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155 Cards in this Set
- Front
- Back
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WINGSPAN
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53FT
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LENGTH
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59FT 10IN
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HEIGHT
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16FT 3IN
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MAX SPEED AND CRUISE SPEED
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575 KTS
450 KTS |
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SERVICE CEILING
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40,000 FT
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MINIMUM TAKEOFF DISTANCE
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2,750FT
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WEIGHT
EMPTY GROSS |
32,574 LBS
61,043 LBS |
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101
RESPIRATORY PROTECTION 3 TYPES OF RESPIRATORS |
AIR-PURIFYING 19.5-23.5% O2 AVAILABLE
SUPPLIED AIR- PROVIDE BREATHING AIR INDEPENDENT OF THE ENVIORNMENT SELF-CONTAINED- ALLOWS USER INDEPENDANCE FROM FROM A FIXED SOURCE OF AIR. GREATEST DEGREE OF PROTECTION |
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101
HEARING CONSERVATION |
REQUIRED WHEN PERSONNEL ARE EXPOSED TO 84db for 8hrs OR 140db IMPULSE NOISE
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101
SIGHT CONSERVATION |
ANNUAL EYE EXAMS REQUIRED
SAFETY GLASSES WILL BE WORN WHEN PERFORMING: HANDLING MOLTEN METALS OR CORROSIVE MATERIALS CUTTING AND WELDING DRILLING, GRINDING MELTING, CHIPPING SANDBLASTING OR OTHER DUST PRODUCING |
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101
PPE |
DETERMINED BY COMPETENT AUTHORITY THAT ITS USE IS REQUIRED TO LESSEN THE LIKELYHOOD OF OCCCUPATIONAL INJURIES OR ILLNESS
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101
PPE AT FLIGHT QUARTERS |
CRANIAL W/ EYE PROTECTION
LONG SLEEVE SHIRT FLOAT COAT FLIGHT DECK BOOTS OR LOX BOOTS GLOVES |
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101
BLUE CRANIAL/JERSEY |
AIRCRAFT HANDILING CREW/CHOCKS
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101
YELLOW CRANIAL/JERSEY |
AIRCRAFT HANDILING CREW/PLANE DIRECTORS
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101
GREEN CRANIAL/JERSEY WITH AN "A" |
ARRESTING GEAR CREW
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101
PURPLE CRANIAL/JERSEY |
AVAITION FUEL CREW
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101
GREEN CRANIAL/JERSEY WITH A "C" |
CATAPULT CREW
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101
GREEN CRANIAL WHITE JERSEY |
CATAPULT/AG QA
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101
GREEN CRANIAL GREEN AND WHITE JERSEY |
JBD SAFETY
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101
RED CRANAIL/JERSEY |
CRASH AND SALVAGE
EOD AO |
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101
RED CRANIAL GREEN JERSEY |
HELICOPTER LSE
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101
RED CRANIAL BROWN JERSEY |
HELICOPTER PLANE CAPTAIN
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101
GREEN CRANIAL/JERSEY WITH "GSE" |
GSE troubleshooter
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101
NO CRAINIAL WHITE JERSEY WITH "LSO" |
LANDING SIGNALS OFFICER
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101
WHITE CRANIAL/JERSEY "LOX" "RED CROSS" "SAFETY" |
LOX CREW
MEDICAL SAFETY |
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101
GREEN CRANIAL/JERSEY WITH "AT,AM,AD,ECT" |
MAINTENANCE CREWS
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101
BROWN CRANIAL/JERSEY |
PLANE CAPTAINS
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101
LPO/QA |
LINE SHACK: GREEN CRANIAL BROWN JERSEY
MAINTENANCE: GREEN CRANIAL/JERSEY QA: BROWN CRANIAL WHITE JERSEY |
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101
EA-6B DANGER AREAS |
ALL MOVABLE SURFACES:
RADOME CANOPIES EJECTION SEATS BIRDCAGE FLAPS,SLATS RUDDER, ECT. |
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101
EA-6B DANGER AREAS RADIATION |
APS 130 RADAR MINIMUM DISTANCE
15 FT PERSONNEL 10FT ORDNANCE |
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101
EA-6B DANGER AREAS MINIMUM DISTANCE FROM EXHAUST |
34 MPH 50FT
68 MPH 100FT 136 MPH 200FT 204 MPH 300FT 341 MPH 500FT 408 MPH 700FT |
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101
WHAT IS THE MINIMUM DISTANCE FROM INTAKE |
25FT
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101
LIST THE GROUND SAFETY PINS |
8 FWD CANOPY EJECTION SEATS(EA)
7 AFT CANOPY EJECTION SEATS(EA) FWD AND AFT CANOPY JETISON CANOPY MANUAL CONTROL NOSE WHEEL 2 MAIN LANDING GEAR ARRESTING HOOK 5 PYLONS |
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101
SAFETY PRECAUTIONS WHEN APPLYING EXTERNAL POWER |
ALL SWITCHS "OFF, SAFE OR NORMAL"
AIRCRAFT GROUNDED ALL PERSONNEL KNOW POWER IS BEING APPLIED |
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102
NUMBER AND LOCATION OF TIE DOWN POINTS |
1 NOSE GEAR DRAG BRACE
2 FWD STATION ONE OUTBOARD 3 AFT STATION ONE OUTBOARD 4 FWD STATION 5 OUTBOARD 5 AFT STATON 5 OUTBOARD 6 UPPER LEFT MAIN LG 7 UPPER RIGHT MAIN LG 8 LEFT MAIN LG AXEL 9 RIGHT MAIN LG AXEL 10 TAIL SCAG |
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102
PROPER GROUNDING PROCEDURES |
ATTACH CABLE TO GROUND
ATTACH CABLE TO AIRCRAFT GROUND POINT |
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102
FUELING/DE-FUELING PROCEDURES |
GROUND AIRCRAFT
GROUND FUEL TRUCK CONNECT BONDING CABLE TO FUEL TRUCK AND AIRCRAFT WAIT TWO MINUTES BEFORE REMOVING BONDING CABLE |
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102
WHO IS REPSONSIBLE FOR OVERALL EXECUTION OF AIRCRAFT MOVE |
MOVE DIRECTOR
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102
WHO CONDUCTS PRE-MOVEMENT INSPECTION |
BRAKE RIDER
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103
WHEN IS THEIR NOT A BRAKE RIDER DURING AN AIRCRAFT MOVE |
WHEN THE SEATS HAVE BEEN REMOVED
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102
WHAT DOES THE TRACTOR DRIVER DO |
POSSES A VALID SE LICENSE
PRE-OPS TRACTOR AND TOW BAR TAKES DIRECTIONS FROM MOVE DIRECTOR |
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102
RESPONSIBILITIES OF SAFETY OBSERVER |
WATCHES FOR OBSTRUCTONS AND ALERTS MOVE DIRECTOR
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102
WHAT IS THE MINIMUM NUMBER OF PERSONNEL REQUIRED FOR A MOVE |
6
1.MOVE DIRECTOR 2.BRAKE RIDER 3.TRACTOR DRIVER 4. 2 CHOCK WALKERS/SAFETY OBSERVER 5.TAIL WALKER |
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103
HYDRUALIC PATCH TEST |
CONTAMINATION ANALYSIS TO DETERMINE THE PARTICULATE LEVEL OF THE HYDRAULIC SYSTEM
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103
PURPOSE OF TACTICAL PAINT SCHEME |
DECEPTION
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103
PURPOSE OF SPIN RECOVERY SYSTEM |
INCREASES STABILIZER AND RUDDER THROWS DURING CLEAN CONFIGURATION
STAB INCREASES FROM 10 DEGREES TO 24 RUDDER INCREASES FROM 4 DEGREES TO 35 |
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103
WING FOLD SYSTEM |
ALLOWS AIRCRAFT TO PARK IN LIMITED SPACE
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103
HYDRAULIC SYSTEM FLIGHT |
PROVIDES POWER FOR THE OPERATION OF THE PRIMARY FLIGHT CONTROLS
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103
HYDRAULIC SYSTEM COMBINED |
PROVIDES POWER TO PRIMARY FLIGHT CONTROLS AND GENERAL UTILITY PRESSURIZED AT 3000 PSI
EX NOSE WHEEL STEERING NORMAL BRAKE FLAPS/SLATS |
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103
HYDRAULIC SYSTEM AUXILLARY |
SUPPLIES HYDRAULIC POWER FOR GROUND OPS
BIRDCAGE RADOME WHEEL BRAKE ACCUMULATOR |
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104
PURPOSE AND LOCATION OF IFR (IN-FLIGHT REFUELING PROBE) |
RE-FUEL IN FLIGHT
CENTERLINE FWD OF THE WINDSHIELD |
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104
TYPE OF ENGINES ON EA-6B |
J-52-P-408/408A
11,200 LBS OF THRUST |
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104
SIX BASIC SECTIONS OF ENGINE |
Turbine exhaust
Accessory section Combustion chamber Diffuser Inlet Compression |
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104
TWO METHODS OF STARING ENGINES |
1. GROUND STARTING CART (HUFFER)
2. BLEED AIR FROM OTHER OPERATING ENGINE (CROSS-BLEEDING) |
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104
PURPOSE OF THE ENGINE FUEL SYSTEM |
MAINTAIN A SUPPLY OF FUEL BY WEIGHT TO MEET ENGINES DEMANDS
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105
IFF INS RADAR TACAN ESM ACLS APC AFCS EFIS OAT |
IDENTIFICATION FRIEND OR FOE
INERTIAL NAVAGATION SYSTEM TACTICAL AIR NAVAGATION ELECTRONIC SUPPORT MEASURES AUTOMATIC CARRIER LANDING SYSTEM APPROACH POWER COMPENSATOR AUTOMATIC FLIGHT CONTROL SYSTEM ELECTRONIC FLIGHT INSTRUMENT SYSTEM OUTSIDE AIR TEMPATURE |
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105
PURPOSE OF ECM EQUIPMENT |
TO DECTECT, ANALYZE, LOCATE AND DEGRADE THE USE OF THE ENEMIES ELECTRONIC WARFARE EQUIPMENT
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105
TWO CATAGORIES OF ECM |
ELECTRONIC- JAM
NON-ELECTRONIC-CHAFF |
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105
RADAR ALTIMETER |
RANGE TRACKING RADAR THAT MEASURES THE SURFACE OR TERAIN CLEARANCE BELOW THE AIRCRAFT. ONLY WORKS UP TO 5000FT
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105
BAROMETRIC ALTIMETER |
GIVES ALTITUDE BY MEASURING OUTSIDE AIR PRESSURE IN HUNDREDS OF FEET
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106
OBJECTIVE OF THE EXPLOSIVE HANDLING PERSONNEL QUALIFICATION AND CERTIFICATION PROGRAM |
ENSURE EACH PERSON HANDLING EXPLOSIVE DEVICES IS QUALIFIED
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106
SAFETY PRECAUTIONS FOR A HOT SEAT PROCEDURE |
A/C IN DESIGNATED AREA
WEAPONS MUST BE SAFED ONE CHOCK INSTALLED ANY A/C CARRING HARM MUST BE IN AN ARM/DEARM AREA |
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107
MINIMUM PPE REQUIREMENTS FOR AIRCREW |
HELMET
BOOTS GLOVES ID TAGS SURVIVAL KNIFE SIGNAL DEVICE SURVIVAL RADIO ANTI-G SUIT |
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107
PURPOSE OF OXYGEN MASK |
PROVIDES OXYGEN TO AIRCREW AND CAN BE USED FOR BREATHING UNDERWATER UP TO 16FT
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107
OXYGEN REGULATOR |
REGULATES OXYGEN PRESSURE FOR BREATHING OF 100% OXYGEN AND AUTOMATICALLY PROVIDES POSITIVE PRESSURE AT ALTITUES ABOVE 34,000FT
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107
LIFE PRESERVER |
AUTOMATIC FLOTATION DEVICE ON SV-2B SURVIVAL VEST. MAINTAINS A MINIMUM BUOYANCY OF 65LBS
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107
ANTI-G SUIT |
PROVIDES PROTECTION FROM EXCESSIVE G FORCES
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107
DROUGE PARACHUTE |
2 PARACHUTES CONTROL AND STABILIZER
STABILIZES THE SEAT AND WITHDRAWLS PERSONNEL PARACHUTE |
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107
MAIN PARACHUTE |
ALLOWS AIRCREW TO DECEND SAFELY
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107
SEAT SURVIVAL KIT |
EMERGENCY OXYGEN
LIFE RAFT EMERGENCY RADIO BEACON SIGNAL FLARE DYE MARKER SPONGE CAN OPENER CASUALTY BLANKET CODE CARD MEDICAL PACKET |
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107
PURPOSE OF EGRESS SYSTEM CHECKOUT CERTIFICATION PROGRAM |
ESTABLISHES POLICY, RESOPNSIBILTIES AND REQUIREMENTS FOR CHECKOUT PROCEDURES
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107
DEFINE HYPOXIA DEFINE ANOXIA |
DECREASE IN OXYGEN
COMPLETE LACK OF OXYGEN |
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107
TWO TYPES OF AVIATORS BREATHING OXYGEN |
TYPE 1 GASEOUS- EMERGENCY
TYPE 2- LIQUID- NORMAL USE |
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201
AIRCRAFT STRUCTURE |
FUSELAGE
EMPANNAGE WING |
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201
FLIGHT CONTROL SURFACES FLAPS |
SEMI-FOWLER TYPE
TRAILING EGDE OF WINGS GIVE MORE LIFT FOR TAKEOFF AND LANDING |
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201
FLIGHT CONTROL SURFACES SLATS |
LEADING EDGE OF WINGS
USED TO PROVIDE MORE LIFT DURING TAKEOFF AND LANDING |
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201
FLIGHT CONTROL SURFACES FLAPERONS |
LATERAL CONTROL (ROLL)
JUST FORWARD OF THE FLAPS |
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201
FLIGHT CONTROL SURFACES HORIZONTAL STABILIZER |
LONGITUDINAL CONTROL (PITCH)
EMPENNAGE BELOW THE VERTICAL STABILIZER |
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201
FLIGHT CONTROL SURFACES RUDDER |
DIRECTIONAL CONTROL (YAW)
LOCTATED ON THE VERTICAL STABILIZER |
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201
FLIGHT CONTROL SURFACES SPEED BRAKES |
KEEP AIRCRAFT FROM BUILDING EXCESSIVE SPEED DURING DIVES AND LANDING
TRAILING EDGE OF WINGTIPS |
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201
NAME AND LOCATION OF HYDRAULIC RESERVOIRS |
FLIGHT- RIGHT ENGINE INLET SECTION. FWRD OF ENGINE ACCESS DOOR.
COMBINED-LEFT WING FILLET COMPARTMENT, BELOW THE LEADING EDGE OF THE WING |
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201
FUNCTION OF HYDRAULIC PUMPS |
PRIMARY POWER FOR HYDRAULIC SYSTEMS. MAY BE ENGINE DRIVEN, ELECTRICALLY DRIVEN OR HAND PUMP
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201
FUNCTION OF HYDRAULIC ACTUATORS |
TRANSFORM HYDRAULIC FLUID PRESSURE INTO MECHANICAL FORCE. TWO TYPES: ACTUATING CYLINDERS AND HYDRAULIC MOTORS
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201
FUNCTION OF HYDRAULIC ACCUMULATORS |
STORE A OF VOLUME OF FLUID UNDER PRESSURE TO ACT AS CUSHION AGAINST PRESSURE SURGES
SUPPLEMENT THE PUMPS OUTPUT UNDER A PEAK LOAD |
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201
PRIMARY PURPOSE OF LANDING GEAR |
TO SUPPORT AND MANEUVER AIRCRAFT
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201
FUNCTION AND LOCATION OF WHEEL BRAKES |
USED FOR MANEUVERING AND STOPPING AIRCRAFT ON GROUND.
MAIN LANDING GEAR WHEEL WELL |
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201
FUNCTION OF THE NOSE TOW CATAPULT SYSTEM |
THE TOW LINK GUIDES AND HOLDS A/C TO SHUTTLE
HOLDBACK IS A BELL CRANK AFT OF THE NOSE GEAR STRUT THAT ATTACHS THE A/C TO THE CATAPULT |
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201
FUNCTION OF THE ARRESTING HOOK |
PROVIDES CARRIER LANDING CAPABILITY
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201
WHAT ARE THE THREE MODES OF CABIN AIR CONDITIONING |
AUTO- MAINTAINS TEMP BETWEEN 60 AND 80 WITH THUMB WHEEL
MANUAL- ALLOWS CREW TO MANUALLY SWITCH TEMP RAM AIR- EMERGENCY BACK-UP |
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201
WHAT ARE THE THREE CABIN PRESSURIZATIONS |
UNPRESSURIZED-0 TO 8000FT
ISOBARIC- 8000 TO 23000 FT CABIN ALTITIUDE REMAINS AT 8000FT DIFFERENTIAL- 23000FT PLUS CABIN PRESSURE AT 5PSI |
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201
WHAT IS THE TEMPERATURE OF THE DEFOGGING SYSTEM |
240 DEGRESS F
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201
WHAT IS THE PURPOSE OF THE VENT SUIT |
TO PROVIDE CONDITIONED AIR TO EACH CREW MEMBER. AUTOMATICALLY MAINTIANED AT 75 DEGREES
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201
WHAT TEMPERATURE DOES THE EQUIPMENT COOLING SYSTEM KEEP |
75 DEGREES
85 FOR EMERGENCY |
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201
WHAT IS THE WINDSHIELD WASH MADE OF |
50% WATER
50% METHAL ALCOHOL |
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201
HOW MANY NOZZELS ARE THERE IN THE RAIN REMOVAL SYSTEM |
26
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201
NAME THE THREE SUBSYSTEMS OF THE CANOPY OPENING SYSTEM |
NORMAL- OPENS AND CLOSES CANOPIES USING PNEUMATIC PRESSURE
AUXILLARY- ONE TIME USE IF NORMAL SYSTEM FAILS. HANDLES MUST BE IN OPEN POSITION JETTISON- EMERGENCY HANDLE IN FWD COCKPIT OPERATES BOTH. AFT ONLY AFT |
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201
WHAT IS THE FUNCTION OF THE MAIN LANDING GEAR OVERRIDE VALVE |
TO OPEN THE FORWARD MAIN LANDING GEAR DOOR DURING GROUND MAINTENANCE.
LOCATED IN NACELLE AFT OF MAIN LANDING GEAR SHOCK STRUT |
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201
PURPOSE OF THE NOSE LANDING GEAR STRUT LOCK |
RENDERS THE SHOCK ALMOST RIGID FOR A CATAPULT LAUNCH
ACTIVATED BY THE COMBINED HYDRAULIC SYSTEM |
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201
PURPOSE OF THE LANDING GEAR EMERGENCY SYSTEM |
LOWERS THE LANDING GEAR USING PNEUMATIC PRESSURE
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201
PURPOSE OF THE IPI |
INTEGRATED POSTIONING SYSTEM
DISPLAYS THE POSITION OF THE SLATS, STAB, FLAPS, SPEED BRAKES,WHEELS AND TOW LINKS |
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201
SAFETY PRECAUTIONS EJECTION SEAT |
ENSURE ALL SAFETY PINS ARE INSTALLED BEFORE ENTERING COCKPITS
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201
SAFETY PRECAUTIONS CANOPY JETTISON SYSTEM |
ENSURE SAFETY PINS ARE INSTALLED BEFORE ENTERING COCKPITS
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201
SAFETY PRECAUTIONS CANOPY NORMAL SYSTEM |
ENSURE SAFETY PINS ARE INSTALLED ANYTIME CANOPIES ARE OPEN
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201
SAFETY PRECAUTIONS LOX |
ONLY TRAINED AND LICENSED PERSONNEL CAN SERVICE LOX
BOILS -297 DEGREES HIGHLY COMBUSTABLE EXPANSION RATE OF 862 TO 1 |
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202
ENGINES STARTER |
TURNS OVER THE ENGINES
ALSO DRIVES THE CSD/GENERATOR |
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202
ENGINES FUEL CONTROL |
LIGHTWEIGHT , HIGH CAPACITY, FUEL FLOW METERING UNIT THAT PERMITS SELECTION OF DESIRED ENGINE THRUST
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202
ENGINES POWER LEVEL CONTROL QUANDRANT |
PROVIDES CONTROL OF THE ENGINES THROUGHOUT RANGE OF OPERATION
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202
ENGINES ENGINE OIL SYSTEM |
SELF CONTAINED HIGH PRESSURE SYSTEM CONSISTING OF A PRESSURE OIL SYSTEM, SCAVENGE OIL SYSTEM AND BREATHER SYSTEM. PRESSURIZES, FILTERS, COOLS AND RE-CIRCULATES OIL
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202
ENGINES FIRE/OVER TEMP DETECTION SYSTEM |
PROVIDES COCKPIT INDICATION OF FIRE/OVERTEMP OF THE ENGINES, BIRDCAGE OR NOSE WHEEL WELL
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202
ENGINE INDICATING SYSTEM OIL PRESSURE INDICATOR |
0-100PSI INDICATES OIL PRESSURE
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202
ENGINE INDICATING SYSTEM FUEL FLOW INDICATOR |
INDICATES FUEL FLOW FROM ENGINES
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202
ENGINE INDICATING SYSTEM ENGINE SPEED INDICATOR |
SHOWS ENGINE RPM'S IN PERCENT
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202
ENGINE INDICATING SYSTEM EXHAUST GAS TEMP INDICATOR |
6 THERMOCOUPLES SHOW EXHAUST TEMP
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202
FUEL SYSTEM FOWARD FUEL CELL |
SELF SEALING
392 GALLONS |
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202
FUEL SYSTEM MID FUEL CELL |
BLADDER TYPE
256 GALLONS |
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202
FUEL SYSTEM AFT FUEL CELL |
SELF SEALING
643 GALLONS |
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202
FUEL SYSTEM WING TANKS |
TWO OUTBOARD
ONE INBOARD |
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202
FUEL SYSTEM DROP TANKS |
AERO-1D
300 GALLONS |
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202
FUEL SYSTEM TOTAL FUEL CAPACITY |
FUSELAGE-1291 GAL
WINGS-977 GAL TOTAL-2,268 GAL |
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202
SAFETY PRECAUTIONS ENGINE GROUND TURN-UP |
REMAIN CLEAR OF DANGER AREAS
MUST WEAR HEARING AND EYE PROTECTION FIRE EXTINGUISHER MUST BE MANNED |
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202
SAFETY PRECAUTIONS FUELING/DEFUELING |
FUELING- DO NOT REFUEL OUTBOARD WING TANKS WHEN FOLDED
NO RADIO OR RADAR WITHIN 100FT AIRCRAFT AND TRUCK MUST BE GROUNDED DISCHARGE ANY STATIC ELCTRICITY DEFUELING-100FT FROM RADIO AND 300FT FROM RADAR PROPERLY GROUNDED AIRCRAFT AND TRUCK DISCHARGE ANY STATIC ELECTRICITY |
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203
UHF |
225 MHZ TO 399.95 MHZ
COMS, AUTOMATIC DIRECTION FINDING |
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203
VHF |
116 MHZ TO 151.95 MHZ
COMS |
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203
HF |
2 MHZ TO 29.999MHZ
UPPER AND LOWER SINGLE SIDE BAND OR AM COMS |
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203
AIC-14/AIC-45 ICS |
PROVIDES AMPLIFICATION FOR RADIO TRANSMISSION AND RECEPTION ALSO FOR RADIO RECIEVER OUTPUTS, RADIO NAVIGATION INFO, WARNING, AND ECM SIGNALS
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203
TACAN |
ARN/84
SLANT RANGE AND AZIMUTH TO ANY SELECTED SURFACE STATION RANGE 300NM |
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203
INS |
INTERIAL NAVAGATION SYSTEM
AIRCRAFT ATITTUDE REFERENCE AND PROVIDES PRESENT POSITION, AS WELL AS HORIZONTAL AND VERTICAL VELOCITIES |
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203
RADAR |
APS-130
PRESENTS A GROUND MAP DISPLAY OF TERRIAN AHEAD |
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203
GPS |
SPACE BASED RADIO POSITIONING SYSTEM
HIGHLY ACCURATE POSITION, VELOCITY, AND TIME DATA |
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203
ATTITUDE HEADING REFERENCE |
ASN-50
HEADING INFO TO THE ADI IN PRIMARY MODE PITCH, ROLL AND HEADING INFO IN SECONDARY MODE |
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203
RADIO COUNTERMEASURES SET |
USQ-113
PROVIDES ESM,ECM AND COMMS |
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203
ALQ-99/ALQ-218 |
TATICAL RECEIVER AND JAMMING SYSTEM
DETECTS, ANALYZES AND JAMS HOSTILE RADAR THREATS |
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203
TACTICAL COMPUTER |
AYK-14
GENERAL PURPOSE COMPUTER. USED FOR BOTH NAVAGATION AND TACTICAL JAMMING |
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203
TACTICAL NAVIGATION SET |
AN/ASN-123
PROVIDES INTERFACE WITH THE CENTRAL COMPUTER AND DIPLAYS TJS/NAV DATA |
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203
IDENTIFY THE LOCATION AND PURPOSE OF THE TJS POD COMPONENTS |
HARBACK- TOP OF POD CONNECTS TRANSMITTERS AND UEU TO AIRCRAFT
TRANSMITTERS- 1 FORWARD. 1 AFT. GENERATE JAMMING SIGNALS UEU- MID BETWEEN TRANSMITTERS. INTERFACE BETWEEN TX AND TJS SYSTEM RAM-AIR TURBINE GENERATOR- FRONT OF POD. PROVIDES POWER TO TJS POD DURING FLIGHT RADOME-BOTTOM OF POD. |
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203
AFCS |
AUTOMATIC FLIGHT CONTROL SYSTEM
ERROR SENSING COUPLING AND AMPLIFYING SYSTEM PROVIDES TWO-AXIS STABILITY AUGMENTATION, THREE-AXIS ATTITUDE CONTROL AND FLIGHT PATH CONTROL |
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203
ACLS |
AUTOMATIC CARRIER LANDING SYSTEM
CLOSED LOOP SYSTEM THAT USES PULSE CODED KU-BAND INFO AND KA-BAND INTERROGATION FROM THE AIRCRAFT CARRIER FOR LANDINGS IN ALL CONDITIONS |
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203
ICLS |
INSTRUMENT CARRIER LANDING SYSTEM
RECIEVES AND DECODES GLIDE SLOPE INFO, AZIMUTH AND ELEVATION SIGNALS. WORKS WITH AN/SPN-41 ON CARRIER |
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203
APC |
APPROACH POWER COMPENSATOR
MAINTAIN AN AIRSPEED THAT WILL GIVE A CONSTANT AVERAGE ANGLE OF ATTACK |
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203
PURPOSE OF GENERATORS |
SUPPLY A CONSTANT 115/200 VAC THREE PHASE 400HZ POWER TO THE A/C
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203
PURPOSE OF TRANSFORMER RECTIFIER |
TO TAKE AC POWER AND TURN IT INTO DC POWER
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203
REGULATOR-SUPERVISOR PANEL |
SENSING CIRCUITS FOR VOLTAGE REGULATION AND PROTECTIVE FUNCTIONS
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203
EXTERIOR LIGHTS ANTI-COLLISION |
TWO
CENTERLINE TOP DECK CENTERLINE FORWARD OF THE NOSE WHEEL FAIRING |
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203
EXTERIOR LIGHTS FORMATION |
FOUR
TWO ON THE WINGS AND TWO ON THE FUSELAGE |
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203
EXTERIOR LIGHTS PYLON |
AFT END OF THE OUTBOARD PYLONS
USED FOR POSTITION REFERENCE DURING IN-FLIGHT RE-FUELING |
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203
EXTERIOR LIGHTS POSITION LIGHTS |
THREE
ONE ON EACH LEADING EDGE OF THE WINGS ON THE TIP AND ON THE TAIL AT THE BASE OF THE VERT STAB. INDICATES DIRECTION OF TRAVEL |
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203
EXTERIOR LIGHTS IN FLIGHT REFUELING PROBE |
FWD OF THE PILOTS WINDSHIELD. ILLUMINATES THE PROBE DURING IN-FLIGHT REFUELING
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203
EXTERIOR LIGHTS TAXI |
NOSE LANDING GEAR DOOR FAIRING
LIGHTS THE WAY DURING TAXIING, TAKE OFF AND LANDING |
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203
EXTERIOR LIGHTS APPROACH LIGHTS |
FOWARD NOSE WHEEL DOOR
GREEN- HIGH ANGLE OF ATTACK AMBER- OPTIMUM ANGLE OF ATTACK RED- LOW ANGLE OF ATTACK |
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204
BOMB RACKS |
AREO7A-WINGS
AREO7B-CENTERLINE 2 INCHES SHORTER 4 PAIRS OF SUSPENSION HOOKS 14 INCHES APART AND 30 INCHES APART |
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204
WHEN ARE JETTISON CHECKS REQUIRED |
WITHIN 24HRS PRIOR TO LOADING
AFTER RECONFIGURATION AFTER ANY MALFUNCTION HAS BEEN CORRECTED |
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204
PURPOSE OF THE AGM-88 HARM |
DESTROY SHORE OR SEA BASED ENEMY RADAR. USED WITH THE LAU-118/A
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204
STATE THE PURPOSE OF FLARES |
USED AGIANST HEAT SEAKING MISSILES
MK-46 MJU-8/B |
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204
STATE THE PURPOSE OF CHAFF |
CONSISTS OF SMALL METAL STRIPS. JAMS RADAR INSTALLATIONS OR RADAR MISSLES
RR-129 RR-144 |
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204
STATE THE PURPOSE OF THE AN/ALE-39 |
CHAFF AND FLARE DISPENSER
INSTALLED IN ALMOST EVERY NAVAL AIRCRAFT TWO DISPENSERS AND A PROGRAMMER |
