DA 40 NG AFM
Emergency
Procedures
Doc. # 6.01.15-E
Rev. 3
01-Jul-2014
Page 3 - 45
3.8
RECOVERY FROM AN UNINTENTIONAL SPIN
CAUTION
Steps 1 to 4 must be carried out
immediately
and
simultaneously
.
1.
POWER lever . . . . . . . . . . . . . . . . . . . . . . . . IDLE
2.
Ailerons . . . . . . . . . . . . . . . . . . . . . . . . . . . . neutral
3.
Rudder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . full deflection against
direction of spin
4.
Elevator (control stick) . . . . . . . . . . . . . . . . . fully forward
When Rotation Has Stopped:
5.
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
6.
Rudder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . neutral
7.
Elevator (control stick) . . . . . . . . . . . . . . . . . pull carefully
8.
Return the airplane from a descending into a normal flight attitude. Do not exceed
the 'never exceed speed', v
NE
= 172 KIAS.
END OF CHECKLIST
Summary of Contents for DA 40 NG
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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...
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