Emergency
Procedures
DA 62 AFM
3.13.7 EMERGENCY DESCENT
1. FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
2. Gear. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN
3. POWER lever. . . . . . . . . . . . . . . . . . . . . . . . . IDLE
4. Airspeed. . . . . . . . . . . . . . . . . . . . . . . . . . . . . as required
WARNING
Max. structural cruising speed . . . . . . . . v
NO
= 162 KIAS.
Never exceed speed in smooth air. . . . . v
NE
= 205 KIAS.
END OF CHECKLIST
3.13.8 EMERGENCY EXIT
In case of a roll over of the airplane on ground, any door can be used as exit. In case
the doors are blocked, the egress hammer may be used to break through the door
windows.
If OÄM 62-019 is installed, a maximum of seven seats may be installed.
In case of an emergency, the passengers on passenger row I must exit the airplane first.
The LH seat backrest of passenger row I can be released by pulling the red emergency
handle on the backside of the seat pan. The released backrest can be put away and the
passengers of passenger row II can exit the airplane.
Page 3 - 72 Rev. 0 11-Jan-2019 Doc. No. 11.01.05-E