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47 Cards in this Set
- Front
- Back
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HOW MANY GROUND SAFETY PINS ARE THERE?
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8 IN FWD COCKPIT, 7 IN AFT COKPIT
ONE IN EACH COCKPIT FOR CANOPY EJECTION 3 LNDG GR-1 NWW AND 1 EACH MN MOUNT 5 PYLON PINS 1 PIN IN TAIL HOOK |
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WHERE ARE AIRCRAFT GROUNDING POINTS
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1- TAIL BUMPER STATIC GROUND POINT
2- NWW STATIC GROUNDING POINT |
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GENERAL SAFETY PRECAUTIONS FOR APPLYING AND REMOVING PWR
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1-CHECK SWITCHES
2- GROUND PWR SUPPLY SOURCE AND AIRCRAFT 3- INFORM ALL PERSONNEL ON OR AROUND AIRCRAT OF APLLICATION OF PWR |
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STATE THE # OF TIE DOWN POINTS
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10
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WHERE ARE THE TIE DOWN POINTS LOCATED
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1-NOSE GEAR DRAG BRACE
2- TAIL SCAG 3- FWD LT OUTBOARD PYLON 4-AFT LT OUTBOARD PYLON 5-FWD RT OUTBOARD PYLON 6- AFT RT OUTBOARD PYLON 7- LT MAIN GEAR 8-RT MAIN GEAR 9- LEFT MAIN GEAR WHEEL AXLE 10- RT MAIN GEAR WHEEL AXLE |
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PROPER PRCEDURE FOR AIRCRAFT GROUNDING
CONNECT THE GROUNDING STRAP TO_____ AND THEN TO THE ______ |
DECK THEN TO THE AIRCRAFT
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WHO ASSEMBLES AND BRIEFS THE TEAM BEFORE AND AIRCRAFT MOVE?
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MOVE DIRECTOR
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WHO PULLS INSTALLS AND CARRIES CHOCKS DURING AN AIRCRAFT MOVE
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CHOCK WALKER
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WHO CONDUCTS A PREMOVEMENT INSPECTION TO ENSURE ALL CABLES ARE REMOVED FROM THE AIRCRAFT BEFORE AND AIRCRAFT MOVE.
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BRAKE RIDER
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IF THERE IS NOT A QULIFIED BRAKE RIDER, DURING AN AIRCRAFT MOVE, WHOSE RESPONSIBILITY IS IT TO ENSURE THEY GET ONE
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MOVE DIRECTOR
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THSI INDIVIDUAL IS RESPONSIBLE TO THE MOVE DIRECTOR, AND FOR THE SLOW AND SAFE MOVEMENT OF THE AIRCRAFT, FROM HOOK UP TO FINAL PARKING SPOT.
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TRACTOR DRIVER
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WHAT IS HYDRAULIC PATCH TESTING
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THE PRIMARY CONTAMINATION METHOD USED AT ALL LEVELS OF MAINTENACE
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TACTICAL PAINT SCHEMES ARE USE FOR
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DECEPTION, AND REDUCTION OF DETECTION RANGE, OR TO CONFUSE AND MISLEAD OBSERVERS
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PURPOSE OF THE 01-1A-509
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PROVIDE INFORMATION ON PREVENTION AND REPAIR OF CORROSION DAMAGE TO EQUIPMENT ON LAND AND SEA
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WHAT IS THE PURPOSE OF THE NOSE WHEEL STEERING ACTUATING SWITCH
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ACTIVATES NOSE WHEEL STEERING WITH WEIGHT ON WHEELS.
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WHERE IS THE NOSE WHEEL STEERING SWITCH LOCATED
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PILOTS HANDGRIP OF THE CONTROL STICK
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USED PRIMARILY TO AID THE PILOT IN RECOVERING FROM A SPIN. _________ PROVIDES....
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PROVIDES AN ALTERNATE METHOD OF INCREASING STABILIZER AND RUDDER (CONTROL SURFACE) THROWS DURING A CLEAN FLT CONFIGURATION.
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TYPE AND MODEL OF ENGINES USED ON EA-6B AIRCRAFT
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J52-P-408/408A
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SIX BASIC SECTIONS OF THE EA-6B ENGINE ARE
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1- INLET SECTION
2- COMPRESSOR SECTION 3- DIFFUSER SECTION 4- COMBUSTION SECTION 5- TURBINE EXHAUST SECTION 6- ACCESORY SECTION |
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WHAT ARE THE TWO METHODS OF STARTING THE ENGINE
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1- BY USING THE EXTERNAL AIR FROM A STARTER OR CART HUFFER
2- TAPING BLEED AIR FROM OPERATIONG ENGINE (CROSS-BLEEDING) RESTARTS |
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IFF IS
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IDENTIFICATION FRIEND OR FOE
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INS IS
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INERTIAL NAVIGATION SYSTEM
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RADAR IS
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RADIO DETECTION AND RANGING
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TACAN IS
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TACTICAL AIR NAVIGATION
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ESM STANDS FOR
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ELECTRONIC SURVEILLANCE MISSION
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ACLS IS
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AUTOMATED CARRIER LANDING SYSTEM
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APC IS
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APPROACH POWER COMPNSATOR
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AFCS STANDS FOR
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AUTMATIC FLIGHT CONTROL SYSTEM
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EFIS STANDS FOR
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ELECTRONIC FLIGHT INSTRUMENTATION SYSTEM
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OAT STANDS FOR
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OUTSIDE AIR TEMPERATURE
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WHAT IS THE PURPOSE OF ECM
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DECIEVE AND JAM ENEMY RADAR
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WHAT ARE THE TWO BASIC CATEGORIES OF AIRBORNE ECM
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1- NON ELECTRIC
CHAFF 2- ELECTRIC USED FOR JAMMING |
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WHAT IS THE PRIMARY ELECTRIC SOURCE FOR THE AN/ALQ-99
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self contained ram air turbine/ generator
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the rat provides ... ___v, ___hz __ phase pwr
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115 v, 400 hz ac 3 phase power
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WHAT IS THE DIFFERENCE BETWEEN AC AND DC CURRENT
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AC IS ALTERANTING CURRENT CHANGES CONSTANTLY REVERSING DIRECTION AND AMPLITUDE AT REGULAR INTERVALS
DC FLOWS IN ONE DIRECTION NUMBER OF ELECTRONS FLOWING PAST A POINT INT HE CIRCUIT IN ONE SECOND DETERMINES AMPLITUDE |
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WHAT IS A RADAR ALTIMETER
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A RANGE TRACKING RADAR THAT MEASURES THE SURFACE OR TERRAIN CLEARANCE BELOW THE AIRCRAFT
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WHAT IS A BAROMETRIC ALTIMETER
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IT WORKS AS A PRESSURE ALTIMETER COMBINED WITH AN AC POWERED SERVO MECHANISM TO GIVE AN ALTITUDE READ OUT IN HUNDREDS OF FEET BY THE OUTSIDE AIR PRESSURE OR DENSITY
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WHAT ARE THE MIN REQUIREMENTS FOR AIRCREW PPE?
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1- PROTECTIVE HELMET
2- AIRCREW SAFETY FLYER BOOTS 3- FIRE RESISTANT FLT SUIT 4- FIRE RESISTANT GLOVES 5- LASER PRETECTING EYEWEAR 6- FLASH LIGHT 7- KNIFE AND SHEATH 8- LIFE PRESERVER 9- IDENTIFICATION TAGS 10- ANTI EXPOSURE SUIT 11- ANTI BLACKOUT-G- SUIT 12- HELICOPTER EMERGENCY EGRESS DEVICE 13- PERSONAL SURVIVAL KIT 14- SIGNAL DEVICE 15- SURVIVAL RADIO AND BEACON |
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WHAT IS THE PURPOSE OF A OXYGEN MASK
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DESIGNED FOR USE IN AN AIRCRAFT WHERE THE MASK IS REQUIRED AT ALL TIMES
AUDIO AMPLIFIER IS REQUIRED FOR COMMINUCATION CAPABILITY |
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WHAT IS THE PURPOSE OF AN OXYGEN REGULATOR
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DESIGNED TO REGULATE 100% OXYGEN TO THE AIRCREW DURING FLIGHT
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WHAT IS THE PURPOSE OF A LIFE PRESERVER
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DESIGNED FOR USE IN AN EJECTION SEAT EQUIPPED AIRCRAFT AND PROVIDES A MIN OF 65 POUNDS BOUYANCY
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WHAT IS THE PURPOSE OF A ANTI G SUIT
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DESIGNED TO PROVIDE PROTECTION FOR THE AIRCREWMAN AGAINST THE EFFECTS OF THE HIGH G FORCES EXPERIENCED IN HIGH PERFORMANCE AIRCRAFT
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PURPOSE OF A DROGUE PARACHUTE IS
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TO STABILIZE AND DECELERATE THE SEAT TO POSITION THE SEAT IN PROPER ATTITUDE FOR AIRCREW SEPERATION
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PURPOSE OF A MIAN PARACHUTE IS
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PULLS OCCUPANT, SURVIVAL KIT AND LOWER RESTRAINT HARNESS FREE OF STICKER CLIPS ALLOWING SEAT TO FALL FREE AND OCCUPANT TO CONTINUE NORMAL PARACHUTE DESCENT
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WHAT ARE THE ITEMS CONTAINED IN A SEAT SURVIVAL KIT
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1 NYLON CORD
2 SEA DYE MARKER 3 SRU-31/P SURVIVAL KIT #1 4 CANNED DRINKING WATER 5 COMBAT CASUALTY BLANKET 6 EMERGENCY CODE CARD 7 RADIO BEACON SET 8 SIGNAL AND SMOKE FLARES 9 BAILING SPONGE 10 SRU-13/P SURVIVAL KIT #2 11 EMERGENCY DRINKING WATER 12 CAN OPENER 13 PACKING LIST 14 INFLATABLE LIFE RAFT |
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PURPOSE OF ENGINE FUEL SYSTEM
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MAINTAINS ENOUGH FUEL BY WEIGHT TO MEET ENGINE DEMANDS
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PURPOSE AND LOCATION OF ENGINE INFLIGHT FUELING PROBE
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FLIGHT REFUELING
CENTERLINE-FWD WIND SCREEN |
