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STUDENT GUIDE T-39N/G NATOPS
UNIT SIX: ANTI-ICE/DE-ICE SYSTEMS
REFERENCE: T-39 NATOPS MANUAL
ENABLING OBJECTIVE:
A.1
Locate and operate T-39N/G aircraft systems, given a mission in a T-39 in accordance with
NATOPS.
ENABLING STEP:
A.1.7 Recall the basic description, related systems, and operating limitations of the T-39N/G
anti-ice/de-ice system.
NATOPS SIX: ANTI-ICE/DE-ICE SYSTEMS
A. Activate anti-ice system when OAT is +5 to - 20C and in visible moisture.
B. Sources of anti-ice
1. Engine compressor bleed air (9th stage) is provided to the following:
a. Engine inlet duct.
b. Engine flow straightener vanes.
c. Engine guide vanes.
d. Engine nose bullet.
2. Electrical heat is provided to the following:
a. Pitot tubes.
b. Stall warning vanes.
c. EPR probes.
d. Ram air inlet.
e. AOA probe.
f. Windshield.
g. AC and DC generator inlets.
ANTI-ICE/DE-ICE SYSTEMS
6-1


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