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IQT > Contact/Remotes > Flashcards

Contact/Remotes Flashcards

1
Q

Maximum touchdown sink rate is ___ ft per minute on level terrain and ___ ft per minute on slopes for helicopters weighing LESS than 16,825

A

540ft Level Terrain

360ft Slopes

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2
Q

Maximum touchdown sink rate is ___ ft per minute on level terrain and ___ ft per minute on slopes for helicopters weighing MORE than 16,825

A

300ft Level Terrain

180ft Sloped Terrain

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3
Q

All slope limits shall be reduced by __ degrees for every 5 knots of wind.

A

2 degrees

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4
Q

Nose upslope, right wheel upslope, and left wheel upslope landing limit is __ degrees.

(10 for ski equipped aircraft)

Nose downslope landing limit is ___ degrees.

A

Nose up, right, and left is 15 degrees

Nose down is 6 degrees

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5
Q

High Recon is performed at ___ft Above Site Elevation (ASE) at a min speed of ___ KIAS

v3

A

150 ft ASE

50 KIAS

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6
Q

Low Recon is performed at ___ft Above Highest Obstacle (AHO) at a min speed of ___ KIAS

v3

A

50 ft AHO

50 KIAS

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7
Q

A Marginal Power Takeoff uses a target torque value of __ ft hover power and a simulated __ ft obstacle

A

10 foot hover power / 50 foot simulated obstacle

terminate above SEAS or 80 kts

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8
Q

A Maximum Performance Takeoff uses a target torque value of OGE + __% power and a simulated __ ft obstacle

A

OGE + 5% / 100 foot simulated obstacle

terminate above SEAS or 80 kts

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9
Q

A Rolling Takeoff uses a target torque value of __% below __ ft hover power

A

10% below 10ft hover power

terminate above SEAS or 80 kts

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10
Q

A normal approach will be initiated from ___ AGL and __ KIAS using a __ degree apparent angle

A

300 ft AGL

80 KIAS

30 Degree apparent angle

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11
Q

A shallow approach will be initiated from ___ AGL and __ KIAS using a __ degree apparent angle

A

300 ft AGL

80 KIAS

10 Degree apparent angle

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12
Q

A steep approach will be initiated from ___ AGL and __ Knots ground speed using a __ degree apparent angle

A

300 ft AGL

50 Knots ground speed

45 Degree apparent angle

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13
Q

A roll on landing uses an entry airspeed no less than ____, or 70 KIAS. Max touchdown speed is __ Knots ground speed.

A

No less than safe SEAS

60 Knots ground speed

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14
Q

What is the max ground taxi speed?

A

15 knots ground speed

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15
Q

Do not taxi within ___ ft of a refueling operation

A

50 feet

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16
Q

When anticipated power margin is __ % or less, a second crewmember will reconfirm power computations

A

10%

17
Q

The aircraft may be flown with __ strobe light inoperative.

A

one

18
Q

What kind of power is required for a ridgeline or pinnacle landing?

A

OGE hover power

19
Q

What kind of power is required for a CLEAR escape route?

Training and Operational

A

Training: Power available must be equal to or greater than power required for intended hover +5%

Operational: Power available must be equal to or greater than power required

20
Q

What kind of power is required for a RESTRICTED escape route?

Training and Operational

A

Training: Power available must be equal to or greater than OGE hover power +5%

Operational: Power available must be equal to or greater than OGE hover power

21
Q

What kind of power is required for water operations?

Training and Operational

A

Training: Power available must be equal to or greater than OGE hover power +5%

Operational: Power available must be equal to or greater than OGE hover power

22
Q

What kind of power is required for Restricted Visibility Operations?

Training and Operational

A

Training: Power available must be equal to or greater than OGE hover power +5%

Operational: Power available will not be less than 10 foot hover power +5%

**If the LZ has a restricted escape route, OGE power must be available

23
Q

Name the 4 prohibited procedures/maneuvers in training

A

Actual engine shutdown in flight

Deliberately entering vortex ring state or power settling

Dual DEC malfunctions

Intentional removal of primary A/C power in flight

24
Q

In regards to traffic patters, downwind legs will be flown at ___ft AGL and ___ KIAS

During the turn to base, descend to ___ft AGL and slow the aircraft to __ KIAS

A

flown at 500ft AGL / 100 KIAS

turn to base descend to 300ft AGL and 80 KIAS

25
Q

Do not initiate a stab malfunction when the aircraft attitude is greater than __ degrees nose low

A

10 degrees

26
Q

When initiating BOOST/SAS OFF, initiate on the ground or in straight and level flight at a minimum of __ft AGL and __ KIAS

A

300ft AGL

80 KIAS

27
Q

When going to DEC lockout, initiate on the ground or in flight at a minimum of ___ AGL and __ KIAS

A

300ft AGL

80 KIAS

28
Q

Practice Autorotations: Throttles will remain in ___

A

Fly

29
Q

Practice Autorotations: Aircraft heading will be no greater than __ degrees from the wind direction when winds exceed 15 knots and no greater than __ degrees from the wind direction when winds are 15 knots or below.

A

No greater than 45 degrees from the wind direction when winds exceed 15 knots

No greater than 90 degrees from the wind direction when winds are 15 knots or below

30
Q

The minimum entry altitude for a 91 degree - 180 degree autorotation is ___ft AGL

A

800ft AGL

31
Q

The minimum entry altitude for a straight ahead to 90 degree autorotation is ___ft AGL

A

500ft AGL

32
Q

The minimum entry altitude for a low altitude autorotation is ___ft AGL

A

100ft AGL

33
Q

Minimum autorotation entry airspeed is __ KIAS and Rotor RPM within limits

A

80 KIAS

34
Q

Maximum offset angle from intended termination point is __ degrees

A

30

35
Q

For an autorotation the aircraft must be wings level, have a minimum of __ KIAS, rotor RPM within limits, and be aligned for landing/recovery heading at no lower than ___ft AGL.

If any of these conditions are not met, initiate a power recovery immediately

A

min 80 KIAS

no lower than 150ft AGL

36
Q

Rate of descent with a hoist load is limited to ___ft per minute

A

1000 feet per minute

37
Q

The ambient temperature range for operation of the Breeze eastern and Lucas Western external rescue hoist is ___ - ___ degrees C

A

-40 - +60 degrees C

38
Q

Power required to hover can vary significantly (greater than __% torque) in light winds, due to their unpredictable nature

A

5% TQ

39
Q

A __ - __ knot crosswind or tailwind may increase torque required by up to __% over zero wind values

A

3 - 5 knot crosswind may increase torque required by up to 5% over zero wind values

IQT (9 decks)

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