1.
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. 
Quick turnaround inspection
C. 
D. 
2.
Outer mold line inspection will be accomplished on the F-22 when maintenance notices
A. 
B. 
Worn nose landing gear tire
C. 
D. 
3.
On the F-22, the responsibility for all low observable maintenance rests with the
A. 
B. 
C. 
Aircraft structural maintenance
D. 
4.
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. 
Upgrade of the portable maintenance aid
C. 
D. 
Repair and reclamation cycles
5.
On the F-22, what is the output pressure for the hydraulic system's pump?
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.
On the F-22, what prevents the maintainer from installing the filter bowl without a filter element inside?
A. 
B. 
C. 
D. 
8.
On the F-22 hydraulic control software monitors, the hydraulic system is hosted by the
A. 
B. 
C. 
D. 
9.
On the F-22, what performs the BIT on the hydraulic components?
A. 
B. 
C. 
Fault component indicator
D. 
10.
On the F-22, the pressure transducer operates over a pressure range of
A. 
B. 
C. 
D. 
11.
On the F-22, what provides the maintainer an indication that the filter element requires replacement?
A. 
B. 
C. 
D. 
Differential pressure indicator
12.
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. 
13.
On the F-22, a base plate and two interchangeable brake modules make up what valve?
A. 
B. 
C. 
D. 
14.
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. 
15.
The F-22 nose wheel may normally be turned up to 48 depending on
A. 
Main landing gear wheel speed
B. 
C. 
Deceleration of the aircraft
D. 
16.
In the F-22 nose wheel steering system, what valve allows free castering of the nose wheel?
A. 
B. 
C. 
D. 
17.
The F-22 arresting gear system is pneumatically actuated and controlled
A. 
B. 
C. 
D. 
18.
The F-22's engine fan variable vanes position is controlled by
A. 
B. 
C. 
D. 
19.
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. 
20.
The F-22's engine lube system contains oil in the bearing compartment by using
A. 
B. 
Engine supplied compressor air
C. 
APU supplied compressor air
D. 
21.
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. 
22.
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. 
Turbine engine monitoring
B. 
Integrated management information system
C. 
Advanced engine failure resolution
D. 
Engine data collection unit
23.
IMIS displays input screens to enable the maintainer to enter suspected
A. 
Airframe management codes
B. 
Turbine engine management codes
C. 
Fault identification codes
D. 
24.
The presence of an overheat on the F-22 is reported for display in the cockpit by the
A. 
B. 
Integrated vehicle subsystem controller
C. 
D. 
Fire detection and warning system
25.
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
B. 
C. 
D.