TM 1-1510-224-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
NOTE
If conditions permit, reduce power on the operative
engine to obtain at TGT of 700o C or less to reduce
the possibility of exceeding TGT limit. Reduce
electrical load to minimum consistent with flight
conditions.
False fuel flow indications may be observed with the
starter engaged and the CONDITION lever in FUEL
CUTOFF.
(10) ENG START switch - START-
IGNITION. Check IGN ON
annunciator illuminated.
(11) CONDITION
lever
-
LOW
IDLE.
(12) ENG START switch - OFF,
after TGT peaks.
(13) CONDITION
lever
-
HIGH
IDLE.
(14) POWER lever - As required.
(15) GENERATOR
switch
-
RESET, then ON.
(16) Engine AUTO IGNITION - As
required.
(17) PROP SYNC switch - As
required.
(18) Electrical
equipment
-
As
required.
(h)
Repeat step g for opposite engine if
required.
*12.
Propeller
autofeathering
system
and
propeller
unfeathering
-
Check
as
follows:
2-75