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ENGINE MALFUNCTION AFTER LIFTOFF (FLIGHT CONTINUED)
ENGINE MALFUNCTION DURING FINAL APPROACH)
TM-55-1510-219-CL Army Model RU-21H(Guardrail V) Avionics Upgrade Aircraft Manual
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TM 55--1510--219--CL
E--2.1/(E--2.2 blank)
C3
ENGINE MALFUNCTION DURING FLIGHT
1.
Auopilot/yaw
damp
--
DISENGAGE
.
2.
Power
--
AS
REQUIRED
.
3.
Dead
engine
--
IDENTIFY
4.
Power
lever
(affected
engine)
--
IDLE
.
5.
Propeller
lever
(affected
engine)
--
FEATHER
.
6.
Gear
--
AS
REQUIRED
.
7.
Flaps
--
AS
REQUIRED
.
8. Power -- SET.
9. Engine cleanup -- PERFORM.
10.
Generator
Load -- 100% MAXIMUM.
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