This quiz tests knowledge on Aircrew Egress Systems for the F-16 dual seat aircraft, covering modes of ejection, system components, and safety procedures.
M53 initiators.
M99 initiators.
Time delay initiators.
Canopy actuator release bolt (CARB).
Rate this question:
The left-side JAU-8/A25 ejection control initiator.
The right-side JAU-8/A25 ejection control initiator.
A gas-SMDC initiator.
A SMDC-gas initiator.
Rate this question:
A JAU-8/A25 initiator.
A catapult initiator.
An M99 initiator.
An M53 initiator.
Rate this question:
Electronic wiring harness.
FLSC.
SMDC.
DTA.
Rate this question:
Slip-joint pliers.
Flat-nosed pliers.
Diagonal cutting pliers.
Lineman's side cutting pliers.
Rate this question:
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.
Rate this question:
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.
Rate this question:
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.
Rate this question:
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.
Rate this question:
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.
Rate this question:
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.
Rate this question:
Under the canopy actuator.
On each side of the cockpit.
On each side of the canopy.
Forward of the canopy frame.
Rate this question:
Frangible bolt.
Canopy remover rocket.
Canopy actuator release bolt (CARB).
Emergency canopy release line (ECRL).
Rate this question:
Gas-actuated cartridges.
Electrically-actuated cartridges.
Mechanically-actuated cartridges.
The detonation transfer assembly (DTA).
Rate this question:
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.
Rate this question:
1.
2.
3.
4.
Rate this question:
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.
Rate this question:
5.
10.
15.
20.
Rate this question:
Internal canopy switch.
External canopy switch.
Internal manual drive handcrank.
External manual drive receptacle.
Rate this question:
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.
Rate this question:
The upper and lower roller bearings have freedom of rotation.
Access panels 2415 and 2416 do not bind against the fuselage.
Both sides of the canopy hinge track engage the roller bearings.
The lower roller bearing contacts the canopy track with no rotation.
Rate this question:
V pattern with the lower point of the V pointing forward and the upper connection points of the V pointing aft.
V pattern with the lower point of the V pointing aft and the upper connection points of the V pointing forward.
W pattern with the lower point of the W pointing forward and the upper connection points of the W pointing aft.
W pattern with the lower point of the W pointing aft and the upper connection points of the W pointing forward.
Rate this question:
27.
35.
41.
47.
Rate this question:
0.040 to 0.080 inch.
0.030 to 0.150 inch.
0.004 to 0.025 inch.
0.000 to 0.030 inch.
Rate this question:
Section III, Log Book Report.
Section V, Supplemental Data.
Section IV, Fault Isolation Information.
Section I, Fault Identification and Description.
Rate this question:
Canopy actuator.
Canopy unlock handle.
Unlock warning switch.
Canopy manual drive assembly.
Rate this question:
Actuator.
Switches.
Warning light.
Canopy latches.
Rate this question:
FWD, SOLO, and AFT INITIATE.
NORM, FWD, and AFT INITIATE.
NORM, SOLO, and AFT INITIATE.
NORM, SOLO, and FWD INITIATE.
Rate this question:
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.
Rate this question:
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.
Rate this question:
LOCKED, DN, HOLD, and UP.
LOCKED, DN, OPEN, and UP.
UNLOCKED, DN, OPEN, and UP.
UNLOCKED, DN, HOLD, and UP.
Rate this question:
Electronic wiring harness.
FLSC.
SMDC.
DTA.
Rate this question:
The left-hand JAU-8/A25 ejection control initiator.
The right-hand JAU-8/A25 ejection control initiator.
A gas-SMDC initiator.
A SMDC-gas initiator.
Rate this question:
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.
Rate this question:
Canopy remover cartridge.
Canopy actuated initiator.
1.5-second time delay initiator.
External canopy jettison initiator.
Rate this question:
Canopy actuated initiator.
The canopy remover cartridge.
The 1.5-second time delay initiator.
The 0.400-second time delay initiator.
Rate this question:
Mounded on the right interior side of the canopy.
Mounted on the left interior side of the canopy.
Under the right canopy sill in either cockpit.
Under the left canopy sill in either cockpit.
Rate this question:
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.
Rate this question:
A thickness feeler gauge.
A 10X magnifier.
A 3X magnifier.
A steel rule.
Rate this question:
5.
10.
15.
20.
Rate this question:
110 degrees.
128 degrees.
135 degrees.
360 degrees.
Rate this question:
Reject the SMDC.
Fill the cut with sealant.
Replace the rubber seal.
Replace the seat with sealant.
Rate this question:
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.
Rate this question:
The ACES II.
Any SMDC lines.
All hoses and electrical disconnects from the pyrotechnic module.
Mounting bolts attaching the pyrotechnic module to the bulkhead.
Rate this question:
Seat actuator/rocket catapult.
External canopy initiator.
Fired warning indicator.
Pyro panel #5.
Rate this question:
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.
Rate this question:
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.
Rate this question:
Quiz Review Timeline (Updated): Aug 31, 2023 +
Our quizzes are rigorously reviewed, monitored and continuously updated by our expert board to maintain accuracy, relevance, and timeliness.
Wait!
Here's an interesting quiz for you.