Introduction to T-45C Configuration
T-45C TS, ADV & IUT ENG-01
(5) Command ejection selector and SEAT
LIGHT switch: left console, aft cockpit only
PROGRESS CHECK
Question 4 — 1.3.5.1.4.1
What is the minimum speed and altitude at which the
ejection seat may be used?
ANSWER: The T-45C uses a zero/zero ejection seat. Ejection
may be accomplished at zero speed and zero altitude when the
aircraft is in a level attitude.
N.
On-board oxygen generation system (OBOGS)
Sg 3, fr 17
1.4.16.3.1.1
Fig 15: OBOGS
AFT
FWD
PLENUM
OXYGEN
MONITOR
INTERNAL
HEAT EXCHANGER
PLENUM
CABIN
DISCHARGE
DIFFUSER
AIR
MOL
SIEVES
TEMP
OVERBOARD
SWITCH
ROTARY
BLEED AIR
TO ANTI-G VALVES
VALVE
SHUTOFF
VALVE
HEATER
OXYGEN CONCENTRATOR
LEGEND
CHECK VALVE
MANUAL SHUTOFF
VALVE
TO COCKPIT
Figure 15: OBOGS
1.
Description: consists of engine bleed air shutoff
valve, heat exchanger, oxygen concentrator,
plenum, and regulator
2.
Function: converts engine compressor bleed air to
oxygen-rich breathing air and pressurized air for
anti-g system
3.
Control location: pilot services panel, left console,
both cockpits
(9-98) Original
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