5. Simulate declaring an emergency.
6. Recover at designated altitude.
*** A positive load factor should be maintained throughout the maneuver. Therefore, a 30°-45° angle of
bank should be used to establish the decent and maintained throughout the maneuver, both for extra
visual scanning and for load factor.
In-Flight Engine Failure
This procedure is used when there is a failure or partial loss of power for one of the engines in our
aircraft. For a conventional twin aircraft, this situation would be the most adverse with a loss of the
critical engine, normally the left engine. The maneuver shall be completed above 4000 ft AGL over an
area where a landing can be made with a single engine. No engine failures may be made below 3000 ft
AGL using the fuel selector or ignition switches and no engine securing is authorized below 4000 ft AGL
for training purposes.
***
All Steps below need to be memorized
. They are instant action items and should be accomplished
from memory with no hesitation. The troubleshoot checklist should be performed as a flow with a
confirmation using the checklist. After this, proceed to the
Engine Failure Secure Checklist
.
Procedures:
1.
Maintain Directional Control/Pitch Attitude/Airspeed/ Vyse 84 KIAS
2. Props
Full FWD
4. Throttles
Full FWD
5. Flaps
UP
6. Gear
UP
7. Identify
Dead Foot
8. Verify
Close Dead Throttle
--
Troubleshoot Flow Checklist/Altitude Permitting
Ignitions
ON/Check
Fuel Qty/Pressure
Check
Oil Temp/Pressure
Check
Fuel Pumps
ON
Carb Heat
ON/Check/OFF
Fuel Selectors
ON
--If Engine is still Inoperative,
proceed
:
9. Prop
Inop
Engine
Feather
If altitude permits, proceed to the Engine Failure Secure checklist (next page).
