MH 60R Practice Test A Flashcards

1
Q

___________________ is a cancer causing agent (Airframes Safety).

A. Nitrous Oxide
B. Copper Beryllium
C. Aircraft Paint
D. Corrosion Preventive Compound

A

B. Copper Beryllium

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2
Q

The main rotor blade has a ________________ swept tips that provide both sound attenuation and increased rotor blade efficiency.

A. 20 degrees
B. 12 degrees
C. 22 degrees
D. 30 degrees

A

A. 20 degrees

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3
Q

The tail landing gear is of a cantilever deign, with an integral shock strut capable of _____________.

A. Swiveling 90 degrees
B. Swiveling 180 degrees
C. Swiveling 120 degrees
D. Swiveling 360 degrees

A

D. Swiveling 360 degrees

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4
Q

What are the two types of Auxiliary Power Unit’s (APU)?

A. Turbo Jet and Mach 1
B. Fischer and Garrett
C. Turbomach and Garrett
D. T-700 GE 401C and Turbomach

A

C. Turbomach and Garrett

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5
Q

The main tank system is composed of two cells interconnected to form one tank. The system capacity is _______________ usable gallons.

A. 686
B. 590
C. 800
D. 120

A

B. 590

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6
Q

There are ______________ different pneumatic sources for engine start.

A. 1
B. 2
C. 3
D. 4

A

C. 3

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7
Q

_______________ is the Aviation Hydraulics Manual.

A. NAVAIR 01-1A-17
B. A1-H60CA-490-100
C. A1-H60RA-NFM-000
D. NWP 3-50.1

A

A. NAVAIR 01-1A-17

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8
Q

There are ____________ hydraulic pumps on the MH-60R.

A. 2
B. 3
C. 4
D. 5

A

C. 4

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9
Q

T/F. The rescue hoist is hydraulically controlled, with an electrically powered back up winch that provides a means of rescuing downed personnel. It is located on the starboard side of the aircraft above the cargo door.

A. True
B. False

A

B. False

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10
Q

A measurement of cycles in a given period of time also referred to as frequency.

A. Current (I)
B. Voltage (E)
C. Resistance (R)
D. Hertz (Hz)

A

D. Hertz (Hz)

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11
Q

The ________________ smooches out the flight controls to enable the pilot to handle the aircraft.

A. Automatic Flight Control System (AFCS)
B. Stability Augmentation System (SASI)
C. Stabilator
D. Digital Automatic Flight Control System (DAFCS)

A

A. Automatic Flight Control System (AFCS)

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12
Q

The ______________ displays the radar altitude in a dial format with indicators for decision height and hover altitude bugs.

A. The Horizontal Situation Indicator (HIS)
B. The Altitude Direction Indicator (ADI)
C. The Radar Altimeter (RADALT)
D. Integrated Self-Defense System (IDS)

A

C. Radar Altimeter

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13
Q

T/F. An Explosive Mishap Report provides a standard system for reporting malfunctions or induced defects involving live ordnance, ammunition, explosives, explosive systems and devices such as bomb racks, missile launchers, gun systems, rocket launcher, sonobuoy launchers, leaking spilled or OTTO II fuel, and armament weapons support equipment.

A. True
B. False

A

B. False

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14
Q

The MK 58 Mod 0 Marine Location Marker is deployed from the aircraft to provide day or night, long burning reference point marks on the ocean surface for a period of _____________.

A. 10-20 minutes
B. 10-20 seconds
C. 40-60 minutes
D. 20 seconds

A

C. 40-60 minutes

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15
Q

The GAU-21 has an effective range of ______________.

A. 6500 meters
B. 1200 meters
C. 1850 meters
D. 950 meters

A

C. 1850 meters

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16
Q

Water supply bottles should filled at least every _______________.

A. 45 days
B. 35 days
C. 60 days
D. 7 days

A

B. 30 days

17
Q

Double Rescue Hook is designed to connect personnel and/or equipment to the aircraft hoist assembly during sea and land rescue operations. The double rescue hook consists of a large spring-loaded hook that supports _____________ pounds, a small spring loaded hook that supports _____________ pounds and a bottom ring which supports _____________ pounds.

A. 1000, 3000, 1500
B. 1500, 1000, 3000
C. 3000, 1000, 1500
D. 3000, 1500, 1000

A

C. 3000, 1000, 1500

18
Q

T/F. The components of the LPU-32 life preserver include a sea dye marker, whistle, chemlite, and manual/auto inflation.

A. True
B. False

A

A. True

19
Q

With the MH 60R configured for ASW, there are ___________ seats available and maximum passenger capacity of __________.

A. 3, 2
B. 2, 1
C. 2, 2
D. 3, 3

A

B. 2, 1

20
Q

SAR Condition II is ______________.

A. Alert 5
B. Alert 20
C. Alert 15
D. Alert 30

A

C. Alert 15