TM 1-1510-224-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
(b)
Pilot’s alternate static air source
switch - ALTERNATE. Verify that
airspeed indicator, altimeter, and
vertical speed indicator readings
increase.
(c)
Pilot’s alternate static air source
switch
-
NORMAL.
Airspeed
indicator,
altimeter,
and
vertical
speed indicator indications should
return to their original readings.
*12.
Propeller
synchrophaser
-
Check
capturing ability of the synchrophaser by
establishing
a
small
out
of
synchronization condition, then turning
the synchronization is established and
held within a few seconds.
13.
Maximum TGT/N1 availability - Perform
as required (Chapter 4).
14.
Speed performance at maximum cruise
power - Perform as required (Chapter 4).
15.
Engine
performance
at
maximum
continuous power - Perform as required
(Chapter 4).
16.
Engine performance at maximum cruise
power - Perform as required (Chapter 4).
*17.
Engine ice vanes - Check operation as
follows:
(a)
#1 and #2 ICE VANE POWER
SELECT switches (2) - MAIN.
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