Egress System
T-45C TS, ADV & IUT ENG-15
c.
Ejection seat safety pin - REMOVED AND
STOWED
Sg 7, fr 3
d.
Ejection seat - INSPECT
SAFE/ARMED Handle
SAFE Position
(1) Ejection seat SAFE/ARMED handle - SAFE
Fig 8: Ejection Seat
Inspection
Sg 7, fr 4
(2) Emergency restraint release - FULLY
Emergency Restraint
DOWN AND LOCKED
Release Handle
Sg 7, fr 5
(3) Ejection control handle safety pin -
Ejection Control Handle
REMOVED AND STOWED
Without Safety Pin
Sg 7, fr 6
Emergency Oxygen
(4) Emergency oxygen actuator - OFF
Actuator - OFF
Sg 7, fr 7
(5) Emergency oxygen gauge - 1,800 to
Emergency Oxygen
2,500 PSI
Gauge
Sg 7, fr 8
(6) Leg restraint cables - CONDITION/
Leg Restraint Cables
PROPERLY ROUTED
Sg 7, fr 9
Emergency Locator
Transmitter and Oxygen
(7) Emergency locator transmitter and oxygen
Lanyards
lanyards - CONNECTED
Sg 7, fr 10
(8) Catapult manifold valve - SECURED,
Top of Ejection Seat
HOSE CONNECTED AND RETAINING
Sg 7, fr 11
PIN INSTALLED
Catapult Manifold Valve,
Hoses, and Retaining Pin
(9) Parachute withdrawal line - CORRECTLY
Sg 7, fr 12
SECURED TO PARACHUTE
Catapult Manifold
DEPLOYMENT ROCKET STIRRUP
Valve Lock-in Plunger
Correctly Installed
CAUTION: To prevent SEAWARS/
Sg 7, fr 13
Catapult Manifold
trombone damage, do not adjust seat
Valve Lock-in Plunger
prior to strapping in.
Incorrectly Installed
Sg 7, fr 14
(10) Top latch mechanism - SPIGOT INDICA-
Parachute Withdrawal
TOR IS FLUSH WITH END OF TOP
Lines
LATCH PLUNGER
Sg 7, fr 15
Jammed Upper Koch
WARNING: If top latch mechanism does
Fitting
not meet outlined requirements, seat
Sg 7, fr 16
Top Latch Mechanism
could rise up catapult guide rail during
Spigot Indicator Flush
aircraft maneuvers.
Page 15-34
(9-98) Change 4
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