BLOCK A REVIEW (2018) Flashcards
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
Q
- During climb out with ACCL mode selected, initiate flap retraction at flap retraction speed, provided aircraft altitude is at least ________ ft AGL.
A
200
26
Q
- In the ACCL mode, once the flaps are retracted above 16.5 degrees, the command bars command a pitch attitude which ________.
A
Transitions to a constant airspeed climb
27
Q
- 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.
A
10, 2000
28
Q
- 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.
A
Ignored
29
Q
- Always set the FD mode selector to _______ before changing the NAV aid frequency or switching NAV receivers.
A
HDG or GYRO
30
Q
- During cruise, the AOA indicator can be used to maintain an optimum AOA for _________.
A
Max Endurance or Range
31
Q
- The _________ mode provides a command bar for intercepting andtracking a localized beam and GS path.
A
APPR AUTO
32
Q
- 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.
A
HDG
