Autoflight Flashcards

0
Q

The flight guidance system provides input to the ______ to position the command bars to be followed by the pilot flying.

A

PDF

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1
Q

The Primus autoflight system is divided into two systems:
_____________
_____________

A

Autoflight

Flight Guidance

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2
Q

The _________ button on the FGC is represented by a green arrow that indicates the ________ pilot.

A

couple

Flying

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3
Q

The Low Bank mode allows selection of a reduced bank angle from 27º down to ________ when the ______ mode only. The Low Bank mode is automatically selected when climbing above ________ feet and automatically cancelled when descending below __________ feet.

A

14º

HDG

25,000

24,750

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4
Q

The ____ mode is utilized for capturing VOR airways, FMS navigation and for GPS approaches.

A

NAV

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5
Q

The ______ mode is used for ILS and VOR approaches.

A

APR

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6
Q

When NAV mode is selected using FMS navigation, course capture is indicated left of the coupled arrow on the PFD by the caption _______.

A

LNAV

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7
Q

Basic _______ and ________ modes are controlled using the ______ knob and ___________ wheel located on the center pedestal.

A

ROL

PIT

Turn control

Pitch control

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8
Q

Pressing the ______ button allows the pilot to climb or descend at a desired airspeed which is set by using the _______ knob.

A

SPD

SPD

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9
Q

The _____ button allows the aircraft to climb at preset speeds of ____ knots below 10,000 and _____ knots above 10,000 feet until reaching _________ feet where the preset speed reverts to _______ mach. In descents, the preset rates are _______ fpm down to _______ feet and then a gradual reduction in the rate to ________ fpm below _________ feet

A
FLC
240
270
25,000
0.65
2,000
12,000
1,000
10,000
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10
Q

The ____ button allows the aircraft to climb or descend at a desired feet per minute which is set by using the _____ knob.

A

V/S

SPD

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11
Q

A desired altitude is set using the _________ ________ knob and is presented at the top of the altitude tape

A

altitude preselect

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12
Q

The normal flight guidance control selections for takeoff are _____ submode _____ and ______ bank

A

TO

HDG

LOW

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13
Q

The _________ submode provides for a fixed pitch of 14º nose up on takeoff with the flaps set at ____º, and is set while the aircraft is on the ground by pressing the _______ buttons

A

takeoff

9

Go Around

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14
Q

On the PFD, preselected lateral modes are presented on the _______ side of the couple arrow, and vertical modes are presented to the ______ side of the arrow.

A

Left

Right

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15
Q

Pressing the center of the heading select knob ________ the heading to the current heading

A

synchronizes

16
Q

An armed lateral or vertical mode is displayed in ______.

A

White

17
Q

A captured lateral or vertical mode is displayed in _________.

A

Green

18
Q

if the turn control knob is out of the center detent position, an amber _______ is presented on the PDF.

A

TKNB

19
Q

The autopilot can be disconnected by pressing the autopilot disconnect button or by activating the ____________.

A

Pitch Trim Button

20
Q

The autopilot is inhibited by pressing the ______ button on the control yoke and automatically reactivates once the button is no longer depressed

A

TCS

21
Q

If the autopilot is engaged, pressing the __________ button will disengaged the autopilot but not the __________.

A

AP or pitch trim

yaw damper

22
Q

Pressing the center of the speed select knob toggles the airspeed indication at the top of the airspeed tape between ____ and ______.

A

IAS

Mach

23
Q

When an armed mode transition to a captured mode, the transition is annunciated by a _____ around the mode for five seconds

A

Box

24
Q

A single engine go-around with the autopilot engaged is _______

A

Prohibited

25
Q

Approach mode selection during localizer capture is allowed ONLY when the aircraft is ______________.

A

Inbound

26
Q

Upon execution of a normal missed approach, pressing the ___________ buttons on the thrust levers will cause the command bars to ____ º with noting displayed as the lateral mode and _____ presented at the top of the PFD as the vertical mode

A

Go Around

10

GA

27
Q
The go-around submode is inhibited for any of the following reasons:
\_\_\_\_\_\_\_\_\_\_\_\_\_
\_\_\_\_\_\_\_\_\_\_\_\_\_
\_\_\_\_\_\_\_\_\_\_\_\_\_
\_\_\_\_\_\_\_\_\_\_\_\_\_
A

Current airspeed is in low speed awareness tape (below 1.23 Vs)

Current airspeed above 170 KIAS

Aircraft is above 2,500 feet AGL

If GA has been engaged for more than 20 seconds

28
Q

The minimum altitude for engagement of the autopilot is ______ feet.

A

500

29
Q

The minimum disengagement altitude for the autopilot during an ILS approach is _____ feet

A

200

30
Q

The minimum altitude for autopilot use on a non-precision approach is _________.

A

the MDA