T-45C TS, ADV & IUT EMFP-04
Engine and Hydraulic Emergency Procedures
NOTE: Under normal conditions an engine
flameout would be followed by an "Immediate
Airstart". The parameters defined by
altitude, and/or airspeed will dictate your
course of action.
D.
Airstart procedures - See NATOPS
1.
Airstart parameters/requirements 1.5.3.1.5.7.1
a.
Immediate - Any airspeed any altitude
b.
Windmill - Below 25,000' MSL, 13% N2 or greater
RPM (Recommended a minimum of 250 knots)
c.
Assisted - Below 15,000' MSL, Airspeed
165 - 250 knots
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.
Original (9-98)
Page 4-21
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