DA 42 NG AFM
Abnormal Operating
Procedures
4B.5 FAILURES IN FLAP OPERATING SYSTEM
Failure in Position Indication or Function
1. |
FLAPS position . . . . . . . . . . . . . . . . . . . . . . . |
check visually |
2. |
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
keep in white sector |
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(max. 113 KIAS) |
3. |
FLAPS switch . . . . . . . . . . . . . . . . . . . . . . . . |
re-check all positions |
Modified Approach Procedure Depending on the Available Flap Setting
NOTE
Refer to 5.3.10 - LANDING DISTANCES for landing distances with abnormal flap positions.
(a) Only UP available:
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . min. 86 KIAS
Land at a flat approach angle, use power lever to control airplane speed and rate of descent.
(b) Only APP available: |
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Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
min. 84 KIAS |
Land at a flat approach angle, use power lever to control airplane speed and rate of descent.
(c)Only LDG available:
Perform normal landing.
END OF CHECKLIST
Doc. No. 7.01.15-E |
Rev. 1 |
18-Feb-2009 |
Page 4B - 25 |
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Abnormal Operating
DA 42 NG AFM
Procedures
4B.6 FAILURES IN ELECTRICAL RUDDER PEDAL ADJUSTMENT
Runaway of Electrical Rudder Pedal Adjustment (Optional Equipment, OÄM 42-070)
NOTE
The circuit breaker for the rudder pedal adjustment is located below the related switch, on the rear wall of the leg room.
1. Circuit breaker . . . . . . . . . . . . . . . . . . . . . . . . pull
END OF CHECKLIST
Page 4B - 26 |
Rev. 1 |
18-Feb-2009 |
Doc. No. 7.01.15-E |
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