 05102008 a Pilot Operation Handbook _ Aircraft Type CT LSA FLIGHT DESIGN Page 11 Operating speeds and limits 912 ULS S 1 Speed Take off speed 5800 1 min 5 min Max continuous speed 5500 1 min Idle speed cues ca 1400 1 min 2 Performance ISA International Standard Atmosphere Take off performance 73 5 kW at 5800 1 min Max continuous performance 69 kW at 5500 1 min 3 Acceleration Limit of engine operation at zero gravity and in negative g conditions MAK soak aiias oc inc ora dor 5 seconds at max 0 5 g 4 Oil pressure su cen en eee 7 bar ATTENTION For short period admissible at cold start IPRC EN 0 8 bar 12 psi below 3500 rpm normal cecinit 2 0 5 0 bar 29 73 psi above 3500 rpm 5 Oil temperature 130 266 F mibi cea t ca ce ad e a da 50 C use 120 F normal operating temperature ca 90 110
5. PS 0 1 X Indicator of cylinder series for which the exhaust gas temperature is indicated NOTICE Arrowhead pointer symbolizes left cylinder series Arrowhead pointer symbolizes right cylinder series Switching of exhaust gas temperature is carried out in 6 8 sec intervals Rotax 912UL 912 ULS Indicator Unit Warning limits RPM rotation speed 1 min 5800 EGT Exhaust gas temperature F 1616 CHT cylinder head temperature UL F 300 CHT cylinder head temperature ULS F 284 Oil temperature UL 285 Oil temperature 015 266 pressure max PSI 102 pressure min PSI 12 Oil pressure normal PSI 29 73 Original Date 28 02 2005 AU 010 01000 Revision Da 05102006 Pilot Operation Handbook Page 21 At exceeding one or more warning limits they are indicated on the display blinking and the alarm lamp blinks At exceeding one or more not permissible values alarm limit values they are also indicated on the display blinking and the alarm lamp blinks with long term blinking Rotax Operation Manual should always be followed 5 Weight and Balance Information 5 1 Installed equipment list A 10000 Airplane CT2K LSA SPORT version ready to fly Equipment Drooped tips reduce induced drag and increase directional stability 3 tones paint inside the cabin 2 components outside paint white 2 layers Swiss or German aeronautical windows with green tone
6. Check the coolant level on the Rotax overflow bottle and add more if needed Check the oil level and add more if needed The oil level should be between the two markings max min of the oil dipstick and should not be lower than the minimum mark in any case Before a long term engine operation the oil level should be in the middle of two marks at least Carefully examine the oil cooling and fuel system for leaks e n case of the any equipment the engine should not be started before proper maintenance is performed Check that all visible bolts fastened and secured e Incase of cracks or scratches on the paint finish their cause must be determined Repair if necessary 8 1 Preflight check Check the fuel in both tanks using the dipstick Check that the tank vents are clear Make sure both tank caps are closed tightly Move the fuel valve lever to on This exposes the starting key switch Remove possible water from fuel system and control fuel flow by draining the fuel gascolator Check fuel for contamination If contaminated drain until fuel is clear Make certain the control stick and rudder pedals are free Check flaps Run the flaps to each of the settings within normal operating range of 6 12 to 40 and watch for corresponding indicator readings Specifically watch that for 6 and 40 settings the indicator must not blink Otherwise refer to the CT
7. Rotax 912 012 80 HP ready to fly installed Airbox amp Carburetor heating RPM meter Oil pressure Oil temperature Cylinder head water temperature measurer Large Battery Rotax engine guarantee Propeller Neuform ground adjustable Ground adjustable Neuform propeller with Spinner and Spinner plate already mounted Flight and service manual B 00010X Addition on price 912 ULS 100PS n Sec S Rotax 912 ULS with big Starter instead 912 UL2 C 00203X Add On Warp Drive 3 Blade Prop w L E protection C 00205 Add On Neuform 3 Blade Prop Black amp White Z 11020X Rotax slipper clutch Protection against shock loading of engine by ground contact of propeller Z 15101X Add on price Rotax FlyDat F amp PSI Digital engine information system instead of analog instruments black box 4 EGT 1 CHT oil temp RPM hours oil pressure Warning when maximum values are exceeded D 12300X BRS 1350 Rescue system Mounted belts inside structure D 12200X BRS front harness Special BRS Kevlar belts instead of standard belts Z 10010 3 Axes trim system manual Manual stabilizer Rudder Aileron Wheel trim Z 10020X TruTrack Digitrak 1 Axes Autopilot not certified Aileron Z 10025X Pictoral Pilot 1 Axes Autopilot not certified Aileron amp turn amp bank indicator Z 10030X TruTrack DigiFlight 2 Axes Autopilot not certified Ailero
8. Minimum fuel two passenger and baggage most rearward CG mi Xi xi mi Ib kg ft m Ib ft kg m Empty aeroplane 666 302 1 03 0 314 685 8 95 Rescue system 28 5 13 4 17 1 27 119 4 17 Passengers 501 227 1 71 0 52 853 7 118 Baggage 109 50 3 58 1 09 3942 55 Fuel 17 5 8 0 98 0 3 17 4 2 Total weight 1320 600 2070 5 286 3 CG location 1 565 0 477 CG location in MAC percent 40 896 Full fuel tank and light passenger most forward CG mi Xi xi mi Ib kg ft m Ib ft kg m Empty aeroplane 666 302 1 08 0 314 685 8 95 Rescue system 0 0 4 17 1 27 0 0 0 Passengers 119 54 1 71 0 52 203 1 28 Baggage 0 0 3 58 1 09 0 0 0 Fuel 205 93 0 98 0 3 201 8 28 Total weight 990 449 1090 7 151 CG location 1 102 0 335 CG location in MAC percent 27 6 AU 010 01000 Original Issue Date 28 02 2005 Revision Date 05 10 2005 Pilot Operation Handbook Page 15 4 Operating Limitations 4 1 Stalling speeds at maximum takeoff weight Vs and Vso flaps 6 12 44 kts 43 kts flaps 0 Vs 42 kts 41 kts flaps 40 Vso 39 kts 37 kts 4 2 Flap extended speed range Vsoto Vre Maximum speed with flaps extended to 0 is 100kts to 15 is 80kts to 30 is 62kts to 40 is 62kts 4 3 Maximum maneuvering speed V 98 6 kts 100 5 kts 113 mph 115 4 mph Up to the speed Va all control surf
9. Spins In the case of a stall spin entered through crossed controls Oppose a spin with opposite rudder input Center the ailerons and elevator until the rotation stops then level out the airplane gently If the attempt to level out the airplane fail or leveling out is doubtful because of too low altitude the emergency parachute system if equipped should be actuated Banked turn Each of turns should be made with the coordinated use of the aileron and rudder Steep turns in excess of 60 degrees are not recommended At lower speeds in tight turns the airplane loses altitude quickly Banked turns with more than 30 of banking should not Original 1 Date 28 02 2005 AU 010 01000 juu Revision Date e 00102008 Pilot Operation Handbook Page 35 be carried out less than 54 kts 62 mph If the airplane enters an inadvertent spin push the rudder opposite the spin direction Position the control stick in neutral position for recovery After the spin rotation stops recover to level flight carefully to not exceed Vne or the load limits of the aircraft 9 Aircraft Ground Handling and Servicing 9 1 Servicing fuel oil and coolant To fill up the fuel tank one person is needed 1 Make sure the plane is set on the parking brake Put a support or ladder on the ground near by the wing next to the fuel cap Open the fuel cap Pour in the fuel per specification Check the needed amount of the fuel by the dipstick after pouring Clos
10. 0 15 30 40 flap indicator Oil quality SAE 15 W 40 oil tank Circuit Breakers left side of the central console Main Circuit Breakers right side of the central console Maintenance packing interval BRS Manual amp Chute placard Baggage Compartment max 55 Lbs each side Baggage area Original Issue Date 28 02 2005 AU 010 01000 2 Pilot Operation Handbook Page 37 11 Supplementary Information 11 1 Familiarization flight procedures For familiarization flight procedure refer to the Flight Training Supplement 12 Hevisions The Revisions pages are updated by Flight Design each time revision is issued They contain a list of all revisions made to the Pilot Operation Handbook since its original issue Revision No Date Affected Affected Approved By Released Chapters Pages Original Issue 28 02 2005 N A N A 2 General Information 6 8 3 Airplane and Systems 13 14 Descriptions l 200 2095 4 Operating Limitations 15 17 19 10 Required Placards 36 and Markings 4 5Crosswind and wind 15 limitations 6 Performance 27 8 2 Engine starting 31 2 05 10 2005 Normal takeoff 32 8 5 Best angle of climb 33 speed 8 6 Cruise 10 5Miscellaneous 36 placards and markings Original 1 Date 28 02 2005 AU 010 01000 Revision Date 00102008
11. 190 230 F 6 Cylinder head temperature Mak REN 284 reading at observation point of the hotter cylinder head either no 2 or no 3 T Engine start operating temperature ES 120 F cere 225 C 13 F 8 Fuel pressure sae tege 1 0 4 5 8 psi TER 0 15 bar 2 2 psi NOTE Exceeding the max admissible fuel pressure will override the float valve of the carburetor The delivery pressure of an additional backing pump e g electric standby pump must not exceed 0 3 bar 4 4 psi in order not to override the float valve More engine data is available in the Rotax operation manual supplied with the aircraft 3 2 Propeller 1 Neuform TXR2 65 47 101 6 2 blade composite propeller ground adjustable standard 2 Warp Drive 3 blade Tapered tip Ground adjustable propeller with HPL R hub optional 3 Neuform carbon fiber three blade CR3 65 47 101 6 optional Original 1 Date 28 02 2005 AU 010 01000 Revision Date 05 102008 Pilot Operation Handbook _ Aircraft CT LSA Page 12 3 3 Fuel and fuel capacity Fuel specification Premium Automotive Unleaded per ASTM D 4814 minimum AKI 89 for Rotax 912UL and minimum AKI 91 for Rotax 912ULS For complete fuel specifications see the original Rotax Operator s Manual Fuel capacity 2 wing fuel tanks 17 16gal 651 each 34
12. 65 Best rate of climb 885 fpm 4 5 m s at Vv 78 kts 89 mph at 5100 RPM at 0 flaps position 6 3 Cruise speeds For 912 ULS and Neuform TXR2 65 Maximum cruising speed at 75 112 kts 129 mph max range ability with 1320 Lbs 600 Kg 783 nm 900 Miles 6 4 RPM ROTAX 912 UL 912 ULS Take off performance 4500 4800 Max continuous performance 5500 Min RPM before take off 4400 RPM 4700 RPM Idle speed 1400 1500 RPM Maximum RPM Redline 5800 RPM max 5 min Cruising flight RPM 4200 5500 RPM 75 Percent cruise RPM 5200 RPM 6 5 Fuel consumption Fuel consumption at take off power 5 12 Gph 19 I h Fuel consumption at cruising power 3 44 5 82 Gph 13 22 I h Fuel consumption at 5500 RPM 6 88 Gph 26 I h For more engine data refer to the Rotax Operator s Manual supplied with the airplane Original 1 Date 28 02 2005 AU 010 01000 Revision Date 05 102008 Pilot Operation Handbook Page 28 7 Emergency Procedures Stalls The loss in altitude during stalls is approximately 165ft with a maximum pitch down of 25 In the case of a stall spin entered through crossed controls Oppose a spin with opposite rudder input Center the ailerons and elevator until the rotation stops then level out the airplane gently If the attempt to level out the airplane fail or leveling out is doubtful because of too low altitude the emergency parachute system if equipped should be actuated Engine failure At
13. Adjustable seats length and height 4 points safety belts for each seat 2 luggage compartments accessible from outside amp inside Fabric cover for the luggage compartments Luggage security hooks in the luggage compartment 2 lockers on the cabin floor Huge cockpit with three single instrument panels Inspection door on cowling for quick oil and water check Extra wide cabin doors with gas struts Dual controls 3 Axis Pre installed bridges for BRS Parachute system Plexiglas inspection window for bellcrank Manual stabilizer trim by lever Electrical flap for 12 to 40 with pre selector switch Switch board panel with circuit breakers Combination key switch Central fuel valve 2 wing tanks for 17 gallons 34 gallons Steerable spring damped front wheel Hydraulic disk brakes Flight Instruments Airspeed indicator in knots Three point altimeter Magnetic compass Slip amp bank indicator Original 1 Date 28 02 2005 AU 010 01000 Revision Da 05 102005 Pilot Operation Handbook Aircraft CT LSA Page 22 Engine Rotax 912 UL2 80 HP ready to fly installed Airbox amp Carburetor heating Tachometer Large Battery Rotax engine guarantee Propeller Neuform ground adjustable Ground adjustable Neuform propeller with Spinner and Spinner plate already mounted Fli
14. LSA Maintenance Manual Check that the main spar bolts are secure Check that the trim system is functioning Check that all the hinge points are free Check that all the wing control surfaces are secure and free Check the stabilator attach bolts for security Check that the trim tab is bolted and the spring pin is secured Check that the Pitot tube cover is removed Check that the Pitot tube is clear Check the conditions of the tires Check the tire air pressure 28 PSI Check that the wheel pants and fairings are secure Check that the air intakes for the oil cooler water radiator and cylinder air cooling are clear Original 1 Date 28 02 2005 AU 010 01000 Revision Dato 05 102005 8 2 Pilot Operation Handbook Page 31 Check that the propeller is free and without nicks or defects Check the spinner attachment In the case of baggage is carried check that it is properly fastened Follow the weight and balance loading plan For solo flight check that the passenger side harness is fastened and door is closed Engine starting Checklist before engine start Check that the Pre flight checklist is completed Check that the baggage doors are closed Check that the pilot and the passenger harnesses are fastened correctly Check that the emergency parachute system is ready for operation Check that the safety pin is removed Check that the elevator trim tab is set Check that the altimeter is set Check tha
15. an altitude of less than 330 ft no attempt to re start the engine should be made Below and altitude of 820 ft no attempt to return to the runway should be made Choose a landing spot without trees or obstacles and with sufficient length Below an altitude of 165 ft any turns are to be avoided because of increased loss of in altitude and or control Keep a minimum speed of 54 kts 62 mph until final approach In case of landing on a field with crops or in a forest Look for a flat spot in the plants treetops or bushes e For final approach the flap position should be 40 degrees and airspeed should be 43 kts 50 mph on short final The final flair for landing should be carried out at a height of about 1 5 ft over the chosen spot e Ignition should be turned off The elevator control should be fully pulled back Carburetor In case of engine fire shut down the engine take out the key close the fuel valve full open throttle Slip away from the location of the smoke if possible land as quickly as possible perform an emergency landing If the fire is extinguished and there is no emergency landing possibility without engine help insert the key and try to start the engine again if it starts land as quickly as safely possible e If the airplane is not under control during a fire or there is no emergency landing possibility the optional parachute system should not be used at higher altitudes The airplane sh
16. cooled during the landing approach and rollout therefore it can be stopped through ignition switching off The radios and instruments should be switched off before stopping the engine 8 9 Short field takeoff and landing procedures Set the airplane fully on brakes Set flaps on 15 position Apply full power maximum RPM Release the brakes Pull the control stick at stall speed 44kts 8 10 Balked landing procedures If the runway and approach to the runway are clear Apply the throttle smoothly to fully open forward Engine speed 4800 5300 RPM Pull the control stick backward smoothly as airspeed builds up to 55kts Climb to a minimum altitude 350ft Set the flaps to 15 position Climb to a minimum height of 600 ft in straight ahead flight at 59 kts 68 mph before attempting to turn the aircraft Do notreduce the flaps to below 09 with less than 59 kts 68 mph airspeed 8 11 Information on stalls spins and any other useful pilot information Stalls Refer to Operating Limitations section for stalling speeds The stall is noted through light buffeting At 2 kts 3 mph above the stall speed the rudder becomes soft When flying close to stall speed only the rudder and elevator are fully controllable The ailerons have less effectiveness in very slow flight The airplane loses about 165 ft in altitude during a stall Close to the ground do not fly slower than a minimum speed of about 62 kts 72 mph
17. 32gal 1301 total 3 4 Oil For complete oil specifications see the original Rotax Operator s Manual Cil Motorcycle oil of a registered brand with gear additives If using aircraft engine oil than only blonded one n ATTENTION At the selection of suitable lubricants refer to the additional information in the Service Information 18 UL 97 Cil specification Use only oil with API classification SF or SG Due to the high stresses in the reduction gears oils with gear additives such as high performance motor cycle oils are required Because of the incorporated friction clutch oils with friction modifier additives are unsuitable as this could result in a slipping clutch during normal operation dury 4 stroke motor cycle oils meet all the requirements These oils are normally no mineral oils but semi or full synthetic oils Oils primarity for Diesel engines are due to insufficient high temperature properties and additives which favour clutch slipping generally unsuitable n ATTENTION If the engine is mainly run on AVGAS more frequent oil changes will be required See Service Information 18 UL 97 Cil capacity 31 min 2 I 6 4 liq pt min 4 2 liq pt Oil consumption max 0 1 I h 0 2 liq pt h Oil viscosity see Chapter 10 of the Rotax Operator s Manual Use of multi grade oils is recommended 3 5 Operating weights and loading occupants baggage fuel ballas
18. 54 i SS e 4 E 1 E 1 a e e 111 i glo y Y Original 1 28 02 2005 AU 010 01000 Revision Date 05102005 Pilot Operation Handbook Page 8 Areas ft Wing 116 25 Stabilator 17 745 Vertical fin 12 978 Aspect ratio Wing 8 Stabilator 3 4 Original 1 Date 28 02 2005 AU 010 01000 Revision Date 05102005 Pilot Operation Handbook Page 9 3 Airplane and Systems Descriptions 3 1 Engine NOTE for actual and complete information read the Rotax operation manual supplied with the aircraft Type 912 4 horizontally opposed normal aspirated engine Description of design 4 stroke 4 cylinder horizontally opposed spark ignition engine one central camshaft push rods OHV Liquid cooled cylinder heads Ram air cooled cylinders Dry sump forced lubrication Dual breakerless capacitor discharge ignition 2 constant depression carburetors Mechanical fuel pump Prop drive via reduction gear with integrated shock absorber and overload clutch Electric starter 12V 0 6 kW Integrated AC generator with external rectifier regulator 12V 20A DC Propeller gearbox OIZULTATF 912 ULS7S 2 27 1 crankshaft propeller shaft 2 43 1 2 43 1 optional For the engine type 912 two reduction ratios are available Depending on engine type certification and configuration the propeller gearbox is supplied with or without an over
19. Flight Design CT LSA Pilot Operating Handbook CT2K amp CTSW LSA Sport Models FLIGHT DESIGN SERIAL NUMBER THIS DOCUMENT AND THE TECHNICAL DATA HEREON DISCLOSED ARE PROPRIETARY TO FLIGHT DESIGN AND SHALL NOT BE USED RELEASED OR DISCLOSED IN WHOLE OR IN PART WITHOUT EXPRESS WRITTEN PERMISSION FROM FLIGHT DESIGN 1 Table of Content Flight Design CT LSA Pilot Operating 1 17 Pales Content eu Segue Shes inr idt uer bon TEN ERA RIP UL Ed UE 2 2 General a 4 Airplane and Systems Descriptions 9 adu a 9 9 25 Propeller ee I P 11 3 9 Fueland fuel capacity LEE 12 Qub And a SU DIS D aa 12 3 5 Operating weights and loading occupants baggage fuel ballast 12 4 Operating EImltetlODs eeste eot eee 15 4 1 Stalling speeds at maximum takeoff weight VS1 and VS0 15 4 2 extended speed range VSO to 15 4 3 Maximum maneuvering speed VA eene 15 4 4 Never exceed speed 15 4 5 Crosswind and wind 15 4 0 Service
20. Reinforcement of fuselage amp fin clutch mirror special cooler Z 14100X Add On Reinf of fusel for towing no fin amp clutch Z 14200X Add On Re Fusel amp fin for towing no Clutch Z 13090X Custom made instrument panels Standard Z 13090 1X Custom made instrument panels aluminum 2 13090 2 Custom made instrument panels mahogany Z 13090 2X Custom made instrument panels ash ice blue Z 13090 3X Custom made instrument panels grey Z 16000 2 ASI in mph Z 16000 3 ASI in kts Z 16000 4 ASI in kts amp mph Z 16100 2 Altimeter in hg Z 13070X N Numbers Ordering and mounting of registration number AU 010 01000 Revision Date Original Issue Date 28 02 2005 05 10 2005 a Pilot Operation Handbook _ Aircraft Type CT LSA FLIGHT DESIGN Page 26 5 2 Center of gravity CG range and determination Range of center of gravity 13 110 18 740 333 476 mm behind the leading edge of wing Note that while determining the center of gravity the aircraft must be level The center of gravity is normally located behind the leading edge of wing Spanwise location of the datum is not important as the wings are rectangular and un tapered A Weight and Balance Sheet is supplied with each plane The example of it is shown below Weight amp Balance and Equipment List Tricycle Gear AC Model CTSW Name Model Producer Serial Nr 05 01 02 ASI 6FMS443 Winter Motor Nr 4406791 Altimeter ALT20MBF 3 FALCON Techni
21. aces can be fully deflected Maximum speed in turbulent air Vra Vra 120 kts 138 mph At the speed Vna the aircraft supports a vertical gust of 50 ft s 15 24 m sec without being structurally overloaded 4 44 Never exceed speed Vie 145 kts 166 6 mph Note that the maximum operating speed for BRS1350 emergency parachute system is 178 kts From Va to Vye only use of 1 3 of the maximum deflections of the control surfaces is allowed 4 5 Crosswind and wind limitations Maximum direct cross wind components for take off and landing with flaps from 6 to 15 16 13 kts with flaps more than 15 to 40 13 11 kts Cross wind take offs and landings demand a lot of training and skill the higher the crosswind component the greater your skill must be In gusty wind or wind speed more than 21 kts 24 mph flight operations should be stopped 4 6 Service ceiling Maximum service ceiling is about 14 000ft about 4 250m 4 7 Load factors From Vso up to Vne 49 2 9 Original 1 Date 28 02 2005 AU 010 01000 Revision Date 00102008 Pilot Operation Handbook Page 16 4 8 Prohibited maneuvers The CT LSA is not certified for aerobatics Steep turns beyond 60 should not be performed Other limitations Flights are only to be made under VFR conditions Night flights require special optional equipment Flights in icing conditions not allowed Structures and Systems Description Fuselage Wing The fuselag
22. b ft kg m Empty aeroplane 658 3 299 1 02 0 31 669 7 93 Parachute system 28 6 13 4 17 1 27 119 2 17 Passengers 505 3 230 1 71 0 52 864 120 Baggage 110 50 3 58 1 09 393 8 55 Fuel 17 5 8 0 98 0 3 17 2 2 Total weight 1320 600 2063 9 285 CG location 1 56 0 475 CG location of MAC 40 6 Full fuel tank and light passenger most forward mi Xi xi mi Lb kg ft m Lb ft kg m Empty aeroplane 658 3 299 1 02 0 31 669 7 93 Parachute system 0 0 4 17 1 27 0 0 Passengers 120 54 1 71 0 52 2052 28 0 0 3 58 1 09 0 0 Fuel 205 93 0 98 0 3 201 8 28 Total weight 983 446 1076 7 149 CG location 1 09 0 333 location of MAC 28 4 Original Date 28 02 2005 AU 010 01000 Revision Date 00102008 Pilot Operation Handbook Page 14 Typical loading configurations for CT2K Full fuel tank two passengers most forward CG for maximum takeoff weight mi Xi xi mi Ib kg ft m Ib ft kg m Empty aeroplane 666 302 1 03 0 314 685 8 95 Rescue system 0 0 4 17 1 27 0 0 0 Passengers 452 205 1 71 0 52 771 0 107 Baggage 0 0 3 58 1 09 0 0 0 Fuel 205 93 0 98 0 3 201 8 28 Total weight 1320 600 1658 6 229 3 CG location 1 25 0 382 CG location in MAC percent 32 6 Full tank accommodates 34 32 US gal 130 litres of fuel that multiplied by the fuel density of 6 Ib gal 0 72 kg litre weighs 205 Ib 93 34 kg
23. cal data according data sheet Compass Airpath Variometer VSI Tachometer ROTAX Radio Oilpressure gauge Oiltemp gauge Watertemp gauge Leading Edge Top of fuselage tunnel Emply weight 300 2 kg 259 8 kg Battery SBS8 Rescue system BRS Fly Dat 491 2 kg Clock Al Horizon Reference gross kg tare kg net kg Arm mm from G1 61 0 a 870 from G2 239 2 b 1450 Weight G 300 2 Transponder Turn and Bank GPS ELT Towhook Autopilot CG empty according G2 b G a empty CG limits from 280 to 320 at 300 2 kg Fedchun Kherson Ukraine 27 01 2005 Weighed by Location Date Original 1 Date 28 02 2005 AU 010 01000 Revision Date 00102008 Pilot Operation Handbook Aircraft CT LSA Page 27 6 Performance The performance figures stated below are given at the sea level of the international standard atmosphere conditions Operations at higher altitudes and temperatures will reduce takeoff and climb performance 6 1 Takeoff and landing distances Take off range over 50 Ft 15 m obstacle with 13201 912 ULS engine and Neuform TXR2 65 propeller on an asphalt runway is 762ft Landing distance over 50ft 15m obstacle is 967ft Liftoff speed with 15 of flaps 40kts 46mph 6 2 Rate of climb For 912 ULS and Neuform TXR2
24. diately after icing clears push it back in again For normal cruising flight bring the airplane to the desired cruising speed in level flight by observing the VSI or the altimeter Adjust the throttle and trim to hold altitude 8 7 Approach Land into the wind or the runway with the least crosswind if possible The final approach to landing is to be carried out in level attitude Engine power at about 10 20 96 slightly above idle to confirm that the engine still has power Approach speed about 54 kts 62 mph with experience a slightly slower approach speed can be used Flaps from 15 to 40 In case of carburetor icing hazard pull the carburetor heating 8 8 Normal landing At the distance of 3 ft over the ground close the throttle and land the airplane gently If engine cools too much in descent with the engine at idle and won t increase RPM pull the choke and then increase throttle Close the choke again When landing with crosswind perform a crabbing approach or slip carefully The flights over obstacles during approach to landing should be avoided Control of the emergency transmitter ELT if equipped Before switching off the radio equipment adjust frequency to the international emergency frequency 121 5 and check if the ELT is activated Original 1 Date 28 02 2005 AU 010 01000 Revision Date 05 102008 Pilot Operation Handbook Page 34 Engine stop Under normal conditions the engine is sufficiently
25. duty machined aluminum rods Brakes Hydraulic disk type actuated through a handbrake lever Parking brake is set by simultaneous use of the brake knob and valve Control surfaces The movable surfaces of the CT LSA are of aramid foam aramid carbon foam aramid carbon foam carbon sandwiches with carbon fiber spars and attachment points Original 1 Date 28 02 2005 AU 010 01000 rev no Revision Date 05 10 2005 Pilot Operation Handbook Page 17 Rudder Conventional type with balance Activated by the foot pedals with cables Stabilator Al moving type with trim tab and balance actuated with a ball bearing push pull connected to the twin cockpit located control sticks Ailerons Frise type Controlled with push pull tubes and rod bearings The ailerons move simultaneously with the flaps together from 0 to 6 12 The ailerons also droop automatically with the flaps for reduced stalling speed Flaps Slotted type Pre selector switch activated from 6 to 40 12 to 40 The flap position is indicated on the screen of the flap position indicator on the control panel The flaps run to the next setting selected and are protected by limit switches at the end limits 6 to 40 12 to 40 6 12 09 15 30 40 settings are available Do not exceed the maximum flap extended speed Vre as stated item 4 2 Stabilator Trim System Activated with the wheel near the throttle and choke c
26. e of the CT LSA is made of multiple layers of carbon fiber and aramid Kevlar laminated over a dense foam core creating a sandwich structure The cabin can resist loads from all sides This provides superior pilot and passenger crash protection and low structural weight Wings The cantilevered wing of the CT LSA plugs into 4 hard points at the top of the cabin for attachment to the fuselage The overlapping spars resist lift loads The main spar caps are solid carbon fiber wrapped with S glass fibers over a dense Rohacell core The wing skin is a carbon fiber sandwich The ribs are molded carbon fiber and bonded into place Wingtips The wingtips of the CT are highly developed drooped type They reduce stall speed improve stability and low speed control of the CT Fuel system Fuel is supplied from the two wing tanks by gravity feed with a total capacity of 34 Gallon The ignition key cannot be inserted unless the fuel valve is in the on position Electric system The Rotax 912 series engines have a lighting coil type alternator with a rectifier regulator converting and regulating the accessory voltage to a nominal 13 5 V 14 2V 250W roughly 18A The battery for the electric starting system is 12V sealed AGM type The dual ignition system is a CDI capacitive discharge Landing gear The landing gear of the CT is of tricycle type The nose wheel is steerable through a direct link to the rudder pedals The main gear legs are heavy
27. e the cap and make sure the fuel cap vent is directed to the front Make sure that no spilled fuel is on the plane Remove if necessary NI To service oil one person is required 1 Remove the top cowling Make sure the ignition and both main circuit breakers are OFF Turn the propeller 3 to 4 times counter clockwise standing in front of the aircraft Open the oil tank cap and check the level of the oil by the dipstick Add oil if necessary Close the cap ORAON To service the coolant one person is needed 1 Remove the top cowling Open the cap of the coolant tank and add coolant to fill up the tank Make sure the ignition and both main circuit breakers are OFF Turn the propeller 3 to 4 times counter clockwise standing in front of the aircraft Make sure that no air is inside the cooling system Close the coolant tank cap If necessary add coolant to the expansion tank AO S po Do 9 2 Towing and tie down instructions To tow the aircraft one person is required 1 Make sure the aircraft is off the parking brake 2 Make sure the space near the aircraft is clear of obstacles and people 3 Push the tail beam of the aircraft down to lift the nose gear off the ground 4 Push the aircraft in needed direction To tie the aircraft down one person is needed 1 Make sure the plane is set on the parking brake 2 Attach the tiedown lines to tiedown rings on the wings 3 Attach the lines to the mooring arran
28. er Flight Design CT LSA is a VFR aircraft only Because of the high cruising speed and range of the CT LSA flight into vastly different weather patterns and meteorological conditions can occur The entry into bad weather with IFR conditions by VFR pilots and aircraft is extremely dangerous As the owner or operator of an aircraft you are responsible for the safety of your passenger and yourself Do not attempt to operate CT LSA in any manner that would endanger the aircraft the occupants or persons on the ground Manufacturer Flight Design GmbH Sielminger Str 65 D 70771 L Echterdingen Description of the aircraft Flight Design CT LSA is being delivered in two configurations CT2K and CTSW as shown below CT LSA is a three axis control high wing two seats light sport aircraft of normal scheme with a cruciform tail The primary structures are made of carbon fiber reinforced plastic The aircraft is equipped with an all moving stabilator with a trim tab and tricycle landing gear with a steerable nose wheel Original 1 Date 28 02 2005 AU 010 01000 Revision Date 05 102008 Views dimensions CTSW inches Pa Ss N gt Original Date 28 02 2005 AU 010 01000 Revision Date 05102005 Areas ft Wing Stabilator Vertical fin Aspect ratio Wing Stabilator AU 010 01000 107 4 17 745 12 978 7 29 3 4 Original Issue Date 28 02 2005
29. gements on the ground Make sure the lines ate tightened Original 1 Date 28 02 2005 AU 010 01000 Revision Dato 05102006 Pilot Operation Handbook Page 36 10 Required Placards and Markings 10 1 Airspeed indicator range markings White range flap operating range 39 62 kts Green range normal operating range 44 120 kts Yellow range structural warning area 120 145 kts Red line never exceed speed 145 kts 10 2 Operating limitations on instrument panel MAX RPM 5800 EGT 1616F CHT 284F Oil Temp 266F Oil Press 102psi 10 3 Passenger Warning The warning This aircraft was manufactured in accordance with Light Sport Aircraft airworthiness standards and does not conform to standard category airworthiness requirements is placed at the top of the cabin on the spar box passenger side 10 4 NO INTENTIONAL SPINS The placard INTENTIONAL SPINS is placed under the airspeed indicator 10 5 Miscellaneous placards and markings Type of Fuel 2 x beside filling cap MINIMUM 91 Octane Auto Fuel or 100 LL AvGas 16 5 Useable Red marking 5800 RPM Tachometer Red marking max 102psi min 12psi oil pressure gauge Red marking 266 F for ULS 285 F for UL oil temperature gauge Red marking 300 F for UL 284 Ffor ULS water temp gauge cylinder head Throttle lever box Choke lever box Stabilator Trim lever box Brakes lever box Flaps 6 0 15 30 40 flap indicator 12
30. ght and service manual A 10050 Airplane CTSW LSA SPORT version ready to fly Equipment Short wings with Drooped tips reduce induced drag and increase directional stability 3 tone paint inside the cabin 2 components outside paint white 2 layers Swiss or German aeronautical windows with green tone Adjustable seats length and height 4 point safety belts for each seat 2 luggage compartments accessible from outside amp inside Fabric cover for the luggage compartments Luggage security hooks in the luggage compartment 2 lockers on the cabin floor Huge cockpit with three single instrument panels Inspection door on cowling for quick oil and water check Extra wide cabin doors with gas struts Dual controls 3 Axis Pre installed bridges for BRS Parachute system Plexiglas inspection window for bellcrank Manual stabilizer trim by lever Electrical flap for 6 to 40 with pre selector switch Switch board panel with circuit breakers Combination key switch Central fuel valve 2 wing tanks for 17 Gallons 34 Gallons Steerable spring damped front wheel Hydraulic disk brakes Flight Instruments Airspeed indicator 3 Point altimeter Magnetic compass Slip amp bank indicator AU 01 0 01 000 Revision Date 05 10 2005 Original Issue Date 28 02 2005 Pilot Operation Handbook Page 23 Engine
31. l 1 Date 28 02 2005 AU 010 01000 Revision Date 09102008 Pilot Operation Handbook Page 4 In accordance with the specification F 2245 DESIGN AND PERFORMANCE OF A LIGHT SPORT AIRCRAFT each of CT LSA airplanes includes a Pilot Operating Handbook POH The content and format herewith is defined by F 2245 Additional to F 2245 items are considered where necessary All fight speeds are given in terms of calibrated airspeeds CAS All specifications and limitations are determined from the specification F 2245 2 General Information Read this before your first flight Every pilot has to understand the limitations and specifications of this light sport aircraft The Pilot Operating Handbook must be read thoroughly Please pay attention to the pre flight and daily checks Maintenance instructions for the aircraft are given in a separate Maintenance Manual For maintenance of the Rotax engine BRS emergency parachute system if equipped and other installed equipment refer to the original manufacturers manuals Flight Design CT LSA is being delivered in two configurations CTSW and CT2K hereafter referred to as the CT LSA Both configurations are equipped with non certified engines that meet Practice F 2339 Unless otherwise specified the data are common for both configurations Note where different CT2K data are given in square brackets Flying CT LSA must always be done with the possibility of a safe landing due to loss of the engine pow
32. load clutch Original 1 Date 28 02 2005 AU 010 01000 Revision Date 05102006 LT Pilot Operation Handbook _ Aircraft Type CT LSA FLIGHT DESIGN Page 10 Operating speeds and limits 912 UL A F 1 Speed Take off speed 5800 1 min 5 min Max continuous speed 5500 1 Idle speed ca 1400 1 min 2 Performance ISA International Standard Atmosphere Take off performance 59 6 kW at 5800 1 min Max continuous performance 58 kW at 5500 1 min 3 Acceleration Limit of engine operation at zero gravity and in negative g conditions maX Sete dada atata ted ed 5 seconds at max 0 5 g 4 Oil pressure ur qp 7 bar n ATTENTION For a short period admissible at cold start M Ee ES PROS 0 8 bar 12 psi below 3500 rpm normal 2 5 5 2 0 5 0 bar 29 73 psi above 3500 rpm 5 Oil temperature d 140 285 F 50 120 F normal operating temperature ca 90 110 190 230 6 Cylinder head temperature irte tiet 15006 uie 300 F reading at observation point of the hotter cylinder head either no 2 or no 3 7 Engine start operating temperature 50 120 ES 256Q usps 13 F 8 Fuel pressure MaX iiec edd 0 4 bar
33. n amp Stabilizer Z 10040X TruTrack DigiFlight IIVS 2 Axes Autopilot not certified Aileron amp Stabilizer with vertical steering Z 15451 2X Vertical speed indicator ft min Z 15452X Add on price three pointer Altimeter Z 10200X KX 125 NAV COM VOR Intercom 2 place High Noise Environment Stereo 2 PTT push bottoms 2 Antenna s 2 Peltor Head sets ready mounted TSO amp FAA certified AU 010 01000 Revision Date Original Issue Date 28 02 2005 05 10 2005 Pilot Operation Handbook Aircraft CT LSA Page 24 AU 01 0 01 000 Revision Date 05 10 2005 Z 10300X 97 A Com Intercom 2 place High Noise Environment Stereo 2 PTT push bottoms 2 Antenna s 2 Peltor Head sets ready mounted TSO not certified FAA certified Z 10400X King KT 76 A Mode A C Transponder mont Incl Antenna and altitude encoder ACK A 30 Z 10650X Skyforce IIIC enhanced Atlantic Intl Incl antenna and data cable cockpit mounted Z 10651X Garmin 296 Preparation Cable metal frame Z 10700X ELT Emergency transmitter required in Austria completely mounted TSO amp FAA certified 2 10100 Comfort package not Section S Z 10110X Heating system with stainless steel muffler Z 10120X Wheel and landing gear fairings Z 10150X 12V connector 2 10160 Additional MECAPLEX double fresh air windows in door windo
34. n longer runways If it is possible take off directly into the wind The maximum direct crosswind component at take off is 16 kts 18 5 mph As soon as the airplane accelerates gently pull back on control stick keep the nose wheel slightly elevated until the airplane takes off e After take off release the back pressure on the stick slowly as airspeed builds to 59 kts 68 mph Climb to a minimum height of 600 ft in straight ahead flight at 59 kts 68 mph before attempting to turn the aircraft Do notreduce the flaps to below 09 with less than 59 kts 68 mph airspeed Climb Decrease the flaps to 6 and increase the climb speed to 86kts 100 mph Original Date 28 02 2005 AU 010 01000 Revision Dato 05102008 Pilot Operation Handbook Page 33 8 5 Best angle of climb speed V Best angle of climb speed is 66 kts with flaps at 0 Best rate of climb speed V For 912 ULS engine and Neuform TXR2 65 78 kts 89 mph at 5100 RPM at 0 flaps position at rate of climb 885 fpm 4 5m s 8 6 Cruise During cruising flight an RPM of 4200 5500 RPM should be used redline is 5800 RPM The maximum permissible speed of 145 kts 167 mph should not be exceeded During cruising flight monitor your fuel consumption and total fuel on board for flight planning Fuel consumption at cruising flight is about 4 7 gallons 18L per hour In case of possible carburetor icing pull on the carburetor heat imme
35. ontrols Forward nose down back nose up Aileron Trim System if equipped Activated with the wheel on the top of the tunnel between the pilots Right right bank left left bank Rudder Trim System if equipped Activated with the wheel on the bulkhead right above the tunnel Right right turn left left turn Optional BRS Parachute system Also see separate BRS instruction manual Rocket deployed emergency parachute system Actuated through the red T handle above the console or tunnel between the seats The parachute is secured on the ground with a safety and tag Remove pin for flight operations case of emergency pull the handle hard out to the stop Original 1 Date 28 02 2005 AU 01001000 rev no Revision Date 00102008 Standard equipment with Flydat List and Positions of the Operation Elements Sidestip Indicator Altimeter Heating Carburettor heating Battery charging indicator Speed indicator Alarm Compass Rotax Flap position indicator Pedals Flap switch Control stiek N Switch pannel Main Circuit Breaker 35 A lenition fock Stait Main Circuit Breaker 25 A Lever box Rescue system Aileron Trim mm Rudder 1m Original 1 Date 28 02 2005 AU 010 01000 Revision Date 05 102008 Pilot Operation Handbook _ Aircraft CT LSA Page 19 Control Box
36. ould be flown down to 700 ft 200 m and then the system operated After landing leave the airplane immediately Original Date 28 02 2005 AU 010 01000 Revision Da 05 102005 Pilot Operation Handbook Page 29 Optional 5 Parachute system The data and directions in the 5 1350 LSA Parachute Manual concerning the emergency parachute system should be followed The 5 parachute system has shown the ability to be used for low altitudes as well In an emergency the parachute system should be activated even if at a very low altitude Before activating if possible stop the engine and tighten the pilot and passenger harnesses The parachute system handle is located above the central console between the seats To activate the system the handle has to be pulled to the stop Overturn on land Carefully unfasten the seat belts and lower yourself first then your passenger Becareful of any spilled fuel there be a fire hazard e Leave the airplane immediately Original 1 Date 28 02 2005 AU 010 01000 Revision Date 09102008 Pilot Operation Handbook Page 30 8 Normal Procedures Daily flight check At the start of every new flying day the CT should be checked thoroughly An accidental engine start is very dangerous that is why you must always ensure that the ignition and main switch are turned off Make sure that the throttle and choke controls are free from friction and binding
37. t Minimum load per seat 120 Ib 54 kg Maximum weight per seat 260 Ib 118 kg Empty weight standard 659 3 Ib 665 9lb 299 kg 302kg Maximum permissible take off weight 1320 Ib 600 kg Maximum baggage weight for each side 55 Ib 25 kg Weighing Put the airplane on three scales or one scale with leveling blocks on a plane surface Make certain the plane is leveled using a bubble level put onto the console also called tunnel between the seats Mark the wheel axle positions on the ground using a plumb Original 1 Date 28 02 2005 AU 010 01000 Revision Date 05 102008 Pilot Operation Handbook Page 13 Typical loading configurations for CTSW Full fuel tank two passengers most forward CG for maximum takeoff weight mi Xi xi mi Lb kg ft M Ib ft kg m Empty aeroplane 658 3 299 1 02 0 31 669 7 93 Parachute system 0 0 4 17 1 27 0 0 Passengers 455 208 1 71 0 52 778 1 108 Baggage 0 0 3 58 1 09 0 0 Fuel 205 93 0 98 0 3 201 8 28 Total weight 1320 600 1649 6 229 CG location 1 25 0 380 location of MAC 32 5 Full tank accommodates 34 32 US gal 130 litres of fuel that multiplied by the fuel density of 6 Ib gal 0 72 kg litre weighs 205 Ib 93 34 kg Minimum fuel two passenger and baggage most rearward CG mi Xi xi mi Lb kg ft m l
38. t the wind direction is known Check that the doors are closed and secured Door lever is forward and latch pins visible Check that the radio and other equipment are switched off before starting the airplane Check that the immediate area around the airplane is clear of persons and obstacles especially around the propeller Engine start Fuel valve open Choke with cold engine pull backwards on Throttle level idle position Carburetor heat off Main safety devices Parachute ELT if equipped on All electrical equipment for example radio equipment off Pull the brake lever backwards and fasten the parking brake on Ignition both circuits on Ignition key turn to start position on Crank the engine for a maximum of 10 sec Allow the starter to cool for two minutes if the engine does not start As soon as the engine starts set the throttle level in such a way that the engine runs smoothly at minimum RPM Check the oil pressure immediately it should increase during 10 sec Move the choke forward to close Run the engine until warm at a middle RPM 2 min 2000 1 min then 2500 1 min until the oil temperature rises to 124 F Switch on additional instruments for example radio strobe light position lights GPS ELT Set brakes Original Date 28 02 2005 AU 010 01000 Revision Da 05 102005 Pilot Operation Handbook Page 32 Perform a check on both of the ignition circuits at 4000 RPM the ma
39. ws Z 10170X Additional map holders in the cockpit Z 10130X Door locks Z 10140X Parking brake 2 10180 ACL amp Position lights green white red not certified for night flight Extra capacity heater for very low out side S ADIT Bin peturi 2 10161 Photowindow Add On price instead of ventilation window Z 10200x Tundra Wheels w wheel fairings Stainless steel bolts amp nuts special surface treatment metal parts for float attachment Z 10230 Amphibfloats Czech Artworks 1300 Floats complete mounted Z 10240 Skis additionally to the normal landing gear Z 10250 Part 91 compliant Night Light Package 2 13050 Black leather seats add on price Seats and stick base covered with same leather 2 13050 2 Light Brown leather seats add on price Seats and stick base covered with same leather 2 13060 Three color design 2 13060 1 Three color decals SN 1 Original Issue Date 28 02 2005 Pilot Operation Handbook Page 25 Z 13060 2 Three color decals SN 2 Z 13060 3 Three color decals SN 3 Z 13060 4 Three color decals SN 4 Z 13061 1 Three color decals SW 1 Z 13061 2 Three color decals SW 2 Z 13061 3 Three color decals SW 3 Z 13061 4 Three color decals SW 4 Z 13068X 1 colour Special paint only bright colours Colors according RAL standard only Z 13069X Custom made decals Colors according chart Z 14000X Add On Aero towing equipped
40. ximum allowable drop in RPM is 300 and 120 RPM difference between the two circuits e airplane rolls and cannot be stopped with the brakes the engine should be stopped immediately The airplane tends to roll more easily on asphalt or with a tail wind even with the engine at idle e The nose wheel is directly linked to the rudder pedals for taxiing takeoff and all maneuvers on the ground After practice the airplane can be taxied in crosswinds up to 17kts 20 mph 8 3 Taxiing Before takeoff Make certain the oil temperature is at least 124 F Confirm again both doors are secured Confirm the pilot and the passenger harnesses are properly fastened Check that the controls are free and correct Confirm the main switch and the ignition are on both circuits Choke is closed Check that the alternator warning light is off Do not take off with the red light on Set the flaps to 09 159 Confirm the trim lever is set for takeoff Check that the radio frequency and the squelch are set Check that the runway and taxiways are clear Check that the brakes are off Make certain the clear takeoff distance is sufficient 8 4 Normal takeoff If the runway and approach to the runway are clear Roll out to the take off position Confirm the nose wheel is centered Controls are in proper position for takeoff Apply the throttle smoothly to fully open forward Engine speed 4400 4900 RPM Flaps 15 0 is fine o
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