WorksheetsAutoflight 1
Total questions: 27
Worksheet time: 7hrs 31mins
During an ILS approach below 1,000 feet Radio Altitude, a BELOW G/S alert occurs. To cancel the alert
Select another mode on MCP
The alert cannot be cancelled
Reset the Master Caution
Press either pilots BELOW G/S P-INHIBIT Light, or correct the flight path back to the glide slope
With VNAV engaged, the AFDS pitch and A/T modes are commanded by the
MCP
FMC
CWS
FCC
Under speed limiting (flashing A) appears
FMC speed or selected speed cannot be reached
Minimum speed for current flap setting cannot be reached
When the speed is less than 1.3 VS for current flap setting
The highest of all the answers
When control wheel pressure is released during CWS roll operation, the aircraft will roll wings level when the bank angle is
15 degrees or less
6 degrees or less
10 degrees or less
8 degrees or less
How many independent Flight Control Computers (FCCs) are there in the Autopilot Director System (AFDS)?
One
Two
Tree
Four - one for each channel
The Automatic Flight System (AFS) consists of:
The autopilot flight directors (AFDS) and the autothrottles (A/T)
The autothrottles (A/T) and the autopilots (A/P) only
The flight directors (F/D) and the autothrottles (A/T) only
The autopilots (A/P) and the flight directors (F/D) only
Normally, N1 limits and target N1 values are provided to the A/T by the
FMC
IRU
FCCs
A/T computer
If the autopilot ALT HOLD mode is manually overridden with control column pressure, which of the following occurs?
The autopilot disengages
LNAV disengages
The autopilot changes to CWS P and returns to ALT HLD if control pressure released within 250 feet of selected altitude
LEVEL CHANGE automatically engages
What does the VOR/LOC switch arm the AFDS for
GPS navigation
VOR or localizer tracking
DME tracking
NDB tracking
What must be tuned to an ILS frequency before the approach mode can be selected?
DME
Both VHF 1 and 2
At least 1 VHF receiver
ADF 1
When must the second VHF NAV receiver be tuned to the ILS frequency for a dual A/P approach?
1000 RA
800 RA
Prior to landing
1500 RA
Which of the following occurs when a TO/GA switch is pressed once below 2000 feet radio altitude for an automatic go-around from an ILS channel A/P approach and FLARE armed?
N1 mode is displayed on the FMA
The autopilot disengages
The autothrottle advances thrust levers to full go-around N1
The autothrottle advances thrust levers to reduced go-around N1
After a normal take-off, what pitch command can you expect from the F/D?
V2
V2+5
V2+10
V2+20
What happens with the IAS/MACH display on the MCP if SPD INTV switch is pushed during VNAV operation:
IAS/MACH displays opens up and shows 100 kts
IAS/MACH displays opens up and shows dashes
IAS/MACH displays opens up and shows slashes
IAS/MACH displays opens up and show FMC target speed
LNAV will automatically disengage
When VNAV is engaged
When VNAV is engaged
Upon glideslope capture
Reaching a route discontinuity
Two independent radio altimeters provide radio altitude to the respective FCCs. With one radio altimeter inoperative
The autopilot will disconnect as soon as the failure is detected
Nothing out of the ordinary will occur
The autopilot will continue to command the aircraft down to minimums
The autopilot will disconnect two seconds after LOC and GS capture
During AUTO LAND at which radio altitude should the flare mode be engaged
200 ft
100 ft
50 ft
300 ft
What pitch mode is annunciated in the FMA after takeoff when the autopilot is first engaged in CMD
VNAV
VS
CWS P
MCP SPD
Which is the correct mode on the FMA? Condition: After takeoff, A/P engaged, before flaps up.
THR HLD : HDG SELECT : MCP SPD
ARM : HDG SELECT : VNAV PTH
N1 : LNAV : MCP SPD
N1 : LNAV : FMC SPD
What is the latest altitude (AGL) CMD can be selected on the second autopilot to execute a dual channel A/P approach?
2000
800
1000
350
The autopilot disengages is FLARE mode is not armed by (feet)
350
50
400
100
Which A/T modes permit manual thrust changes without A/T interference?
N1 and ARM
THR HLD and ARM
GA and ARM
THR HLD
In normal operation, what provides the A/T system with N1 limit values
A/T Computer
FCCs
AFDS
FMC
The Air Data Inertial Reference System (ADIRS) produces following flight data
Attitude and speed
Position, speed, attitude
Altitude and speed
Position, attitude, altitude, speed
After lift-off, the A/T remains in THR HLD until
400 feet RA
350 feet RA
800 feet RA
1500 feet RA
At what altitude will both A/Ps automatically disengage if FLARE is not armed during an ILS dual channel approach:
Will not disengage
50 feet RA
500 feet RA
350 feet RA
Which mode must be armed before the second autopilot can be selected during a dual channel A/P approach?
VOR/LOC
LNAV
VNAV
APP
