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111 Cards in this Set
- Front
- Back
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MEH: WHAT DOES IT STAND FOR.
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MAIN ENTRANCE HATCH |
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LOCATION OF MEH
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MEH HAS _____ INTEGRAL STEPS.
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FOUR |
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AIRCRAFT IS CAPABLE OF CARRYING _____ LBS OF CARGO.
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10,000 LBS |
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HOW MANY PEOPLE CAN A/C CARRY?
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CREWMEMBERS. |
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LOCATE CARGO RAMP.
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DESCRIBE POSITIONS OF CARGO RAMP.
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RAMP OPENS TO A LEVEL POSITION AND STOPS, BUT MAY BE FURTHER LOWERED TO CONTACT GROUND OR DECK FOR LOADING. |
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LIST ALL FLIGHT CONTROLS. |
1. AELERONS 2. FLAPS 3. FLAP AND EILERON DROOP SYSTEM 4. RUDDERS 5. ELEVATORS |
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DESCRIBE AILERONS
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LATERAL CONTROL |
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DESCRIBE FLAPS |
TWO FLAPS ON EACH WING, ONE ON EACH WING FOLD JOINT. |
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DESCRIBE FLAP AND AILERON DOOP SYSTEM.
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DESCRIBE RUDDERS. |
DIRECTIONAL CONTROL (YAW). |
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DESCRIBE ELEVATORS. |
LONGITUDINAL CONTROL (PITCH) ON TRAILING EDGE OF FIXED HORIZONTAL STABILIZER. |
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DESCRIBE ARTIFICIAL FEEL. |
SIMULATED FORCE ON COCKPIT CONTROLS. |
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DESCRIBE NOSE GEAR.
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LOCATION: FORWARD SECTION OF A/C UNDER COCKPIT. CONSISTS OF: 2 NOSE WHEELS AND TIRES. |
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DESCRIBE MAIN GEAR. |
CONSISTS OF: ONE MAIN WHEEL AND TIRE MOUNTED ON EACH STRUT. |
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DESCRIBE TAILSKID. |
TAILSKID IS LOWERED AND RAISED IN CONJUNCTION WITH THE LANDING GEAR AND USED TO PREVENT DAMAGE TO A/C.
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EMERGENCY OPERATION OF LANDING GEAR. |
EMERGENCY PNEUMATIC SYSTEM USED WITH FLIGHT HYDRAULIC SYSTEM FAILURE.
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DESCRIBE BRAKE SYSTEM. |
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DESCRIBE EMERGENCY BRAKE HANDLE.
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DESCRIBE NOSE WHEEL STEERING HANDLE. |
PISTOL GRIP LOCATED ON THE FORWARD END OF PILOT SIDE CONSOLE. UNSTOWING HANDLE WHEN WEIGHT IS ON WHEELS ACTIVATES NOSE WHEEL STEERING SYSTEM. |
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DESCRIBE MAIN GEAR STRUT EXTENDER SYSTEM. |
TO PROVIDE SUFFICIENT CLEARANCE BETWEEEN THE AIRCRAFT TAILSKID AND DECK DURING CAT LAUNCH BY EXTENDING THE MAIN GEAR SHOCK STRUTS FROM THEIR NORMAL POSITION.
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DESCRIBE FLIGHT HYDRAULIC POWER SYSTEM. |
SUPPLIES POWER TO THE PRIMARY FLIGHT CONTROLS ONLY. (AILERONS, ELEVATORS, RUDDERS). HAS AN OPERATING PRESSURE OF 3,000 PSI. |
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DESCRIBE COMBINED HYDRAULIC POWER SYSTEM.
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SUPPLIES POWER TO THE PRIMARY FLIGHT CONTROLS AND TO ALL OTHER HYDRAULICALLY OPERATED SUBSYSTEMS. |
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DESCRIBE WINGS SPREAD POSITION. |
USED FOR FLIGHT. WHEN WINGS ARE UP AND LOCKED YOU CAN CONTROL THE FLAPS AND EILERONS FOR FLIGHT. |
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DESCRIBE WINGS FOLD POSITION. |
OUTER WING PANELS CAN BE FOLDED TO OBTAIN REQUIRED CLEARENCE FOR STOWAGE ABOUT CARRIER. |
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DESCRIBE ARRESTING GEAR. |
(CAN BE USED FOR EMERGENCY LANDING ASHORE) |
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DESCRIBE NOSE-TOW CATAPULT SYSTEM. |
PROVIDES ATTACHMENT TO THE CARRIER CATAPULT LAUNCHING SYSTEM. |
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C-2A ENGINE TYPE.
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T56-A-425 TURBO PROP |
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DESCRIBE PROPELLERS.
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CONSTANT-SPEED HAMILTON SUNSTRAND NP2000 PROPELLERS. |
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___ STAGE AXIAL FLOW COMPRESSOR
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__ INTERCONNECTED COMBUSTION LINERS
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6 |
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___ STAGE TURBINE |
4 |
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WHAT COMPONENT ACTS AS THE ENGINE GOVERNOR. |
THE PROPELLER |
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THE ENGINE AND PROPELLER ASSEMBY IS ESSENTIALLY A __________. |
CONSTANT SPEED UNIT. |
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LIST THE 8 COMPONENTS OF THE ENGINE. |
2. TIE STRUTS 3. POWER SECTION ASSEMBY 4. TURBINE SECTION 5. COMBUSTION SECTION 6. COMPRESSOR 7. ACCESSORY DRIVE HOUSING 8. TORQUEMETER ASSEMBY |
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THE PROP HAS ____ BLADES.
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8 |
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EACH BLADES HAS A _____, AN _____ AND A _______.
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COMPOSIT SHELL, AN EXTERNAL BLADE DEICER AND A COUNTERWEIGHT. |
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THE HUB IS MADE FROM _____. |
STEEL. |
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THE HUB IS ATTATCHED TO THE ENGINE SHAFT ADAPTER BY MEANS OF _____. |
15 BOLTS. |
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INTEGRATED OIL CONTROL CONSISTS OF. |
PUMP HOUSING AND ELECTRONIC VALVE HOUSING. |
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THE VARIABLE PITCH ACTUATOR HAS ____.
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INNER AND OUTER TRANSFER TUBES. |
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THE FRONT SPINNER HAS ___ AFT QUARTER SEGMENTS. |
4 |
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LIST PROPELLER BULKHEAD COMPONENTS
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1. 3 SLIP RINGS 2. 1- 4 PRONGED TARGET 3. 3- 3 PRONGED TARGETS 4. PROVISIONS FOR PROP BALANCING |
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THE PROPELLER HAS A _____ WHICH CONNECTS TO THE PROPELLER SHAFT.
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PROPELLER ADAPTER |
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THE "FOUR BLADE TARGETS" ARE LOCATED ON THE ___. |
EVEN BLADES (2,4,6 &8) |
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THE PROPELLER CONSISTS OF AN ACTUATOR _____ MODULE. |
ACTUATOR VALVE MODULE. |
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TYPE OF FUEL SUPPLIED TO A/C. |
JP-4 OR JP-5 FUEL. |
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THE FUEL IS CARRIED IN __ INTEGRAL TANKS |
2 |
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THE FUEL TANKS HAVE A COMBINED CAPACITY OF _____. |
1824 GALLONS. |
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WHAT PROVIDES AN INDICATION OF FUEL QUANTITY ON THE INDICATORS IN THE COCKPIT? |
CAPACITANCE TYPE PROBES LOCATED IN EACH TANK. |
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WHAT WARNS OF A FUEL-LOW LEVEL CONDITION? |
A LOW-LEVEL WARNING SENSOR LOCATED IN EACH TANK. |
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LIST THE COMPONENTS OF THE FUEL SYSTEM. |
2. A/C BOOST PUMPS. 3. FUEL CONTROL. 4. TANK INTERCONNECT VALVE. 5. FUEL QUANTITY PROBES. 6. FUEL DUMP VALVE. 7. FUEL VENT VALVES. 8. FUEL NOZZLES. |
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LIST THE COMPONENTS OF THE PROPELLER.
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2. PITCH CHANGE ACTUATOR. 3. STEEL HUB. 4. BLADES. 5. REAR SPINNER. 6. BULKHEAD. 7. HYDRAULIC PUMP HOUSING. 8. DEICING BRUSH BLOCK. 9. ELECTRONIC VALVE HOUSING. 10. ACTUATOR VALVE MODULE. 11. GEARBOX. |
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THE BLEED AIR SYSTEM USES A 14TH STAGE BLEED AIR TO SUPPLY BLEED AIR FOR THE FOLLOWING FUNCTIONS, BUT NOT LIMITED TO:
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2. AIR-CONDITIONING. 3. AIRCRAFT PRESSURIZATION. 4. HYDRAULIC RESERVOIR PRESSURIZATION. 5. ENGINE COMPARTMENT COOLING. 6. CROSS BLEED START. |
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DEFINE THE "APU". (APU STANDS FOR, WHAT IT DOES)
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AUXILIARY POWER UNITY, PROVIDES BLEED AIR FOR ENGINE STARTS, HYDRAULIC PRESSURE TO COMBINED HYRAULIC SYSTEM ONLY AND ELECTRICITY ON DECK WITHOUT THE USE OF EXTERNAL POWER. |
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DEFINE PFD.
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DEFINE ESI.
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ELECTRONIC STANDBY INDICATOR- FLIGHT INSTRUMENTATION IN CASE OF PFD FAILURE. |
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DEFINE GP/INS.
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GLOBAL POSITIONING/ INERTIAL NAVIGATION SYSTEM- PROVIDES PRIMARY LONG-RANGE NAVIGATION DATA. |
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DEFINE TACAN.
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DEFINE ICS.
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INTERCOMMUNICATION SYSTEM- PROVIDES VOICE COMMUNICATION AMONG FOUR PRIMARY ICS STATIONS (PILOT, COPILOT AND AFT CABIN LEFT AND RIDE SIDE).
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DESCRIBE UHF/VHF.
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COMMUNICATION RADIOS, THERE ARE TWO LOCATED IN AIRCRAFT.
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HIGH FREQUENCY RADIO
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LONG RANGE COMMUNICATION. |
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DESCRIBE PUBLIC ADDRESS |
PERMITS CREW-TO-PASSENGER VOICE COMMUNICATION. |
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DEFINE IFF.
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IDENTIFICATION FRIEND OR FOE- THE TRANSPONDER PROVIDES CODED IDENTIFICATION AND ALTITUDE SIGNALS IN RESPONSE TO INTERROGATIONS FROM STATIONS TO ESTABLISH AIRCRAFT IDENTIFICATION, CONTROL AIR TRAFFIC ADN MAINTAIN VERTICAL SEPARATION. |
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DESCRIBE WEATHER RADAR.
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THE WEATHER RADAR PROVIDES WEATHER INFORMATION OUT TO A 240 MILE RANGE.
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LOW PROXIMITY INTERCEPT ALTIMETER
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WORKS IN CONJUNCTION WITH THE RADAR ALTIMETER TO PROVIDE AIRCRAFT HEIGHT UP TO 5000 FT. |
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DEFINE CSFIR.
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CRASH SURVIVABILITY FLIGHT INCIDENT RECORDER- THE FLIGHT RECORDER ACQUIRES SELECTED FLIGHT DATA AND RECORDS A MINIMUM OF 2 HOURS OF INFORMATION INTO CRASH- PROTECTED MEMORY. |
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DEFINE ACLS. |
AUTOMATIC CARRIER LANDING SYSTEM- ASSISTS AIRCRAFT IN LANDING ONBOARD SHIP WITH USE OF RADIO SIGNALS. |
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DEFINE AACS.
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AIRCRAFT APPROACH CONTROL SYSTEM- THE AACS RECEIVER -DECODER IS A RECEIVER USED WITH CARRIER-BASED TRANSMITTERS FOR MANUAL INSTRUMENT APPROACHES AND LANDING. |
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DESCRIBE THE WING AND TAIL POSITION LIGHTS.
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THE LIGHTS PROVIDE A VISUAL INDICATION OF AIRCRAFT ATTITUDE AND DIRECTION. |
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DESCRIBE THE ANTICOLLISION LIGHTS. |
THERE ARE TWO DUAL LAMP UNIT ANTI-COLLISION STROBE LIGHTS. ONE ON THE RIGHT OUTBOARD VERTICAL STABILIZER AND ONE ON THE LOWER FUSELAGE AFT OF THE NOSE WHEEL WELL.
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DESCRIBE THE LANDING/TAXI LIGHT. |
USED TO ILLUMINATE THE AREA, LOCATED IN FRONT OF AIRCRAFT. |
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DESCRIBE APPRACH LIGHTS. |
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DESCRIBE THE ADVISORY LIGHTS.
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LOCATED ON THE LOWER RIGHT OF CENTER INSTURMENT PANEL AND CONSISTS OF 23 LIGHTS AND 1 SPARE. |
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DESCRIBE MASTER CAUTION LIGHTS.
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CENTER INSTRUMENT PANEL. CAUTION LIGHTS ILLUMINATE UPON SYSTEM MALFUNCTION. |
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DESCRIBE PITOT STATIC
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PITOT STATIC PROVIDES AMBIENT AND IMPACT PRESSURES NEEDED FOR THE PILOT AND CO-PILOT'S PRIMARY AND STANDBY AIRSPEED INDICATORS AND ALTIMETERS.
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DESCRIBE ANGLE OF ATTACK (AOA)
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THE AOA SYSTEM MEASURES THE ANGLE BETWEEN THE LONGITUDINAL AXIS OF THE AIRCRAFT AND THE RELATIVE WIND.
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DESCRIBE AC GENERATORS
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AC GENERATORS SUPPLY ALL ELECTRICAL POWER REQUIRED TO OPERATE AIRCRAFT ELECTRICAL SUBSYSTEMS. |
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DESCRIBE VOLTAGE REGULATORS |
VOLTAGE REGULATORS CONTROL GENERATOR OUTPUT BY ADJUSTING THE POWER TO THE EXCITER FIELD WINDING. |
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DESCRIBE THE EMERGENCY GENERATOR |
THE EMERGENCY GENERATOR IS HYDRAULICALLY OPERATED AND PROVIDES ELECTRICAL POWER IN THE EVENT OF GENERATOR FAILURE. |
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WHAT IS AFCS? |
AUTOMATIC FLIGHT CONTROL SYSTEM- PROVIDES THE A/C WITH STRAIGHT AND LEVEL FLIGHT CONTROL. |
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DESCRIBE THE AIR CONDITIONING SYSTEM. |
THE AIR-CONDITIONING SYSTEM USES AN AIR CYCLE REFRIGERATION UNIT AND SUPPLIES BLEED AIR TO PROVIDE HEATING AND COOLING. |
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DESCRIBE CABIN PRESSURIZATION.
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AUTOMATICALLY MAINTAINS AIR PRESSURE IN CABIN. |
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THERE ARE ___ ___ LIQUID OXYGEN BOTTLES. DESCRIBE SYSTEM.
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THERE ARE TWO 10 LITER BOTTLES.
THE LIQID OXYGEN SYSTEM CONVERTS LIQUID OXYGEN TO GASEOUS OXYGEN IN CASE OF AN EMERGENCY. |
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DESCRIBE PASSENGER OXYGEN.
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EACH PASSENGER SERVICE UNIT CONTAINS TWO MASKS BEHIND A DOOR THAT UNLATCHES AND OPENS WHEN SYSTEM PRESSURE IS APPLIED. THIS ALLOWS OXYGEN TO FLOW IN CASE OF AN EMERGENCY. |
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HOW MANY WALK AROUND OXYGEN BOTTLES ARE THERE AND LOCATION? |
2, STOWED IN THE CARGO COMPARTMENT PORT SIDE. |
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DESCRIBE THE WINDSHIELD ANTI-ICING SYSTEM.
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THE WINDSHIELD ANTI-ICING SYSTEM PREVENTS THE FORMATION OF ICE ON THE WINDSCREEN. |
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DESCRIBE THE WING AND TAIL DEICING. |
THE WING AND TAIL SYSTEM USES PULSATING RUBBER BOOTS TO ELIMINATE ICE FORMATION. |
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DESCRIBE THE ENGINE FIRE EXTINGUISHING SYSTEM. |
THERE ARE TWO INDEPENDANT, ELECTRICALLY ACTUATED, HIGH RATE OF DISCHARGE FIRE EXTINGUISHING SYSTEMS THAT COMBAT FIRES IN THE ENGINE NACELLES. |
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LIST SOME SAFETY PRECAUTIONS FOR LOX SYSTEM HANDLING/SERVICING. |
2. WHEN SPLASHED WITH LIQUID OXYGEN, ORGANIC MATERIALS BURN VIOLENTLY IF IGNITED. 3. FLAMES, SPARKS, BURNERS, HEATERS AND EXHAUSTS MUST BE KEPT AWAY FROM STORAGE VESSELS, PORTABLE UNITS AND THE A/C. |
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DESCRIBE THE PORTABLE FIRE EXTINGUISHERS. |
THERE ARE 2 FIRE EXTINGUISHERS, THEY ARE LOCATED IN THE AFT CABIN AND BEHIND THE PILOT SEAT. BOTH ARE CHARGED WITH 2 LBS OF CO2. |
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DESCRIBE THE UNDERWATER ACOUSTIC BEACON. |
A BATTERY OPERATED BEACON WHICH EMITS PULSES OF SOUND AT ONE PULSE PER SECOND AFTER BEING ACTUATED BY IMMERSION IN EITHER FRESH OR SALT WATER.
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LIST THE ITEMS CONTAINED WITHIN THE STANDARD SOFT PACK.
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A. 2 DYE MARKERS B. 2 DISTRESS SIGNALS (MK-124 MOD0&2) C. 1 BATTERY POWER SUPPLY D. 2 EMERGENCY BAGGED WATER E. 1 INDIVIDUAL SURVIVAL KIT SRU-31/P F. 1 COMBAT CASUALTY BLANKET |
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DESCRIBE THE MBU.
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MASK BREATHING UNIT, OXYGEN MASK. USED ABOARD FIXED WING AIRCRAFT. |
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WHAT IS THE CAPACITY OF THE LRU-13A LIFE RAFT. |
THE LIFE RAFT HAS A 7 MAN CAPACITY. |
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LIST THE LRU-13A LIFE RAFT EQUIPMENT. |
B. 5 DISTRESS SIGNAL C. 2 WATER STORAGE BAGS D. 7 WATER DRINKING BAGS E. 1 FIRST AID F. 1 DESALINATOR G. 7 FOOD PACKETS H. 1 HAND PUMP I. 1 CASUALTY BLANKET J. 1 FLASHLIGHT K. 1 FLARE GUN L. 1 SIGNAL LIGHT M. 2 CHEMI-LUMINESCENT LIGHT N. 1 SIGNAL MIRROR O. 1 WHISTLE P. 1 COMPASS Q. 1 POCKET KNIFE |
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DESCRIBE THE MISSION.
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TO PROVIDE FLEET LOGISTIC, OPERATIONAL, AND SPECIAL WARFARE SUPPORT FROM FIXED LAND-BASES AND AIRCRAFT CARRIERS. C-2A IS OFTEN UTILIZED TO CARRY CARGO, PASSENGERS ADN MAIL. |
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DESCRIBE FLEET SUPPORT OPERATIONS. |
THE ROLE IS TO PROVIDE SUPPORT SERVICES TO OTHER UNITS. |
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WHAT IS THE ROLE OF THE C-2A IN LOGISTICS MISSIONS. |
THE ROLE IS TO PROVIDE SCHEDULED CARRIER ONBOARD DELIVERY FLIGHTS AND ASSOCIATED RECIEPT/DISTRIBUTION OF MATERIAL, MAIL AND PASSENGERS. |
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DESCRIBE THE NSW (NAVAL SPECIAL WARFARE) MISSION. |
TO DELIVER, SUPPORT AND RECOVER ELEMENTS OF SEAL AND SDV TEAMS. OR COVERTLY INFILTRATE/EXFILTERATE EQUIPMENT, OPERATORS, AGENTS, EVADERS AND ESCAPEES INTO/FROM CONTESTED OR DENIED COASTAL ZONES. |
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LIST PERSONNEL RESPONSIBILITIES.
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1. TAKE ACTION TO CORRECT ALL UNSAFE CONDITIONS. 2. COMPLY WITH MAINTENANCE SAFETY MEASURES, PPE. 3. REPORT ALL PERSONNEL INJURIES/PROPERTY DAMAGE. |
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FALL HAZARD PREVENTION AND CONTROL INCLUDES WORKERS TO WALK OR PERFORM TASKS WHERE THEY CAN FALL FOUR FEET OR MORE TO A LOWER LEVEL, THE FOLLOWING WILL APPLY. |
2. REFRESHER TRAINING. 3. WEAR SHOES WITH NON SLIP SOLES. 4. FALL PROTECTION EQUIPMENT. 5. FALL PROTECTION EQUIPMENT ON FLIGHT LINE. 6. GOOD HOUSEKEEPING PRACTICES. 7. BE AWARE OF WIND LEVELS. |
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INSPECTION WORK CONSISTS OF.
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1. WEARING FALL PROTECTION EQUIPMENT. 2. USING DESIGNATED WALKWAYS. 3. USE CAUTION WITH WET, SNOWY GROUND. 4. USING RISK ANALYSIS. |
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CLEANING AND WASHING A/C CONSISTS OF
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2. USE SEPARATE ELEVATED WORK PLATFORMS TO MAXIMIZE EXTENT. 3. USE CAUTION AROUND WET SURFACES. |
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HAZARDOUS MATERIAL PROGRAM |
HAZMAT RELATED TO THE PROGRAMS WILL BE PROCURED, HANDLED AND DISPOSED OF AS DIRECTED. |
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HAZARDOUS WASTE MANAGEMENT INCLUDES. |
2. HAZWASTE INVENTORY WILL BE MAINTAINED. 3. EMERGENCY PROCEDURES WILL BE MAINTAINED. 4. MAINTENANCE WILL BE IMMEDIATELY IMFORMED IN LUE OF SPILLS. |
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SAFETY PRECAUTION PROCEDURE |
2. ENLIST AID OF OTHER PERSON TO ASSIST. 3. CALL 911 (GIVE NAME, NUMBER, LOCATION, TYPE OF HAZMAT) 4. USE EMERGENCY SHOWER OR EYE WASH. 5. PROVIDE INFO TO 1ST RESPONDERS. 6. IF NO 1ST RESPONDER DRIVE INDIVIDUAL TO HOSPITAL. 7. SEEK MEDICAL ATTENTION WHETHER INDIVIDUAL IS EXPERIENCING EFFECTS. 8. RESCUE INDIVIDUAL, KEEP SELF OUT OF HARMS WAY. |
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DISCUSS FUEL SPILLS
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FUEL SPILLS ARE A FIRE HAZARD. NOTIFY FIRE DEPARTMENT IMMEDIATLY IF SPILL IS LARGER THAN LOCAL AREA DICTATES OR IF SPILL REACHES A STORM DRAIN. USE SPILL KIT IF POSSIBLE. DON CORRECT PPE. USE MSDS. |
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DISCUSS DISPOSAL AND HANDLING OF HM. |
ESTABLISHED WITH HAZMINCEN WITH EFFORTS TO REDUCE HAZARDOUS WASTE AND TIGHTENING OF RULES CONCERNING HM DISOPOSAL. |
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HAZWASTE FACTS. |
KEEP HAZWASTE CONTAINERS TIGHTLY SEALED. ENSURE HAZWASTE IS DISPOSED OF IN SPECIFIC WASTE STREAM. IGNORED OR DELIBERATE SPILLS ARE CRIMINAL OFFENSES RESULTING IN CIVIL FINES OF 50,000$ OR MORE. |
