NATOPS Chapter 9 Special Procedures HSM-50 Flashcards

1
Q

To avoid Electomagnetic Interference with the RMCU do not dip with in _______ of naval vessels

A

1 mile

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2
Q

Sonar cable shall ___________________ in HVR mode once the DOME SUBMERGED light is on.

A

Not be payed out

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3
Q

Order that control inputs should be made in to correct the dome position?

Time for solution?

A

4-way trim
Fly against lateral trim
Use TRIM REL button
Fly against longitudinal trim

25 seconds

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4
Q

How long does it take for the longitudinal solution to reincorporate after being removed?

A

20 seconds

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5
Q

A rise in ____ TGT could be indication of ________? A rise greater than ________ may result in compressor stalls.

A

20* C

Engine degradation and salt encrustation

40* C

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6
Q

Do not decelerate below _______ until within 90* of the ________.

Do not descend below __________ until into the wind.

A

50 kias, windline

90ft

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7
Q

Bottom proximity on the dome is inactive when __________ or __________.

A

Unfolded

SUBMRG is not indicted.

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8
Q

While training the Aux Hyd and Aux Elec modes for the reeling machine shall only be used for __________________.

A

Maintenance checks

Simulating EPs

Actual EPs

Dome shall remain in the water during operation unless actual EP.

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9
Q

Maintain _____ rotor distance from a parachute.

Use caution if there could be fuel near the crash site. The helicopter needs to be _________ due to ______________ build up.

A

1

Grounded, static electricity

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10
Q

What are the 5 methods to effect a rescue?

A
Landing 
Rescue via 1 or 2 wheels
Hoist
Rappelling
Direct Deployment
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11
Q

1 or 2 wheel landing require _______________.

A

Operational Necessity

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12
Q

Vertrep power margin of _______ provides increased safety and controllability.

A

6%

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13
Q

Loss of tail rotor Authority is manifested in what 2 ways?

A

No yaw response with left pedal.

Uncommanded right yaw

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14
Q

SWEEP checks stand for what?

A
Size, slope, suitability, surface
Winds
Escape routes
Elevation of LZ
Power available
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15
Q

Hover checks shall include

A

Sync BARALT

Check TGT/Torque

OEI intentions

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16
Q

Gate position

A

Into wind, wings level, FTP on nose

17
Q

Daytime dipping engage hover mode when

A

Less than 5 KGS

18
Q

Steady coupled hover

A

70 ft, less than 4 KGS

19
Q

Cable angle hover engages when

A

27 +/- 12 ft

20
Q

What had to be manually disengaged if in submerged override

A

Cable angle hover mode

21
Q

Requirements for cable angle hover

A

KADADA

KGS +/- 5
Altitude within 10 ft of selected (pots)
dome wet indication
AFCS degraded not illuminated
Depart or crew hover not activated
Auto pilot on