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HH-60G > HH-60G Vol. 3 > Flashcards

HH-60G Vol. 3 Flashcards

1
Q

How long is a preflight good for?

A

72 hours

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2
Q

Weather Minimums

A

Day: 700 ft. ceiling & 1 SM
Night Unaided: 1,000 ft. ceiling & 3 SM
Night Aided: 700 ft. ceiling, 2 SM

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3
Q

What is the minimum fuel quantity we are required to land with?

A

500 lbs.

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4
Q

Single ship LZ minimum

A

25 ft. clearance from any portion of the helicopter from the nearest obstacle

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5
Q

Multi-ship LZ minimum

A

Must provide one rotor diameter width between aircraft and 25 ft. of clearance from the nearest obstacle

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6
Q

When ambient illumination doesn’t meet NVG requirements, what are the minimums?

A

Non-mountainous: 500 ft. AGL
Mountainous: 500 ft. AHO within 2 NM of course centerline

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7
Q

How are mountainous areas defined?

A

An area of changing terrain where terrain elevation exceeds 3,000 ft. within 10 NM

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8
Q

What is the minimum HAAR altitude?

A

1,000 ft. AGL/AWL

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9
Q

What are the parameters for fuel dumping?

A

Must be at a minimum 3,000 ft. AGL, cannot be over agricultural or populated areas, and only in an emergency or out of operational necessity.

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10
Q

When will TOLD be computed and briefed?

A

Prior to takeoff

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11
Q

What is the maximum airspeed of forward flight with personnel attached to the rope ladder?

A

40 KIAS

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12
Q

How many strobes can be inoperative for flight?

A

One

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13
Q

What are the aircraft taxi restrictions?

A

Taxi no closer than 25 ft. without a wing walker, 10 ft. with a wing walker, and no faster than 15 knots ground

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14
Q

When will power have to be recomputed for verification of numbers? What might be needed after that?

A

When required power is within 10% of of available power. The use of contingency power for the T/O or landing.

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15
Q

Pinnacle power requirement

A

Operational/Training: OGE

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16
Q

Clear Escape Route power requirement

A

Operational/Training: 10ft. / 10ft. + 5%

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17
Q

Restricted Escape Route power requirement

A

Operational/Training: OGE/ OGE + 5%

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18
Q

Water operations power requirement

A

Operational/Training: OGE/OGE + 5%

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19
Q

Restricted Visibility operations power requirement

A

Operational/Training: 10 ft. + 5%/ OGE + 5%

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20
Q

High reconnaissance parameters

A

No lower than 150 ft. ASE and no faster than 50 KIAS

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21
Q

Low reconnaissance parameters

A

Minimum of 50 ft. AHO and a minimum of 50 KIAS or SEAS

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22
Q

Prohibited maneuvers

A

Actual engine shutdown, deliberately entering vortex ring state or power settling, dual DEC malfunctions, intentional removal of primary AC power

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23
Q

A minimum of _____ mainwheel clearance will be used for all contact hovering maneuvers.

A

10 ft. AGL

24
Q

Marginal power takeoff

A

10 ft. hover power w/ a simulated 50 ft. obstacle

25
Q

Maximum performance takeoff

A

OGE + 5% or as specified by IP and a simulated 100 ft. obstacle

26
Q

Rolling Takeoff

A

10 ft. hover power -10%

27
Q

Down wind legs will be flown at ____ and ____. During the turn to base, descend to ____ and slow the aircraft to ____.

A

500 ft. AGL/ 100 KIAS
300 ft. AGL/ 80 KIAS

28
Q

Normal Approach Parameters

A

300 ft. AGL, 80 KIAS, and a 30° apparent angle

29
Q

Shallow Approach Parameters

A

300 ft. AGL, 80 KIAS, 10° apparent angle

30
Q

Steep Approach Parameters

A

300 ft. AGL, 50 knots ground, and a 45° apparent angle

31
Q

Roll-on Landing Parameters

A

Entry airspeed cannot be more than 70 KIAS or SEAS, max touchdown speed is 60 knots ground

32
Q

What EPs are approved for contact training?

A

Single-engine training, stabilator malfunctions, boost/SAS off, and DEC lockout

33
Q

0-90° Autorotation Entry Altitude

A

500 ft. AGL

34
Q

91-180° Autorotation Entry Altitude

A

800 ft. AGL

35
Q

Aircraft heading will be no greater than ___ from wind direction when winds exceed ___ knots and will be no greater than ___ from wind direction when winds are ____ and below.

A

45°/15 knots
90°/15 knots

36
Q

Minimum Entry Altitude for Low Altitude Autorotation

A

100 ft. AGL

37
Q

What does WAR80 stand for? When does it apply?

A
  • Wings level, aligned for landing, RPM within limits, and minimum of 80 KIAS
  • When recovering from an autorotation. Must occur before 150 ft. AGL
38
Q

When must a power recovery be performed? When must it be terminated?

A
  • In case of excessive sink rate, rotor RPM out of briefed parameters, ineffective flare maneuver, or if a touchdown might occur.
  • No lower than 15 ft. AGL
39
Q

Night Autorotation Parameters

A

All crew members must be aided by NVGs and illumination must be at or above 40% when performing on an unlit surface.

40
Q

What are the standard crew call times for deploying personnel?

A

20, 10, 5, and 1 minute

41
Q

Minimum rotor diameter separation in formation is ____ rotor diameter. This is based on the ______ rotor disk in the formation.

A

1, largest

42
Q

Night turning rejoins are limited to ___ angle of bank and ____ .

A

20°/80 KIAS

43
Q

When flying in formation less than 3 rotor disk, what are the only authorized maneuvers?

A

Shackle, split, cover, and dig

44
Q

What two turns will not be accomplished at night?

A

Cross and center turns

45
Q

When conducting TFM maneuvers at night, what maneuvers must a rollout heading be called out for?

A

Break, split, hook, and tac turns

46
Q

Low illumination definition and restrictions

A

Defined as less than 10% illumination. Formation geometry will not exceed 1-3 rotor disk and 30° apparent aspect unless additional non-visual station keeping methods are used.

47
Q

Medium illumination definition and restrictions

A

Defined as a range between 10-40% illumination. Formation geometry will not exceed 1-10 rotor disks and a 45° apparent aspect unless additional non-visual station keeping methods are used.

48
Q

High illumination definition and restrictions

A

Defined as greater than 40% illumination. Minimum aircraft separation is 1 rotor disk. The maximum is based on environmental conditions, crew experience, threat situation, and mission requirements IAW AFTTP 3-3

49
Q

Minimum distance required between taxiing aircraft?

A

100 ft. of spacing from main rotor to tail rotor.

50
Q

During NVG water ops do not exceed ____ when below ____.

A

30° angle of bank, 100 ft. AWL

51
Q

The observation pass will be performed above translational lift and a minimum of ___. Do not perform during NVG water operations.

A

25 ft. AWL

52
Q

The FRIES bar must be extended and locked prior to _____.

A

Final approach.

53
Q

If requested by the deploying rope master, the aircraft may have a maximum forward ground speed of ___.

A

5 knots

54
Q

What are the primary and secondary rappelling attachment points?

A

Primary I the FRIES bar releasing mechanism. Secondary can be the upper cargo net restraint ring, cargo tie down ring, or opposite FRIES bar release mechanism.

55
Q

What is the maximum number of personnel allowed on the ladder?

A

3

56
Q

What is anticipated blind?

A

When terrain/environmental factors cause a loss of visual cues for a short duration or when visual cues are lost when using a pre-coordinated non-visual station keeping that provides sufficient situational awareness to ensure deconfliction

57
Q

What is unanticipated blind?

A

Visual cues required for formation separation no longer provide sufficient distance, aspect, or closure rate cues to ensure deconfliction. Could also occur when non-visual methods do not provide sufficient situational awareness to ensure positive deconfliction.

HH-60G (8 decks)

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