4. NORMAL PROCEDURES
Contents
1. OFF Alternator switch OFF Anti collision OFF Ria EXTENDED Master switch OFF Tank selector switch CLOSED 4 3 16 Manoeuvres For any aerobatics manoeuvre e the overall weight of the aircraft must be less than 780 kg 1 720 Ib e centre of gravity must be forward of 26 96 e aft tank must be empty use fwd tank Minimum recommended speeds when beginning trick Single seater Two seater Manoeuvres km h kt km h kt Loop 220 119 230 124 Split S 210 113 220 119 Slow roll 220 119 230 124 Snap manoeuvre 140 76 140 76 Inverted loop 250 135 270 146 Wingover 200 108 200 108 Electrical flaps system switched off in category A A C equipped with an electrical tab switch system off in category A Original issue 31 January 2002 Document 1000809 GB Page 4 14 Revision 0 NORMAL PROCEDURES CAP 10C 4 3 17 Stalls You can perform stalls with or without engine in all permitted weight and C G configurations Generally stalling is not preceded by warning signs Only the indicator light comes on in a positive stall In negative flight stalls must always happen in clean configuration 4 3 18 ELT The emergency beacon must be removed by the pilot or a mechanic before any aerobatic flight 42. 120 km h 65 kt Original issue 31 January 2002 Document 1000809 GB Page 4 12 Revision 0 NORMAL PROCEDURES CAP 10C 4 3 14 Interrupted landing Go around Configuration cccccececeeseeeeeeeeeeeeeeeees FULL THROTTLE Full flaps Best rate of climb speed Vy 135 km h 73 kt SL 15 To obtain the best rate of climb Vz max keep full power and check the engine speed for 2 350 rpm retract flaps adjust speed for best rate of climb i e 160 km h 86 kt and check pressures and temperatures In category A these performance levels are improved in relation to reduction in weight 4 3 15 Engine shut down Parking brake ON If brakes are used intensively during landing and taxiing up to the parking area do not apply the parking brake before the wheels have cooled down use chocks Electrical equipment OFF Cut off test 1 000 rpm DONE then 1 2 For a short taxiing period before shut down let the engine run for 1 one minute at 1 100 rpm Engine speed 1 100 rpm Original issue 31 January 2002 Document 1000809 GB Page 4 13 Revision 0 NORMAL PROCEDURES CAP 10C SIT CHECKED Mixture LEAN Magnetos
3. 5 min if use intended Takeoff is authorised when the oil temperature reaches the green zone 4 3 6 Taxiing Parking brake RELEASED Brakes and conjugation test DONE When starting off make certain the tail wheel conjugation is operative by checking that the aircraft responds correctly to rudder pedal movements 4 3 7 Run up Te APPLIED use the pedals Temperatures and pressures CHECKED le ot FULL RICH Magnetos check at 1 800 rpm 1 then 1 2 2 then 1 2 Permitted engine drop 125 rpm per magneto Maximum difference between magnetos 50 rpm e aa uu E OE test Magnetos cut off test lt iig qz que LEAN then RICH Original issue 31 January 2002 Document 1000809 GB Page 4 9 Revision 0 NORMAL PROCEDURES CAP 10C 4 3 8 Vital actions before takeoff Engine Tank selector switch FWD AINONOMY E CHECKED Mixture SET MAX POWER Master switch ON Alternator switch ON Battery charge CHECKED E ei cp cdicrccosvunadapsitevetsemncisaveidecieenstas 1 2 Flight controls Elevator free in c
4. hinges and control Elevator tab hinges and control Tail wheel Tail wheel rubber Good condition Conjugation springs Condition and operation Aft left fuselage Static port EE CLEAN NOT CLOGGED Tank drains qty 2 CHECKED Inspection door under fuselage Closed and locked BET CAD CLOSED and LOCKED Original issue 31 January 2002 Document 1000809 GB Page 4 6 Revision 0 NORMAL PROCEDURES CAP 10C Pilot and passenger seat belts ATTACHED Master switch OFF Alternator switch OFF Magnetos OFF Electrical equipment OFF Flaps trim switch as appropriate ON Avionics switch as appropriate ON DILE TE CS u usa Qhasa ia NO LEAN Cockpit heating CLOSED 4 3 3 Starting up cold engine Master switch ON WISI NT RETRACTED CHECKED Anti collision light ON Throttle lever PUSHED FULL THROTTLE Mixture FULL RICH Tank selector switch F
5. CAP 10C 4 NORMAL PROCEDURES 4 1 PresentallOl sos siiis onec Pea MEN AREE UH FEDERE CE 4 3 42 SDBOUSi cousc induere Sig uvccvo don dou du agat D mxu dud DERE VUR 4 3 4 3 Check list of normal procedures 4 4 P MEME RN 4 15 Original issue 31 January 2002 Document 1000809 GB Page 4 1 Revision O NORMAL PROCEDURES CAP 10C age intentionally left blank Original issue 31 January 2002 Document 1000809 GB Page 4 2 Revision 0 NORMAL PROCEDURES CAP 10C 4 NORMAL PROCEDURES 4 1 PRESENTATION This section describes the procedures for normal operation Normal procedures associated with optional systems are in section 9 Supplements 4 2 SPEEDS I cop 110 km h 59 kt Normal climb 160 km h 86 kt Best climb angle Vx 130 km h 70 kt cat U 120 km h 65 kt cat A Optimum climb Vy allowing for Best climb rate Vz max 150 km h 81 kt 15 flap 160 km h 86 kt clean config Brel lp pm P T 200 km h 108 kt Yale jor e 150 km h 81 kt 15 flap 120 km h 65 kt Full flaps Recommended speed for turbulence penetration 200 km h 108 kt Maximum demonstrated crosswind 37 km h 20 kt Original issue 31 January 2002 Document 1000809 GB Page 4 3 Revision 0 NORMAL PROCEDURES CAP 10C 4 3 CHECK LIST OF NOR
6. 4 SPINS Spinning on CAP10 is authorised with engine on idle in category A The loss of altitude is about 400 feet per rotation i e 120 metres Each spin rotation takes about 2 seconds 4 4 1 Instructions for recovery from positive or negative spin Positive spin Kill TE full opposite rudder opposite to direction of rotation Elevator E nose up sector Lateral control roll towards spin Original issue 31 January 2002 Document 1000809 GB Page 4 15 Revision 0 NORMAL PROCEDURES CAP 10C Negative spin Rudder full opposite rudder opposite to direction of rotation Elevator nose up sector Lateral control neutral If the rudder elevators or ailerons are not kept in the position indicated above recovery still remains possible but will tend to take more time In all events you must BE SURE TO KEEP DIRECTION OF RUDDER FULL OPPOSITE TO DIRECTION OF ROTATION 4 4 2 Influence of centre of gravity CAUTION Mainly by acting on the aircrafts attitude the centre of gravity has tremendous influence on CAP10 s behaviour in spin Aft C G 24 to 26 Flat attitude about 50 indicated airspeeds of about 150 km h tendency to level out more to left than to right Fwd C G 22 to 20 Dive attitude up to 70 indicated ai
7. MAL PROCEDURES 4 3 1 Pre flight inspection Cockpit Make certain cockpit is clean Master switch OFF Alternator switch ccccccseceseeseeseeeenes OFF Magnetos OFF Fuel selector switch OPEN FWD TANK CAUTION For aerobatics the rear tank must be empty and the ELT must be removed Flight controls FREE in CORRECT DIRECTION Engine controls FREE Battery contact ON Stall warning indicator CHECKED Warning lights CHECKED Fuel gauges CHECKED Battery contact OFF Seat belts and harnesses CHECKED Canopy attachment CHECKED Release handle CHECKED Before getting down from aircraft PUG ANA c visual inspection Fuel CAO rreren closed and locked Original issue 31 January 2002 Document 1000809 GB Page 4 4 Revision 0 NORMAL PROCEDURES CAP 10C go unu u EC hinges and control Te E hinges and control Balance plates and deflection lio NM clean not clogged Main landing gear sh
8. WD Electric pump ON Fuel flow meter CHECKED Electric pump STOP Throttle lever 1 cm EIER eebe LEAN Magnetos 1 2 SANET ee on request Original issue 31 January 2002 Document 1000809 GB Page 4 7 Revision 0 NORMAL PROCEDURES Mixture Throttle lever 4 3 4 Starting up hot engine Master switch Anti collision light as appropriate Throttle lever Mixture Magnetos Starter Mixture Throttle lever 4 3 5 Engine he Engine speed ating CAP 10C RICH as soon as engine is running set for 1 000 rpm ON ON 4 to 5 cm LEAN 1 2 on request RICH as soon as engine is running set for 1 000 rpm 1 000 to 2 000 rpm Do not exceed 1 000 rpm for the first minute Oil pressure CHECKED 4 to 6 bars If the oil pressure did not rise to above 1 8 bar within 30 seconds after start up stop the engine and proceed with verification Fuel pressure Cut off test magnetos Alternator switch Original issue 31 J Revision 0 anuary 2002 Document 1000809 GB Page 4 8 NORMAL PROCEDURES CAP 10C Battery charge CHECKED Electrical equipment ON Rear tank test
9. full power and check the engine speed for 2 350 rpm retract flaps check pressures and temperatures Original issue 31 January 2002 Document 1000809 GB Page 4 11 Revision 0 NORMAL PROCEDURES CAP 10C 4 3 11 Cruise In cruising flight you are advised to use the mixture control at all altitudes Consumption is then reduced and can be diminished by about 15 96 The maximum continuous engine speed of 2 700 rpm must in no event be exceeded To obtain the best mixture slowly reduce the mixture going from the full rich position until you obtain maximum power in the case of a fixed pitch propeller gradually reduce the mixture until the tachometer shows start of engine speed loss If the aircraft is equipped with an EGT indicator this point represents the maximum temperature We advise enriching the mixture until the temperature is 50 F generally 2 graduations below the maximum observed temperature Where there is no EGT we advise you to enrich the mixture by rotating the mixture knob over two complete turns Also see the Engine User s Manual 4 3 12 Descent le Au e FULL RICH j ER ERR EU THE FULLEST Engine speed 1 700 to 1 800 rpm Recommended speed 200 km h 108 kt Pitot heat REI according to weather conditions 4 3 13 Approach Speed flaps 15 150 km h 81 kt Speed flaps 40
10. ock absorber checked and tyre inflated Underwing inspection door locked Fwd fuselage Tah k drain vince uuu u u u u punas checked Su EEN checked Lower inspection door closed and locked Cowl left door closed and locked Propeller condition and attachment SDIIHII8T 1 al sssssa qa desse siet na bleues condition and attachment Air inlet free Qil level uuu E checked 6 qt maximum for aerobatics Cowl right door closed and locked Right wing Main landing gear shock absorber checked and tyre inflated Underwing inspection door locked Original issue 31 January 2002 Document 1000809 GB Page 4 5 Revision 0 NORMAL PROCEDURES CAP 10C ENEE eege natives hinges and control Balance plates and deflection gi put M M Mn hinges and control Rear right fuselage Static OM EEN clean and not clogged Antennas VISUAL INSPECTION Door puna terest EN locked Horizontal stabiliser Horizontal stabiliser ATTACHMENT Elevator and vertical stabiliser hinges and control Deflection and cable tension Rudder tab
11. orrect direction Lateral control free in correct direction Rudder pedals free in correct direction Elevator tab CHECKED then NEUTRAL Flaps e E FULL FLAPS then 15 Equipment Mechanical accelerometer reset Altimeter SET dE SET Cockpit KEE Closed and locked Seat belt and harnesses ATTACHED EE RELEASED Original issue 31 January 2002 Document 1000809 GB Page 4 10 Revision 0 NORMAL PROCEDURES CAP 10C us FULL THROTTLE OO CHECKED 2 250 x 50 rpm from 50 km h 27 kt S 110 km h 59 kt Propeller torque is to the left on this aircraft Engine speed check 2300 rpm x 50rpm Initial climb 140 km h 76 kt gio MNT RR NR OTRO OPERE NOUS RETRACTED 91 m 300 ft Normal climb 160 km h 86 kt clean config 4 3 10 Climb speed Best climb angle VXx 130 km h 70 kt cat U 120 km h 65 kt cat A Optimum climb Vy allowing for Best climb rate Vz max 160 km h 86 kt clean config To obtain the best rate of climb Vz max keep
12. rspeed being capable of exceeding 180 km h tendency to dive more to right than to left Risk of Va being exceeded during spin and recovery Immediately apply instructions for recovery as soon as speed reaches 180 km h Original issue 31 January 2002 Document 1000809 GB Page 4 16 Revision 0 NORMAL PROCEDURES CAP 10C 4 4 3 Influence of stick position CAUTION The stick position roll control has an influence on the CAP10 s behaviour during spin Stick to counter spin For example in left spin the stick to the right tends to level spin out and as a result reduce the indicated airspeed CAUTION In the case of spin with centre of gravity aft this manoeuvre may prove to be dangerous by exacerbating the tendency to level out and delaying the recovery time Stick in direction of spin For example in left spin the stick to the left tends to agitate and or deepen the spin and as a result increase the indicated airspeed CAUTION Whatever the centre of gravity this manoeuvre may prove to be dangerous due to the increased risk of e turbulent to very turbulent spin e increase in speed e transition to a flick roll In all cases listed above apply the instructions for recovery see S 4 4 1 In the event of engine shut down during spin immediately apply the instructions for recovery from spin then apply the instructions for engine re sta
13. rt SECTION 3 Original issue 31 January 2002 Document 1000809 GB Page 4 17 Revision 0 NORMAL PROCEDURES CAP 10C Summary CAP10 s behaviour in spin can be summarised as follows Spin stick against direction of spin e calm e low speed e long recovery time Spin stick in direction of spin e turbulent to very turbulent e high speed and unstable e short recovery time Original issue 31 January 2002 Document 1000809 GB Page 4 18 Revision 0 NORMAL PROCEDURES
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