A) AIM-54 Phoenix B) AIM-9 Sidewinder C) AIM-7 Sparrow D) AIM-120 AMRAAM
A) Ground controller B) Radar Intercept Officer (RIO) C) Pilot D) Weapons Systems Officer
A) Rolls-Royce Pegasus B) General Electric F101 C) Pratt & Whitney TF33 D) General Electric F110-GE-400
A) F-14A B) F-14B C) F-14D D) F-14A+
A) Link 16 Datalink B) LANTIRN Targeting Pod C) Digital Flight Control System (DFCS) D) TARPS-DI
A) F-14A-Plus B) F-14 Super Tomcat C) F-14A+ D) F-14C
A) 1998 B) 1992 C) 2003 D) 1984
A) LANTIRN B) ROVER C) T3 D) TARPS
A) Centerline station B) Left engine intake C) Under the nose D) Right wing glove pylon
A) TARPS-CD B) PTID C) LANTIRN 40K D) ROVER III
A) F-4 Phantom B) F-111B C) F/A-18 Hornet D) A-6 Intruder
A) Introduction of night vision B) Introduction of laser targeting C) Introduction of a digital camera D) Introduction of terrain following radar
A) GBU-38 JDAM B) AIM-7M C) AIM-9M D) AIM-54C
A) A custom three-pod configuration B) Only the targeting pod C) Both the navigation and targeting pods D) Only the navigation pod
A) Air defense operations B) Deep strike bombing C) Electronic warfare jamming D) Close air support
A) Mach 2.5 B) Mach 1.8 C) Mach 2.0 D) Mach 2.2
A) 20 mm M61 Vulcan B) 20 mm M39 C) 25 mm GAU-12 Equalizer D) 30 mm GAU-8 Avenger
A) Three B) Four C) Six D) Five
A) Delta B) Folding C) Variable-geometry D) Swept-back
A) Connolly B) Vought C) Rockwell D) Grumman
A) Seacat B) Hellcat C) Wildcat D) Bearcat
A) It was not a feline name B) It sounded too aggressive C) Sexual connotations D) It was already taken
A) December 1968 B) January 1969 C) July 1968 D) December 1970
A) F100 B) F401-PW-400 C) TF30 D) J79
A) 20,000 lb B) 18,000 lb C) 12,000 lb D) 16,000 lb
A) 6,000 hours B) 8,000 hours C) 5,000 hours D) 7,200 hours
A) 1975 B) 1970 C) 1972 D) 1973
A) 1990s B) 1980s C) 1970s D) 2000s
A) January 1969 B) April 1973 C) December 1970 D) April 1972
A) 110 nmi B) 80 nmi C) 100 nmi D) 150 nmi
A) Five B) Six C) Four D) Ten
A) 80% B) 75% C) 66% D) 100%
A) 21 December 1970 B) 21 December 1973 C) 21 December 1969 D) 1 January 1969
A) F-4 Phantom II B) F-16 Fighting Falcon C) F-15 Eagle D) F-111 Aardvark
A) Fleet Air Defense (FAD) B) Tactical Fighter Experimental (TFX) C) Naval Fighter Experimental (VFX) D) VFAX
A) Boeing F/A-18E/F Super Hornet B) McDonnell Douglas F-4 Phantom II C) Douglas F6D Missileer D) General Dynamics F-111B
A) Electronic warfare B) Aerial refueling C) Precision ground-attack missions D) Long-range interception
A) 22 September 2006 B) 22 September 2000 C) 21 December 1970 D) 1 January 2005
A) Boeing F/A-18E/F Super Hornet B) McDonnell Douglas F-4 Phantom II C) Douglas F6D Missileer D) General Dynamics F-111B
A) Vietnam B) Iraq C) Iran D) Soviet Union
A) It entered service in 1959 B) It was renamed to the F-14 C) It was used in the Vietnam War D) It was canceled
A) General Dynamics B) Shah Mohammad Reza Pahlavi C) Thomas F. Connolly D) Robert McNamara
A) Grumman B) Boeing C) Douglas D) McDonnell Douglas
A) FAD-1 B) TFX-2 C) VFX-1 D) Model 303
A) Excessive fuel consumption B) Difficulty going supersonic C) Too much maneuverability D) Failure to carrier landing
A) At least 160 B) 16 C) 100 D) 55
A) Single-seat B) Twin-engine C) Supersonic D) Twin-tail
A) VFMX B) NATF C) F/A-18E/F Super Hornet D) A-12 Avenger II
A) F/A-18 B) F-22 C) A-6 D) A-12
A) 1989 B) 1993 C) 1988 D) 1991
A) 2015 B) 1995 C) 2010 D) 2000
A) 18 B) 132 C) 37 D) 55
A) Dick Cheney B) Robert McNamara C) Caspar Weinberger D) Donald Rumsfeld
A) Engine thrust upgrade B) Radar range extension C) Stealth coating application D) AIM-120 AMRAAM capability
A) 1960s technology B) 1950s technology C) 1970s technology D) Outdated Cold War technology
A) 55 B) 100 C) 80 D) 132
A) Jobs program B) Expensive relic C) National security asset D) Technological failure
A) 1993 Bottom-Up Review B) 1991 Procurement Review C) 1995 Strategic Review D) 1989 Defense Review
A) General Dynamics B) Boeing C) Northrop Corporation D) Lockheed Corporation
A) Single-seat cockpit with a flat canopy B) Two-seat cockpit with a bubble canopy C) Tandem three-seat cockpit D) Side-by-side cockpit
A) Twin-tail empennage B) V-tail empennage C) T-tail empennage D) Single vertical stabilizer
A) In the center of the fuselage B) Under the nose C) On the left side D) On the right side
A) 40 to 60 percent B) 70 to 80 percent C) 5 to 10 percent D) 10 to 20 percent
A) To support heavy ground bombs B) To handle high-speed taxiing C) To withstand carrier catapult launches and recoveries D) To allow for off-road landings
A) Fuel, avionics, and weaponry B) Extra jet engines C) Folding wing motors only D) Crew sleeping quarters
A) In widely spaced nacelles B) Stacked vertically on top of each other C) Deep inside the main fuselage D) Within the wings
A) 75 degrees B) 55 degrees C) 80 degrees D) 68 degrees
A) Aluminum riveting B) Electron beam welding C) Laser cutting D) Cold forging
A) They lock in the neutral position B) They function as air brakes C) They are disabled D) They double their effectiveness
A) 17 degrees B) 10 degrees C) 35 degrees D) 7 degrees
A) 17 degrees B) 35 degrees C) 10 degrees D) 7 degrees
A) The tailhook B) The fuel dump valve C) The drag chute D) The auxiliary power unit exhaust
A) Pratt & Whitney F401 B) General Electric F110-GE-400 C) Pratt & Whitney F100 D) Pratt & Whitney TF30-P-412A
A) Pratt & Whitney F401 B) Pratt & Whitney TF30-P-414A C) General Electric F100 D) General Electric F110-GE-400
A) 10% B) 28% C) 15% D) 40%
A) Fuel leakage B) Overheating C) Compressor stalls D) Oil pressure loss
A) Immediate flameout B) Engine explosion C) Loss of all electrical power D) Unrecoverable flat spin
A) Excessive engine heat damage B) High fuel consumption C) Structural stress on the catapult D) Engine failure could cause uncorrectable yawing moments
A) Increased by 61% B) Increased by 100% C) Increased by 25% D) Decreased by 10%
A) The vibration damaged the engine bay B) Exhaust gases could cause compressor stalls C) The engine intake became blocked by debris D) The bleed air pressure dropped too low
A) 0.85 B) 0.56 C) 0.73 D) 0.95
A) Lockheed Martin E-1 B) Boeing ACES II C) Martin-Baker GRU-5B D) Martin-Baker GRU-7A
A) Northrop Grumman B) General Electric C) Garrett AiResearch D) Hughes Aircraft
A) Hughes AN/AWG-9 B) Westinghouse AN/APG-66 C) Northrop APG-71 D) Raytheon AN/APG-65
A) 36 B) 24 C) 6 D) 12
A) AN/APG-63 B) APG-71 C) AN/APG-73 D) AN/AWG-10
A) TV Set B) Tactical Control System C) Thermal Calibration System D) Target Capture Sensor
A) Gallium nitride semiconductors B) Bipolar junction transistor modules C) MOSFET-based large-scale integration D) Vacuum tube vacuum arrays
A) Cadmium telluride B) Silicon carbide C) Gallium arsenide D) Indium antimonide
A) Four B) Three C) Six D) Two
A) AN/AWG-11 B) AN/AAS-42 C) AAX-2 D) AN/ALR-67
A) 300 knots B) 600 knots C) 550 knots D) 450 knots
A) AN/ALR-23 B) AN/ALR-50 C) AN/ALR-67 D) AN/ALR-45
A) Japanese long-range bombers B) Chinese reconnaissance drones C) Soviet anti-ship cruise missiles D) German jet fighters
A) Ground-Cat B) Bombcat C) Attack-F14 D) Strike-Tom
A) Zero times B) Once C) Twice D) Five times
A) The pilot accidentally jettisoned the missiles B) The missiles hit the wrong targets C) The rocket motors did not ignite D) The missiles scored two kills
A) The pilot forgot to turn on the master arm B) The missiles were improperly armed C) Enemy jamming prevented a lock D) The radar malfunctioned
A) R-73 Archer B) R-27R Alamo C) R-60 Aphid D) R-77 Adder
A) Project Desert Shield B) Project Persian Tomcat C) Project Hawk Eye D) Project Sky Hawk |