2a352 H F-16 Avionics
URE QUIZ FOR FIRST SET OF 2A352 CDC'S
- 1.1. (001) On the F–16 aircraft, fuselage station zero (FS 0.0) is located
- A.
AT THE AFT END OF THE NOSE RADOME
- B.
AT THE FORWARD END OF THE NOSE RADOME
- C.
5.0 INCHES AFT OF THE FORWARD END OF THE NOSE RADOME
- D.
5.0 INCHES FORWARD OF THE FORWARD END OF THE NOSE RADOME
- 2.2. (001) On the F-16 aircraft, waterline 65.0 (WL 65.0) is ocated 65.0 inches in which direction from waterline 0.0?
- A.
AFT
- B.
ABOVE
- C.
BELOW
- D.
FORWARD
- 3.3. (001) When should worn door/panel fasteners be replaced?
- A.
IMMEDIATELY
- B.
BEFORE THE AIRCRAFT TAXIS
- C.
WHEN SHEET METAL SHOP SEES FIT
- D.
THE NEXT TIME YOU PERFORM MAINTENANCE UNDER THAT DOOR/PANEL
- 4.4. (001) Which of the following structures is not part of the empennage group?
- A.
WINGS
- B.
RUDDER
- C.
VENTRAL FINS
- D.
HORIZONTAL STABILIZERS
- 5.5. (001) The leading edge flaps for the F-16 are located on the
- A.
WING ASSEMBLY
- B.
EMPENNAGE GROUP
- C.
FUSELAGE ASSEMBLY
- D.
HORIZONTAL STABILIZERS
- 6.6. (002) On the F-16 installing the emergency power unit (EPU) safety pin will
- A.
Not prevent the firing of the EPU in flight
- B.
Prevent the accidental firing of the EPU only in flight
- C.
Not prevent the firing of the EPUif the external source shuts down
- D.
Prevent the accidental firing of the EPU during ground maintenance
- 7.7. (002) To operate the aircraft primary flight controls, the F–16 hydraulic systems provide hydraulic pressure at approximately
- A.
1,100 psi
- B.
2,100 psi
- C.
3,100 psi
- D.
4,100 psi
- 8.8. (002) At aircraft altitudes between 8,000 feet and 23,000 feet, the F–16 cabin pressure is regulated to
- A.
The 8,000 foot air pressure
- B.
The 23,000 foot air pressure
- C.
Ambient (outside) air pressure
- D.
5 psi above ambient (outside) air pressure
- 9.9. (002) The digital flight control system uses what means to transfer inputs to the control surfaces?
- A.
Control cables
- B.
Full fly-by-wire
- C.
Mechanical linkage
- D.
A combination of control cables and electrical wire
- 10.10. (002) Artificial feel in the digital flight control system is provided by beams and coil springs
- A.
Internal to the handgrip assembly
- B.
Internal to the transducer assembly
- C.
External to the handgrip assembly
- D.
External to the transducer assembly
- 11.11. (002) In addition to rudder control, the rudder pedals are also used to generate
- A.
Brake command signals only
- B.
Nosewheel steering signals only
- C.
Brake command and nosewheel steering signals
- D.
Anti-skid command and nosewheel steering signals
Questions: 25 | Attempts: 2675 | Last updated: Mar 22, 2022
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Questions: 15 | Attempts: 1800 | Last updated: Mar 22, 2022
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Sample QuestionVOR generates two signals on the carrier frequency?
Questions: 10 | Attempts: 1320 | Last updated: Mar 22, 2022
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Sample QuestionThe ADF requires two seperate antenna?
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