UJPT, E2-C2, ADV, & IUT EMFP-03
Engine and Hydraulic Emergency Procedures
D.
Airstart procedures - See NATOPS
1.
A i s a t p r m e tr / e u r ment 1.5.3.1.5.7.1
rtr aa esrqie
s
a.
Immediate - Any airspeed any altitude
b.
Windmill - Below 25,000 ft MSL, 13% N2 or
greater RPM (Recommended a minimum of
250 KIAS)
c.
Assisted - Below 15,000 ft MSL, Airspeed
165 - 250 KIAS
2.
Airstart procedures - See NATOPS 1.5.3.1.5.7.2
NOTE: Engine flameout indications generally
consist of falling rpm and EGT with corresponding
reduction in thrust. The airstart procedures you will
use are divided into three categories -- immediate,
windmill, and assisted. It is important to quickly
identify and initiate the procedure appropriate to the
situation.
a.
Immediate Airstart - These procedures will
precede both the Windmill Airstart and the
Assisted Airstart attempts in all cases
LESSON NOTE
Emphasize to the class the importance of timely execution of
the engine failure procedures above 1,500 feet AGL or
airspeed above 180 KIAS. When the engine fails, the OBOGS
system no longer is functional. The pilot's only source of
oxygen is the EMERGENCY OXYGEN system in the seat.
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(9-98) Original
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