Maximum Range Descent 1 / 2
NOTE
This procedure is designed for an airplane with propeller feathered, which can
be achieved only by shuting down the engine.
CAUTION
The cabin pressurization system no longer operates with the engine shut down.
If airplane altitude is > 10,000 ft:
1 - Oxygen masks ............................................................................... Use
Refer to procedure Oxygen Use in Subsection 3.13.
2 - THROTTLE ............................................................................................. IDLE
3 -
ENGINE MODE switch ............................................................................ OFF
4 - FUEL TANK SELECTOR ......................................................................... OFF
5 - FLAPS lever .............................................................................................. UP
6 - LANDING GEAR lever ............................................................................... UP
7 - Airspeed .......................................................................................... 120 KIAS
8 - DUMP switch ......................................................................................... Press
9 - EMERGENCY RAM AIR control knob ...................................................... Pull
If VMC and non icing conditions are possible:
10 - ESS BUS TIE switch ................................................................... EMER
11 - Prepare for a forced landing.
Refer to procedure
Forced Landing or Ditching in
Subsection 3.7. .
End of procedure ■
Continue ►
Pilot's Information Manual
Section 3
Emergency Procedures
PIM TBM 960 - Edition 0
Rev. 00
Page 3.6.3
PIM - DO NOT USE FOR FLIGHT OPERATIONS
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