Day 7 - Flight Controls, Navigation
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B737
- 1.What does operation of the aileron trim switches do?
- A.
Repositions the neutral position of the aileron feel and centering unit & displaces both control wheels.
- B.
Repositions the neutral position of the aileron feel and centering unit & displaces FOs control wheels.
- C.
Repositions the neutral position of the aileron feel and centering unit & displaces Cpts control wheels.
- D.
Repositions the up position of the aileron feel and centering unit & displaces both control wheels.
- 2.During alternate flap extension, when will the LE FLAPS TRANSIT amber light be illuminated?
- A.
It is illuminated until the LEDs are fully extended (trailing edge flaps are greater than 5 units )
- B.
It is illuminated until the LEDs are half extended (trailing edge flaps are greater than 15 units )
- C.
It is illuminated until the LEDs are fully extracted (trailing edge flaps are greater than 5 units )
- D.
Only on Approach
- 3.The auto-slat system can operate when the aircraft is airborne with flaps ….. selected?
- A.
1 to 5
- B.
5 to 30
- C.
15 to 40
- D.
1 to 15
- 4.The amber flight control LOW PRESSURE lights are extinguished when the associated flight control switch is in what position?
- A.
STBY RUD and the standby rudder shutoff valve is open
- B.
STBY RUD and the standby rudder shutoff valve is closed
- C.
STBY RUD and the standby rudder shutoff valve is in motion
- D.
In UP position
- 5.The leading edge slats will be at the EXT position until the trailing edge flaps are beyond which flap position?
- A.
1
- B.
5
- C.
15
- D.
30
- 6.The leading edge devices are normally operated by which hydraulic system?
- A.
A
- B.
B
- C.
Stb system
- D.
A and B
- 7.During an RTO with main gear wheel speed more than 60kts, the spoilers will automatically deploy when the thrust levers are at what position?
- A.
Idle and reverser is selected
- B.
At Full stop position
- C.
Idle trust
- D.
Max 20 % N1
- 8.With regard to the alternate flap duty cycle: after a complete extend/retract cycle what cooling period should be allowed before attempting another cycle?
- A.
Four minutes
- B.
Five minutes.
- C.
Two minutes
- D.
One minutes
- 9.The flaps/slats electronic unit (FSEU) provides “skew” detection for which devices?
- A.
TE flaps and LE slats but NOT the outer LE slates numbered 1 and 8
- B.
TE flaps and TE slats but NOT the outer LE slates numbered 2 and 7
- C.
TE flaps and LE slats and the outer LE slates numbered 1 and 8
- D.
Only on TE flaps
- 10.What is the maximum altitude for flap section?
- A.
10 000 ft
- B.
20 000 ft
- C.
30 000 ft
- D.
18 000 ft
- 11.How is the aileron trim position indicated?
- A.
Displacement of both control wheels, and the indication on the scale on the top of each control column
- B.
On the PFD
- C.
Lower panel
- D.
Displacement of both control wheels, and the indication on the scale on the top of each control column
- 12.The trailing edge flaps are operated by which systems?
- A.
A system
- B.
A and B system
- C.
B system, with an electrical motor as a backup
- D.
B system, with bleed airfrom the APU as backup
- 13.What causes the yaw damper to disengage?
- A.
Positioning the B system flight control switch to STBY RUD or OFF, or a SMYD fault or SMYD senses a yaw damper system fault/yaw damper does not respond to a command.
- B.
Positioning the A system flight control switch to STBY RUD or OFF, or a SMYD fault or SMYD senses a yaw damper system fault/yaw damper does not respond to a command.
- C.
Positioning the B system flight control switch to ON, or a SMYD fault or SMYD senses a yaw damper system fault/yaw damper does not respond to a command.
- D.
Extreem turbulence
- 14.At what speed will the flap load relief system move the trailing edge flaps from 40 to 30?
- A.
163 knots
- B.
145 knots
- C.
122 knots
- D.
165 knots
- 15.At what Mach number does the Mach trim start to operate?
- A.
0,650 Mach
- B.
0,616 Mach
- C.
0,82 Mach
- D.
0.615 Mach.
- 16.The Primary (most accurate) mode for updating the FMC position is from?
- A.
Either GPS receiver
- B.
DME DME
- C.
The front GPS receiver
- D.
The aft GPS receiver
- 17.What does positioning the VHF NAV Transfer switch to BOTH ON 1 do?
- A.
Select No2 VOR receiver to supply data to both FCCs and displays
- B.
Select No1 GPS receiver to supply data to both FCCs and displays
- C.
Uses the NAV info from left EDU on all displays
- D.
Select No1 VOR receiver to supply data to both FCCs and displays
- 18.What position should be selected on the IRS control panel to initiate a full IRS alignment procedure?
- A.
OFF then ALIGN
- B.
OFF then NAV.
- C.
To ALIGN
- D.
OFF for five minutes
- 19.The left IRS ON DC light illuminates in flight. AC power is normal. How long will the left IRS operate in this configuration?
- A.
5 minutes
- B.
Indefinitely
- C.
3 minutes
- D.
A half hour
- 20.Are HDG and WIND displays on the IRS display unit true or magnetic?
- A.
True
- B.
Magnetic
- 21.Before start with all AC busses powered, the IRSs are selected from OFF to ALIGN. The ON DC light momentarily illuminates. What does this indicate?
- A.
No DC-backup power
- B.
A short DC power test, with no action required.
- C.
A DC power test, wait 5 min before reset to NAV
- D.
Antenna malfunction
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