Contact/Remotes Flashcards

(39 cards)

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

17
Q

The aircraft may be flown with __ strobe light inoperative.

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
Do not initiate a stab malfunction when the aircraft attitude is greater than __ degrees nose low
10 degrees
26
When initiating BOOST/SAS OFF, initiate on the ground or in straight and level flight at a minimum of __ft AGL and __ KIAS
300ft AGL 80 KIAS
27
When going to DEC lockout, initiate on the ground or in flight at a minimum of ___ AGL and __ KIAS
300ft AGL 80 KIAS
28
Practice Autorotations: Throttles will remain in ___
Fly
29
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.
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
The minimum entry altitude for a 91 degree - 180 degree autorotation is ___ft AGL
800ft AGL
31
The minimum entry altitude for a straight ahead to 90 degree autorotation is ___ft AGL
500ft AGL
32
The minimum entry altitude for a low altitude autorotation is ___ft AGL
100ft AGL
33
Minimum autorotation entry airspeed is __ KIAS and Rotor RPM within limits
80 KIAS
34
Maximum offset angle from intended termination point is __ degrees
30
35
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
min 80 KIAS no lower than 150ft AGL
36
Rate of descent with a hoist load is limited to ___ft per minute
1000 feet per minute
37
The ambient temperature range for operation of the Breeze eastern and Lucas Western external rescue hoist is ___ - ___ degrees C
-40 - +60 degrees C
38
Power required to hover can vary significantly (greater than __% torque) in light winds, due to their unpredictable nature
5% TQ
39
A __ - __ knot crosswind or tailwind may increase torque required by up to __% over zero wind values
3 - 5 knot crosswind may increase torque required by up to 5% over zero wind values