Introduction to NATOPS & T-45A Configuration
T-45A UJPT, E2-C2, ADV, & IUT Eng-01
b.
Function: provides environmental and
atmospheric protection while allowing
maximum visibility
2.
Ejection seat
Sg 3, fr 12
a.
Description: ballistic catapult and
Oxygen/Communications
Hose
Emergency
Oxygen Gauge
rocket-powered seat, containing
ELT Lanyard
Emergency Oxygen
Lanyard
emergency life-support systems
Emergency Restraint
Ejection
Release
Handle
Emergency
Safe/ArmedHandle
Oxygen
b.
Function: provides emergency egress
E
SAF
Actuator
Ejection Handle
Safety Pin
Shoulder Harness
Control Lever
SeatHeightSwitch
EJECTION SEAT AND CONTROLS
LECTURE NOTES
Highlight the fact that when on the ground the aircraft
has a zero/zero capability of ejection. When in flight,
changes in roll and pitch can degrade the probability of
a safe ejection at very low altitudes.
N.
On-board oxygen generation system (OBOGS)
Sg 3, fr 13
1.4.16.3.1.1
OFF
2
1
O
N
OBOGS
2
ALT
VENT
SWITCH
28VDC
BLEED AIR
2
ESSBUS
2
WARMAIR
OXYGEN
ENRICHED
ANEROID
PLENUM
AIR
1.
Description: consists of engine bleed air
LOWO2
OXYGEN
MONITOR
OXYGEN
GEN BUS
DEPLETED
HEATER
HEAT EXCHANGER
AIR
CABIN
WARNING LIGHT
CONTROL
DISCHARGE
OVER
ELECTRICAL
OXYGEN
AIR
BOARD
TEMP SWITCH
<250F
MECHANICAL
2
DIFFUSER
>250F
FOR/AFTCOCKPIT
shutoff valve, heat exchanger, oxygen
CIRCUIT
FILTER/
TEST
BREAKER
PORT
CHECK
PLENUM
CONTR
VALVE
AFT
EQUIPMENT
RELIEF
BAY
VALVE
concentrator, plenum, and regulator
ANTI-G
VALVES
MANUAL
HEATER
SHUTOFF
ENGINEBLEED
VALVE
AIRSHUTOFF
MOL
MOL
VALVE
SIEVE
SIEVE
MOT
MOTOR
CLOSED
OVERBOARD
OPEN
ROTARY
MOT
VALVE
2.
Function: converts engine compressor
SHROUD
PRESSURE
BLEED
HEAT CONTROL
REGULATOR
PORT
VALVE
CONCENTRATOR
bleed air to oxygen-rich breathing air and
OBOGS
pressurized air for anti-g system
Sg 3, fr 14
O. Environmental control system (ECS)
COCKPIT
1.4.15.3.1.1
FORWARD
AFT
RAM AIR
RAMAIR
INLET
OUTLET
RAMAIR
CONTROLVALVE
WATER EXTRACTOR
MAX DEFOG
MAIN
PRESSURE
1.
Description: consists of the air conditioning
REGULATOR
& SHUTOFF
VALVE
VENTILATION
SECONDARY
TEMPERATURE
DUCTS
HEAT
EXCHANGER
CONTROL
VALVE
PRIMARY
system, the cockpit pressurization system,
COLD
HEAT EXCHANGER
CANOPY
AIR
UNIT
DEFOGDUCTS
T
O
AVIONICS
IPRSOV
CANOPY
OPERATED VALVE
LOCK
and the avionics equipment cooling system
CONNECTION
FORWARD
DISCHARGE VALVES CONTROL PRESSURE
DISCHARGE
LEGEND
AVIONICS
LEGEND
EQUIPMENT
VALVE
BAY
CANOPYSEAL/
HOT AIR
CABIN
CANOPYPSEALURE LINES
RESS/
ENGINE HP
DISCHARGE
PRESSURE
PRESSURETRACTED
EXLINES
PARTIALLY
VALVE
SAFETYAND
AIR
COCKPIT
COOLEDAIR
ELECTRICATER
WALLY
PRESSURE
INWARDRELIEF
CONTROLLEDRICALLY
AMBIENT
ELECT
CONTROL VALVE
VALVE
COLDAIR
VALVE CONTROLLED
(ALTITUDE)
VALVE
PRESSURE
FORWARD
AFT
CHANGEOVERGEOVER
MIXED
CHAN
VALVE VALVE
HOT/COLDAIR
ENVIRONMENTAL CONTROL SYSTEM
(8-03) Original
Page 1-25
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