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HH 60L > -10 Test > Flashcards

-10 Test Flashcards

0
Q

During operation of the air conditioner system the right cabin door should remain closed. If opening is required the cabin door should not remain open for more than _____ minutes due to heat from ECS.

A

One minute

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1
Q

To enable emergency exit keep Center medical seat facing to the ____ unless litter pans and or ambulatory seats in full up position.

A

Rear

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2
Q

ECS operations involving the use of heat mode: do not remove main power from the ECS without first turning the ECS switch off and waiting ______. Failure to do so may result in an extreme over temperature condition of the heater element.

A

60 seconds (ref: pg 2-59; para 2-58)

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3
Q

T/F Either main generator or ground power unit must be connected to the helicopter for operation of the ECS air conditioning.

A

True

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4
Q

Operation of the ECS causes an approximately _____ loss in helicopter power available

A

One percent

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5
Q

T/F Use of the ECS may cause an inadvertent power on reset command to the SAS FPS computer, illuminating the FPS and trim cautions and the CPTR advisory on the AFCS Control Panel

A

True

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6
Q

T/F Three pilot defined fight Plans are available in the AMS?

A

True (ref. 3-45 para. 3.12.1)

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7
Q

The major components of the ECS are started in spaced intervals to prevent power surges, which results in a delay of up to ____ between turning the system on and feeling cooler air through the vents.

A

30 seconds (p. 2-61 para. 2.58.2)

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8
Q

The bearing pointer no. 1 operates in conjunction with:

A

TACAN & Doppler GPS

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9
Q

T/F Master cautions will appear if both MFDs have failed?

A

False (p. 2-87; para 2.78)

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10
Q

T/F The CDU cautions and advisories are available in the event of a dual MFD failure.

A

True (9-24 para 9.32.4)

AC-ESS, ACC LOW, #1 and #2 PRI SERV, # 1 & #2 T/R SERVO

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11
Q

On the status line of the CDU a _____ indicates that the CDU is the bus controller

A

Boxed B

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12
Q

T/F The first CDU to finish up BIT becomes the bus controller while the other becomes the remote terminal.

A

TRUE (3-10)

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13
Q

T/F. Each pilot must individually select the local datum for CDU position entry and presentation that corresponds to the horizontal datum listed on the tactical map being used for the mission.

A

True (3-10)

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14
Q

Navigation information is processed based on the BC CDU active datum, ignoring the datum of the RT CDU.

A

True (3-10)

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15
Q

Use the _____ setting whenever the ASN-43 Compass System is set to ______.

A

AUTO; SLAVED

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16
Q

On the AN/ARC 222 radio (COM 3) band frequency range is from ____ to _____ MHz.

A

108.00 to 135.975

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17
Q

On the AN/ARC-222 radio, the POLC band frequency range is for. ____ to ____ MHz.

A

136.000 to 173.995

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18
Q

T/F. Crypto functions are available for COM 3 in emergency operations

A

False ( p.3-32)

Only FM Single channel, VHF single channel, police and marine bands are available

19
Q

Placing the EMERG COMM switch to EMERG COMM disables the CDUs and tunes ____ radios to Guard (243.0).

A

COM 2 (AN/ARC 164 UHF AM/FM)

20
Q

T/F. There is no connection between the AMS and the helicopters fuel measuring system.

A

True (p. 3-57, para. 3.12.5.3

21
Q

If operating in Doppler only mode without flyover updates for more than _____ minutes, a DOP UPDT RQD alert appears on the CDU status line.

A

15 ( pg. 3-60 par. 3.13)

22
Q

Navigation information consisting of bearing and slant distances to station are available in what modes on the TACAN?

A

Normal Operation Transmit / Recieve mode (pg. 3-70)

23
Q

The Storm scope weather mapping antenna senses _____ associated with a storm cell.

A

Electrical discharges (p. 3-78)

24
Q

If the helicopter external source (gyro) fails, the _____ feature on the storm scope should be turned off manually.

A

HDG Stabilization

25
Q

What is the warning associated with the AN/AQ-22 FLIR?

A

The FLIR shall not be used for pilotage (pg. 4-19)

26
Q

Allow _____ minutes for the FLIR to reach operating temperature. Do not move the controls until READY is displayed.

A

Three to five (pg. 4-21)

27
Q

Rescue hoist speed is variable from ___ to____ in the cabin control.
Pilot has fixed rate control of ______.

A

0 - 350 fpm

100+-20 fpm (p. 4-41)

28
Q

The hoist contains _____ feet of usable cable.

A

290 (pg. 4-37)

29
Q

What are the pre operational checks for the rescue hoist?

A
  1. Preflight extraction devices
  2. Visually check hoist unit structure and support for defects, cracks,a or material surface imperfections.
  3. Check hook unit assembly for free swivel, keeper retention in closed position, and damage free condition
  4. Check bumper for proper resilience and shock absorbing capacity
  5. Check fairings and covers for proper attachment
  6. Check electrical connectors for installation and security.
30
Q

When reeling in the cable without a load, apply tension with gloved hands to ensure smooth and even wrapping. A minimum of _____ pounds tension is recommended.

A

25 (p. 4-40, note)

31
Q

T/F. POWER WILL BE REMOVED FROM ECS WHEN HOIST POWER SWITCH IS PLACED ON.

A

True (p. 4-41 note)

32
Q

T/F. Rescue hoist operational daily checks prior to use require that the backup pump be off to facilitate use with APU power.

A

True

33
Q

T/F. The rescue hoist shear capability is disabled on the ground.

A

False it is active (p. 4-42)

34
Q

To configure the cabin for cargo, move the litter platforms

A

All he way to the ceiling (p. 4-77)

35
Q

The OBOGS will charge from empty in _____ minutes with either the APU or engine bleed air power.

A

30 minutes (p. 4-71)

36
Q

OBOGS is fully operational with either APU power or when engines apply greater than _____ torque.

A

30% (p. 4-71)

37
Q

When bleed air is removed from the system, a self contained backup oxygen supply (BOG) with a capacity of _____liters, provides _____ minutes of oxygen to six litter patients at 3 liters per minute.

A

260; 15 (p. 4-71)

38
Q

Due to mechanical limits, the litter platforms must not be tilted, from their horizontal position more than ____.

A

17 degrees (p. 4-74)

39
Q

The ARS-6(V)3 PLS provides the pilot with heading and distance information to locate survivors with a transmitting CSEL radio set.

A

TRUE (p. 3-71)

40
Q

What are the nose down up left and right wheel upslope limits?

A

6 degrees nose up
15 degree left or right wheel upslope
6 degrees nose downslope (15 degrees max tailwind downslope)
Slope limits reduced 2 degrees every 5 kts of wind

41
Q

The drag multiplying factor for the HH60L configuration is ______.

A

0.53 (p.7-147)

42
Q

What is the underlined step in the EP for dual CDU and dual MFD failure?

A

Land as soon as possible (p. 9-23)

43
Q

What are the steps in the EP for single CDU failure?

A
  1. Verify operating CDU is the bus controller

If operating CDU is not the BC

  1. On the EMERGENCY CONTROL PANEL place the CDU 1 AUTO CDU 2 switch to the good CDU
  2. Check status of the good AMS
    p. 9-24
44
Q

What is the emergency procedure for hoist runaway?

A
  1. Pilots hoist control panel PILOT OVERRIDE switch UP or DOWN as required

If control is not possible

  1. Pilots hoist panel HOIST POWER switch-OFF
45
Q

What are the underlined steps in the EP for litter lift runaway?

A

From any one of the four cabin medical control panels:

  1. EMERGENCY STOP switch - STOP

If litter continues to runaway:

  1. Cockpit AUX SW panel MED INT switch - OFF

HH 60L (5 decks)

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