2a673 (Edit Code 03) Volume 2, Aircrew Egress Systems Craftsman

Reviewed by Editorial Team
The ProProfs editorial team is comprised of experienced subject matter experts. They've collectively created over 10,000 quizzes and lessons, serving over 100 million users. Our team includes in-house content moderators and subject matter experts, as well as a global network of rigorously trained contributors. All adhere to our comprehensive editorial guidelines, ensuring the delivery of high-quality content.
Learn about Our Editorial Process
| By Am315216
A
Am315216
Community Contributor
Quizzes Created: 2 | Total Attempts: 1,347
| Attempts: 573 | Questions: 67
Please wait...
Question 1 / 67
0 %
0/100
Score 0/100
1. What tool should you always use to remove the safety wire from a detonation transfer assembly (DTA)?

Explanation

Diagonal cutting pliers should always be used to remove the safety wire from a detonation transfer assembly (DTA). These pliers have a sharp cutting edge that allows for easy and precise cutting of the wire. Slip-joint pliers, flat-nosed pliers, and lineman's side cutting pliers are not specifically designed for cutting wire and may not provide the same level of precision and ease of use as diagonal cutting pliers.

Submit
Please wait...
About This Quiz
Egress Systems Quizzes & Trivia

This quiz tests knowledge on Aircrew Egress Systems for the F-16 dual seat aircraft, covering modes of ejection, system components, and safety procedures.

Personalize your quiz and earn a certificate with your name on it!
2. When using the fault isolation (FI) manual to troubleshoot an F-16, which section in Chapter 2 would you find the fault isolation tree?

Explanation

In the fault isolation (FI) manual for troubleshooting an F-16, the fault isolation tree can be found in Section IV, Fault Isolation Information. This section provides detailed information on how to isolate and identify faults in the aircraft. The fault isolation tree is a visual representation of the troubleshooting process, helping technicians to systematically narrow down the possible causes of a problem. By following the steps in the fault isolation tree, technicians can efficiently diagnose and fix issues with the F-16.

Submit
3. Before operational use or during assembly and buildup involving SMDCs, what is the first thing you should do?

Explanation

The correct answer is to perform a 100 percent visual inspection. Before operational use or during assembly and buildup involving SMDCs, it is important to visually inspect all components to ensure they are in good condition and free from any visible wear and tear. This step helps to identify any potential issues or damage that may affect the performance or safety of the SMDCs. By conducting a thorough visual inspection, any problems can be addressed and resolved before proceeding with further operations or assembly.

Submit
4. When removing the F-15 #3 pyrotechnic module on an aircraft, you prevent damage to SMDC lines by

Explanation

Rotating the fittings only, not the lines, prevents damage to SMDC (Secondary Multiplex Data Concentrator) lines when removing the F-15 #3 pyrotechnic module on an aircraft. This is because rotating the fittings allows for a controlled and secure disconnection of the module without putting strain or stress on the lines themselves. By rotating only the fittings, the lines can be safely disconnected and removed without causing any damage or compromising the integrity of the SMDC lines.

Submit
5. Except for SOLO mode, what is the sequence of operation for two-seat F-15Es during an AFT INITIATE ejection?

Explanation

The correct sequence of operation for two-seat F-15Es during an AFT INITIATE ejection is to first jettison the canopy, then eject the rear seat, and finally eject the front seat. This order ensures that the rear seat occupant can safely exit the aircraft before the front seat occupant.

Submit
6. When performing a dual-seat F-16 canopy removal, Technician C's job is to

Explanation

Technician C's job in a dual-seat F-16 canopy removal is to assist in the removal of the canopy and operate the hoist. This means that Technician C is responsible for providing support during the removal process and also operating the hoist, which is used to lift and lower the canopy. The other options are not correct because they do not encompass both assisting in the removal and operating the hoist.

Submit
7. When troubleshooting an F-16 canopy system, if you have verified that the canopy manual drive hand crank does not engage and operate the manual drive assembly, your only course of action is to replace the 

Explanation

If the canopy manual drive hand crank does not engage and operate the manual drive assembly, it suggests that there is a problem with the assembly itself. Since the manual drive assembly is responsible for operating the canopy system, it is likely that replacing it will resolve the issue. The other options, such as the canopy actuator, unlock handle, and unlock warning switch, may be related to the canopy system but do not directly address the problem of the manual drive not engaging. Therefore, the only logical course of action is to replace the canopy manual drive assembly.

Submit
8. While performing the operational checkout of the F-16 seat height adjustment switch, when you position the seat height adjustment switch to the UP position and release the switch, the seat should

Explanation

When performing the operational checkout of the F-16 seat height adjustment switch, if the switch is positioned to the UP position and released, the seat should start moving upwards and then stop at the desired height. After that, the switch should automatically return to the center position. This ensures that the seat can be adjusted to the desired height and that the switch functions properly by returning to its original position after use.

Submit
9. To gain access to the F-15 #3 pyrotechnic module when removing it on the aircraft, you must reposition the 

Explanation

To gain access to the F-15 #3 pyrotechnic module when removing it on the aircraft, the seat actuator/rocket catapult must be repositioned. This implies that the seat actuator/rocket catapult is obstructing the access to the pyrotechnic module and needs to be moved in order to remove it.

Submit
10. When installing the F-15 #3 pyrotechnic module, remove foreign objects from an explosive device port by

Explanation

When installing the F-15 #3 pyrotechnic module, it is important to remove any foreign objects from the explosive device port to ensure proper functioning and safety. The most effective method mentioned in the answer choices is to turn the component upside down and shake it. This action will allow any foreign object to fall out of the port due to gravity, minimizing the risk of the object interfering with the module's operation.

Submit
11. When installing the F-15 #3 pyrotechnic module on the aircraft, what is a good way to prevent damage to SMDC lines?

Explanation

Using two wrenches while tightening connectors is a good way to prevent damage to SMDC lines when installing the F-15 #3 pyrotechnic module on the aircraft. This technique ensures that equal force is applied to both sides of the connector, preventing any twisting or torque that could damage the SMDC lines. By using two wrenches, the risk of over-tightening or under-tightening the connectors is minimized, ensuring a secure and damage-free installation.

Submit
12. What should be done if the F-22 oxygen system pressure gauge reads below limits?

Explanation

If the F-22 oxygen system pressure gauge reads below limits, the best course of action is to completely purge and refill the cylinder. This will ensure that the cylinder is filled with the proper amount of oxygen and will bring the pressure gauge back within the acceptable limits.

Submit
13. When performing the operational checkout of the ejection seat arm-safe ejection control handle and switch on an F-16, when you place the ejection control safety handle in the EJECTION CONTROLS LOCKED position, the handle should move freely and the

Explanation

When the ejection control safety handle is placed in the EJECTION CONTROLS LOCKED position, the SEAT NOT ARMED light should come on. This indicates that the ejection seat is not armed and is in a safe position. The other options, such as the CANOPY warning light coming on or going out, are not related to the position of the ejection control safety handle and are therefore incorrect.

Submit
14. When inspecting SMDCs, what tool do you use to compare the size and depth of depressions?

Explanation

When inspecting SMDCs, a thickness feeler gauge is used to compare the size and depth of depressions. This tool is specifically designed to measure the thickness or depth of small gaps or depressions. It consists of a set of individual blades of varying thicknesses that can be inserted into the depression to determine its size. The other options, such as magnifiers and a steel rule, are not suitable for this purpose as they do not provide accurate measurements of the size and depth of depressions.

Submit
15. Which F-22 escape system component provides sequenced firing signals for the electronic explosive devices (EED)?

Explanation

The Emergency Escape Sequencing System (EESS) is the component of the F-22 escape system that provides sequenced firing signals for the electronic explosive devices (EED). It is responsible for coordinating the activation of the various explosive devices involved in the escape process, ensuring that they are fired in the correct sequence and at the appropriate times. This system plays a crucial role in the safe ejection of the pilot from the aircraft during an emergency situation.

Submit
16. During an F-22 ejection, at what speed and altitude is Mode 1 selected?

Explanation

During an F-22 ejection, Mode 1 is selected when the speed is less than 250 knots and the altitude is less than 15,000 feet.

Submit
17. What type of energy transfer line does the F-16 emergency escape sequencing system use?

Explanation

The F-16 emergency escape sequencing system uses DTA, which stands for Dual Tandem Actuation. This type of energy transfer line allows for a reliable and efficient transfer of energy in emergency situations. It is designed to activate various systems and mechanisms that are necessary for the safe ejection of the pilot from the aircraft. The DTA system ensures that the energy is transferred accurately and quickly, enabling a timely response during emergencies.

Submit
18. During an F-22 ACES II Mode 3 ejection, when does the pilot's chute and recovery parachute deploy?  

Explanation

not-available-via-ai

Submit
19. What F-16 canopy jettison explosive component releases the canopy from the canopy actuator?

Explanation

The correct answer is "Canopy actuator release bolt (CARB)". The CARB is the explosive component that releases the canopy from the canopy actuator. It is designed to be easily jettisoned in emergency situations, allowing the canopy to be quickly and safely removed.

Submit
20. What types of DTA lines contain a primary explosive that may be detonated by impact, shock, abrasion, or excessive heat?

Explanation

The correct answer is Receptor (R) or shock tube receptor (STR) types. These types of DTA lines contain a primary explosive that can be detonated by impact, shock, abrasion, or excessive heat. This means that any force or heat applied to these types of DTA lines can cause the primary explosive to detonate.

Submit
21. When removing the f-15 #3 pyrotechnic module on the aircraft, what is a concern that sets this job apart from other egress jobs?

Explanation

The concern that sets removing the f-15 #3 pyrotechnic module apart from other egress jobs is the increased potential for cockpit foreign object debris (FOD) from pyrotechnic hardware. This means that there is a higher risk of debris or objects getting into the cockpit during the removal process, which can be dangerous and cause damage to the aircraft or harm to the personnel working on it.

Submit
22. The F-22's rocket motor fires during canopy jettison through

Explanation

The F-22's rocket motor fires during canopy jettison through impulses sent through the Emergency Escape Sequencing System (EESS) wire harness. This means that the EESS wire harness is responsible for transmitting the necessary electrical impulses to initiate the firing of the rocket motor. It is through this system that the necessary signals are sent to activate the rocket motor and ensure a successful canopy jettison process.

Submit
23. When rigging a dual-seat F-16 canopy actuator, what should the canopy lock handle's cam and lock lug measure?

Explanation

The correct answer is 0.040 to 0.080 inch. This measurement refers to the distance between the canopy lock handle's cam and lock lug. This measurement is important in order to ensure that the canopy is securely locked in place during flight. If the measurement is too small, the canopy may not be properly locked, posing a safety risk. On the other hand, if the measurement is too large, it may be difficult to properly engage or disengage the canopy lock. Therefore, the ideal measurement range is between 0.040 to 0.080 inch.

Submit
24. F-16 canopy remover rockets are initiated by

Explanation

The F-16 canopy remover rockets are initiated by the detonation transfer assembly (DTA). The DTA is responsible for transferring the detonation signal from the rocket's initiator to the main charge. This assembly ensures that the rockets are activated at the right time and with the necessary force to remove the canopy. It acts as a crucial component in the rocket's ignition system, allowing for a controlled and precise initiation of the rockets.

Submit
25. During a dual seat F-16 ejection when the ejection mode selector valve is set in aft mode and the aft seat ejection handle is pulled, what explosive component is specifically designed to provide an automatic sequence to eject the forward seat?

Explanation

The M53 initiator is specifically designed to provide an automatic sequence to eject the forward seat during a dual seat F-16 ejection when the ejection mode selector valve is set in aft mode and the aft seat ejection handle is pulled.

Submit
26. When installing a dual-seat F-16 canopy, you stop lowering the canopy before you install the keeper when the protractor reflects the canopy angle with the longeron at approximately how many degrees?

Explanation

The correct answer is 27. When installing a dual-seat F-16 canopy, the protractor reflects the canopy angle with the longeron at approximately 27 degrees. This means that when lowering the canopy, you should stop before installing the keeper at this angle to ensure proper installation.

Submit
27. If detonation transfer assembly (DTA) line threads are not coated with a light coat of solid film lubricant, lubricate them by sliding the nut back from the tip and 

Explanation

not-available-via-ai

Submit
28. To how many inch-pounds should you torque DTA nuts?

Explanation

The correct answer is 50-70. This range indicates the recommended torque in inch-pounds for tightening DTA nuts. Torque is a measure of the force applied to rotate an object, in this case, the nuts. The range of 50-70 inch-pounds ensures that the nuts are securely tightened without being over-tightened, which could potentially damage the nuts or the equipment they are being used on.

Submit
29. The first thing you must remove before removing an F-15 #3 pyrotechnic module is 

Explanation

Before removing an F-15 #3 pyrotechnic module, the first thing that must be removed is the ACES II ejection seat.

Submit
30. When troubleshooting an F-16 canopy system, if the canopy warning light stays on with the canopy down and the canopy lock handle is verified down, but manually pressing the unlock warning switch and both hook warning switches simultaneously causes the light to go out, the first step you take to correct the problem is to rig the 

Explanation

The given scenario suggests that the issue lies with the switches. Even though the canopy lock handle is verified down, the canopy warning light stays on. However, when the unlock warning switch and both hook warning switches are manually pressed simultaneously, the light goes out. This indicates that there might be a problem with the switches, causing the light to stay on incorrectly. Rigging the switches would be the first step to correct this issue.

Submit
31. What are the three modes of operation on the F-15E emergency escape sequencing system?

Explanation

The correct answer is NORM, SOLO, and AFT INITIATE. These are the three modes of operation on the F-15E emergency escape sequencing system. The NORM mode is the normal mode of operation, the SOLO mode is used when only one seat needs to be ejected, and the AFT INITIATE mode is used to initiate ejection from the rear seat.

Submit
32. What action should you take if you find a cut on the rubber seal at the end of a SMDC booster?

Explanation

If a cut is found on the rubber seal at the end of a SMDC booster, the appropriate action to take would be to replace the rubber seal. This is because a cut in the rubber seal can compromise its integrity and effectiveness in sealing the booster. By replacing the rubber seal, the functionality and safety of the SMDC booster can be ensured.

Submit
33. What begins the ejection sequence on an F-22?

Explanation

The ejection sequence on an F-22 is initiated by electrical voltage produced from the thermal battery initiators. This voltage is responsible for activating the necessary mechanisms and systems for a successful ejection.

Submit
34. What are the four positions for setting the F-15 canopy control handles?

Explanation

The correct answer is LOCKED, DN, HOLD, and UP. This is because these four positions represent the different states of the F-15 canopy control handles. LOCKED refers to when the canopy is securely closed and locked in place. DN stands for down, indicating that the canopy is being lowered. HOLD means that the canopy is being held in a partially open position. UP signifies that the canopy is fully open and raised.

Submit
35. How many canopy jettison initiators are installed on a dual seat F-16?

Explanation

There are four canopy jettison initiators installed on a dual-seat F-16. This means that there are four mechanisms or devices that can be used to initiate the jettisoning or removal of the canopy on the aircraft.

Submit
36. What are the modes of ejection available for an F-16 dual seat aircraft?

Explanation

The correct answer is NORM, SOLO, and AFT. This means that the F-16 dual seat aircraft has three modes of ejection available: NORM (normal mode) which is used when both seats need to be ejected, SOLO which is used when only the front seat needs to be ejected, and AFT which is used when only the rear seat needs to be ejected. These modes provide flexibility and safety in different emergency situations.

Submit
37. The best description of the F-15E canopy is that it's a

Explanation

The F-15E canopy is described as a clamshell type because it is made of formed, transparent plastic that is mounted in a metal frame. This design allows for easy jettisoning of the canopy from the aircraft frame when needed.

Submit
38. During dual-seat F-16 canopy jettison during seat ejection, the detonation transfer assembly (DTA) initiators are fired by hot gas from the

Explanation

The correct answer is M53 initiators through the sequence valves. This means that during dual-seat F-16 canopy jettison during seat ejection, the M53 initiators are fired by hot gas from the sequence valves.

Submit
39. What F-16 escape system component keeps the pressure of the gas in the escape system at an acceptably high level?

Explanation

The M53 initiators are responsible for maintaining the pressure of the gas in the F-16 escape system at an acceptably high level. These initiators play a crucial role in ensuring the effectiveness and efficiency of the escape system by regulating the gas pressure.

Submit
40. You should cease F-16 canopy maintenance if wind speed exceeds how many knots?

Explanation

If the wind speed exceeds 20 knots, F-16 canopy maintenance should be ceased. This is because high wind speeds can make it difficult and unsafe to work on the canopy. Strong winds can cause the canopy to move or slam shut unexpectedly, posing a risk to the maintenance personnel. Therefore, it is important to stop maintenance activities when wind speeds reach or exceed 20 knots to ensure the safety of the personnel and prevent any potential damage to the canopy.

Submit
41. During a Mode 2 ejection on the F-22, what begins the same time the sequence start switch is detected?

Explanation

During a Mode 2 ejection on the F-22, the drogue parachute deploys at the same time the sequence start switch is detected. This means that as soon as the sequence start switch is activated, the drogue parachute is immediately deployed.

Submit
42. What type of energy transfer lines does the F-15E emergency escape sequencing system use?

Explanation

The F-15E emergency escape sequencing system uses SMDC (Solid Motor Disconnect Circuit) energy transfer lines. SMDC is a type of circuit that is designed to disconnect the solid rocket motor from the aircraft during an emergency escape sequence. It ensures a safe separation of the motor from the aircraft by transferring the necessary energy to activate the separation mechanism. This system is crucial for the safety of the pilot in case of emergencies.

Submit
43. Using the detonation transfer assembly (DTA) and emergency canopy release line (ECRL) inspection gauge set, how do you check the DTA minimum tip length?

Explanation

To check the DTA minimum tip length, the -25 inspection gauge should be positioned across the lower surfaces of the inspection gauge containing the DTA. This means that the -25 inspection gauge should be placed underneath the DTA, allowing for measurement of the tip length. This method ensures accurate measurement and assessment of the DTA's minimum tip length.

Submit
44. The F-15E external canopy jettison initiator is fired by

Explanation

The correct answer is pulling the canopy jettison handle to extend the cable for 8 feet then jerking the handle. This is because the F-15E external canopy jettison initiator is fired by pulling the canopy jettison handle to extend the cable for a certain distance, in this case, 8 feet, and then jerking the handle. This action activates the mechanism that breaks the frangible panel and allows the canopy to be jettisoned.

Submit
45. The total surface area of dents on a SMDC booster tip cannot exceed what percent of the outside surface area?

Explanation

The total surface area of dents on a SMDC booster tip cannot exceed 10% of the outside surface area. This means that the dents should not cover more than 10% of the total surface area of the booster tip.

Submit
46. At least how many degrees of arc should be allowed between adjacent dents on a SMDC booster tip?

Explanation

Adjacent dents on a SMDC booster tip should be allowed to have at least 135 degrees of arc between them. This is because the question is asking for the minimum angle between the dents, and 135 degrees is the option that provides the largest angle. A larger angle between the dents would allow for better stability and structural integrity of the booster tip.

Submit
47. How many broken strands are allowable on wire braid outer coverings of flexible DTA lines?

Explanation

The correct answer is that no more than one broken strand per 12-inch section or more than three broken strands total are allowable on wire braid outer coverings of flexible DTA lines. This means that if there is any damage to the wire braid, it should not exceed one broken strand per 12-inch section, and the total number of broken strands should not exceed three. This ensures that the wire braid remains intact and provides sufficient protection for the flexible DTA lines.

Submit
48. Where is the F-16's emergency canopy release line (ECRL) located?

Explanation

The F-16's emergency canopy release line (ECRL) is located on each side of the cockpit. This means that there is a release line on both the left and right sides of the cockpit, allowing the pilot to quickly and easily release the canopy in case of an emergency.

Submit
49. During F-16 canopy removal, you should check that

Explanation

During the F-16 canopy removal, it is important to check that the upper and lower roller bearings have freedom of rotation. This is because the roller bearings are responsible for allowing smooth movement of the canopy along the hinge track. If the roller bearings do not have freedom of rotation, it could lead to binding or difficulty in opening and closing the canopy. Therefore, ensuring that the roller bearings can rotate freely is crucial for a successful canopy removal process.

Submit
50. When performing a dual-seat F-16 canopy removal, you should fully open the canopy prior to installing the two canopy maintenance supports using the

Explanation

When performing a dual-seat F-16 canopy removal, the correct procedure is to fully open the canopy prior to installing the two canopy maintenance supports. This is done using the external canopy switch. The external canopy switch allows for easy and convenient control of the canopy, ensuring that it is fully open before proceeding with the installation of the maintenance supports. The internal canopy switch, internal manual drive handcrank, and external manual drive receptacle are not suitable for this task as they do not provide the necessary control and functionality required for fully opening the canopy.

Submit
51. When the F-15E canopy jettison system is initiated externally, what actuates the fired warning indicator?

Explanation

The fired warning indicator is actuated by the canopy actuated initiator when the F-15E canopy jettison system is initiated externally. This means that when the canopy is jettisoned, the actuator within the canopy actuated initiator triggers the fired warning indicator to alert the pilot or crew.

Submit
52. When you install the tension tubes on a dual-seat F-16 during canopy installation, what pattern should they form with the canopy in the full up position?

Explanation

When installing the tension tubes on a dual-seat F-16 during canopy installation, they should form a V pattern. The lower point of the V should be pointing forward, while the upper connection points of the V should be pointing aft. This configuration ensures proper tension and stability for the canopy.

Submit
53. When installing the F-15 #3 pyrotechnic module, apply a dry air or nitrogen source to flow check ballistic hoses between

Explanation

not-available-via-ai

Submit
54. When installing an F-15 #3 pyrotechnic module, what do you do after the SMDC lines are installed?

Explanation

After the SMDC lines are installed, the next step is to connect the electrical receptacle to the IFF seat switch. This ensures that the pyrotechnic module is properly connected and ready for use.

Submit
55. Which dual seat F-16 explosive component fires each seat's inertia reel initiator?

Explanation

The correct answer is the right-side JAU-8/A25 ejection control initiator. This component is responsible for firing each seat's inertia reel initiator in a dual-seat F-16 aircraft.

Submit
56. Where are the F-15E's internal canopy jettison handles located?

Explanation

The F-15E's internal canopy jettison handles are located under the left canopy sill in either cockpit.

Submit
57. What is the danger area if the canopy is jettisoned on the F-22 during a ground emergency?

Explanation

The danger area if the canopy is jettisoned on the F-22 during a ground emergency is 60 feet away, aft and to the right of the aircraft centerline.

Submit
58. Which component extends the canopy remover piston when the F-15E canopy jettison system is initiated externally?

Explanation

The correct answer is the Canopy remover cartridge. When the F-15E canopy jettison system is initiated externally, the canopy remover cartridge is responsible for extending the canopy remover piston. This allows for the quick and efficient removal of the canopy from the aircraft.

Submit
59. Which F-22 components are actuated by the internal or external canopy jettison handles to initiate the canopy jettison system?

Explanation

The correct answer is thermal batteries. Thermal batteries are responsible for providing the necessary power to initiate the canopy jettison system in the F-22. They are designed to deliver a high amount of energy in a short period of time, making them suitable for activating various systems in the aircraft, including the canopy jettison handles. The other options listed, such as ejection cartridges and initiators, are not directly related to the canopy jettison system.

Submit
60. After the F-16 canopy is installed, you should check that

Explanation

After the F-16 canopy is installed, it is important to check that the lower roller bearing contacts the canopy track with no rotation. This ensures that the canopy will move smoothly along the track without any friction or obstruction. If the lower roller bearing rotates, it may cause the canopy to bind or get stuck, which can be a safety hazard. Therefore, ensuring that the lower roller bearing remains stationary while in contact with the canopy track is necessary for proper functioning of the canopy system.

Submit
61. Approximately ho far is the lanyard pulled when externally initiating an F-22 canopy jettison?

Explanation

The correct answer is 6 inches. When externally initiating an F-22 canopy jettison, the lanyard is only pulled approximately 6 inches. This means that the lanyard is only required to be pulled a short distance in order to activate the canopy jettison system on the F-22 aircraft.

Submit
62. How is the F-22 drogue parachute deployed?

Explanation

The F-22 drogue parachute is deployed by ballistic pressure from a mortar cartridge that propels the outer tube, pushing the chute out of a canister.

Submit
63. During normal operation, which F-22 canopy jettison component acts as a fixed structural element between the canopy actuator and the canopy frame?

Explanation

The canopy thruster acts as a fixed structural element between the canopy actuator and the canopy frame during normal operation of the F-22. It helps to maintain the stability and integrity of the canopy by providing support and ensuring proper alignment between the actuator and the frame. The canopy thruster plays a crucial role in the safe and efficient functioning of the canopy jettison system in the F-22 aircraft.

Submit
64. When F-15E ejection is initiated in NORM mode by the front crewmember, what component fires the rear seat's inertia reel initiator?

Explanation

In the given scenario, when the F-15E ejection is initiated in NORM mode by the front crewmember, the component that fires the rear seat's inertia reel initiator is a SMDC-gas initiator.

Submit
65. Which F-22 canopy jettison feature ensures full latch release prior to the rocket motor's ignition?

Explanation

The rocket motor is initiated after 1.2 inches of thruster extension, ensuring that the canopy disconnects once 2.0 inches of thruster extension separates the thruster into two segments. This sequence ensures that the canopy is fully released before the rocket motor ignites, preventing any potential issues or obstructions during the jettison process.

Submit
66. During F-22 canopy jettison, how many inches does the canopy travel aft before the canopy rotates around the aft hinge line of the canopy?

Explanation

During F-22 canopy jettison, the canopy travels aft before rotating around the aft hinge line. The correct answer is 2.5 inches.

Submit
67. Where inside the F-22 cockpit is the internal canopy jettison handle located?

Explanation

The internal canopy jettison handle in the F-22 cockpit is located on top of the left console. This means that the handle can be easily accessed and operated by the pilot from this position.

Submit
View My Results

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.

  • Current Version
  • Aug 31, 2023
    Quiz Edited by
    ProProfs Editorial Team
  • Jun 08, 2020
    Quiz Created by
    Am315216
Cancel
  • All
    All (67)
  • Unanswered
    Unanswered ()
  • Answered
    Answered ()
What tool should you always use to remove the safety wire from a...
When using the fault isolation (FI) manual to troubleshoot an F-16,...
Before operational use or during assembly and buildup involving SMDCs,...
When removing the F-15 #3 pyrotechnic module on an aircraft, you...
Except for SOLO mode, what is the sequence of operation for two-seat...
When performing a dual-seat F-16 canopy removal, Technician C's...
When troubleshooting an F-16 canopy system, if you have verified that...
While performing the operational checkout of the F-16 seat height...
To gain access to the F-15 #3 pyrotechnic module when removing it on...
When installing the F-15 #3 pyrotechnic module, remove foreign objects...
When installing the F-15 #3 pyrotechnic module on the aircraft, what...
What should be done if the F-22 oxygen system pressure gauge reads...
When performing the operational checkout of the ejection seat arm-safe...
When inspecting SMDCs, what tool do you use to compare the size and...
Which F-22 escape system component provides sequenced firing signals...
During an F-22 ejection, at what speed and altitude is Mode 1...
What type of energy transfer line does the F-16 emergency escape...
During an F-22 ACES II Mode 3 ejection, when does the pilot's...
What F-16 canopy jettison explosive component releases the canopy from...
What types of DTA lines contain a primary explosive that may be...
When removing the f-15 #3 pyrotechnic module on the aircraft, what is...
The F-22's rocket motor fires during canopy jettison through
When rigging a dual-seat F-16 canopy actuator, what should the canopy...
F-16 canopy remover rockets are initiated by
During a dual seat F-16 ejection when the ejection mode selector valve...
When installing a dual-seat F-16 canopy, you stop lowering the...
If detonation transfer assembly (DTA) line threads are not...
To how many inch-pounds should you torque DTA nuts?
The first thing you must remove before removing an F-15 #3...
When troubleshooting an F-16 canopy system, if the canopy warning...
What are the three modes of operation on the F-15E emergency escape...
What action should you take if you find a cut on the rubber seal at...
What begins the ejection sequence on an F-22?
What are the four positions for setting the F-15 canopy control...
How many canopy jettison initiators are installed on...
What are the modes of ejection available for an F-16 dual seat...
The best description of the F-15E canopy is that it's a
During dual-seat F-16 canopy jettison during seat ejection, the...
What F-16 escape system component keeps the pressure of the gas in the...
You should cease F-16 canopy maintenance if wind speed exceeds how...
During a Mode 2 ejection on the F-22, what begins the same time the...
What type of energy transfer lines does the F-15E emergency escape...
Using the detonation transfer assembly (DTA) and emergency canopy...
The F-15E external canopy jettison initiator is fired by
The total surface area of dents on a SMDC booster...
At least how many degrees of arc should be allowed between adjacent...
How many broken strands are allowable on wire braid outer coverings of...
Where is the F-16's emergency canopy release line (ECRL) located?
During F-16 canopy removal, you should check that
When performing a dual-seat F-16 canopy removal, you should fully open...
When the F-15E canopy jettison system is initiated externally, what...
When you install the tension tubes on a dual-seat F-16 during canopy...
When installing the F-15 #3 pyrotechnic module, apply a dry air or...
When installing an F-15 #3 pyrotechnic module, what do you...
Which dual seat F-16 explosive component fires each seat's inertia...
Where are the F-15E's internal canopy jettison handles...
What is the danger area if the canopy is jettisoned on the F-22 during...
Which component extends the canopy remover piston when the F-15E...
Which F-22 components are actuated by the internal or external canopy...
After the F-16 canopy is installed, you should check that
Approximately ho far is the lanyard pulled when externally initiating...
How is the F-22 drogue parachute deployed?
During normal operation, which F-22 canopy jettison component acts as...
When F-15E ejection is initiated in NORM mode by...
Which F-22 canopy jettison feature ensures full latch release prior to...
During F-22 canopy jettison, how many inches does the canopy travel...
Where inside the F-22 cockpit is the internal canopy jettison handle...
Alert!

Advertisement