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40 Cards in this Set
- Front
- Back
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State the critical memory items for UNDERWATER EGRESS |
1.Emergency Breathing device -as required 2.cords - disconnect 3.door/window - open/jettison 4.place hand on known reference point 5.harness - release 6.exit helicopter after egress 7. swim clear of helicopter and inflate LPU |
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State the critical memoiry items for IMMEDIATE LANDING/DITCHING |
1. harness locked 2. seat up and aft 3. windows jettison as required 4.table up and locked 5.assume crash position |
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all essential engine electrical functions are powered by |
the alternator |
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what is the max launch and recovery gross weight for aviation ships |
23,500 |
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Ensure cable within limits, press (raise Switch) and report dome depth every____ |
15-20 seconds |
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Windows ______ not be installed or removed in flight, except during actual aircraft emergencies |
shall |
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SEL JETT ______ to jettison when less than 40 gallons of fuel (approximately ______ pounds) remain in tank |
Must be used / 272 |
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Aircrewman safety belts do not provide impact protection; therefore, use of the belts _____be restricted to only those occurrences when mission accomplishment requires personnel to be out of their seats. Such belts ______ be worn when strapped into a seat. |
shall / shall not |
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A head check _____ be conducted any time the BLADE FOLD switch is moved from the OFF position. |
May |
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Night/IMC dissent over water procedures______ be used for all dissents overwater at 1000' AGL or below. Descents____be commenced and conducted in a wings level attitude |
Shall / should |
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During dipping sonar transducer recovery and hover departure procedures, if cable angle exceeds inner ring prior to or when reaching___feet of dome depth, stop dome and center cable. |
120 feet |
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On the first flight following reeling machine installation, perform a daytime shallow dip cycle, lowering dome approximately____feet of water depth and raising to a seated position prior to sending transducer to depth. |
50 to 100 |
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Release of the load will be performed by the____or___electrically, the Aircrewman manually, or, in case of emergency, by use of the cyclic emergency release button. |
Aircrewman / PAC |
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Which weapons control procedure states: do not fire except in self-defense or in response to a formal order |
Weapons hold |
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NVD adjustment and focus procedures shall be conducted in accordance with the___USN/USMC NVD manual or the operations manual |
MAWTS - 1 |
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On launching from an aircraft carrier the helicopter____be rolled forward slightly to make sure chocks/tiedowns are removed. |
may |
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When the ON/OFF/ARM switch of the ELT is switched to ON, it translates a distress signal on____ |
282.8 243.0 |
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True or false: gravity fueling is authorized with APU operating |
False |
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Aircraft ____ not fly at low altitude over a burning Mk ____ marker. Ignition of the second candle can be forceful, with flame occasionally eject thing up to 50 feet |
Should MK-58 |
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The goal of ____is to improve mission effectiveness, minimize crew preventable errors, maximize crew coordination, and optimize risk management |
Crew resource management (CRM) |
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True or false: the SO shall maintain continuous calms with pilots concerning dipping sonar raising and lowering and any possible danger to the helicopter? |
True |
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After initial setting, the S0 cable angle pots should require __________ during subsequent dips if wind/C conditions remain constant and the AFCS LAT VEL and LONG VEL control knobs have not changed |
Minimum readjustment |
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The aircraft may maintain some degree of buoyancy in the fuel-cell transition section approximately _______ after water landing. |
2 to 5 minutes |
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Unfolding the sonar ray disables the____________ |
Bottom proximity sensor |
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See stepping operations after ______ consecutive faults requiring auxiliary modes of operation |
Two |
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If Dome is in air, do not attempt to lower TA into water with ________ selected. electro static discharge (ESD) sequence is bypassed and will result in damage to electronic components. |
Auxiliary hydraulic mode |
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The center rear seat shall be removed if_________ |
RAST probe is installed conducting VERTREP |
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Exceeding 8 KGS with array folded or 4 KGS with array unfolded may cause _____ |
TA cable séparation |
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Rigged for rescue checklist: radiation hazard exists to the rescue swimmer and survivor from the _______ |
APS - 147 radar APS - 153 radar |
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Define VERTREP call: load is not swinging, shifting, or oscillating |
Load riding well |
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Mode ______ is a civil air traffic control surveillance system that can respond to selective interrogations and provide air to air and air to ground data link of aircraft identification and flight parameters |
Mode S |
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_______ Is the maximum lateral angle of slope that can be negotiated in a takeoff or landing |
Critical rollover angle |
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It shall be the responsibility of the______ to ensure all ______ are adequately briefed before the flight |
HAC / PAX |
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Electromagnetic hazards: due to the adverse effects of EMI on aircraft operating in the vicinity of SPY-1 radars, MH-60R aircraft -_______ not close within 2 NM of CG or DDG class ships unless the SP Y – one is operating at low power, the controller has broken datalink, and the helicopter track has been dropped |
should
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The _____ attenuates the magnitude and reduces the duration of the peak vibratory loads produced by the main rotor at the main rotor blade passage vibration frequency
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Active vibration control system (AVCS) |
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When unstrapping to don safety belt, Aircrewman _________ report, "UNSTRAPPING" |
Shall
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During VERTREP, the ICS call for "jettison immediately". " load endangering safety of flight" is ___________________ |
Pickle pickle pickle |
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Do not toe the transducer in the water above _______ with array folded and _______ without array unfolded. |
8 KGS / 4 KGS |
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During VERTREP what is the voice call for "Load is clear of the deck and obstructions" |
Clear to go |
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Define: SWEEP for conducting overland operations. |
S - size, slope, suitability, surface W - winds E - Elevation E - egress P - power |
