T-45A UJPT, E2-C2, ADV, & IUT Eng-15
Egress System
(b) Actuation of fwd ejection
handle ejects fwd seat only
(No 0.4-second delay)
(c) Actuation of aft ejection handle
ejects aft seat only
WARNING: Automatic command
ejection sequencing is
impossible with the selector in
the SOLO position. If ejection is
simultaneously initiated in this
mode, the seats may collide.
C.
Operating characteristics 1.3.5.1.3
1.
Secures crew member
2.
Supplies life support and communication
connection points
3.
Ejection
a.
Ejection seat has 0-0 (airspeed-altitude)
ejection capability, electronic sequencer
adjusts to altitude and airspeed
requirements
NOTE: Assumes no rate of descent
and wings-level attitude, nose on
horizon. (Zero rate of descent, zero
rate of roll, and zero rate of pitch).
b.
Assumes pilot falls within the weight
limits established for this ejection seat.
(Prior to Aircrew Systems Change 646
installation)
WARNING: During ejection seat
evelopment and testing, the SJU-17V
5/A and SJU 17(V)6/A were qualified
for use by aviators with nude
weights from 136 lbs. to 212 lbs.
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(8-03) Original
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