T-45C TS, ADV & IUT EMFP-03
Operational and Ejection Emergency Procedures
(1) As in low altitude ejection, climb to slow
aircraft to safer speed, improve ejection
seat trajectory, and provide more altitude, if
desirable
NOTE: If aircraft is controllable and not on
fire (i.e., after engine fire with engine shut
down and fire out), consider descending to
a lower altitude prior to ejection.
(2) After high altitude ejection, seat and pilot
free-fall to 18,000 ft, at which time seat/
man separation occurs and parachute
deploys
NOTE: Manual seat/man separation may
be accomplished by pulling the emergency
restraint release handle on the right side of
the seat bucket.
g.
Over-water ejection
(1) Inflate LPU, and snap lobes together,
primary mode of LPU inflation - manual
(beaded handle), automatic mode (only a
backup)
WARNING: Failure to snap waist lobes
before water entry may result in face-
down flotation.
(2) Deploy the raft by pulling either right or left
release prior to entering the water
(3) Upon water impact, manual release of
parachute Koch fittings is recommended,
even though they should release
automatically (SEAWARS)
Original (9-98)
Page 3-13
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