BLOCK A REVIEW (2018) Flashcards
(32 cards)
1
Q
- ADI FD flag in view indicates that ________________ is/are unreliable.
A
Command Bars
2
Q
- Normally __________ provides heading information to the pilot’s HIS and ________ provides heading information to the co-pilot’s HIS.
A
INU #1 & INU #2
3
Q
- The command bars in the ADI cannot display _________ commands.
A
Constant Airspeed
4
Q
- If the bearing pointer is set to VOR 1 and subsequently a localizer freq is set into the NAV radios, the bearing pointer will _____________.
A
Not Display
5
Q
- The ________ flag in view indicates a heading is invalid.
A
HDG
6
Q
- The bearing on either HIS can display ________ information.
A
TACAN, FMS or ADF, VOR 1 or VOR 2
7
Q
- The ADF feature of the bearing pointer receives signals from the ______ radio.
A
COMM #1 UHF
8
Q
- The radio altimeter decision height for the pilot flying the approach will be sent to the _________ for the approach being flown.
A
HHT or HHA
9
Q
- The radio altimeter indicates absolute altitude only, and should not be used as the primary _______.
A
Decision Height Altitude
10
Q
- Normalized AOA means ________.
A
AOA is displayed in % of lift by the pointer on Zero to 1.0 scale
11
Q
- Pilot and co-pilot AOA indicators operate _____ and indicate ______readings when the airflow around the AOA probe varies, as in a side slip.
A
Independently and different
12
Q
- The ______ illuminates anytime a comparator warning monitor light illuminates.
A
MSTR DISC Light and COMPAR warning light
13
Q
- Depress the ______ to extinguish the COMPAR WARN light.
A
MASTR DISC Light or the COMPAR WARN Light
14
Q
- When the glide slope COMPAR warning light illuminates, ________.
A
The difference between the pilot’s and co-pilot’s GS subsystem has exceeded the predetermined limit.
15
Q
- The capture point of a VOR or TACAN radial, when using the NAV/LOC mode of the FD-109 system is approximately _______ degree the _____ dot on the HIS scale.
A
5 degree, inner
16
Q
- The pitch command knob is used to manually set the command bars at any desired climb or descent pitch angle within the limit of ________ degrees of climb or ________ degrees of dive.
A
15, 10
17
Q
- Momentarily depressing (1/2 sec or less) the remote slew on the yoke causes the heading marker to ________.
A
Move in 1degree increments
18
Q
- When taxing the aircraft, do not set the flight director mode selector switch to the ________ position if turning, accelerating or decelerating.
A
RGA
19
Q
- Just prior to reaching ________ speed both the pilot and co pilot will actuate their RGA push button switches.
A
Rotation
20
Q
- If the rotation is delayed (speed increased), the command bars willcommand a reduced pitch during climb out and provide an increase in climb out speed _____ the increase in rotation speed.
A
Approximately Equal to
21
Q
- Aircraft rotation for take off ________ be delayed in order to actuate the RGA push button switch.
A
Will not
22
Q
- If the RGA push button switch is not pressed prior to rotation or an incorrect rotation command is displayed on the ADI, rotate to ______ degrees on the ADI pitch tape.
A
8 to 9
23
Q
- The RGA System does not ______.
A
Provide lateral steering commands
24
Q
- In ACCL mode, the RGA system is programmed to command a _____ pitch change during climb out at a rate of _____ every 6 to 7 seconds.
A
Nose down, 1 degree
25
25. During climb out with ACCL mode selected, initiate flap retraction at flap retraction speed, provided aircraft altitude is at least ________ ft AGL.
200
26
26. In the ACCL mode, once the flaps are retracted above 16.5 degrees, the command bars command a pitch attitude which ________.
Transitions to a constant airspeed climb
27
27. With 4 engines operating, MAX mode, accelerate to recommended 3 engine climb out speed plus ______ knots and climb out to ________ ft above the runway or obstacle clearance height, whichever is higher.
10, 2000
28
28. Since the constant speed maximum climb command is normally less than the flap retraction speed, the command bars display must be _______ when the appropriate altitude is reached for acceleration to flap retraction speed.
Ignored
29
29. Always set the FD mode selector to _______ before changing the NAV aid frequency or switching NAV receivers.
HDG or GYRO
30
30. During cruise, the AOA indicator can be used to maintain an optimum AOA for _________.
Max Endurance or Range
31
31. The _________ mode provides a command bar for intercepting andtracking a localized beam and GS path.
APPR AUTO
32
32. Setting flight director mode selector to APPR AUTO while a localizer frequency is tuned causes the steering commands of the command bars to operate in the _______ mode until entering the capture range.
HDG
