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60 Cards in this Set
- Front
- Back
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general safety precautions with fueling with rotors engaged
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a chocked and intial four point tie down
b all people fuel are trained c all movement via the nose dremoval of hose in evacuated condition e fueling stopped when fuel spill is noticed |
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MH60S DANGER AREAS
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A ROTOR ARCS
B ENGINE INTAKES C ENGINE EXHAUST D APU EXHAUST E ECS EXHAUST |
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HAZARDS AND SAFTEY PRECAUTIONS WHEN HANDLING BERRYLIUM
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CANCER CAUSING AGENT AVOID TOUCHING, NEVER GRIND OR SAND AVOID INHALING DUST OR SPLINTERING THE SKIN
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RESPIRATORY PROGRAM
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EVERY COMMAND WHO HAS HAZMAT THAT REQUIRES A RESPIRATOR A RESPIRATOR PROGRAM WILL BE ESTABLISHED. A RPPM SHALL BE APPOINTED IN WRITING TO THE CO
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HEARING PROTECTION
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TO PREVENT OCCUPATIONAL HEARING LOSS
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STATE THE WARNINGS TO BE OBSERVE BEFORE APPLYING EXTERNAL POWER
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A ALL SWITCHES OFF SAFE OR NORMAL, REQUIRED CIRCUIT BREAKERS PULLED
B POWER CORD NOT ENERGIZED DURING HOOK UP C LEAR STAB OF PERSONNEL |
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DOUBLE RESCUE HOOK
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PRIMARY RESCUE DEVICE
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RESCUE STROP
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BOUYANT DEVICES USED TO LIFE ONE PERSON AT A TIME PROVIDES FLOATATION FOR THE RESCUE HOOK DURING RESCUE
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MEDEVAC LITTER
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BOYANT FOLDABLE LITTER TRANSPORT INJURED PERSONNEL ATTACHED TO RESCUE HOOK CAN BE LIFTED HORIZONTAL/VERTICAL RED HEAD WHITE FEET FOUR RETENTION STRAPS HOLD PERSON IN
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HELICPTER RESCUE EQUIPMENT BAG
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HOISTING GLOVES CHEMICAL LIGHTS CHEMICAL LIGHT STRAPS 3 CREWMAN SAFETY BELTS CABLE CHICAGO GRIP HOIST QUICK SPLICE PNEUMATIC RESCUE HAND TOOL OR MANUAL RERSCUE HAND TOOL RESCUE LITTER SLING ASSEMBLY RESCUE STROP BLANKETS CRANIAL AND TRAIL LINE ASSEMBLY
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LPU-32 LIFE PRESERVERS
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HORSE COLLAR TYPE PRESERVER,PROVIDES 40LBS OF BUOYANCY CONTAINS WHISTLE SEA DYE MARKER AND CHEMLIGHT REPLACED LPU-30 FLOAT COAT
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RESCUE HARNESS
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KNIFE, 4 CHEMICAL LIGHTS, STOBE LIGHT, SHROUD LINE CUTTER, AND 2 MK 124 V RING AND SNAP HOOK FOR DOUBLE RESCUES
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LPU-28 SAR 1
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USED WITH HELICOPTER AIRCREW MAN HELMETS THEY PROVIDE STORAGE AND VELCRO ATTACHMENT POINTS FOR THE DISTRESS LIGHT AND THE AN/PRC-125 RADIO
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WET SUIT
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thermal protection swimmer from outside water environment
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AN/PRC-90-2
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2 FIXED FREQUENCIES BEACON OR VOICE MODES, WATER-RESISTANT RADIO CARRIED IN AIRCREWS SV-2
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AN/PRC-112
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CSAR RADIO. 2 PROGRAMMABLE FREQUENCIES AND 2 FIXED FREQUENCIES. USED IN OVERLAND RESCUE AND USED WITH DALS AUTHENTICATOR CARRIED IN AIRCREW S-2
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STATE THE REASON WHY ELECTRICAL POWER IS REQUIRED WHEN FOLDING THE TAIL ROTOR PYLON
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POWER IS REQUIRED TO INDEX THE TAIL ROTOR TO KEEP THE TAIL ROTOR BLADES FROM CATCHING WIND AND SPINNING
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STATE TEH WIND RESTRICTION FOR FOLDING THE MAIN AND TAIL ROTOR PYLON
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DO NOT FOLD BLADES OR TAIL ROTOR PYLON IF THE WINDS ARE OVER 45 KNOTS
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STATE THE LOCATION OF TIE DOWN FITTINGS ON THE MH60S
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TIE DOWN FITTINGS ARE INSTALLED AT SIX POINTS ON THE HELICOPTER
ONE ON EACH MAIN LANDING GEAR WHEEL HUB ONE HIGH POINT ABOVE THE STRUT ON EACH SIDE OF THE AIRCRAFT TWO MORE FITTING ARE ATTACHED ON THE AFT TRANSTION SECTION ABOVE THE TAIL WHEEL ONE ON EACH SIDE |
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STATE THE GROUND RECEPTACLE LOCATIONS AND PROPER PROCEDURES FOR AIRCRAFT GROUNDING
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MAIN LOCATIONS ARE ON THE PORT SIDE OF TRANSITION SECTION
GROUNDING PROCEDURES ATTACH GROUNDING WIRE TO GROUND FIRST THEN TO AIRCRAFT UN GROUNDING PROCEDURE DISCONNECT GROUNDING WIRE FRON THE AIRCRAFT THEN DISCONNECT FROM THE GROUND |
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STATE THE PROCEDURES AND CAUTIOONS THAT MUST BE OBSERVED DURING AIRCRAFT JACKING
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A DO NOT JACK WHILE ENGINES ARE RUNNING OR ROTOR TURNING
B DO ENGAGE TAIL WHEEL LOCK PIN C DO ENSURE WHEELS NOT BEING RAISED ARE CHOCKED D DO ENSURE OVERHEAD IS CLEAR E DO ENDURE JACK IS POSITIONED UNDER JACK PAD F CAUTION A MINIMUM OF ONE PERSON PER JACK |
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EXPLAIN WHY TIEDOWN DEFLECTION OF BLADE TIPS SHOULD BE SIX TO TWELVE INCHES FROM STATIC POSITION
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TO PREVENT DAMAGE FROM EXCESSICE TIGHTENING OF TIEDOWN CABLES OR FROM WIND FLAPPING
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IDENTIFY THE PERSONNEL REQUIRED FOR AN AIRCRAFT MOVE
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2 WING WALKERS
1 TOW TRACTOR DRIVER 1 SAFETY OBSERVER 1 DIRECTOR 1 BRAKE RIDER |
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STATE THE IMPORTANCE OF A WHISLE DURING AND AIRCRAFT MOVE
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WHEN THE WHISTLE IS BLOWN THE TOW TRACTER DRIVER STOPS IMMEDIATELY
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STATE THE PURPOSE OF A HYDRAULIC PATCH TEST
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TO ENSURE THE CLEANLINESS AND PURITY IN THE HYDRAULIC SYSTEM
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STATE THE PURPOSE OF THE BLADE INSPECTION METHOD INDICATOR
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IN THE LEADING EDGE OF THE BLADE IS A SPAR THAT RUNS THE LENGTH OF THE BLADE. THE SPAR CONTAINS NITROGEN AND IF THERE IS A LEAK IN THE SPAR THE BIN WILL CHANGE TO 3 BLACK LINES
THE BM UNDER PROPER CONDITIONS IS WHITE |
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STATE THE PURPOSE OF CONDUCTING FLIGHT CONTROL RIGGING
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TO BRING FLIGHT CONTROL PERIMETERS INTO STRAIGHT LEVEL FLIGHT AS SET BY THE FACTOR
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STATE THE PURPOSE OF A TATICAL PAINT SCHEME
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THE PAINT DESIGN IS FOR EACH A/C TYPE TO REDUCE VISUAL DETECTION BY MATCHING REFLECTION OF OPERATION AL SURROUNDINGS
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STATE THE TWO METHODS OF LOCKING AND UNLOCKING THE TAIL WHEEL LOCKPIN
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MANUALLY, ELECTRICALLY
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STATED THE FACTORS THAT AFFECT HELICOPTER FLIGHT
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LIFT: COUNTER ACTS THE FORCE OF WEIFHT CAUSING THE HELO TO RISE
WEIGHT: FORCE OF GRAVITY PULLING DOWN THE HELO DRAG: FRICTION OF AIR PUSHING ON THE HELO THRUST: COUNTER ACTS THE FORCE OF DRAG CAUSING HELO TO GO FORWARD |
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STATE THE LOCATION AND PURPOSE OF THGE MAIN ROTOR HEAD DAMPERS
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BETWEEN EACH SPINDLE AND HUB. PURPOSE TO REDUCE THE LEAD AND LAG OF THE MAIN ROTOR BLADE AND ABSORB MAIN ROTOR HEAD START LOAD
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STATE THE TYPE MODEL AND CHARACTERISTICS OF THE ENGINE USED IN THE MH60S
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T700-GE-401C FRON DRIVEN TURBO SHAFT ENGINE
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STATE THE DIFFERENT PNEUMATIC SOURCES FOR ENGINE START
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OUT SIDE AIR SOURCE
APU ENGINE CROSS BLEED |
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STATE THE PURPOSE OF THE INLET PARTICLE SEPARATOR
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TO PREVENT FOREIGN PARTICLES FROM ENTERING THE COMPRESSOR.PROVIDES CLEAN AIR FOR THE ENGINE
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STATE THE PURPOSE OF THE HOVER INFARED SUPPRESSION SYSTEM
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INSTALLED ON MH60S MODEL REDUCES EXHAUST GAS RADIATION AND LINE OF SIGHT HOT SURFACES
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STATE THE FIVE MAIN COMPONENTS OF THE H 60 POWER TRAIN
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MAIN TRANSMISSION MODULES
DRIVE SHAFTS OIL COOLER INTERMEDIATE GEARBOX TAIL GEARBOX |
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DEFINE THE FOLLOWING OHMS LAW
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THE CURRENT(I) IN A CIRCUIT IS DIRECTLY PROPORTIONAL TO THE VOLTAGE (E) AND INVERSELY PROPORTIONAL TO THE RESISTANCE (R)
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DEFINE THERMOCOUPLE
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A JUNCTION OF TWO DISSIMILAR METALS THAT PRODUCE VOLTAGE WHEN HEATED
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ALTERNATING CURRENT
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CURRENT WHICH CONSTANTLY CHANGES IN AMPLITUDE, AND WHICH REVERSES DIRECTION AT REGULAR INTERVALS
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DIRECT CURRENT
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FLOWS ONLY IN ONE DIRECTION AND THAT THE NUMBER OF ELECTRONS FLOWING PAST A POINT IN A CIRCUIT IN ONE SECOND DETERMINES THE AMPLITUDE OF CURRENT
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STATE THE OUTPUT OF THE MH60S AIRCRAFT GENERATOR IN REFERANCE TO THE FOLLOWING PARAMETERS
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VOLTAFE 115 VOLTS A/C
3 PHASE FREQUENCY 400 HZ |
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STATE THE PURPOSE AND LOCATION OF THE AIRCRAFT BATTERY
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THE BATTERY IS UNDER THE CO PILOTS SEAT
THE PURPOSE 24 VOLTS DC NI CAD BATTERY PROVIDES PRIMARY SOURCE OF POWER TO START APU |
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CONTINUITY
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MAKES SURE THERE IS NO SHORTS OR BREAKS IN THE WIRE, FROM ONE END TO THE OTHER END OF THE WIRE
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VOLTAGE
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CHECKING FOR REQUIRED VOLTAGE AS SPECIFIED
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DIGITAL MULTIMETER
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MEASURE VOLTAGE, AMPERAGE, AND RESISTANCE OHMS ALSO DIODE CHECK
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DEFINE THE TERM PYROTECHNICS
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PYROTECHNICS ARE FIREWORKS ADAPTED TO MILITARY USE THE WORD PYROTECHNIC MEANS THE ART OF FIRE. THEREFORE PYROTECHNICS ARE ITEMS THAT PRODUCE EFFECT BY BURNING AND ARE CONSUMED IN THE PROCESS. PYROTECHNICS ARE USED IN THE MILITARY ARE ITEMS THAT PRODUCES A BRIGHT LIGHT FOR ILUMINATION OR COLORED LIGHTS OR SMOKE FOR SIGNALING
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MK 80 MOD O SIGNAL FLARE
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MK 79 MOD O SIGNAL FLARE KIT CONSIDST OF A MK 31 MOD O SIGNAL PROJECTOR A PLASTIC BANDOLEER THAT HOLDS 7 MK 80 MOD O SIGNALS DOWNED AIRCREW USE THE KIT AS A DISTRESS SIGNALING DEVICE EACH SIGNAL CONTAINS A SINGLE RED STAR ON ACTIVATION THIS STAR IS PROPELLED UPWARD TO HEIGHT OF BETWEEN 250 AND 650 FEET
THE STAR BURNS FOR A MINIMUM OF 4 1/2 SECONDS |
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MK 124 MOD O SIGNAL FLARE
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HAS TWO SIDES DAY(ORANGE) NIGHT (RED) BOTH SIDE LAST APPROX 20 SECONDS
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MK 25 MOD 4 MARINE LOCATION MARKER
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LAUNCHED FROM AIRCRAFT TO PROVIDE DAU AND NIGHT TIME REFERANCE POINTS FOR MARKING THE COURSE OF ENEMY SUBMARINES IN ANTISUBMARINE WARFARE. BURN FOR A PERIOD OF 10 TO 20 MINUTES
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MK 58 MOD O MARINE LOCATION MARKER
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USED IN SAR MAN OVERBOARD AND TARGET PRACTICE FOR BOMBING AT SEA
BURN FOR 40 TO 60 MINUTES |
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CODR CONVENTIONAL ORDNANCE DISCREPANCY REPORT
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STANDARD SYSTEM FOR REPORTING MALFUNCTIONS OR INDUCED DEFECTS INVOLVING LIVE ORDNANCE, AMMUNITION, EXPLOSIVES, EXPLOSIVE SYSTEMS AND DEVICES SUCH AS BOMB RACKS, MISSLE LAUNCHERS, GUN SYSTEMS, ROCKET LAUNCHER, SONOBUOY LAUNCHERS LEAKING OR SPILLED OTTO FUEL AND ARMAMENT WEAPONS SUPPORT EQUIPMENT
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EMR EXPLOSIVE MISHAP REPORT
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A REPORT THAT APPLIES TO EXPLOSIVE INCIDENTS INVOLVING CONVENTIONAL ORDNANCE, AMMUNITION, EXPLOSIVES, EXPLOSIVE SYSTEM AND DEVICES RESULTING IN ACTUAL UNINTENTIONAL DETONATION, FIRING, BURNING, LAUNCHING OF ORDNANCE MATERIAL LEAKING OF SPILLED PROPELLANT FUELS AND OXIDIZERS, OR CHEMICAL AGENTS RELEASED
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STATE THE PURPSE OF THE NAVAL ORDNANCE MAINTENANCE MANAGEMENT PROGRAM NOMMP
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IT ISSUES THE POLICIES PROCEDURES AND RESPONSIBILITES FOR ACTIVITIES SUPPORTING OR PERFORMING AIRBORNE WEAPONS MAINTENANCE
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DISCUSS THE SECTIONS OF A PASSENGER BRIEF
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SURVIVAL EQUIPMENT (PROPER WEARING AND USE)
ENTRY/EXIT PROCEDURES EMERGENCY PROCEDURES (CRASHING/DITCHING OVER LAND/ WATER, EMERGENCY EXITS DOOORS AND JETTISON ABLE WINDOWS) |
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STATE THE RATED CAPACITY OF THE CARGO HOOK
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9,000 LBS LIMITED TO 8,000 BY NATOPS DUE TO WEIGHT OF AIRCRAFT
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FAST ROPE
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MAXIMUM LIMIT OF TWO WHEN ATTCHED TO RESCUE HOOK OR SIX WHEN ROPE IS ATTACHED TO FRIES BAR TROOPS ON THE ROPE AT ANY TIME
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MCGUIRE RIG
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LIMIT OF TWO LINES DEPLOYED ON AIRCRAFT AND LIMIT OF ONE TROOP PER LINE AT ANY TIME
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SPECIAL PATROL INSERTION/EXTRACTION(SPIE)
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MAXIMUM LIMIT OF EIGHT TROOPS ON SPIE RIG AT A TIME
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CRRC COMBAT RUBBER RATING CRAFT
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THIS IS A MTHOD OF RAPIDLY INSERTING TROOPS AND A COMBAT RUBBER RATING CRAFT INTO OVER WATER AREAS
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BRIEFLY DISCUSS THE FACTORS TO BE CONSIDERED FOR RESCUE SWIMMER DEPLOYMENT
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A NUMBER OF SURVIVOR
B LOCATION OF SURVIVOR C VISUAL INJURIES D FLOATATION DEVICES INFLATED/ NOT INFLATED E PARACHUTE ENTANGLEMENT F SEA STATE G FUEL/DEBRIS IN WATER H SEA PREDATORS I FEASIBILITY OF ATTEMPTING RESUE J RESCUE ORDER |
