On-board Maintenance

Question 1

395. To force to transfer from CMC 1 to CMC 2 you have to:a. set the CMC 2 pb to ON on the aft overhead panel
     b. set the CMC 1 pb to OFF on the aft overhead panel
     c. monitor the automatic transfer on ECAM

Answer 1

b. set the CMC 1 pb to OFF on the aft overhead
panel

Question 2

396. What is the purpose of the Built in Test Equipment (BITE)?a. To monitor the aircraft system
     b. To memorize failures
     c. To monitor A/C systems and memorize failures

Answer 2

c. To monitor A/C systems and memorize failures

Question 3

397. In flight. What are the CMS functions available?a. The current flight report and the avionic status
     b. The post flight report and the avionic status
     c. a and b are correct

Answer 3

a. The current flight report and the avionic status

Question 4

398. The normal mode or reporting mode can be used:a. in flight
     b. on ground
     c. in flight and on ground

Answer 4

a. in flight

Question 5

399. What can be found in the previous flight report?a. ECAM and failure messages recorded during the last flight
     b. ECAM and failure messages recorded during the 63 previous flights
     c. ECAM and failure messages recorded during the last flight and the 63 previous flights

Answer 5

b. ECAM and failure messages recorded during the 63 previous flights

Question 6

400. When must a class 1 failure be fixed?a. Always before the next flight.
     b. At the next scheduled maintenance check.
     c. Before the next flight only when it is a NO GO item.

Answer 6

c. Before the next flight only when it is a NO GO
item.

Question 7

401. Which information can be found in the current flight report page?a. The list of computers affected by a class 1 or 2 failure
     b. The list of all class 1 and 2 failures during the flight
     c. The list of all failures during the flight

Answer 7

b. The list of all class 1 and 2 failures during the flight

Question 8

402. Which information can be found in the avionic status page?
     a. All failures
     b. The list of the computers affected by a class 1 and 2 failure
     c. ECAM messages when there is a failure

Answer 8

b. The list of the computers affected by a class 1 and 2 failure

Question 9

403. In normal mode the UTC on the lower ECAM comes from:a. the external clock and transmitted by the CMC
     b. directly by the MCDU
     c. directly by the external clock

Answer 9

a. the external clock and transmitted by the CMC

Question 10

404. In case of a cockpit clock failure the UTC comes from:a. a second cockpit clock
     b. the internal clock of the CMC
     c. the MCDU

Answer 10

b. the internal clock of the CMC

Question 11

405. In case of a cockpit clock failure and a CMC power interruption:a. it is not possible to have the UTC on the lower ECAM
     b. the pilot must enter UTC/DATE INIT using the MCDU
     c. the pilot must utilize the CMC

Answer 11

b. the pilot must enter UTC/DATE INIT using the MCDU

Question 12

406. The operator interface with the Central Maintenance System (CMC) is:a. the ECAM
     b. the MCDU and the printer
     c. the FWC

Answer 12

b. the MCDU and the printer