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MH-60R HAC NOTECARDS > AFCS Functions > Flashcards

Flashcards in AFCS Functions Deck (44)
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1
Q

What does SAS do?

What is the difference between SAS 1 and 2?

What percent control do they have?

A

Senses acceleration and apples control to reduce the rate.

SAS 1 is Analog, SAS 2 is Digital. They are identical except for the hover aug/ gust alleviation and alt hold/ hover coupler provided by SAS 2.

They have 10% authority With each providing 5%.

2
Q

SAS 2 commands the collective inner-loop actuator by operating with ___________

A

RADALT, BARALT, APP/HVR and DEPART MODES ENGAGED.

3
Q

Which SAS must be manually disengaged by the pilot if it has failed?

A

SAS 1

SAS 2 will be turned off by the AFCC.

4
Q

Which trim servos are electric?

Hydraulic?

A

Yaw, collective

Pitch, roll

5
Q

Trim is limited in movement by _________

A

10% percent per second

6
Q

To disengage yaw trim above 50 kias the pilot must _________

Below 50 kias?

A

Push the cyclic button and the trim micro switches

Just the pedal micro switches

7
Q

Auto pilot does what?

A

Maintains pitch and roll attitude, airspeed, heading during cruise

And

Provides a coordinated turn above 50 kias.

8
Q

Attitude hold is engaged below _______, and using the 4-way trim switch will adjust pitch attitude at a rate of _________.

A

50 kias

5* per second

9
Q

Airspeed hold is engaged ___________. The 4-way trim switch will adjust the airspeed by ___________. The lateral trim roll rate is _________. It resets to __________ when you ___________.

A

Above 50 KIAS and AOB less than 30*

6 KIAS per second

6* per second

Wings level

Accelerate through 50 kias

10
Q

Heading hold is slewed at ____ below 50 kias and _______ above 50 kias.

A

3* per second

1* per click or 1* per second

11
Q

Heading hold is re-engaged when what 2 conditions are met?

A

Roll attitude is within 2* of wings level

Yaw rate is less than 2* per second

Disengaged by WOW switch.

12
Q

Altitude hold: The AFCC commands both the ____ and the ____ to maintain the reference altitude.

It will stop increasing power if torque hits _______ above 80 kias or ________ below 80 kias.

A

Collective SAS actuator and collective trim actuator

106%

120%

13
Q

Altitude that RADALT will work?

A

0 to 5000ft AGL.

14
Q

RADALT and BAR ALT require what push buttons to be engaged?

A

SAS 2, TRIM, and AUTOPILOT

15
Q

RADALT climb and descent rates?

A

1000 ft per minute

200 ft per minute

16
Q

What does hover augmentation/gust alleviation do?

A

Improves aircraft stability at low airspeeds by using attitude retention, longitudinal acceleration, and lateral acceleration to eliminate drift.

17
Q

Turn coordination is provided ______. It will engage when _________ and any of what 3 conditions exist?

A

Above 50 KIAS

Roll attitude is greater than 1*

And either:

1) lateral cyclic displacement is greater than 3%
2) Cyclic TRIM REL is pressed
3) roll attitude is more than 2.5* using 4-way trim

18
Q

The purpose of Maneuvering stability is to __________. It is provided by _________ between _______.

The ___________ push button must be engaged for it to function.

A

Increase pilot effort to maintain pitch rate at greater than 30* AOB

Pushing the cyclic forward by 1% for every 1.5* AOB. Between 30* and 75* AOB.

Autopilot

19
Q

Automatic approach assumes _______ when engaged and again at ________.

A

Wings level

80 KIAS

20
Q

The 4-way trim switch changes the deceleration rate by ________ during the automatic approach.

It will reset the deceleration profile at _____________. Pressing the ________ will reset the profile.

A

+- 1kt per second, 2 seconds for a full knot.

40KGS

TRIM REL

21
Q

Automatic approach profile numbers?

ON (above 40KGS and below 40KGS)

Below-

Above-

A

Above 40: 2.5kt/sec 215 ft/min

Below 40: 1.5kt/sec 130 ft/min

Below profile: 2.5 kt/sec w/RADALT hold

Above profile: 360 ft/min w/airspeed hold

22
Q

What is the Warning associated with an automatic approach?

A

If auto approach is turned on while in a trimmed turn it will spiral downward past the selected altitude and crash.

23
Q

Hover coupler speeds can be varied by ________ with the 4-way trim switch.

Hover coupler will automatically engage after an automatic approach when __________ and manually when within ________

A

+- 10

Within 2 ft and 1KGS
Or
5KGS

24
Q

The hover coupler will stop increasing the _______ at ________.

A

Collective torque

116%

25
Q

During couple hover if winds are greater than 50KIAS and the cyclic trim is depressed the ____________

A

Heading hold will be disabled. This could cause rapid deviation from the desired helicopter heading.

26
Q

Automatic depart, if not interrupted, will reach _____ and ______.

A

150ft and 120kias

27
Q

Automatic depart assumes __________ at _______ if bank angle is ________.

If bank angle is greater than ____.

Automatic departure will limit power at __________.

A

Wings level attitude, 50KIAS

Less than 5*

5* it will maintain a coordinated turn.

106 and 120% dependent on airspeed.

28
Q

Automatic departure profile?

A

240ft/min climb
3kt/sec below 85 kts

1kt/sec above 100 kts

29
Q

Crew hover control authority?

A

+- 5 KGS

30
Q

Cable angle is decoupled from the AFCS for ____ when dome raising/lowering is stopped or started in the water.

A

9 seconds

31
Q

Scale on the cable angle display is _________. The rings are at _____ and ______.

A

2 degrees per tick

  1. 25 degrees
  2. 5 degrees
32
Q

CABLE ANGLE AT LIMIT caution appears when ___.

A

cable angle has exceeded 7.5 degrees total deflection.

33
Q

The helicopter will default to HVR mode at _________ during cable angle hover.

If either axis is failed it must be _________.

What should you not continue if both axis are failed?

A

27+- 12 ft water depth.

Manually controlled

Dipping operations.

34
Q

What is required for Cable Angle Hover Mode?

A

KGS of +-5

Altitude hold w/in 10 ft.

Dome wet indication.

35
Q

The ______ are inoperative when CABLE ANGLE HOVER is engaged.

A

LONG VEL and LAT VEL potentiometers.

36
Q

Cable angle takes ______ to come up with a solution.

A

25 seconds. Do not make inputs during this time.

37
Q

Cable angle hover will not _________ with ____________ engaged.

A

Disengage

Cable angle override on. (Must be manually disengaged)

38
Q

To conduct AFCS preflight checks you need:

WERBS

A
WOW
Engine torque below 10%
Rotor brake ON
Both EGIs attitudes valid
SAS 1 ON (AFCC must be on for at least 20seconds)
39
Q

If one of the SAS channels fail, what is the operable control authority is the operable channel limited to?

A

+-5 percent authority, but it operates at twice the normal gain to compensate for the failed SAS channel

40
Q

When does the SAS caution appear?

A

Whenever SAS 1 and SAS 2 lose electrical power or when hyd pressure is lost to the actuators.

41
Q

Is Trim an outer-loop functions, or inner-loop?

A

Outer-loop

42
Q

Cable angle is used to keep the cable ____ to the water.

A

Perpendicular

43
Q

What does the SUBM OVRD button do?

A

Provides override capability of the 27+-12 ft submerge requirement to engage cable angle hover mode. (in case you’re dipping in shallow water or don’t have the dome wet indication.)

44
Q

How do you initiate the automatic preflight check?

A

by pressing the SAS 1 pushbutton. Takes approx 10 seconds to complete.