Rotor Systems - NATOPS CH. 2.2 Flashcards

1
Q

What type of rotor head do we have?

A

Fully articulated

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2
Q

What component enables the blades to lead, lag, flap, etc?

A

Elastomeric bearings

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3
Q

How is the rotor head dampened?

A

Main rotor dampers that are supplied with nitrogen pressurized hydraulic fluid.

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4
Q

Where is the reservoir for the hydraulic fluid used to dampen?

A

1 gallon reservoir inside the main rotor mast.

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5
Q

WARNING: A sheared _________ _________ _____ will instantaneously deplete the reservoir, degrading all four main rotor dampers, and may result in _________ _________ or unusual vibrations on deck.

A

Hydraulic damper line

Ground resonance

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6
Q

How is the rotor controlled?

A

Flight control hydraulic servos, which move control rods attached to the swashplate assembly.

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7
Q

How does the rotating swashplate transmit flight control inputs to the main rotor?

A

Four pitch control rods

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8
Q

At what speed do the antiflspping restraints get pulled out?

A

35% Nr

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9
Q

At what speed do the droop stops get pulled out? When do they seat?

A

70% Nr

Approximately 50% Nr

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10
Q

What two things do the 20 degree swept tips on the blade provide?

A

Sound attenuation and increased rotor blade efficiency

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11
Q

The spar of the main rotor blade is pressurized with what?

A

Nitrogen

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12
Q

The tail rotor indexing system positions the tail rotor blades during pylon fold operations and prevents the tail rotor from windmilling in winds up to _______.

A

60 knots

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13
Q

CAUTION: Failure to hold the gust lock switch in the LKD or UNLK position for a minimum of ____ seconds during operation may result in a partially engaged gust lock without a gust lock caution, causing damage when the rotor is engaged.

A

5 seconds

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14
Q

What does the AVCS system consist of?

A

AVCC
Ten feedback accelerometers
VCAS

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15
Q

What does the VCAS system contain?

A

Electronics Unit
5 force generators

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16
Q

How long is the solution cycle for AVCS?

A

300 seconds

17
Q

CAUTION: The AVCS IBIT shall only be initiated with rotors ______ to avoid damage to dynamic components.

A

Static

18
Q

What is required for a Spread Light?

A

Blade lock pins engaged with main rotor index pinion retracted. Pitch locks retracted.

19
Q

What are required for Pylon Flight Light?

A

5 micro switches:
Pylon lock pin switch
Tail rotor blade indexer switch
5 degree switch
Two stabilator lock pin switches