Automatic Flight
問題一覧
1
D. F/D system, A/T system and three autopilots ,the AFDS can be controlled via de MCP or integrated with the FMC for a full automated flight.
2
B. HDG SEL or TRK SEL.
3
A. Set the heading or track in the MCP heading/track window and on the PFDs and NDs.
4
A. FLT DIR and LAND 3 in green, and NO AUTOLAND in amber.
5
B. 15 degrees if the roll mode is HDG SEL, regardeless of airspeed.
6
C. LNAV is armed and activates at 50 ft RA.
7
D. VNAV is armed and activates at 400 ft above runway elevation.
8
C. 1250 feet/min at ECON speed.
9
B. 120 degrees
10
A. selecting a TO/GA mode.
11
A. TRUE.
12
D. The Automatic Flight system has complete satisfactorily the pre-autoland test and the aircraft is below 1500 feet RA.
13
C. Between 40 and 60 feet RA.
14
B. The aircraft is less than 2 feet RA and the A/P controls the rudder and nose wheel steering to track the centerline.
15
D. Answers 1 and 2 are correct.
16
D. above 200 fett RA when A/P is engaged.
17
A. The A/P is operating in a degraded mode.
18
C. Stall protection and bank angle protection.
19
C. Message is a caution if fault occurs after LAND 3 is annunciated.
20
D. The pitch mode has failed and the A/P is engaged.
21
B. The Autoland system is "Fail Passive"
22
A. 10 seconds.
23
D. On the ground when F/D is "ON", TO/GA annunciates for both roll and pitch.
24
B. 1000 feet.
25
C. Disengages all autopilots.
26
A. Resets the Master Warning light.
27
D. All of the above.
28
D. When both F/D switches are "OFF"and the bank angle is greater than 10 degrees the A/P engages in attitude hold "ATT" as the roll mode.
29
C. At 24 100 feet.
30
A. TRUE.
31
B. Autothrottle controls airspeed.
32
A. Autothrottle controls the vertical path.
33
A. Position both A/T arm switches, left and right on the MCP to the "OFF" positon
34
B. FALSE.
35
D. A/T remains armed.
36
D. It will remove the derate and assumed temperature reductions.
37
C. The left F/D switch activates the F/D steering indications on the left PFD.
38
C. Pushing the autothrottle switch a second time.
39
A. TRUE.
40
B. ROLLOUT and LNAV.
41
B. FLARE and VNAV.
42
D. The pitch mode controls the vertical path and the A/T mode controls speed.
43
B. If the airpalne touches down while executing the go-around the pitch mode remains active.
44
A. Go-around.
45
C. above 200 feet RA when A/P is engaged.
46
D. At 400 feet above runway elevation.
47
B. 200 knots.
48
D. ALT will be displayed on the FMA as the active pitch mode.
49
C. 80 knots
50
D. Disarms LNAV and VNAV, if armed.
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1
D. F/D system, A/T system and three autopilots ,the AFDS can be controlled via de MCP or integrated with the FMC for a full automated flight.
2
B. HDG SEL or TRK SEL.
3
A. Set the heading or track in the MCP heading/track window and on the PFDs and NDs.
4
A. FLT DIR and LAND 3 in green, and NO AUTOLAND in amber.
5
B. 15 degrees if the roll mode is HDG SEL, regardeless of airspeed.
6
C. LNAV is armed and activates at 50 ft RA.
7
D. VNAV is armed and activates at 400 ft above runway elevation.
8
C. 1250 feet/min at ECON speed.
9
B. 120 degrees
10
A. selecting a TO/GA mode.
11
A. TRUE.
12
D. The Automatic Flight system has complete satisfactorily the pre-autoland test and the aircraft is below 1500 feet RA.
13
C. Between 40 and 60 feet RA.
14
B. The aircraft is less than 2 feet RA and the A/P controls the rudder and nose wheel steering to track the centerline.
15
D. Answers 1 and 2 are correct.
16
D. above 200 fett RA when A/P is engaged.
17
A. The A/P is operating in a degraded mode.
18
C. Stall protection and bank angle protection.
19
C. Message is a caution if fault occurs after LAND 3 is annunciated.
20
D. The pitch mode has failed and the A/P is engaged.
21
B. The Autoland system is "Fail Passive"
22
A. 10 seconds.
23
D. On the ground when F/D is "ON", TO/GA annunciates for both roll and pitch.
24
B. 1000 feet.
25
C. Disengages all autopilots.
26
A. Resets the Master Warning light.
27
D. All of the above.
28
D. When both F/D switches are "OFF"and the bank angle is greater than 10 degrees the A/P engages in attitude hold "ATT" as the roll mode.
29
C. At 24 100 feet.
30
A. TRUE.
31
B. Autothrottle controls airspeed.
32
A. Autothrottle controls the vertical path.
33
A. Position both A/T arm switches, left and right on the MCP to the "OFF" positon
34
B. FALSE.
35
D. A/T remains armed.
36
D. It will remove the derate and assumed temperature reductions.
37
C. The left F/D switch activates the F/D steering indications on the left PFD.
38
C. Pushing the autothrottle switch a second time.
39
A. TRUE.
40
B. ROLLOUT and LNAV.
41
B. FLARE and VNAV.
42
D. The pitch mode controls the vertical path and the A/T mode controls speed.
43
B. If the airpalne touches down while executing the go-around the pitch mode remains active.
44
A. Go-around.
45
C. above 200 feet RA when A/P is engaged.
46
D. At 400 feet above runway elevation.
47
B. 200 knots.
48
D. ALT will be displayed on the FMA as the active pitch mode.
49
C. 80 knots
50
D. Disarms LNAV and VNAV, if armed.