Cdc 2a353 Volume 5. F-22

85 Questions  I  By Mike872208 on January 27, 2010
F-22 maintenance

  
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1.  On the F-22, the responsibility for all low observable maintenance rests with the
A.
B.
C.
D.
2.  The primary source for introducing the F-22's operational flight program is the
A.
B.
C.
D.
3.  The F-22 system that dehumidifies the pre-cooled air utilizing a boot strapped compressor, turbine, and water collector is the
A.
B.
C.
D.
4.  The F-22 MVI cable provides the electrical interconnect between the PMA and the
A.
B.
C.
D.
5.  It is imprtant to keep the hydraulic test stand as far away as possible from the flight control travel path to prevent
A.
B.
C.
D.
6.  On the F-22 hydraulic system, what service coupling quick disconnect provides an alternate method to fill the hydraulic reservoir?
A.
B.
C.
D.
7.  The function of the PMA that shows a listing of all discrepancies and warnings for a particular aircraft is the functional category of
A.
B.
C.
D.
8.  The F-22's engine lube system contains oil in the bearing compartment by using
A.
B.
C.
D.
9.  On the F-22 hydraulic control software monitors, the hydraulic system is hosted by the
A.
B.
C.
D.
10.  On the F-22, the pressure transducer operates over a pressure range of
A.
B.
C.
D.
11.  The air storage bottles on the F-22 provide air to the APU door actuation system and the
A.
B.
C.
D.
12.  On the F-22, the weapons bay door drive slows doors prior to reaching travel limits to prevent
A.
B.
C.
D.
13.  The purpose of the AVEL on the F-22 is to stow and launch the
A.
B.
C.
D.
14.  The engine on the F-22 contains three assemblies; external hardware, supporting ring and the fan bypass ducts that are referred to as
A.
B.
C.
D.
15.  The F-22 arresting gear system is pneumatically actuated and controlled
A.
B.
C.
D.
16.  The F-22 unit designed to detect abd shutdown and over-voltage condition is the
A.
B.
C.
D.
17.  The F-22's vehicle management system, utilites and subsystems, and the avionics system are all supported by the
A.
B.
C.
D.
18.  The air turbine starter system, airframe mounted accessory drive, and power take-off shaft make up the F-22's
A.
B.
C.
D.
19.  For temerature control, the F-22 uses bleed air, ram air, polyalphaolefin and
A.
B.
C.
D.
20.  In the avionics hardware architecture of the F-22, the item that sends information to the line replacable units (LRU) is the
A.
B.
C.
D.
21.  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.
B.
C.
D.
22.  The landing gear handle controls flap setting when norm is selected on the F-22s
A.
B.
C.
D.
23.  The presence of an overheat on the F-22 is reported for display in the cockpit by the
A.
B.
C.
D.
24.  On the F-22, what provides the maintainer an indication that the filter element requires replacement?
A.
B.
C.
D.
25.  The F-22's air recharge compressor provides air to the
A.
B.
C.
D.
26.  On the F-22, the wheels and tires are protected from excessive brake heat by a heat shield made out of
A.
B.
C.
D.
27.  The F-22 program that acquires data for engine mission capability, on-board diagnostic system failures, propulsion data, and characterizing mission usage is the
A.
B.
C.
D.
28.  The F-22's engine fan variable vanes position is controlled by
A.
B.
C.
D.
29.  The F-22's PMA battery pack can increase the battery life in cold temperatures and facilitate effective charging of the battery with the use of
A.
B.
C.
D.
30.  The back-up air supply for the F-22's forced air cooled avionics system is
A.
B.
C.
D.
31.  The F-22 weapon system minimizes barrel erosion and heat generation; thus extending the life of the system by
A.
B.
C.
D.
32.  Emergency gear swings and arresting gear operations effects the F-22 SES by
A.
B.
C.
D.
33.  The two configurations the F-22 pylons are built for are
A.
B.
C.
D.
34.  The mode on the F-22 that uses the pneumatic backup system to pressurize the unlock devices to release the landing gear for extending and locking it into position is
A.
B.
C.
D.
35.  The F-22 nose wheel may normally be turned up to 48 depending on
A.
B.
C.
D.
36.  On the F-22, how many pumps are attached to the AMAD?
A.
B.
C.
D.
37.  The external canopy control switch on the F-22 is located
A.
B.
C.
D.
38.  Access to the required technical data is provided when the user selects the
A.
B.
C.
D.
39.  Normal start and normal operating state are the two sytem operations of the
A.
B.
C.
D.
40.  The purpose of the SAS is to outline the repair and restoration process, reliability, and maintainability data collection, and time accounting for the managing the F-22's.
A.
B.
C.
D.
41.  The system designed to be used in amintenance units, maintenance operation centers, and off equipment maintenance ship is
A.
B.
C.
D.
42.  The F-22 pitch system is augmented by
A.
B.
C.
D.
43.  The F-22 support equipment that is built from predominantly commercial off the self items
A.
B.
C.
D.
44.  The F-22's primary source of power for the full authority digital electric control, the comprehensive diagnostic unit, and the ignition exciters is the
A.
B.
C.
D.
45.  The F-22 leading edge flap position is based on AOA, Mach and altitude information computed by the
A.
B.
C.
D.
46.  The primary integrated maintenance information tool used by F-22 technicians during the performance of maintenance task is the
A.
B.
C.
D.
47.  How many minutes is the F-22 ejection seat emergency oxygen bottle capable of providing the pilot with oxygen for?
A.
B.
C.
D.
48.  The two ways maintainers can start the F-22 APU are the
A.
B.
C.
D.
49.  On the F-22, what performs the BIT on the hydraulic components?
A.
B.
C.
D.
50.  When F-22 hydraulic pressure is lost the ailerons are
A.
B.
C.
D.
51.  The F-22 inspection that is accomplished within six hours of launch and only if the preflight is over 48 hours but still valid is the
A.
B.
C.
D.
52.  On the F-22, what components take care of the on-board engine monitoring diagnostic functions?
A.
B.
C.
D.
53.  On the F-22, what is the output pressure for the hydraulic system's pump?
A.
B.
C.
D.
54.  The three methods for opening the F-22 canopy are
A.
B.
C.
D.
55.  The primary flight control surfaces, engine inlet bypass louvers, nose wheel steering, engine thrust and thrust vectoring all receive commands generated by the
A.
B.
C.
D.
56.  F-22 lift augmentation is performed by
A.
B.
C.
D.
57.  On the F-22, what prevents the maintainer from installing the filter bowl without a filter element inside?
A.
B.
C.
D.
58.  All PMS screens are provided guaranteed communication through the
A.
B.
C.
D.
59.  The F-22 engine monitoring system uses how many temperature sensors?
A.
B.
C.
D.
60.  On the F-22, a base plate and two interchangeable brake modules make up what valve?
A.
B.
C.
D.
61.  ON the F-22, which valve allows aerioal refuel flow to the aircraft plumbing and prevents flow in the reverse direction?
A.
B.
C.
D.
62.  The F-22 generator control units receive their power from the
A.
B.
C.
D.
63.  The F-22 program that deals with the computer software configuration for the respective aircraft system is
A.
B.
C.
D.
64.  When using the PMA to start the APU, the maintainer needs to verify the SES air pressure protective covers are removed and the
A.
B.
C.
D.
65.  The two major components that must be installed on the PMS for the F-22 are the battery pack and
A.
B.
C.
D.
66.  Outer mold line inspection will be accomplished on the F-22 when maintenance notices
A.
B.
C.
D.
67.  In the F-22 nose wheel steering system, what valve allows free castering of the nose wheel?
A.
B.
C.
D.
68.  The  F-22 system component that provides all electrical interconnects between the vehicle management system modules and the aircraft wiring connectors is the
A.
B.
C.
D.
69.  The stored energy system servicing carts surfaces remain hot after shutdown for up to how many minutes?
A.
B.
C.
D.
70.  The F-22 diagnostics are controlled by the
A.
B.
C.
D.
71.  The fan and compressor vaiable vanes, as well as the modulated exhaust cooling and exhaust nozzle make up the F-22's engine
A.
B.
C.
D.
72.  IMIS displays input screens to enable the maintainer to enter suspected
A.
B.
C.
D.
73.  The SES on the F-22 uses aircraft fuel and high pressure air to power the
A.
B.
C.
D.
74.  The interface between the electrical power system generators and the electrical power subsystem on the F-22 is the
A.
B.
C.
D.
75.  On the F-22, what in the lubrication system pressurizes the AMAD to 5 psi above ambient pressure?
A.
B.
C.
D.
76.  The F-22 is provided pneumatic, hydraulic, and electrical power during emergencies and within operating envelope by the
A.
B.
C.
D.
77.  The system the F-22 uses for avionics cooling during ground maintenance is
A.
B.
C.
D.
78.  The three-position, momentary action, center off switch on the F-22 flight control system panel is for the
A.
B.
C.
D.
79.  The F-22 component that communicates with the MSC and PMA to provide a single source of information to meet the requirements of maintenance personnel is the
A.
B.
C.
D.
80.  Vibrations, oil debris, oil level signals, along with condition monitoring and fault information, are stored in the F-22's resident memory of the
A.
B.
C.
D.
81.  The presence of a fire in the F-22 engine or APU compartment is reported to the fire protection module by the
A.
B.
C.
D.
82.  The oil level on the F-22's PDU is checked by a
A.
B.
C.
D.
83.  During ground shutdown the APY on the F-22 enters a cool-down cycle of
A.
B.
C.
D.
84.  The F-22 cockpit distribution and defog system provides air for the canopy seal, cockpit pressurization , canopy defog and the
A.
B.
C.
D.
85.  The main generator control units on the F-22 are cooled by what kind of air?
A.
B.
C.
D.
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