Digital Autopilot Flashcards

1
Q

what is minimum altitude for engagement?

A

500 AGL provided below 180IAS and one pilot has control wheel

1000 AGL otherwise

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2
Q

what flap setting can we use with the AP engaged?

A

1 or up

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3
Q

when is the only time the A/P can be engaged below 1000ft?

A

coupled approach

or down to 500 AGL with one pilot on control wheel, except for coupled approach

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4
Q

what is max airspeed for autopilot operation?

A

Vmo

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5
Q

what is minimum airspeed for autopilot operation?

A

85IAS in IAS mode or Vmc in any other mode

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6
Q

when can we not use altitude hold mode?

A

in severe turbulence

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7
Q

what must we do with the autopilot when flying in non-certificated/icing conditions?

A

disengage

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8
Q

what is the roll command limit?

A

+- 25 degrees

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9
Q

what is the pitch command limit?

A

+18 degrees -15 degrees

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10
Q

what 6 conditions will cause the AP to automatically disengage?

A
  1. electrical power failure
  2. AFGS failure
  3. AHRS failure
  4. STALL warning
  5. pitch and/or roll servo failure disengages the AP only
  6. yaw servo failure disengages the yaw damper only
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11
Q

what is a hardover?

A

A servo failure, the pilot will recognise that the airplane leaves the intended flight path

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12
Q

what action should we take with the yaw damper if the engine fails?

A
  1. disconnect the yaw damper
  2. retrim
  3. reconnect yaw damper
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13
Q

what will we see if we have a DCU failure?

A

amber boxed DCU indication is displayed on the PFD and all flight guidance info is lost on the pilots and co pilots PFD

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14
Q

what signals a trim runaway?

A

TRIM IN MOTION aural announcement triggered by a 12 second auto trim motion

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15
Q

what will stay active if VOR/LOC signal becomes invalid or is lost?

A

lateral NAV/APPR modes

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16
Q

when must the autopilot be disconnected on an ILS coupled approach?

A

before a descent through 150ft AGL

17
Q

can we operate the autopilot with a DCU failure?

18
Q

what will we hear if the AP is switched off then back on within a couple of minutes?

A

a beep tone

19
Q

what can we expect if flying a coupled approach that doesn’t start from the normal FAP/FAF?

A

slightly more roll and pitch motion than normal at DA

20
Q

what provides roll, pitch and body acceleration data to the autopilot?

A

2 AHRS’s on an ARINC 429 bus via 2 AHRS systems installed in the aircraft

21
Q

what provides air data such as altitude, IAS and vertical speed to the autopilot?

22
Q

what provides flap position info to the autopilot?

23
Q

what provides pitch trim up and down commands?

24
Q

what does the flight guidance computer do?

A

controls roll, pitch and yaw axes through selected modes of operation

25
what does the flight guidance control panel do?
provides push buttons to select flight director/autopilot modes
26
what are the AP servos used for?
as an interface of the flight guidance computer to the aircraft control systems
27
what does each servo incorporate?
a DC motor, capstan and digital bus interface electronics
28
if the FD is disengaged and we engage it with no preselected modes, what will it default to?
pitch and roll it will hold the roll if greater than 5 degrees or level the wings if less than 5
29
what does the yaw damper do when engaged?
dampens any excessive yaw and coordinates turns
30
when must the yaw damper be disengaged?
T/O and landing
31
what nav sources does the AP use in NAV mode?
VOR 1/2 FMS
32
what happens in NAV mode if the reference signal fails?
NAV mode fails until the signal is valid again
33
if in NAV mode the reference signal is lost what will the autopilot hold?
last known crosswind corrected course
34
when will GS mode arm on the approach?
half scale delfection
35
what does half bank mode do?
reduces maximum bank angle to 12.5 degrees
36
if on the ground what will pressing TOGA do?
- 11.2 degree pitch up command - roll hold at wings level as default - ROLL and PITCH indications on EFIS - change to HDG mode when HDG is pushed - change to NAV mode when NAV is pushed