Hyd SYS - 2 Flashcards

1
Q

where is the pedal adj handle?

A

on side of instrument panel

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2
Q

outputs from the cockpit controls are carried by mechanical linkage through the pilot assist servos

A

MMU

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3
Q

which panel has the tail servo and backup hyd switches

A

misc sw. panel

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4
Q

The MMU is designed to reduce

A

INHERENT CONTROL COUPLING

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5
Q

Name the four mechanical mixes provided by the MMU

A

Collective to: Pitch/roll/yaw
AND
Yaw to Pitch

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6
Q

Describe collective to pitch

A

MMU put fwd input to rotor disk to prevent nose-high attitude

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7
Q

Collective to yaw

A

MMU inputs left pedal to compensate for torque effect

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8
Q

Yaw to pitch

A

Aft input to M/R system as T/R pitch is increased. It compensates for vertical thrust

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9
Q

Collective/Airspeed to yaw

A

As collective and A/S increase, T/R pitch is decreased and vise versa

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10
Q

Collective to roll

A

MMU makes left rotor disk to compensate for translating tendency.

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11
Q

The SERVO OFF switch has an __ ___ to prevent both servo stages from being turned off

A

electrical interlock

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12
Q

5 lights that have to come on for backup pump to come on?

A
"ROY HAS TO HURRY AWAY "
#1 Reservoir
#1 Hyd pump
#1 T/R Servo
#2 Hyd pump
Accum low
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13
Q

With a leak, it takes how many seconds to lose both systems?

A

11-13

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14
Q

Servos are the only thing that can ___

A

jam or hardover

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15
Q

How long does the MMU minimize inherent control coupling?

A

by combining, summing and coupling collective pitch, roll and yaw inputs

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16
Q

What is the only trim actuator that receives hydraulic power from the number 2 hyd system

A

Pitch control

17
Q

why is collective/airspeed to yaw mixing completely phased out when the airspeed is above 100kts

A

efficiency of the T/R and the cambered fin

18
Q

Moving servo off SW from norm to 1st stg or 2nd stg will

A

turn off that stage of servos

19
Q

What is the reason for the depressurization valve to only connect to the backup pump?

A

to reduce output pressure of the pump upon startup of the electric motor

20
Q

the #1 hyd system supplies hyd fluid through its xfer module to what servos?

A

1st stage primary servos and first stage tail rotor servo

21
Q

Hyd leak test sw. allows testing of the _?

A

LDI

22
Q

What hyd pump is the depressurized valve on?

A

Backup hyd pump

23
Q

the rsvr 1/2backup low caution illuminates when?

A

when there is 60% fluid remaining in the reservoir (leak in the system)

24
Q

if a tail rotor cable breaks, what caution and/or advisory would appear?

A

T/R quad fail caution

25
Q

the #2 hyd system supplies pressure through the transfer mod to what servos?

A

2nd stage primary servos and the pilot-assist servos

26
Q

appearance of the boost servo off caution indicates?

A

loss of hyd pressure to the collective and/or yaw boost servo

27
Q

what is the purpose of the APU accumulator?

A

provide hydraulic charge to the APU starter motor

28
Q

in flight the backup pump mode automatically sets to ?

A

the auto mode is even on if the switch is in the off or on position

29
Q

what does the backup pump supply pressure to?

A

1 and/or #2 hyd system, 2nd stage tail rotor servo and APU accumulator.

30
Q

Name the trim actuators

A

yaw, roll, collective, pitch

31
Q

what FCC drives the trim actuator

A

FCC #2

32
Q

utility module

A

directs flow of pressure from the backup pump to the number 1/2 transfer module second stage tail rotor and apu accumulator.

33
Q

what piece isolates the primary servos?

located on the?

A

primary shutoff valve
transfer mods - after moving servo off sw.
(think primary servos primary shutoff valve)