boeing 777
1. Access panel 543DB is
a. panel 3DB in zone 54
b. the 4th panel in zone 54
c. –
2. How many ARINC 629 in Boeing 777
a. 7
b. 11
c. 4
3. How can u identify fibre optic cable
a. outer jacket is purple
b. outer jacket is blue
c. –
4. Lower cargo compartment has 3 doors, which is
a. the forward cargo is same size with aft cargo door
b. the forward cargo is bigger than aft cargo door
c. the forward cargo is smaller than aft cargo door
5. Boeing 777 has 8 zones, zone 300 is
a. Upper fuselage
b. lower fuselage
c. Empennage
6. To turn ON the standby power on unpowered aircraft
a. push battery switch to ON
b. standby power to batt and batt switch to ON
c. –
7. To load the data into the LRU, we use
a. CDU
b. MAT/PMAT
c. MFD
8. Software for the CMCF is in?
a. Right AIMS cabinet
b. Left AIMS cabinet
c. Both AIMS cabinet
9. To load the main terminal function (MTF) into MAT
a. select the data load from extended menu
b. type load MTF on the MAT keyboard
c. select the self load button on MAT ______________
10. The type of CMCS ground test contains all adjustment specification and tolerance to maintain system or unit at maximum efficiency
a. System test
b. Operational test
c. Bite test
11. What component controlled the backup generator (BUG)?
a. BPCU
b. ELMS
c. Backup generator converter
12. Backup generator converter automatically test the BUG immediately after
a. power transfer
b. –
c. engine start
13. EEU + ELMS at
a. power management panel
14. Where is the RATgenerator location?
a. Rat strut R/H wing to body fairing
15. The airplane on the ground, no electrical power, when u push the batt switch on, wht receives power?
a. batt bus
b. batt #2 bus
c. Captain flight instrument bus
16. The CMCS notes and health information is stored in the
a. airline modifiable information
b. –
c. operational programme software
17. When does a flight leg transition usually occur?
a. power on
b. engine start
c. take off
18. Ground test switch has power interface to
a. testing function of MAT
b. PMAT in the MEC
c. CMCS
19. Which of the following pages can be printed in the cockpit printer?
a. maintenance pages
b. synoptic pages
c. –
20. How many WES channel must detect warning/alert ?
a. 1
b. 2
c. 3
21. Which line replaceable module (LRM) in the AIMS cabinet transmit video signal to display unit (DU)
a. CPM/GG
22. CMCF software is in which of these AIMS cabinet?
a. CPM COMM
23. The purposes of AIMS cabinet CPM/COMM, CPM/GG is to do calculation for the
a. PFCS
b. PDS
c. AMCS
24. MFD format can show in which display unit
a. upper center
b. right inboard
c. right outboard
25. ND format can show at how many location at the same time
a. 1
b. 2
c. 3
26. The ground crew call from the flight deck can be made from?
a. center CDU on the P8 panel
27. The primary airplane jacking point
a. 1 at L/E wing root each and aft fuselage
28. The RAT can be deployed manually/automatically, it is used to provide backup
a. electrical
b. hydraulic
c. both
29. The E7 rack in the cabin contain the following component
a. CVR, FDR and APUC
30. Which documents do you use to get maintenance practices to do maintenance on a airplane?
a. AMM part 2
31. You erase latch status message from the
a. maintenance task maintenance page
b. engine exceedence maintenance page
32. Before you install the new display unit in the center lower position, you must.
a. turn display unit 90 degrees
b. move throttle lever
c. turn display unit 180 degrees
33. EICAS is in the limited mode of operational, on the DSP which switches are still active
a. ELEC
b. ELEC, HYD, ….
c. ENG, AIR, FUEL
34. To enable maintenance pages menu on MFD, you must use which control to use on the CDU menu.
a. line select key (LSK) 1R on CDU
b. line select key (LSK) 1R on center CDU only
c. line select key (LSK) 5R at any CDU
35. which display show the dynamic position of moveable flight surfaces?
a. FLT CTRL synoptic
36. engine over temperature profile show in which pages
a. performance maintenance pages
b. EPCS maintenance pages
c. engine exceedence maintenance pages
37. There are 15 status message, only 11 are display. How do you see the others?
a. use CNCL/RECALL switchon the DSP
b. use maintenance page switch on CDU
c. use status page on the DSP
38. You can use the ALT EFIS control function on the same CDU
a. –
b. at any time
c. In the air only
39. Which component do you use to control the maintenance pages and MFD
a. CDU and CCD
40. The related display unit failed. Which display can switch automatically?
a. PFD and EICAS
41. For most passenger cabin light, set light by
a. any of the 3 cabin area CSCP ( CACP )
42. which CMCS menu do you use to do a data load?
a. –
b. other function
c. extended maint
43. You are working on a fault that did not cause a flight deck effect. Where can you find information on the MAT.
a. existing FDE
b. present leg faults
c. special function
44. Which of the following is FDE?
a. a fault reported by flight crew
b. –
c. an EFIS flag or EICAS message
45. When do you do a test on emergency lights. The light stays on how long?
a. 5 minutes
b. 60 seconds
c. a minimum of 15 minutes
46. The primary external power system has a fault. To supply a secondary power to the airplane, you must
a. turn the batt switch to ON position
47. Primary external power connected to and not in use light is on. There is primary external power on the
a. left main a/c bus
b. ground handling a/c bus
c. right main a/c bus
48. an engine running, an IDG oil is become too hot. What protects the IDG
a. a thermal plug in the IDG plug melts and the drive disconnect
49. If BUG has too much oil ( overserviced ), the electrical maintenance page oil level shows
a. service
50. What conditions tells you that IDG has a clog oil filter
a. electrical maintenance page 1 shows service
