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WAPS Testing > 2A353 Volume 5 > Flashcards

2A353 Volume 5 Flashcards

1
Q

1The F-22 inspection that is accomplished within six hours of launch and only if the pre-fight is over 48 hours but still valid is the

A

Walk around inspection

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2
Q

2Outer mold line inspection will be accomplished on the F-22 when maintenance notices

A

Low observable damage

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3
Q

3On the F-22, the responsibility for all low Observable maintenance rest with the: crewchief, aero repair, system specialists, or aircraft structural maint

A

Aircraft structural maintenance

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4
Q

The purpose of the SAS is to outline the repair and restoration process, reliability and maintainability data collection, and time accounting for managing the F-22’s

A

Low observable system

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5
Q

On the F-22, what is the output pressure for the hydraulic systems pumps

A

4050 to 4150 psi

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6
Q

On the F-22 hydraulic system, what service coupling quick disconnect provides an alternate method to fill the hydraulic reservoir

A

Return ground service

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7
Q

On the F-22, what prevents the maintainer from installing the filter bowl without a filter inside

A

Spring-loaded lever

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8
Q

On the F-22 hydraulic control software monitors, the hydraulic system is hosted by the

A

IVSC

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9
Q

On the F-22, what performs the bit on the hydraulic components

A

Software

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10
Q

On the F-22, the pressure transducer operates over A pressure range of

A

0 to 5000 psig

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11
Q

On the F-22, What provides the maintainer an indication that the filter element requires replacement

A

Differential pressure indicator

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12
Q

The mode on the F-22 that uses the pneumatic back up system to pressurize the unlock devices to release the landing gear for extending and locking it into the extended position is

A

Emergency flight

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13
Q

On the F-22, a base plate and two interchangeable brake modules make up what valve

A

Brake control

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14
Q

On the F-22, the wheels and tires are protected from excessive Brake heat by a heatshield made out of

A

Stainless steel

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15
Q

The F-22 nosewheel may normally be turned up to 48 depending on

A

Main landing gear wheel speed

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16
Q

In the F-22 nosewheel steering system, what valve allows free castering of the nose wheel: shuttle, control, antiskid, or bleeder

A

Control

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17
Q

The F-22 arresting gear system is pneumatically actuated and controlled

A

Electrically

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18
Q

F-22’s engine fan variable vanes position is controlled by

A

And actuator

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19
Q

The engine on the F-22 contains three assemblies; External hardware, supporting ring and the fan bypass ducts that are referred to as

A

Non-modular

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20
Q

The F-22’s engine lube system contains oil in the bearing compartment by using

A

Engine supplied compressor air

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21
Q

The F-22’s primary source of power for the full authority digital electric Control, the comprehensive engine diagnostic unit, and the ignition exciters is the

A

Engine generator

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22
Q

The F-22 program that acquires data for engine mission capability, onboard diagnostic system failures, propulsion data, and characterizing mission usage is the

A

Advanced engine failure resolution

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23
Q

IMIS Displays input screens to enable The maintainer to enter suspected

A

Fault identification codes

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24
Q

The presence of an overheat on the F-22 is reported for display in the cockpit by the

A

Integrated vehicle subsystem controller

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25
Q

The presence of a fire in the F-22 engine or APU compartment is reported to the fire protection module by the

A

Optical fire detection system

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26
Q

On the F-22, what components take care of the onboard engine monitoring diagnostics functions

A

FADEC and CEDU

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27
Q

Vibration, oil debris, oil level signals, along with condition monitoring and fault information, are stored in the F-22’s resident memory of the

A

CEDU

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28
Q

The fan and compressor variable vanes, as well as the modulated exhaust cooling and exhaust nozzle all make up the F-22’s engine

A

Variable geometry system

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29
Q

The f-22 engine monitoring system uses how many temperature sensors

A

3

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30
Q

The F-22 system component that provides all electrical interconnects between the vehicle management system modules and the aircraft wiring connectors is the

A

Backplane assembly

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31
Q

The primary flight control surfaces, engine inlet bypass louvers, nosewheel steering, engine thrust and thrust vectoring all receive commands generated by the: Flight control computer, portable maintenance aid, avionics maintenance bus, or FlightSafety circuit system

A

Flight control computer

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32
Q

The F-22 unit designed to detect and shut down an overvoltage condition is the

A

Power supply module

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33
Q

The F 22 program that deals with the computer and software configuration for the respective aircraft system is

A

Operational flight

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34
Q

Normal start in normal operating state are the two system operations of the

A

Integrated vehicle system controller

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35
Q

When F-22 hydraulic pressure is lost the ailerons are

A

Aerodynamically centered

36
Q

The F-22 pitch system is augmented by

A

Thrust vector nozzles

37
Q

The three position, momentary action, center off switch on the F-22 flight control system panel is for the

A

Yaw trim

38
Q

The landing gear handle controls flap settings when Norm is selected on the F-22’s

A

Flap ALT switch

39
Q

F-22 lift augmentation is performed by

A

Leading edge flaps

40
Q

The F-22 leading-edge flap position is based on AOA, Mach, and altitude information computed by the

A

Vehicle management system

41
Q

On the F-22, which valve allows Ariel refuel flow to the aircraft plumbing and prevents flow in the reverse direction

A

Check

42
Q

The primary integrated maintenance information tool used by F-22 technicians during the performance maintenance tasks is the

A

PMA

43
Q

All PMA screens are provided guaranteed communication through the

A

Trusted path menu

44
Q

The two major components that must be installed on the PMA for the F-22 are the battery pack and

A

Removable disk drive

45
Q

The F-22’s PMA battery pack can increase the battery life in the cold temperatures and facilitate effective charging of the battery With the use of

A

An internal heater

46
Q

The function of the PMA that shows a list of all discrepancies and warnings for a particular aircraft is the functional category of

A

Aircraft forms

47
Q

The F-22 support equipment that is built from predominantly commercial off-the-shelf items is the

A

Integrated management information system

48
Q

The system designed to be Used in maintenance units, maintenance operations centers, and off equipment Maintenance shop is

A

MSU

49
Q

The F-22 component that communicates with that MSC and PMA to provide a single source of information to meet the requirements of maintenance personnel is the

A

Maintenance support workstation

50
Q

The F-22 MVI cable provides the electrical interconnect between the PMA and the

A

Aircraft

51
Q

Access to the required technical data is provided when the user selects the

A

Discrepancy they have been Assigned to work

52
Q

The primary source for introducing the F-22’s operational Flight program is the

A

Portable maintenance aid

53
Q

The F-22 diagnostics are controlled by the

A

Global manager software

54
Q

The system F-22 uses for avionics cooling during ground maintenance is

A

PAO Cooling cart

55
Q

It is important to keep the hydraulic test stand as far away as possible from the flight control travel path to prevent

A

Flight control surfaces from impacting the unit

56
Q

The stored energy system servicing cart surfaces remain hot after shutdown for up to how many minutes

A

30

57
Q

The F-22 generator control units receive their power from the

A

Permanent magnet generator

58
Q

The main generator control units on the F-22 are cooled by what kind of air

A

Forced

59
Q

The interface between the electrical power system generators and electrical power subsystem on the F-22 is the

A

Generator distribution center

60
Q

For temperature control, the F-22 uses bleeder, Ram air Polyalphaolefin and

A

Fuel

61
Q

The F-22 system that dehumidifies the precooled air utilizing a bootstrapped compressor, turbine, and water collector is the

A

Refrigeration system

62
Q

The F-22 cockpit distribution and defog system provides air for the Canopy seal, cockpit pressurization, Canopy defog, and the

A

Pilots thermal cooling garment

63
Q

The back up air supply for the F-22’s forced air cooled avionics system is

A

Ram air

64
Q

The three methods for opening the F-22 Canopy are

A

Normal, manual, and emergency

65
Q

The external canopy control switch on the F-22 is located

A

In the nose wheel well

66
Q

Manual operation of the F-22 canopy with a high-speed low torque, non-impact type pneumatic or battery powered tool will open or close the canopy in

A

Less than three minutes

67
Q

How many minutes is the F-22 ejection seat emergency oxygen bottle capable of providing a pilot with Oxygen for

A

20

68
Q

In the avionics hardware architecture of the F-22, the item that sends information to the line replaceable units Is the

A

Common integrated processors

69
Q

The F-22’s vehicle management system, Utilities and subsystems, and the avionics system are all supported by the

A

Air vehicle software

70
Q

The F-22 is provided pneumatic, hydraulic, and electrical power during emergencies and within operating envelope by the

A

Auxiliary power unit

71
Q

The two Ways maintainers can start the F-22 APU are the

A

Portable maintenance aid and pilot vehicle interface

72
Q

When using the PMA to start the APU, the maintainer needs to verify the SES air pressure protective covers are removed and the

A

APU shutdown switch is in Norm

73
Q

During ground shut down the APU on the F-22 Enters a cool down cycle of

A

20 seconds

74
Q

The air turbine starter system, airframe mounted accessory drive, and power takeoff shaft make up the F-22’s

A

Auxiliary power accessory drive system

75
Q

The F-22’s Air pre-charge compressor provides air to the

A

Stored energy system bottles

76
Q

The air storage bottles on the F-22 provide air to the APU door actuation system and the

A

Emergency gear extension

77
Q

The SES on the F-22 uses aircraft fuel and high-pressure air to power the

A

APU gearbox

78
Q

Emergency gear swings and arresting gear operations affects the F-22 SES by

A

Reducing the number of starts

79
Q

On the F-22, how many pumps are Attached to the AMAD

A

Four

80
Q

On the F-22, what in the lubrication system pressurize is the AMAD to 25 PSI above ambient pressure

A

Air pump assembly

81
Q

On the F-22, the weapons bay door drive slows doors Prior to reaching travel limits to prevent

A

Damage to doors or airframe

82
Q

The oil level on the F-22’s PDU is checked by a

A

Sight glass

83
Q

The two configurations the F-22 pylons are built for are

A

Ferry and combat

84
Q

The purpose of the AVEL on the F-22 is to stow and launch the

A

AIM-120C

85
Q

The F-22 weapon system minimizes barrel erosion and heat generation; thus extending the life of the system by

A

Rotating the barrels

WAPS Testing (35 decks)

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