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3.
Wing Flaps T/O
4.
Airspeed 58 KIAS
4.4.13. After Landing
1.
Throttle as required
2.
Mixture FULL RICH
3.
Wing Flaps CRUISE
4.
Avionics as required
5.
Exterior Lights as required
4.4.14. Engine Shut-down
1.
Parking Brake set
2.
Throttle 1700 RPM
3.
Magneto Check Cycle L - BOTH - R - BOTH (RPM drop: 25-150 RPM) (Max. RPM difference (L/R): 50 RPM)
4.
Throttle IDLE
5.
Fuel Pump OFF
6.
Mixture IDLE CUT-OFF
7.
Ignition Switch OFF
8.
ELT Check (by listening to 121.5 MHZ for signal)
9.
Avionics Master Switch OFF
10.
Electric Consumers OFF
11.
GEN/BAT Master Switch OFF
12.
Tie Downs and Wheel Chocks as required
4.4.15. Flight in Rain
NOTE
Flight performance might be reduced, especially for the T/O-distance and the maximum horizontal air speed. The influence on flight characteristics of the airplane is negligible. Flights through heavy rain should be avoided due to the reduced visibility.
4.4.16. Spinning
A. Spin Entry
1.
Loose Items stowed
2.
Seat Belts fastened
3.
Altitude and Airspace check
4.
Fuel Pump ON
5.
Wing Flaps CRUISE
6.
Mixture FULL RICH
7.
Throttle IDLE
8.
Entry Speed trim to 58 KIAS
9.
Reduce speed with elevator speed reduction rate 2-3 kts per second
10.
When stall warning sounds apply simultaneously, full aft stick and full rudder
CAUTION
INTENTIONAL SPINNING IS ONLY PERMITTED WITH FLAPS IN CRUISE POSITION.
CAUTION
DEPENDING ON CG AND SPIN ENTRY TECHNIQUE, ATTEMPTS TO ENTER SPINS MAY DEVELOP INTO SPIRAL DIVES. MONITOR THE AIRSPEED DURING THE FIRST TURN AND RECOVER IMMEDIATELY IF IT INCREASES TO 65 KIAS.
NOTE
Spins with aft CG may oscillate in yaw rate and pitch attitude. This has no effect on recovery procedure or recovery time.
B. Recovery from Spinning
1.
Throttle IDLE
2.
Rudder fully applied in opposite to direction of spin
3.
Control Stick ease stick forward until spinning stops
4.
Rudder neutral, immediately after rotation has stopped
5.
Wing Flaps check CRUISE
6.
Control Stick ease stick backward cautiously Bring airplane from descent into level flight position. Do not exceed maximum permissible speed (vNE).
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本文链接地址：钻石20系列飞机维护手册 DA 20 SERIES AIRPLANE MAINTENANCE MANUAL(35)
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