EGRESS CDCS 4
EGRESS CDCS 4 Quiz
Test your knowledge and expertise in aircraft egress systems with our comprehensive EGRESS CDCS 4 Quiz. Designed for professionals in the aviation and maintenance fields, this quiz covers essential inspections, component checks, and operational protocols.
Highlights of the quiz include:
- 38 detailed multiple-choice questions
- Focus on aircraft safety and maintenance standards
- Challenging content for both budding and experienced egress professionals
Which inspection requires skills, equipment, and facilities beyond your normal duties
Phase inspection
Isochronal inspection
Programmed depot maintenance
Aerospace vehicle manufacturer A or B check
During which aircraft inspection are safety pins removed to prepare for flight
Periodic
Thru flight
Postflight
End of runway
Which aircraft inspection is performed prior to takeoff at intermediate stops for refueling or other normal requirements
Preflight
Thru flight
Postflight
End of runway
What would an egress journeyman inspect during an hourly postflight inspection
The condition of ballistic hose O-rings
The contents of ejection seat survival kits
Corrosion on ejection seats and components
The integrity of safety wire on components inside access panels
During which aircraft inspection would ejection seats be removed from the aircraft, disassembled, cleaned, and painted?
Phase inspection
Periodic inspection
Preflight inspection
Hourly postflight inspection
What interval does the isochronal inspection concept use for scheduling inspections
Shelf life
Service life
Flying hours
Calendar intervals
A major inspection is computed from the programmed
Start date of the last minor inspections
Start date of the last major inspection
End date of the last minor inspection
End date of the last major inspection
Which isochronal inspection is a combination inspection of former basic postflight and hourly postflight inspection
Major inspection
Minor inspection
Phase inspection
Home station check
Who can approve home station check schedule deviations
Operational wing commander
Operations group commander
Mx group commander
Lead command functional manager
Who performs acceptance inspections
Mx personnel from the depot
Mx personnel from the losing unit
Mx personnel from the gaining unit
Major command HQ functional managers
On the martin baker seat, components made from which type of metal are highly susceptible to corrosion?
Steel
Tungsten
Aluminium
Magnesium
During an F16 canopy inspection, what would you use to check for cracks around bolt holes which would otherwise not be visible
Magnifying glass
Borescope
Mirrior
Prism
Which ACES II component would you functionally check during a 36 month inspection
Seat sidecap
Survival kit radio
Sequence start switch
Pitch stabilization control assembly
Who decides to alert the rest of the AF to the results of a one time inspection (OTI)
Supervisors
QA
The lead command
The mx group commander
During which inspection phase would personnel discuss what can reasonably be accomplished during the time allotted?
Fix phase
Look phase
Pre inspection phase
Post inspection phase
Which inspection phase prepares the aircraft for a functional check flight
Fix phase
Look phase
Pre inspection phase
Post inspection phase
On the ACES II seat which explosive component rolls the seat about its horizontal axis to impart a horizontal vector to its trajectory
Drogue parachute
Restraint release thruster
Trajectory divergence rocket
Pitch stabilization control assembly
On the ACES II seat which type of aircraft seats have single firing control handles
A10 and F15
B-1B and B2
B52 and T38
F16 and F22
During ACES II seat ejection, the flip up pitot tubes actuate when the
Ejection control handles is/are pulled
Parachute portion of the seat clears the rails
Pitot inputs are sensed by the speed transducers in the sensor
Static pressure inputs are sensed by altitude transducers in the sensor
Which explosive components do/does not fire during an ACES II ejection if the digital recovery sequencer (DRS) selects mode 1 ejection?
Drogue gun
Restraint release thruster
Drogue severance cutters
Trajectory divergence rocket
During ACES II Ejection, if the DRS selects mode 3 ejection, when will the pilot chute and recovery chute deploy?
0.032 seconds after sequence start switch detection
0.192 seconds after sequence start switch detection
When mode 1 speed and altitude conditions are met
When mode 2 speed and altitude conditions are met
During ACES II Sequence start switch checkout, when checking pins with the switch bellcrank arm depressed, there should be continuity at pins
A and B
A and C
A and D
B and C
If the sequence start switch bellcrank is discovered twisted, what would be the correct action to take
Gently bend/flex the bellcrank into tolerable limits
Replace the bellcrank and test new one with the Go/No-Go gauge
Place bellcrank in a vice and straighten to pass the go no go test
Place bellcrank on a hard, flat, level surface and use a soft faced hammer to straighten into tolerable limits that will pass the go no go gauge
What are you required to do after making sure the striker stop pin is installed during the emergency manual parachute deployment handle test
Pull ground servicing cable
Remove the recovery parachute
Remove the ejection seat pin assembly
Disconnect P-11 from the emergency power supply
What is the first thing to happen after pulling the ground servicing cable during the emergency manual parachute deployment handle test
Lap belt end fittings should release
Mortar disconnect pins should retract
Bellcrank should rotate to the down position
Shoulder restraint retaining pins and lap belt pins should fully retract
During the ACES II firing control handle test for the F15 seat, how many force readings do you record and what is the maximum pull force
Two force readings and 42.5 LBS
Four force readings and 42.5 LBS
Two force readings and 57.5 LBS
Four force readings and 57.5 LBS
What ACES II components should be checked for presence of lubrication when the seat is removed from the aircraft
Packings
Seat rollers
Pulley bellcranks
Canopy actuator release bolts
If your shop cannot resolve a technical problem with the advanced concept ejection seat ACES II where should you seek assistance
Engineering
The item manager at the air logistics complex
The system manager at the air logistics complex
Air force material command depot engineers
When troubleshooting an ACES II inertia reel, if the strap width does not meet .69 to .75 inches, correct it by
Replacing the inertia reel straps
Rerouting the inertia reel straps
Readjusting the control assembly terminal
Replacing the inertia reel because it is probably faulty
If an ACES II inertia reel control assembly is binding, the first thing you should check is if
The inertia reel cam level is against the stop in the "A" position
The terminal holes inside the inertia reel cam lever are lined up
The inertia reel cam lever is slightly preloaded to the full travel position
There is presence of lubricant inside the inertial reel control assembly handle slot
On a schematic, if you are uncertain as to what you are looking at, then refer to the
Legend
Previous schematic
Theory of operation
IPB
In which technical order would you usually find escape system schematics
Abbreviated
Fault isolation
General system
Troubleshooting
After you choose the correct technical order for an ejection system schematic, make sure you choose the correct schematic
For the correct item and/or mode of ejection
From the company that engineered the aircraft
That illustrates direction of travel for ballistic gasses
For location of valves, gates, sequencers, and linkages
On the T38 martin baker seat, what controls which of the two aircrew members starts the ejection sequence
AND gates
Check valves
Input cartridges
Interseat sequencing system
The t38 martin baker seats have 5 main assemblies, including the seat survival kit, the parachute assembly, the seat bucket assembly, the catapult and cross beams assembly, and the
Intermediate rails assembly
Guide rails assembly
Seat back assembly
Headrest assembly
On the T38 martin baker seat, if the automatic seat separation sequence does NOT operate, the aircrew can
Pull the emergency manual chute deployment handle
Cut the restrains and leap from the seat
Pull the manual parachute release cord
Pull the manual override handle
On the T38 martin baker seat, which component starts the ejection sequence?
Firing handle
Main rocket catapult
Sequence start switch
Analog recovery sequencer
On the T38 martin baker seat, what fires the under seat rocket motor (USRM) after the end of the catapult stroke?
Bleed off gas pressure from the secondary cartridges
The length of the left multi purpose initiator static line
The length of the right multi purpose initiator static line
Bleed off gas pressure from the powered inertia reel device
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