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1. POWER setting ...................... reduce as required
if the problem does not clear:
2. ECU SWAP ......................... ECU B
CAUTION
If the problem does not clear itself, switch back to AUTO and land on the nearest suitable airfield. Prepare for engine malfunction according to 3.5.6 - ENGINE FAILURES IN FLIGHT.
END OF CHECKLIST 3.9.4 UNINTENTIONAL FLIGHT INTO ICING
Doc. No. 7.01.05-E Rev. 5 15-Nov-2007 Page 3 - 57
1.
Leave the icing area (by changing altitude or turning back, in order to reach zones with a higher ambient temperature).
2.
PITOT HEAT......................... ON
3.
Cabin heat & Defrost................... ON
4.
POWER lever ........................ increase power, in order to prevent ice build up on the propeller blades, apply power changes periodically.
5.
ALTERNATE AIR ..................... OPEN
6.
Emergency windows ................... open if required
CAUTION
Ice build-up increases the stalling speed.
7. ATC................................ advise if an emergency is
expected
CAUTION
If the Pitot heating fails:
-Alternate static valve .......... OPEN
-Emergency windows .......... close
END OF CHECKLIST 3.9.5 FUEL SUPPLY FAILURE
Page 3 - 58 Rev. 5 15-Nov-2007 Doc. No. 7.01.05-E
1. FUEL SELECTOR .................... CROSSFEED /
affected engine
WARNING
When the high pressure fuel pump of the engine takes in air an inspection of the pump is necessary prior to next flight.
2. Fuel quantity ......................... monitor
END OF CHECKLIST 3.9.6 RECOVERY FROM AN UNINTENTIONAL SPIN
Doc. No. 7.01.05-E Rev. 5 15-Nov-2007 Page 3 - 59
CAUTION
Spin recovery has NOT been shown during certification as it is NOT required for this airplane category. The given recovery method is based on general experience!
CAUTION
Intentional spins are prohibited in this airplane. In the event
a spin is encountered unintentionally, immediate recovery
actions must be taken.
Single-engine stalling is not permitted.
CAUTION Steps 1 to 4 must be carried out immediately and simultaneously.
1.
POWER lever ........................ IDLE
2.
Rudder ............................. full deflectionagainst direction of spin
3.
Elevator (control stick).................. fully forward
4.
Ailerons ............................. neutral
5.
FLAPS.............................. UP
CONTINUED
Page 3 - 60 Rev. 5 15-Nov-2007 Doc. No. 7.01.05-E
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