1.

Which one of the navigation system has the objective of providing lateral and vertical guidance
to the runway on approach
a. Micro bacon
b. VHF VOR
c. ILS

2. How do you carry out the check of the approach display on the integrated standby flight display
ISFD?
a. By carrying out center ILS operation test from the mat
b. By using the internal bite facility of the ISFD
c. By using special test set connected in ISFD

3. When the integrated standby flight display ISFD is powered on there is no localizer or glide slope
scale visible to display these
a. The app mode switch should be pressed once
b. The app mode switch should be press two time
c. Attitude reset switch should press once

4. Which of the following function on is the flight management computing system

a. Supply navigation calculation and flight plan control data
b. It help maintenance crew to carry out testing
c. It optimize cabin crew workload plans

5. Which one of the statement about marker beacon system is correct

a. Marker beacon function only operates in left VOR marker beacon receiver
b. Marker beacon function only operates in right VOR marker beacon receiver
c. Marker beacon function operates in both VOR marker beacon receiver

6. The ATC mode’s transponder get altitude data from where

a. Radio altimeter
b. AIMS
c. DME

7. On which display does aims shows the 4 color weather pattern display
a. NAV display
b. PD
c. EICAS upper display

8. Where are the autopilot flight director system mode shows in flight deck?
a. On a separate flight mode annoucenter indicator on the captain and firs officer panels
b. On the ND
c. On the Primary Flight Display
9. Calculating thrust limits of the thrust management computing function are shows on the
a. EICAS display
b. Secondary engine display
c. Status page display

10. When is go around mode is armed

a. The aircraft is in the air glide slope mode is active are the trading edge flap is not up
b. The aircraft is in the air glide slope mode is active and landing gear is down
c. The aircraft is in the air landing gear Is down

11. When does cross wind control comes into operation during auto land
a. At 500ft in all condition of cross wind
b. At 500ft at medium cross wind
c. At 500ft for high crosswind

12. “MCP CNTRL panel lane status message show” in which for failure?
a. Fluorescent tube
b. Microprocessor
c. Liquid crystal display

13. How many auto flight director computer (AFDC) must be engaged for auto land
a. At least one AFDC must be engaged
b. At least two of three AFDCs must be engaged
c. All three of the AFDCs must be engaged

14. If the primary flight control system (PFCS) is in the secondary or direct mode, then the primary
flight computer
a. Permit the autopilot to engage
b. Don’t permit the autopilot to get engaged
c. Do not permit the autopilot to engage only if the altitude above the 5000ft

15. Which one of these can generate commands to the Thrust Management Computing Function
(TMCF) to control engine thrust?
a. Flight Management Computing Function (FMCF)
b. EFIS Control Panel
c. EEC Maintenance switch

16. What is the power supply requirement for the AFDCS (Autopilot Fight Director Computers) to
operate?
a. 115VAC
b. 28VAC
c. 28VDC
17. The mode of the Autopilot system is displayed:
a. on both Primary Flight Displays (PFD)
b. on both Navigation Displays (ND)
c. On separate Flight Mode Annunciator (FMA) on the P1 and P3 panel

18. How many Autopilot Flight Director Computers are there in the B777
a. 2
b. 3
c. 4

19. 12 What does the AUTO POP UP mode do?

a. It automatically engages the Autopilot during Go Around
b. It automatically lets the flight director bars display during Take-Off or Go Around when
the TO/CA switch is pushed even if the Flight Director switches are off
c. It automatically engages the Auto throttle system during Go Around

20. Which one of this is the correct order to follow installing the ADIRU on the rack?
a. Slide lock bar down, tighten screws and install electrical connectors.
b. Tighten screws, slide locking bar down and install electrical connectors
c. Tighten screws, install electrical connectors and slide locking bar down.

21. Which statement is correct regarding AFDS modes?

a. The VNAV and LNAV are not FMCS modes. They are AFDS modes.
b. The VNAV and LNAV are not AFDS modes. They are FMCS modes that go through the
AFDCS
c. The VNAV and LNAV are not AFDS or FMCS modes.

22. What does the Suppression Splitter do when the Distance Measuring Equipment (DME)
transmits?
a. it inhibits the transmission of the TCAS and the ATC systems
b. it inhibits the reception of the TCAS and the ATC systems
c. it switches OFF the TCAS and the ATC systems

23. The Ground Proximity Warning Computer sends terrain data to the AIMS Cabinets to show on
a. Navigation Displays
b. Primary Flight Displays
c. EXCAS Displays

24. Which system supplies slant range distance between the airplane and a ground station?
a. DME
b. VOR
c. ADE
25. If the FMC (flight management computers) Selector is in AUTO position, which FMCF (fight
management computing function) becomes the active FMCF after power-up?
a. Left FMCF
b. Right FMCF
c. it is decided by a random selection

26. What mode is the Multi-Mode Receiver (MMR) in when it looks for and locks on to the satellite
signals?
a. Acquisition mode
b. Navigation mode
c. Altitude aided mode

27. Where are the 2 Total Air Temperature (TAT) probe elements connected to?
a. TAT element 1 is connected to left AIMS and TAT element 2 to right AIMS
b. TAT element 1 to ADIRU and TAT element 2 to SAARU
c. TAT element 1 to Captain's Pitot ADM and TAT element 2 to FO's Pitot ADM

28. The DME Interrogator sends the DME (distance measurement equipment) station audio to the
a. Warning Electronic System which can then be heard on the Aural Warning speakers
b. Warning Electronic System which can then be heard on the Flight Interphone speakers
c. Audio Management Unit which can then be heard on the Flight Interphone speakers