2A374
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- 1.Which section of the A–10 aircraft extends from approximately 2 feet aft of the canopy to approximately 18 inches aft of the trailing edge of the wings?
- A.
Empennage
- B.
Fuselage aft section
- C.
Fuselage center section
- D.
Fuselage forward section
- 2.Which section of the A–10 aircraft consists of a horizontal and two vertical stabilizers?
- A.
Empennage
- B.
Fuselage aft section
- C.
Fuselage center section
- D.
Fuselage forward section
- 3.What hazard is present for personnel standing in the area of an A–10 aircraft if a canopy is jettisoned on the ground?
- A.
Burning
- B.
Crushing
- C.
Shocking
- D.
Explosion
- 4.What defensive store from the A–10 aircraft may lodge in your skin or eyes and cause permanent damage when deployed?
- A.
Chaff
- B.
Flare
- C.
Fuels
- D.
Liquid oxygen
- 5.Which hazardous liquid has a hazard of extreme cold temperature when exposed to air?
- A.
Oils
- B.
Fuels
- C.
Hydraulic fluid
- D.
Liquid oxygen
- 6.Which major aircraft system is responsible for cockpit pressurization and crewmember anti-g suit pressurization?
- A.
Electrical (24)
- B.
Flight control (27)
- C.
Environmental control (21)
- D.
Pneudraulics/hydraulics (29)
- 7.Which major aircraft system does the master caution system fall under?
- A.
Electrical (24)
- B.
Flight control (27)
- C.
Environmental control (21)
- D.
Pneudraulics/hydraulics (29)
- 8.The data transfer system (DTS) is part of which major aircraft system?
- A.
Electrical (24)
- B.
Navigation (34)
- C.
Communication (23)
- D.
Electronic warfare (93)
- 9.Under which major aircraft system does the Sniper XR targeting pod fall?
- A.
Electrical (24)
- B.
Navigation (34)
- C.
Communication (23)
- D.
Electronic Warfare (93)
- 10.On the A–10 data transfer system, weapons events and ground collision avoidance system (GCAS) events are recorded by the
- A.
Control display unit (CDU)
- B.
Flight director computer (FDC)
- C.
Integrated flight and fire control computer (IFFCC)
- D.
Embedded global positioning/inertial navigation system (EGI)
- 11.Where is the A–10 master bus controller (MBC) located?
- A.
Control display unit (CDU)
- B.
Flight director computer (FDC)
- C.
Integrated flight and fire control computer (IFFCC)
- D.
Embedded global positioning/inertial navigation system (EGI)
- 12.What assumes control of the A–10 digital data bus if the master bus controller (MBC) fails?
- A.
Control display unit (CDU)
- B.
Flight director computer (FDC)
- C.
Integrated flight and fire control computer (IFFCC)
- D.
Embedded global positioning/inertial navigation system (EGI)
- 13.Which A–10 line replaceable unit (LRU) is primarily a weapons system processor?
- A.
Head-up display (HUD)
- B.
Central interface control unit (CICU)
- C.
Armament HUD control panel (AHCP)
- D.
Integrated flight and fire control computer (IFFCC)
- 14.How many output video interfaces does the A–10 central interface control unit (CICU) provide to drive high resolution multifunction color displays (MFCD)?
- A.
1
- B.
2
- C.
3
- D.
4
- 15.Which A–10 central interface control unit (CICU) built-in test must be performed while the aircraft is on the ground?
- A.
Initiated
- B.
Periodic
- C.
Power-on
- D.
Continuous
- 16.What does the A–10 central interface control unit (CICU) provide to allow the targeting pod to operate properly?
- A.
Location and speed
- B.
Altitude and airspeed
- C.
Current date and time
- D.
Azimuth and elevation signals
- 17.Which A–10 low altitude safety and targeting enhancement (LASTE) component’s function is to turn on the radar altimeter, arm the enhanced attitude control (EAC) function, and control the low altitude autopilot (LAAP)?
- A.
LASTE control panel
- B.
Up-front controller (UFC)
- C.
Armament HUD control panel (AHCP)
- D.
Stability augmentation system (SAS) control panel
- 18.What A–10 low altitude safety and targeting enhancement (LASTE) related component senses aircraft pitch, yaw, and roll rates?
- A.
LASTE control panel
- B.
Avionics auxiliary panel
- C.
Stability augmentation system (SAS) control panel
- D.
Armament head-up display (HUD) control panel (AHCP)
- 19.What A–10 low altitude safety and targeting enhancement (LASTE) related component contains the integrated flight and fire control computer (IFFCC) ON/OFF switch?
- A.
LASTE control panel
- B.
Up-front controller (UFC)
- C.
Stability augmentation system (SAS) control panel
- D.
Armament head-up display (HUD) control panel (AHCP)
- 20.Which A–10 low altitude safety and targeting enhancement (LASTE) related component contains the WEAPONS RELEASE button, NOSE WHEEL STEERING button, and MASTER MODE CONTROL button?
- A.
Stick grip
- B.
Left throttle grip
- C.
Right throttle grip
- D.
Armament head-up display (HUD) control panel (AHCP)
- 21.What navigation (NAV) operating mode does the A–10 head-up display low altitude safety and targeting enhancement (HUD LASTE) system default to as its backup?
- A.
Embedded global positioning and inertial navigation system (EGI) mode
- B.
Heading attitude reference system (HARS) mode
- C.
Integrated flight and fire control computer (IFFCC) mode
- D.
Normal mode
- 22.Which condition must be met in order for the A–10 enhanced attitude control (EAC) to arm?
- A.
Radar altitude must be on and operational
- B.
Low altitude autopilot (LAAP) must be engaged with no failures
- C.
Pitch and yaw stability augmentation system (SAS) must be engaged with no SAS failures
- D.
Heading attitude reference system (HARS) must be selected on the NAV mode select panel and its data valid
- 23.During the A–10 low altitude safety targeting enhancement (LASTE) precision attitude control (PAC)–2 engagement, LASTE is able to stabilize the aircraft for up to
- A.
4 seconds
- B.
5 seconds
- C.
6 seconds
- D.
7 seconds
- 24.The A–10 cockpit color television video sensor (CCTVS) records a video of the
- A.
Control display unit (CDU)
- B.
Television (TV) monitor
- C.
Right and left multifunction color display (MFCD)
- D.
View through the head-up display (HUD)
- 25.What is the recording time of the A–10 removable mass memory device?
- A.
1.5 hours
- B.
2.5 hours
- C.
3.5 hours
- D.
4.5 hours
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