This quiz tests knowledge on Aircrew Egress Systems for the F-16 dual seat aircraft, covering modes of ejection, system components, and safety procedures.
Section III, Log Book Report.
Section V, Supplemental Data.
Section IV, Fault Isolation Information.
Section I, Fault Identification and Description.
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Reject lines with visible wear and tear.
Perform 100 percent visual inspection.
Ensure the shipping container is not damaged in any way.
Make sure all fittings are properly torqued to TO specification.
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Assist in removal of the canopy and operate the hoist.
Perform removal of the canopy from inside the aircraft.
Direct removal of the canopy from either side of the aircraft.
Perform removal of the canopy from either side of the aircraft.
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Canopy jettison, then only the rear seat ejects.
Canopy jettison, rear seat ejection, then front seat ejection.
Canopy jettison, front seat ejection, then rear seat ejection.
Canopy jettison, then simultaneous front and rear seat ejection.
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Rotating the lines only, not the fittings.
Rotating the fittings only, not the lines.
Rotating the ferrule assembly a full 360 degrees.
Only installing protective caps when the lines are back at the shop.
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Start up and stop and the switch should return to the center position.
Rise to the full up position and the switch should lock in the up position.
Rise to the full up position and the switch should return to the center position.
Lower to the full down position and the switch should return to the center position.
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Canopy actuator.
Canopy unlock handle.
Unlock warning switch.
Canopy manual drive assembly.
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Seat actuator/rocket catapult.
External canopy initiator.
Fired warning indicator.
Pyro panel #5.
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Removing the foreign object with a scribe.
Removing the foreign object with a soft cloth.
Turning the component upside down and shaking it.
Removing the foreign object with 45 psi of air pressure.
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Safety wire connectors before applying torque.
Use two wrenches while tightening connectors.
Rotate SMDC lines, not the fittings when tightening.
Use a wrench and a pair of pliers while tightening connectors.
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SEAT NOT ARMED light should come on.
CANOPY warning light should come on.
SEAT NOT ARMED light should go out.
CANOPY warning light should go out.
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A thickness feeler gauge.
A 10X magnifier.
A 3X magnifier.
A steel rule.
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Completely purge and refill the cylinder.
Replace the cylinder and purge the old one to turn into supply.
Top off the cylinder to proper pressure for the applicable climate temperature.
Place the cylinder in warm area and allow pressure to expand to an acceptable level.
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Emergency Escape Sequencing System (EESS).
Central integrated processor (CIP) guillotine.
Analog recovery sequencer.
Digital recovery sequencer (DRS).
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Less than 250 knots, less than 15,000 feet.
Greater than 250 knots, less than 15,000 feet.
Less than 250 knots, greater than 15,000 feet.
Greater than 250 knots, greater than 15,000 feet.
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Electronic wiring harness.
FLSC.
SMDC.
DTA.
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Standard (S) or confined (C) types.
Donor (D) or standard shielded (SS) types.
Shock tube (STD) or flexible confined (FC) types.
Receptor (R) or shock tube receptor (STR) types.
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Frangible bolt.
Canopy remover rocket.
Canopy actuator release bolt (CARB).
Emergency canopy release line (ECRL).
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Increased hazards of working with pyrotechnic modules.
Tool accountability with increased socket and wrench usage.
The increased potential for cockpit FOD from pyrotechnic hardware.
Unexpected aircraft movement, landing gear compressing or expanding.
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Hot gas pressure sent from the canopy jettison hose system.
A detonation transfer wave sent by the SMDC.
A detonation transfer wave sent by the DTA.
Impulses sent through the Emergency Escape Sequencing System (EESS) wire harness.
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When the speed and altitude conditions of Mode 1 are met.
When the speed and altitude conditions of Mode 2 are met.
0.037 seconds after sequence start switch detection.
1.00 seconds after sequence start switch detection.
Gas-actuated cartridges.
Electrically-actuated cartridges.
Mechanically-actuated cartridges.
The detonation transfer assembly (DTA).
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0.040 to 0.080 inch.
0.030 to 0.150 inch.
0.004 to 0.025 inch.
0.000 to 0.030 inch.
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A JAU-8/A25 initiator.
A catapult initiator.
An M99 initiator.
An M53 initiator.
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Spraying a thin film of solid film lubricant on the nut threads.
Applying a thin film of grease to the nut threads with a cotton swab.
Applying a thin film of torque stripe to the nut threads with a cotton swab.
Applying a thin film of anti-seize compound to the nut threads with a cotton swab.
15-20.
30-40.
50-70.
110-120.
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27.
35.
41.
47.
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The ACES II.
Any SMDC lines.
All hoses and electrical disconnects from the pyrotechnic module.
Mounting bolts attaching the pyrotechnic module to the bulkhead.
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1.
2.
3.
4.
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Actuator.
Switches.
Warning light.
Canopy latches.
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FWD, SOLO, and AFT INITIATE.
NORM, FWD, and AFT INITIATE.
NORM, SOLO, and AFT INITIATE.
NORM, SOLO, and FWD INITIATE.
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LOCKED, DN, HOLD, and UP.
LOCKED, DN, OPEN, and UP.
UNLOCKED, DN, OPEN, and UP.
UNLOCKED, DN, HOLD, and UP.
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Reject the SMDC.
Fill the cut with sealant.
Replace the rubber seal.
Replace the seat with sealant.
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Gas pressure from the ejection initiator.
Gas pressure from he ballistic pressure initiator.
Bleed off of electrical voltage from the recovery sequencer.
Electrical voltage produced from the thermal battery initiators.
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FWD, SOLO, and AFT.
NORM, FWD, and AFT.
NORM, SOLO, and AFT.
NORM, SOLO, and FWD.
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Bubble type that's jettisoned from the aircraft frame by a canopy rocket motor.
Clamshell type that's jettisoned from the aircraft frame by an M4 canopy remover.
Clamshell type consisting of formed, transparent plastic mounted in a metal frame.
Bubble type that's designed to give the pilot unobstructed forward and upward vision.
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M53 initiators.
M99 initiators.
Time delay initiators.
Canopy actuator release bolt (CARB).
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M53 initiators through the sequence valves.
M99 initiators through the sequence valves.
Ejection initiators through the sequence valves.
Canopy jettison initiators through the sequence valves.
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5.
10.
15.
20.
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Electronic wiring harness.
FLSC.
SMDC.
DTA.
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Primary drogue severance cutter fires.
Recovery parachute mortar fires.
Drogue parachute deploys.
Vernier rocket activates.
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Insert the -25 inspection gauge into the top of the inspection gauge containing the DTA.
Position the -25 inspection gauge on the upper surface of the inspection gauge containing the DTA.
Position the -25 inspection gauge across lower surfaces of the inspection gauge containing the DTA.
Insert the DTA into the inspection gauge with the ferrule resting firmly against the inside flange of the inspection gauge.
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No more than one broken strand per 12-inch section or more than three broken strands total.
No more than three broken strands per 12-inch section or more than six broken strands total.
No more than one broken strand per 10-inch section or more than three broken strands total.
No more than three broken strands per 10-inch section or more than six broken strands total.
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Breaking the frangible panel, grasping the handle, and pulling the lanyard approximately 6 feet.
Breaking the frangible panel, grasping the handle, and pulling the lanyard approximately 8 feet.
Pulling the canopy jettison handle to extend the cable for 6 feet then jerking the handle.
Pulling the canopy jettison handle to extend the cable for 8 feet then jerking the handle.
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5.
10.
15.
20.
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110 degrees.
128 degrees.
135 degrees.
360 degrees.
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Under the canopy actuator.
On each side of the cockpit.
On each side of the canopy.
Forward of the canopy frame.
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Access panels 2415 and 2416 do not bind against the fuselage.
The upper and lower roller bearings have freedom of rotation.
Both sides of the canopy hinge track engage the roller bearings.
The lower roller bearing contacts the canopy track with no rotation.
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