This is a study guide for Vol 3
EPU switch to ON & battery switch to EMERG
Loss of engine generator & low battery charge
Loss of system-A & system-B hydraulic power
Failure of the main/standby generators & loss of system-A and system-B hydraulic power
Hydraulic System-A only
Hydraulic System-A & System-B
Hydraulic System-B only
Utility Hydraulic System
Normal
Bleed air
EPU/GEN
Augment
EPU Speed controller
EPU nitrogen valve
EPU emergency hydraulic pump
EPU hydrazine fuel
36 lbs
46 lbs
56 lbs
66 lbs
A "red" button indicator
Six equally spaced silver and black triangles
Six equally spaced gray and black triangles
The word "FIRED" appears in the window
NORM
Bleed Air
EPU/GEN
Augment
Bleed air is being commanded by the electrponic speed controller to power the EPU
The nitrogen valve has opened and is bled pressure into the Hydrazine tank
The decomposition chamber has reached 1,200F
A failure of the bleed air speed control and shutoff valve
Another name for the LOX converter
The smallest part of the LOX converter
A double-walled container in the LOX converter that has air evacuated from the space between the walls
The junction between the LOX converter and the regulator
A leak in the Dewar flask
A leak in the LOX system
Failure of the LOX relief valve
Failure of the oxygen heat exchanger
Oxygen relief valve
Oxygen fill valve
Oxygen regulator
Oxygen distribution manifold
Left side of the ejection seat
Right side of the ejection seat
Attached to the right control panel
Attached to the left control panel
Quantity test relay
Probes
Coaxial cables
Test switch
In the forward right console crew comparment matrix assembly
In the vacuum space of the converter's Dewar flask
On the oxygen system TEST panel
Connected to the gaseous oxygen supply tube between the forward OXY FLOW indicator and the forward oxygen regulator
Less than 0.1 liters
Less than 0.3 liters
Less than 0.5 liters
Less than 0.9 liters
The indicator drives towards the empty end of the dial
The indicator rotates CCW
The indicator rotates clockwise
The indicator falls to zero and stops
Pressing the oxygen test switch
Loss of electrical power
A shorted probe (plate to plate)
A short-to-ground in the high voltage side of the circuit
Pressing the oxygen test switch
Loss of electrical power
A shorted probe (plate to plate)
A short-to-ground in the high voltage side of the circuit
Throughout the engine bay and engine nacelles
Throughout the engine bay, engine nacelles, ECS bay, EPU bay and bleed air ducts
Throughout the engine nacelles, ECS bay, EPU bay and the bleed air ducts
Throughout the engine bay and bleed air ducts
Each element grounds to the Fire Detection Unit
Each element grounds to the aircarft frame by the element connectors
Each element grounds to the airframe be electrical terminal ends
Each element grounds to aircraft structural ribs and stringers
765 degrees F
755 degrees F
745 degrees F
775 degrees F
1 minute
5 minutes
10 minutes
15 minuntes
Using the T-handle push-to-test switch
Using the Master Caution push-to-test switch
Using the fire detection test set
Using the fire detection test switch
Only one loop of the control unit circuitry is required to detect a fire/overheat condition
Both loops of the control unit circuitry must detect a fire/overheat condition
Only one loop must sense an overheat condition above 575 degrees F
Only one loop must sense an overheat condition above 765 degrees F
11 pounds
13 pounds
15 pounds
17 pounds
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