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96 Cards in this Set
- Front
- Back
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Towing preparations |
Minimum structural access door must be installed and radome closed/secure hydraulic brake pressure 2900 PSI doors 68L/R closed/removed |
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Corrosion control manual |
Navair 01-1A-509 |
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Wheel brake types |
Normal Break Emergency brake Parking brake |
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Purpose of composite materials |
Limit weight, increase strength, detect effect of corrosion attack |
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3 types of repairs |
Temporary Repair simple, restores capabilities allowing aircraft to be flown until perminent repair One time flight repair Restart your limited capabilities so aircraft can fly to repair station Perminent repair Meets or exceeds strength of original structure |
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What does the hydraulic system contain |
Accumulators, reservoir, pump, lines, valves |
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Launch bar |
Steering aircraft, located on forward side of nose landing gear shock strut |
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Arresting hook |
Underside of aft fuselage Used to stop aircraft on Carrier or when normal runways aren't available |
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Flight control surfaces |
Ailerons Leading edge flaps Trailing edge flaps Stabilizers Rudders Speed brake Lex spoiler |
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Intake safety |
9' radius and 25' radius at mil or Max |
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Exhaust safety |
A 115' idol 925' Max |
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Type of engine |
F-414-ge-400 |
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Auxiliary power unit 3 modes |
Ground maintenance mode Main engine start Environmental control systems |
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IFR probe |
In flight refueling Right forward fuselage |
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Wing tanks |
Foam Self seal holes/damage |
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Anti-ice |
Prevents build-up of ice On hardware |
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Fuel systems |
4 internal tanks, 2 internal wing tanks and up to 5 external takes |
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VEN |
Variable exhaust nozzle |
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FADEC |
Full authority digital engine control Receives information to operate engine in all areas |
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Hot refuel |
Fuel absorbs heat from liquid cooling systems, the amad oil in heat exchanges which keeps system cool |
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Barometric altimetre |
Pitot static pressure Above sea level |
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Radar altimetre |
Radio echoes above ground level |
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Azimuth |
Angular position in horizontal plane measured clockwise True North |
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Bearing |
Angular position from reference point |
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Range |
Distance between object versus observer |
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Heading |
Orian the in of aircraft's longitudinal axis |
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True Heading |
Direction measured by True North |
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Magnetic heading |
Direction of Earth's magnetic field as reference |
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Relative heading |
Direction facing in relation to 360ﾟ |
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VHF/UHF |
Very high/untra high frequency Purpose to communicate with aircraft and ground stations |
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IAS |
Intercommunication audio system Signal between cockpit, rear cockpit and ground crewman |
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TACAN |
Tactical air navigation Determines relative bearing and slant range |
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INS |
Internal navigation systrm Self contained and fully automatic dead reckoning navigation system |
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Gps |
Global positioning system Recieves referance info from sattelite |
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ARI |
Attitude reference indicator Self contained reference system with electronically driven gyro 3 mins after total loss of power |
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ILS |
Instrument landing system All weather guidance system provides steering info |
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Radar |
Radio detection and ranging Air to air and air to ground Modes for target detection, targeting and navigation |
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Fiber optics |
Improved performance and security but fragile and not easily repaired |
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MIDS/JTRS |
Multifunctional information distribution system/ joint tactical radio system Intelligence system that provides voice/communication link for real time info |
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TEWS |
Tactical electronic warfare system Improve survivability, enhance awareness and use of resources |
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Solid state recorder |
Records video and stores pictures from the mids |
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MDG |
Multi purpose display group Heads up display Altitude Steering Navigation Weapons Video in pilots view |
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DDI |
Digital display indicators Night vision RDDI More displayed |
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UFCD |
Up front control display Entry and display aircraft data |
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MPCD |
Multi function display |
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Position lights |
Left red Right green Tail white |
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AOA approach lights |
On nose landing gear when it is down in the air |
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DFIRS |
Deployable flight incident recorder set Retrieve data and deploy data before crash |
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Pitot static system |
Measures temp and pitot static |
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Airspeed indicator |
Airspeed as pitot and static pressure |
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Vertical speed indicator |
Senses changes in air pressure and displays in form of climb or drive |
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Air data pressure transmitters |
Converts pneumatic static and pressure imputs into digital signals proportional to measurements |
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Angle of attack |
Shows approach angle |
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Automatic flight control systems |
Provides auto pilot Automatic throttle control |
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Mission computers |
Everything goes through them |
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AIM |
Air to air missile |
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AGM |
Air to ground missile |
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CATM |
Captive air training missile |
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HERO |
Hazards of electromagnetic radiation to ordinance |
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Bomb fins retarted |
Low level bombing Fins open to slow weapon so jet can move |
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Non retarded bombs |
High level bombing, fins closed |
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Yellow missile |
Highly explosive |
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Brown missile |
Rocket motor |
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Blue missile |
Inert/ training round |
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Gun fire control system |
Air to ground/ air to air/ air combat maneuver |
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Types of missiles |
Active, semi active, passive |
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Flares |
Against heat seeking missiles |
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Chaffs |
Into atmosphere to jam radar installations |
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Integrated countermeasure switch |
Switch between chaffs and flares |
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Type of gun |
M61A1 20 mm |
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AIM 7 |
Sparrow air to air |
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AIM 9 |
Sidewinder air to air |
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AIM 120 |
Advanced medium range air to air missile |
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Gun fire attack mode |
Computer pilot attack and manual attack |
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AGM 65 |
Maverick |
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AGm 84 |
Air to ground |
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AGM 84D |
Harpoon |
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AGM 84E |
Stand off land attack missile (slam) |
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AGM 84H |
Stand off land attack missile expanded responce (slam er) |
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AGM 88 |
High speed anti air radiation missile (harm) |
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Egress ECS |
Provides air supply, cabin pressurization and thermal control |
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Free fall weapons |
Cluster bomb units, fire bomb, aircraft land mines |
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Flight equip. |
Mask, regulator, life preserver, anti g suit |
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Ejection seat |
SJU-17, |
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Hypoxia |
Decrease in amount of oxygen |
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Anoxia |
Death due to lack of oxygen |
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Aviator breathing oxygen types |
Gaseous and liquid |
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Dbfss |
Dry bay fire supression system |
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Type of joint helmet |
A/a 24a-56 |
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HDU (PR) |
Helmet mounted display unit Allows symbols to project on visor |
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Fire detection system |
Monitors AMAD, APU and engine bays with 3 lines and one shot bay system |
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Anti g system |
Delivers air pressure to anti g suit |
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OBOGS |
On board oxygen generating system Regulates pressure and controls flow. Distribute oxygen to crew station |
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Canopy system |
Pyrotechnically operated emergency canopy removal |
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Before entering cock pit |
Safety pins installed, handle in safe position |
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12 Sub systems of ecs |
Bleed air control, bleed air leak detection, air cycle conditioning, cabin cooling/Dfog avionics cooling, cabin pressurization, anti gravity suit, OBOGS, anti-ice rain removal, radar liquid cooling, canopy seal, wave guide pressurization |
