StudyGuide2019 Flashcards

1
Q

What is the maximum ramp weight when the helicopter is static, being towed, or being ground taxied under its own power?

A

9,590 pounds

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2
Q

Airframe components are labeled #____ for the left side and #____ for the right side.

A
  • 1
  • 2

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3
Q

Indirect deployments of the dewatering pump should be made no higher than ____ feet, to prevent damage to the pump.

A

25

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4
Q

While in a hover, indicated fuel is approximately ____ than actual fuel.

A

10% less

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5
Q

When the training switch is in idle 1 or 2, the selected engines N2 is reduced to ____?

A

320 rpm

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6
Q

The Gunners belt shall be worn around the _____.

A

Waist

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7
Q

The DECUs are powered by the engine driven alternators at _____% N1.

A

65%

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8
Q

The maximum speed for rotor brake applications is _____ RPM.

A

170

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9
Q

When using NVGs, altitudes for ___ to ____ are roughly the same as the unaided eye (depth perception).

A
  • 50 ft
  • 500 ft

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10
Q

During the start phase, automatic engine shutdown will occur if TOT reaches ____.

A

840 C

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11
Q

The HSD ____ be used for personnel deployments.

A

should

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12
Q

If winds are not within 20 degrees of either side of the nose, what is the maximum wind speed for rotor engagement?

A

35 knots

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13
Q

What is the minimum outside air temp for engine starts?

A

-25C

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14
Q

While in AEO, a red diode at 10.7 indicates max transient power, if ____ or _____ is the limiting parameter.

A
  • N1
  • TOT

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15
Q

In the normal torque flight limitation envelope, the FADEC stops torque at ____ on the FLI.

A

11.0

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16
Q

____ lbs is considered a heavy hoist load, and requires ____ seconds of rest.

A
  • 300-600
  • 30

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17
Q

What is the minimum safe distance for an operating HF antenna?

A

6ft

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18
Q

An engine is capable of an accumulated ____ seconds of operation in OEI HI.

A

30

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19
Q

The starter/generator starts providing 28 VDC when N1 reaches _____.

A

60%

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20
Q

Operation of the SX-5 search light should be avoided below ____ feet AGL.

A

10

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21
Q

Where is the hoist Static Discharge cable attached?

A

Equipment attachment rig on the hoist hook

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22
Q

What is the minimum ground crew required for hot refueling operations?

A

3

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23
Q

For specific guidance on NVG operations, refer to ____.

A

M3710.1

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24
Q

The portable fire extinguisher has a durations of _____ seconds and a range of _____ to _____ feet.

A
  • 10
  • 9-15

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25
Q

The FADEC system is designed to match ____.

A

N1

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26
Q

The RS seat shall remain in the ____ position for takeoff, taxi, and landings.

A

Neutral

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27
Q

Engine start is self-sustaining at approximately ____ N1.

A

45%

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28
Q

In the event of NR mismanagement, FADEC incorporates ____ safety features.

A

2

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29
Q

The rotor shaft transmits MGB output power to the tail rotor at approximately _____ RPM at a main rotor speed of 355 RPM.

A

4,000 RPM

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30
Q

The assumed breaking strength of the hoist cables is ______.

A

3,200 lbs

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31
Q

When performing external loads, angle of back should not exceed ____.

A

30 degrees

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32
Q

What is the recommended airspeed/altitude for SLDMBv3 deployment?

A
  • 45-120 kais
  • 100-500ft

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33
Q

Engine oil shall be above ___ before advancing the FCS to flight.

A

0 C

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34
Q

Shipboard landing are prohibited above _____.

A

8,900 lbs

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35
Q

Who clears an aircraft for further flight if damage is deemed minor and not a threat to the safety of the aircraft or crew?

A

Commanding Officer

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36
Q

Individual flight hours are cumulating unless ____ hours of rest are completed between sorties.

A

10 hours

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37
Q

At 100% N1, gas generator turns at approximately ____.

A

52,000 RPM

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38
Q

HIPSARM is only available if ____ or ____ is the limiting factor.

A
  • N1
  • TOT

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39
Q

The fuel transfer pump operates at ___ per hour.

A

600 lbs

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40
Q

The crotch strap shall be used at all times when the survivor is _____.

A
  • unconscious
  • unresponsive
  • incapacitated

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41
Q

Minimum water depth for SLDMBv3 deployment?

A

10 ft

Study Guide 2019

42
Q

Flight through or near thunder storms ____ be avoided.

A

shall

Study Guide 2019

43
Q

Aircraft personnel shall obtain permission from the ____ before donating blood or bone marrow.

A

Commanding Officer

Study Guide 2019

44
Q

NVG’s ____ be used whenever practical.

A

Should

Study Guide 2019

45
Q

N1C is directed to ____ and ____.

A
  • EBCAU
  • VEMD

Study Guide 2019

46
Q

The OIL TEMP light will illuminate on the WCA if either engines oil temperature reaches _____.

A

115C

Study Guide 2019

47
Q

An engine is capable of an ACCUMULATED ____ minutes of operation in OEI low.

A

2

Study Guide 2019

48
Q

Which fuel cell does not have a fuel gauge transmitter?

A

FWD Right

Study Guide 2019

49
Q

Practice of single engine maneuvers shall no be accomplished unless the aircraft gross weight is less than _____.

A

8,900 lbs

Study Guide 2019

50
Q

Avionics components are labeled #____ for the left side and #_____ for the right side.

A
  • 2
  • 1

Study Guide 2019

51
Q

Normal engine idle speed is _____ N1.

A

68%

Study Guide 2019

52
Q

What is the maximum pressure for single point pressure refueling?

A

55psi

Study Guide 2019

53
Q

When should the hoist hook be locked?

A
  • Rescue basket deployments and recoveries.
  • Rescue litter deployments.

Study Guide 2019

54
Q

Free fall deployment of the RS require ___ feet or water depth.

A

12 ft

Study Guide 2019

55
Q

Arming of the flotation system is recommended during over-water flight below ____ RADALT.

A

200 feet

Study Guide 2019

56
Q

A ____ certifies that a pilot or aircrew member has gained the training and experience necessary to perform basic operation of a specified aircraft type.

A

Study Guide 2019

57
Q

With all four floats deployed, the helicopter will remain afloat upright for ____ minutes in light seas.

A

4 minutes

Study Guide 2019

58
Q

How many levels of the FACED failures are there?

A

3

Study Guide 2019

59
Q

With NR HI selected, NR is increased to _____.

A

365 RPM

Study Guide 2019

60
Q

With aircraft power secured, the tail rotor isolate switch is in the ____ position.

A

Closed

Study Guide 2019

61
Q

With a flashing GOV, and T0.DISC A/B displayed as the failure, engine start is permitted so long as the temperature difference is more than _____.

A

5 degrees

Study Guide 2019

62
Q

After starting the aircraft with a flashing Gov and T0.DISC A/B, Prior to takeoff the temperature differential shall be less than ____, otherwise takeoff is not authorized.

A

15 degrees

Study Guide 2019

63
Q

Fuel may be jettisoned at speeds between ____ and ____ KIAS.

A
  • 40
  • 120

Study Guide 2019

64
Q

If an aircrewman flys 7.5 hours on a duty day, how many hours is he/she required to have off day?

A

10

Study Guide 2019

65
Q

How many ways are there to inflate the floats?

A

3

Study Guide 2019

66
Q

15 minutes after engine shutdown, the engine oil level should be from the MIN line to….

A

Bottom of the sight glass (visible without shaking)

Study Guide 2019

67
Q

IF the variable NR system fails, what does NR default to?

A

360

Study Guide 2019

68
Q

At the 10-foot cable extremities, hoist speed is limited to ____ feet per second.

A

50

Study Guide 2019

69
Q

SLDMBv3 ______ be deployed from a hover.

A

Shall not

Study Guide 2019

70
Q

Does a catenary hoist need to be pre-briefed?

A

No

Study Guide 2019

71
Q

Prolonged hovering (>1 min) is prohibited above ____.

A

9,200 lbs

Study Guide 2019

72
Q

What signal from the LSO is mandatory?

A

Waveoff

Study Guide 2019

73
Q

A minimum boost pump pressure of ___ is required before attempting an engine start.

A

8.5 psi

Study Guide 2019

74
Q

Max touchdown sink rate is ____ at 8,900 lbs.

A

600fpm

Study Guide 2019

75
Q

If a crewmember is lazed, the member should be assessed using the ___ grid eye chart.

A

Study Guide 2019

76
Q

What is the minimum safe distance from an operating radar?

A

7 feet

Study Guide 2019

77
Q

If attempting an in-flight restart, N1 must be below ____% N1.

A

17%

Study Guide 2019

78
Q

In the event of a dual boost pump failure on the #1 fuel system, the low pressure pump will continue to draw fuel from the system until approximately ____lbs are indicated on the VEMD.

A

280

Study Guide 2019

79
Q

In the event of a dual boost pump failure on the #2 fuel system, the low pressure pump will continue to draw fuel from the system until approximately ____lbs are indicated on the VEMD.

A

60 lbs

Study Guide 2019

80
Q

When making an approach to the water, do not exceed _____ decent rate at any time.

A

400 FPM

Study Guide 2019

81
Q

Hot refuel operations should not exceed a fuel load of ____.

A

1,500 lbs

Study Guide 2019

82
Q

Flight through known icing ____ be avoided.

A

shall

Study Guide 2019

83
Q

The engine oil capacity is approximately ____ gallons.

A

2 gallons

Study Guide 2019

84
Q

The battery may be cycled ____ in an attempt to clear a GOV light (before starting engines).

A

once

Study Guide 2019

85
Q

If either screen fails on the VEMD, which pages will be lost?

A
  • EPC
  • System status

Study Guide 2019

86
Q

HIPSARM is a ____ engine rating.

A

dual

Study Guide 2019

87
Q

The Transformer Rectifier receives power from the ____ AC system.

A

2

Study Guide 2019

88
Q

The best target identification altitude for the SX-5 search light is ____ to ____ feet AGL.

A
  • 500 ft
  • 1,000 ft

Study Guide 2019

89
Q

Once “go on hot mic, check swimmer” is given, the aircraft should be at or below ____ feet radalt if conditions permit.

A

30 feet

Study Guide 2019

90
Q

Turbulence penetration speed is _____ kias.

A

80 kias

Study Guide 2019

91
Q

With the MRH turning and full cyclic forward, what is the ground clearance at the nose of the aircraft for the MRH?

A

5ft 2 inch

Study Guide 2019

92
Q

During a rotor brake start, the engine will idle at ____% N1.

A

51-52%

Study Guide 2019

93
Q

Maximum hover altitude for free fall of the RS is ____ feet radalt.

A

15 feet

Study Guide 2019

94
Q

When assembling the quick splice, the bitter end of the cable shall ____.

A

Extend 3” past the plate

Study Guide 2019

95
Q

The cool switch should be on when the OAT is _____ or above.

A

10 degrees C

Study Guide 2019

96
Q

The use of the training switch is authorized while conducting minimum speed landings. (True/False)

A

False

Study Guide 2019

97
Q

Which AFCS channel is not required while conducting shipboard operations?

A

Collective

Study Guide 2019

98
Q

With aircraft power secured, the 2,000 PSI isolation valve is _____.

A

open

Study Guide 2019

99
Q

The airspeed indicator is unreliable below ____ knots.

A

25 knots

Study Guide 2019