DA 40 NG AFM
Emergency
Procedures
Doc. # 6.01.15-E
Rev. 3
01-Jul-2014
Page 3 - 23
If Engine Does Not Start:
10.
Fuel valve . . . . . . . . . . . . . . . . . . . . . . . . . . . EMERGENCY
If Engine Does Not Start Adopt Glide Configuration:
11.
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
12.
Airspeed88 KIAS
NOTE
The glide ratio is 9.7; i.e., for every 1000 ft (305 m) of altitude
loss the maximum horizontal distance traveled in still air is
1.59 NM (2.94 km). During this the propeller will continue to
windmill.
Carry out an emergency landing in accordance with 3.7.1 -
EMERGENCY LANDING WITH ENGINE OFF.
CAUTION
Engine restart following an engine fire should only be
attempted if it is unlikely that a safe emergency landing can
be made. It must be expected that engine restart is impossible
after an engine fire.
13.
AVIONIC MASTER . . . . . . . . . . . . . . . . . . . . ON, if required
END OF CHECKLIST
Summary of Contents for DA 40 NG
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Page 2: ...DA 40 NG AFM Introduction Page 0 0a Rev 3 01 Jul 2014 Doc 6 01 15 E Intentionally left blank...
Page 240: ...Mass Balance DA 40 NG AFM Page 6 8 Rev 3 01 Jul 2014 Doc 6 01 15 E 6 4 2 LOADING DIAGRAM...
Page 316: ...Handling DA 40 NG AFM Page 8 8 Rev 3 01 Jul 2014 Doc 6 01 15 E...
Page 322: ...Handling DA 40 NG AFM Page 8 14 Rev 3 01 Jul 2014 Doc 6 01 15 E Intentionally left blank...
