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96 Cards in this Set
- Front
- Back
WHAT IS THE FIRST STEP IN PREVENTION AIRCRAFT CORROSION AND WEAR?
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CLEANING
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IN THE ABSENCE OF AIRCRAFT SPECIFIC REQUIREMENTS, NAVY AIRCRAFT SHALL BE CLEANED EVERY ____ DAYS ABOARD SHIP AND AT LEAST EVERY ____ DAYS WHEN ASHORE.
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7,14
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WHAT CONTAINS PROCEDURES FOR DECONTAMINATION OF AIRCRAFT EXPOSED TO CHEMICAL, BIOLOGICAL, OR RADIOLOGICAL MATERIALS?
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NAVAIR 00-80T-121
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HIGHLY ALKALINE CLEANING COMPOUNDS ARE NOT AUTHORIZED FOR NAVY OR ARMY AIRCRAFT DUE TO INCOMPATIBILITY WITH POLYMIDE WIRING INSULATION. TRUE OR FALSE |
TRUE
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WHAT ALKALINE CLEANER IS A MORE EFFECTIVE CLEANER FOR HEAVY OILS AND GREASES, INCLUDING WIRE ROPE LUBRICANT, DIE TO ITS SOLVENT CONTENT, BUT IT SHOULD NOT BE USED IN AREAS WHERE VENTILATION IS POOR?
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MIL-PRF-85570 TYPE I
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WHAT ALKALINE CLEANER IS A WATER BASED CLEANER THAT IS AN EXCELLENT CLEANER FOR LIGHT OILS AND HYDRAULIC FLUIDS, AND CAN BE USED IN AREAS OF REDUCED VENTILATION?
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MIL-PRF-85570 TYPE II
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WHAT IS PRIMARILY USED TO EXTINGUISH FLAMMABLE LIQUID AND GAS FIRES SUCH AS GASOLINE, GREASES, OILS, AND PAINTS.
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PURPLE K POWDER (PKP)
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WHEN MIXED WITH EITHER FRESH OR SALT WATER, IT WILL FORM A DENSE FOAM OVER THE LIQUID FUES TO RAPIDLY SMOTHER AND COOL HYDROCARBON FUEL FIRES SUCH AS GASOLINE, KEROSENE, AND DIESEL. |
AQUEOUS FILM-FOAMING FOAM (AFFF)
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FLUOROCARBON FIRE EXTINGUISHANT THAT IS ELECTRICALLY NONCONDUCTIVE, NON-CORROSIVE, FREE OF RESIDUE, HAS ZERO OZONE DEPLETION POTENTIAL (ODP), AND IS AN INVIRONMENTALLY APPROVED REPLACEMENT FOR HALON SYSTEMS?
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HFC-125 (PENTAFLUOROETHANE)
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WHAT 2 HALONS ARE COLORLESS, ODORLESS GASES. THEY WILL EXTINGUISH MOST TYPE OF FIRES WITHOUT LEAVING A RESIDUE AND ARE SUITABLE FOR DISCHARGE IN CONFINED SPACES.
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HALON 1211 AND HALON 1301
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WHAT ENGINE DOES NOT USE ATMOSPHERIC AIR FOR COMBUSTION?
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ROCKET
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THE THRUST DEVELOPED BY A RAMJET ENGINE IS DUE TO THE INCREASE IN THE AIR'S ____?
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TEMPERATURE
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WHAT EFFECT DOES A DIVERGENT DUCT HAVE ON AIRFLOW?
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AN INCREASE IN PRESSURE AND A DECREASE IN VELOCITY
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ACTION ON A BODY THAT CHANGES ITS STATE OF MOTION IS WHAT?
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FORCE |
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RATE OF DOING WORK?
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POWER
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ENGLISH MEASUREMENT FOR MECHANICAL POWER
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HORSEPOWER
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MEASUREMENT OF FORCE TIMES DISTANCE
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WORK
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CAPACITY FOR DOING WORK
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ENERGY
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AN ENGINE EXERTING 1,375 POUNDS OF FORCE MOVES A VEHICLE 13.5 FEET IN 20 SECONDS. WHAT TOTAL AMOUNT OF WORK WAS ACCOMPLISHED? |
18,562.5 FOOT-PUNDS
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TO CALCULATE THE ACCELERATION OF A GIVEN MASS, WHAT SYMBOL REPRESENTING THE FORCE OF GRAVITY IS NORMALLY USED.
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g
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A STANDARD DAY AT SEA LEVEL IS INDICATED BY WHAT CONDITION?
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29.92 INCHES OF MERCURY, 0.00% HUMIDITY, AND TEMPERATURE OF 59.0F.
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WHAT HAPPENS TO A SLUG OF AIR AS TEMPERATURE INCREASES?
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THE MOLECULES MOVE FASTER, RUN INTO EACH OTHER WITH MORE IMPACT, AND MOVE FURTHER APART, DECREASING AIR DENSITY. |
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WHAT IS RAM EFFECT?
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MORE AIR ARRIVING AT THE ENGINE INTAKE THAN THE ENGINE CAN INGEST. |
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NEWTONS FIRST LAW
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INERTIA
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NEWTONS SECOND LAW
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ACCELERATION
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NEWTONS THIRD LAW
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ACTION/REACTION
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IN THE FORMULA F=M x A, WHICH OF FOLLOWING IS A MEASUREMENT UNIT FOR M?
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SLUGS
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WHAT GROUP OF JET ENGINES WILL YOU, AS AN AD, BE ASSOCIATED WITH MOST?
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TURBOFAN, TURBOJET, TURBOPROP, AND TURBOSHAFT
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DECREASING LIFT ON THE ADVANCING BLADE AND INCREASING LIFT ON THE RETREATING BLADE IS KNOWN BY WHAT TERM?
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BLADE FLAPPING
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WHAT IS THE PRIMARY PURPOSE OF BLADE FLAPPING
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TO EQUALIZE THE LIFT OVER THE ROTOR DISC HALVES
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THE UNCONTROLLED LOSS OF ALTITUDE IN A GELICOPTER IS REFERRED TO AS STALLING. TRUE OR FALSE |
FALSE (POWER SETTLING)
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THE MAIN ROTOR THAT ALLOWS EACH OF ITS BLADES TO MOVE VERTICALLY AND HORIZONTALLY IS KNOWN AS WHAT TYPE OF ROTOR
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ARTICULATED ROTOR
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THE LIFT OF A ROTOR IS AFFECTED BY THE LENGTH OF THE ROTOR IN WHAT MANNER
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LIFT IS PROPORTIONAL TO THE SQUARE OF THE LENGTH OF THE ROTOR.
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UPWARD BENDING OF ROTOR BLADES IS KNOWN BY WHAT TERM
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CONING
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WHAT HAPPENS TO POWER REQUIREMENTS AS THE LENGTH OF THE ROTOR BLADE INCREASES
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INCREASES
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A MECHANICAL OFFSET LINKAGE COMPENSATES FOR WHICH OF THE FOLLOWING CONDITIONS |
GYROSCOPIC PRECESSION
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WHAT FORCE INCREASES AS PITCH INCREASES
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LIFT
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AT WHAT TIME IS THE GROUND CUSHION OR GROUND EFFECT MOST EFFECTIVE?
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WHEN THE HELICOPTER IS AT A HEIGHT OF LESS THAN 1/2 OF THE ROTOR DIAMETER
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ROTOR BLADES THAT HAVE ROUGH, DIRTY SURFACES CAUSE WHAT CONDITION?
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DECREASED LIFT, INCREASED DRAG
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DENSITY ALTITUDE REFERS TO THE ALTITUDE CORRECTED FOR ATMOSPHERIC CONDITIONS? TRUE OR FALSE
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TRUE
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WHAT CONTROL SYSTEM PROVIDES THE MEANS OF CONTROLLING THE LATERAL MOVEMENT OF THE HELICOPTER
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CYCLIC ONLY
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HELICOPTER FLIGHT CONTROLS CONSIST OF WHAT SYSTEMS
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CYCLIC PITCH CONTROL, COLLECTIVE PITCH CONTROL, AND ROTARY RUDDER FLIGHT CONTROL SYSTEMS.
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WHAT CONTROL SYSTEM INCREASE THE PITCH OF ALL THE ROTARY WING BLADES EQUALLY AND SIMUTANEOUSLY
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COLLECTIVE ONLY
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DIRECTIONAL HEADING OF A HELICOPTER IS CONTROLLED BY WHAT MEANS
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BY CHANGING THE PITCH OF THE TAIL ROTOR BLADES
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BY WHICH OF THE FOLLOWING MEANS IS/ARE TORQUE REACTION(S) ELIMINATED?
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BY USING A TAIL ROTOR
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A HELICOPTER MUST USE TWO ENGINE-DRIVEN ROTORS FOR LIFT AND PROPULSION? TRUE OR FALSE
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FALSE
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THE MOST COMMON NAVY HELICOPTER HAS WHAT TYPE OF ROTOR(S)?
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SINGLE MAIN
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WAHT TURBOSHAFT ENGINE IS A MEMBER OF WHAT IS KNOWN AS THE NEW GENERATION OF AVIATION PROPULSION SYSTEMS?
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T700-GE-401
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WHAT TYPE OF ENGINE CONSTRUCTION CONTRIBUTES TO INCREASED ENGINE AVAILABILITY BY DECREASING COMPONENT REPAIR TURNAROUND TIME?
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MODULAR
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WHAT TOTAL NUMBER OF MAJOR SECTIONS MAKE UP THE GAS GENERATOR SECTION OF T58-GE-10?
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FIVE
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THE T58 TURBOSHAFT ENGINE COMPRESSOR IS LOCATED IN WHAT BASIC ENGINE SECTION
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GAS GENERATOR ASSEMBLY
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THE T700-GE-401C COMPRESSOR SECTION IS COMPRISED OF WHAT COMPONENTS?
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A SINGLE-SPOOL, FIVE-STAGE AXIAL AND ONE-STAGE CENTRIFUGAL FLOW COMPRESSOR.
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THE ENGINE GAS GENERATOR TURBINE DRIVES WHAT TYPE OF FREE-POWER TURBINE?
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A TWO-STAGE, AXIAL FLOW
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WHAT COMPOONENT OF THE IPS SYSTEM ACTUALLY CAUSES FOREIGN MATERIAL TO BE DUMPED OVERBOARD?
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THE ENGINE DRIVEN BLOWER
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WHAT TURBINE OR TURBINE STAGES DRIVE THE MAIN GEARBOX IN THE SH-60?
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THE POWER TURBINE
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WHAT TYPE OF COMBUSTION SECTION IN USED IN THE T700-GE-401C TURBOSHAFT ENGINE?
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ANNULAR
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THE SH-3 MAIN GEARBOX DRIVES ALL EXCEPT WHAT COMPONENT
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ROTARY WING HEAD
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WHEN THE ROTARY WING HEAD IS DISENGAGED IN THE SH-3, BY WHAT MEANS ARE THE ACCESSORIES DRIVEN?
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BY THE FREEWHEELING UNIT
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POWER TO DRIVE THE ENGINE ACCESSORIES ON THE GROUND WITHOUT ENGAGING THE HEAD COMES FROM WHICH ENGINE
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BY NO. 1 ENGINE ONLY
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WHAT IS THE PURPOSE OF THE INTERMEDIATE GEARBOX
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THE CHANGE THE ANGLE OF DRIVE FROM THE MAIN GEARBOX TO THE TAIL GEARBOX
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THE ELECTOMAGNETIC CHIP DETECTOR/DRAIN PLUG IN THE INTERMEDIATE GEARBOX ALSO DETECTS OVERHEATING WITHIN THE GEARBOX? TRUE OR FALSE
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TRUE
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THE SH-3H MAIN DRIVE SHAFT TRANSMITS TORQUE FROM THE ENGINE TO THE ___?
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MAIN GEARBOX
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WHAT COMPONENTS IN THE TAIL DRIVE SYSTEM ELIMINATE THE NEED FOR THE UNIVERSAL JOINTS?
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THOMAS COUPLINGS
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HOW IS THE MAIN ROTOR BRAKE APPLIED?
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MANUALLY OR AUTOMATICALLY
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WHAT NDI INSPECTION METHOD IS USED WHEN INSPECTING BLENDED AREAS ON THE BELL CRANK SUPPORT MOUNTING PADS?
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FLUORESCENT DYE PENETRANT
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WHAT DRIVE SHAFT REPAIR, IF ANY, IS ALLOWED ON THE TAIL DRIVE SHAFTS?
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THE OUTSIDE DIAMETER OF THE TUBULAR SHAFT.
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THE TWO TYPES OF ROTARY WING HEADS ARE GREASE-LUBRICATED AND SELF-LUBRICATED HEADS? TRUE OR FALSE
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TRUE
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WHAT IS THE MAIN PURPOSE OF THE PRESSURE INDICATOR?
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GIVES VISUAL INDICATION OF SPAR PRESSURE LOSS OR IMPAIRED INTEGRITY OF BLADE
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WHAT CONVENTIONAL FLIGHT CONTROLS IS/ARE REPLACED BY THE TAIL ROTOR
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RUDDER
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BLADE TRACKING IS NECESSARY TO PREVENT WHAT PROBLEM
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VIBRATION AND STRUCTURAL DAMAGE
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WHAT PROVIDES IN-FLIGHT BLADE CHECK/TRACKING?
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STOBEX METHOD
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WHAT IN-FLIGHT ADVANTAGE DOES THE TURBOPROP HAVE OVER THE TURBOJET ENGINE
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MORE THRUST AT LOW SUBSONIC SPEEDS
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A FEATURE OF THE TURBOPROP IS THAT CHANGES IN POWER ARE RELATED TO ____?
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PROPELLER BLADE ANGLE
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THROUGH WHAT MEANS DOES THE PROPELLER ABSORB INCREASED TORQUE IN FLIGHT?
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BLADE ANGLE INCREASE
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THE FUEL CONTROL AND PROPELLER GOVERNOR ESTABLISH THE CORRECT COMBINATION OF WHAT FACTOR
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RPM, FUEL FLOW, AND PROPELLER BLADE ANGLE
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HOW IS SUPPORT EQUIPEMENT NORMALLY IDENTIFIED
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POWERED AND NON POWERED
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WHAT ENGINE POWERS THE A/S32A-45 MID RANGE TOW TRACTOR
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FOUR CYLINDER DIESEL ENGINE
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WHAT IS THE PURPOSE OF THE ENGINE INSTALLATION AND REMOVAL VEHICLE? (EIRV)
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REMOVE AND ISNTALL T-56 ENGINES AND PROPELLERS
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WHAT DOES THE TCP (TOOL CONTROL PROGRAM) ENSURE?
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TOOL ACCOUNTABILITY BEFORE AND AFTER A MAINTENANCE TASK
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WHO IS RESPONSIBLE FOR ENSURING TOOLS ARE PROCURED AND ISSUED ON A CONTROLLED BASIS
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MATERIAL CONTROL OFFICER
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WHAT IS THE NAVAIR 01-1A-17
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AVIATION HYDRAULICS MANUAL |
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WHAT ARE THE 2 GENERAL CLASSES OF HYDRAULIC CONTAMINATES
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ABRASIVES AND NON ABRASIVES
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WHAT LAW OR PRINCIPLE STATES THAT PRESSURE APPLIED TO A CONFINED LIQUID IS TRANSMITTED UNDIMINISHED IN EVERY DIRECTION
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PASCAL'S LAW
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WHAT MANUAL PROVIDES HYDRAULIC MAINTENANCE PROCEDURES |
NA 01-1A-17
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What section of the engine is bleed air tapped from? |
Compressor section |
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What lubrication system are you most likely to encounter in the fleet |
Dry sump |
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What form should you use when requesting an oil analysis of an oil sample at a labratory |
DD form 2026 |
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What is the electrochemical deterioration of a material or its properties due to its chemical reaction with its surrounding environment |
Corrosion |
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What is a liquid containing ions |
Electrolyte |
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Where do all corrosive attacks begin |
On the surface of the metal |
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What is the most common type of corrosion that results from a direct chemical attack on a metal surface that proceeds over the entire exposed surface |
Uniform surface corrosion |
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What corrosion occurs when different metals are in contact |
Galvanic corrosion |
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What corrosion occurs when the form of extremely localized attacks results in holes in the metal |
Pitting corrosion |
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What metal is most susceptible to pitting |
Stainless steel |
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What corrosion is the attack on the grain boundaries of the metal |
Intergranular corrosion |
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What appearance does exfoliating corrosion have |
Lifting up or swelling |