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47 Cards in this Set

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  • Back
HOW MANY GROUND SAFETY PINS ARE THERE?
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
WHERE ARE AIRCRAFT GROUNDING POINTS
1- TAIL BUMPER STATIC GROUND POINT
2- NWW STATIC GROUNDING POINT
GENERAL SAFETY PRECAUTIONS FOR APPLYING AND REMOVING PWR
1-CHECK SWITCHES
2- GROUND PWR SUPPLY SOURCE AND AIRCRAFT
3- INFORM ALL PERSONNEL ON OR AROUND AIRCRAT OF APLLICATION OF PWR
STATE THE # OF TIE DOWN POINTS
10
WHERE ARE THE TIE DOWN POINTS LOCATED
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
PROPER PRCEDURE FOR AIRCRAFT GROUNDING

CONNECT THE GROUNDING STRAP TO_____ AND THEN TO THE ______
DECK THEN TO THE AIRCRAFT
WHO ASSEMBLES AND BRIEFS THE TEAM BEFORE AND AIRCRAFT MOVE?
MOVE DIRECTOR
WHO PULLS INSTALLS AND CARRIES CHOCKS DURING AN AIRCRAFT MOVE
CHOCK WALKER
WHO CONDUCTS A PREMOVEMENT INSPECTION TO ENSURE ALL CABLES ARE REMOVED FROM THE AIRCRAFT BEFORE AND AIRCRAFT MOVE.
BRAKE RIDER
IF THERE IS NOT A QULIFIED BRAKE RIDER, DURING AN AIRCRAFT MOVE, WHOSE RESPONSIBILITY IS IT TO ENSURE THEY GET ONE
MOVE DIRECTOR
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.
TRACTOR DRIVER
WHAT IS HYDRAULIC PATCH TESTING
THE PRIMARY CONTAMINATION METHOD USED AT ALL LEVELS OF MAINTENACE
TACTICAL PAINT SCHEMES ARE USE FOR
DECEPTION, AND REDUCTION OF DETECTION RANGE, OR TO CONFUSE AND MISLEAD OBSERVERS
PURPOSE OF THE 01-1A-509
PROVIDE INFORMATION ON PREVENTION AND REPAIR OF CORROSION DAMAGE TO EQUIPMENT ON LAND AND SEA
WHAT IS THE PURPOSE OF THE NOSE WHEEL STEERING ACTUATING SWITCH
ACTIVATES NOSE WHEEL STEERING WITH WEIGHT ON WHEELS.
WHERE IS THE NOSE WHEEL STEERING SWITCH LOCATED
PILOTS HANDGRIP OF THE CONTROL STICK
USED PRIMARILY TO AID THE PILOT IN RECOVERING FROM A SPIN. _________ PROVIDES....
PROVIDES AN ALTERNATE METHOD OF INCREASING STABILIZER AND RUDDER (CONTROL SURFACE) THROWS DURING A CLEAN FLT CONFIGURATION.
TYPE AND MODEL OF ENGINES USED ON EA-6B AIRCRAFT
J52-P-408/408A
SIX BASIC SECTIONS OF THE EA-6B ENGINE ARE
1- INLET SECTION
2- COMPRESSOR SECTION
3- DIFFUSER SECTION
4- COMBUSTION SECTION
5- TURBINE EXHAUST SECTION
6- ACCESORY SECTION
WHAT ARE THE TWO METHODS OF STARTING THE ENGINE
1- BY USING THE EXTERNAL AIR FROM A STARTER OR CART HUFFER
2- TAPING BLEED AIR FROM OPERATIONG ENGINE (CROSS-BLEEDING) RESTARTS
IFF IS
IDENTIFICATION FRIEND OR FOE
INS IS
INERTIAL NAVIGATION SYSTEM
RADAR IS
RADIO DETECTION AND RANGING
TACAN IS
TACTICAL AIR NAVIGATION
ESM STANDS FOR
ELECTRONIC SURVEILLANCE MISSION
ACLS IS
AUTOMATED CARRIER LANDING SYSTEM
APC IS
APPROACH POWER COMPNSATOR
AFCS STANDS FOR
AUTMATIC FLIGHT CONTROL SYSTEM
EFIS STANDS FOR
ELECTRONIC FLIGHT INSTRUMENTATION SYSTEM
OAT STANDS FOR
OUTSIDE AIR TEMPERATURE
WHAT IS THE PURPOSE OF ECM
DECIEVE AND JAM ENEMY RADAR
WHAT ARE THE TWO BASIC CATEGORIES OF AIRBORNE ECM
1- NON ELECTRIC
CHAFF
2- ELECTRIC
USED FOR JAMMING
WHAT IS THE PRIMARY ELECTRIC SOURCE FOR THE AN/ALQ-99
self contained ram air turbine/ generator
the rat provides ... ___v, ___hz __ phase pwr
115 v, 400 hz ac 3 phase power
WHAT IS THE DIFFERENCE BETWEEN AC AND DC CURRENT
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
WHAT IS A RADAR ALTIMETER
A RANGE TRACKING RADAR THAT MEASURES THE SURFACE OR TERRAIN CLEARANCE BELOW THE AIRCRAFT
WHAT IS A BAROMETRIC ALTIMETER
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
WHAT ARE THE MIN REQUIREMENTS FOR AIRCREW PPE?
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
WHAT IS THE PURPOSE OF A OXYGEN MASK
DESIGNED FOR USE IN AN AIRCRAFT WHERE THE MASK IS REQUIRED AT ALL TIMES
AUDIO AMPLIFIER IS REQUIRED FOR COMMINUCATION CAPABILITY
WHAT IS THE PURPOSE OF AN OXYGEN REGULATOR
DESIGNED TO REGULATE 100% OXYGEN TO THE AIRCREW DURING FLIGHT
WHAT IS THE PURPOSE OF A LIFE PRESERVER
DESIGNED FOR USE IN AN EJECTION SEAT EQUIPPED AIRCRAFT AND PROVIDES A MIN OF 65 POUNDS BOUYANCY
WHAT IS THE PURPOSE OF A ANTI G SUIT
DESIGNED TO PROVIDE PROTECTION FOR THE AIRCREWMAN AGAINST THE EFFECTS OF THE HIGH G FORCES EXPERIENCED IN HIGH PERFORMANCE AIRCRAFT
PURPOSE OF A DROGUE PARACHUTE IS
TO STABILIZE AND DECELERATE THE SEAT TO POSITION THE SEAT IN PROPER ATTITUDE FOR AIRCREW SEPERATION
PURPOSE OF A MIAN PARACHUTE IS
PULLS OCCUPANT, SURVIVAL KIT AND LOWER RESTRAINT HARNESS FREE OF STICKER CLIPS ALLOWING SEAT TO FALL FREE AND OCCUPANT TO CONTINUE NORMAL PARACHUTE DESCENT
WHAT ARE THE ITEMS CONTAINED IN A SEAT SURVIVAL KIT
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
PURPOSE OF ENGINE FUEL SYSTEM
MAINTAINS ENOUGH FUEL BY WEIGHT TO MEET ENGINE DEMANDS
PURPOSE AND LOCATION OF ENGINE INFLIGHT FUELING PROBE
FLIGHT REFUELING

CENTERLINE-FWD WIND SCREEN