PHASE A – A320 B1 COURSE 2018
AIRCRAFT E-INDICATIONS - MCQs by Zain Hasan (PIA) PART 2 of 2
1. The 3 DMCs can be considered as data concentrators and send data to the DUs through
a- Coaxial cables
b- ARINC 629 output buses.
c- RS422
2. The tele-loading of the operational software is carried out by
a- DMCs
b- On ground in shop
c- Tele loading is not possible.
3. Workshop testing on DMCs is carried out on
a- RS500
b- ARINC 429
c- RS232
4. The ECP outputs discretes for CLEAR (CLR), RECALL (RCL), STATUS (STS) and emergency cancel (EMER
CANC) keys are linked to the
a- DMCs
b- FWCs
c- SDACs
5. The output discrete for ALL key is directly linked to the
a- DMCs.
b- ECAM EWD page
c- FWCs
6. DMCs receive weather radar data on
a- Digital bus
b- ARINC 639 High speed bus
c- ARINC 453 High speed bus
7. When a new DU is installed, a cross loading from the corresponding DMC has to be performed via
a- MDDU
b- DATA loader
c- MCDU
8. The data through MDDU is installed in DMC1 via
a- ARINC 429
b- ARINC 639
c- RS bus
9. A ________ pushbutton can be installed on the FCU. If you push this pushbutton, the selected altitude
is displayed in meters above the altitude scale.
a- METRIC ALT
b- MET
c- ALTERNATE
10. the _____are used by the FWCs to send text messages (warnings, MEMO and status) to the DMCs.
a- ARINC 429 buses
b- RS 422 buses
c- ARINC 639 buses
11. FWC, ECAM Control Panel (ECP), (ATSU), (FDIMU), gets data from DMC through
a- high speed switched bus.
b- low speed switched bus.
c- Either low or high speed bus.
12. CFDIU gets data from DMC through
a- one low speed switching bus.
b- one high speed unswitched bus.
c- one low speed unswitched bus.
13. Weather radar data is not available in
a- rose mode on ND
b- plan mode on ND
c- Mono mode on ND
14. Some of the data on Captain’s side PFD is not available.
a- It means external sources have failed.
b- It means DMC has failed
c- It means DU has problem
15. PFD/ND transfer switching is performed by software switching of
a- the PFD/ND ouputs inside LCDs.
b- the PFD/ND inputs outside DMCs.
c- the PFD/ND ouputs inside DMCs.
16. In case of EWD unit and SD unit failure, each crew member has the possibility to permanently present
the
a- EWD on the ND unit.
b- EWD on PFD unit
c- EWD can not be transferred in both DU failure
17. no reconfiguration is possible In the case of PFD unit and ND unit failure
a- On opposite sides
b- On the same side
c- Reconfiguration is possible in all failure situations
18. In case of both SDAC failure, Wheel ECAM page data is available because
a- It sends data directly to CFDIU
b- It has direct bus connection with DUs
c- it is already in ARINC 429
19. To activate the Elapsed Time (ET) function, the ET selector must be set to
a- SET
b- RUN
c- GPS
20. CFDIU generate current/last leg report in
a- normal mode
b- menu mode
c- advisory mode
21. In menu mode CFDIU dialogues with one computer at a time in order to read
a- RAM
b- Data loops
c- bite memory
22. The CFDIU capacity for failure messages memorization is up to
a- 11 lines
b- 40 lines
c- No line limit.
23. When several identical and consecutive warnings are transmitted, the CFDIU memorizes the first
occurrence only and carries on counting with a maximum of
a- 8
b- 64
c- 11
24. PFR recording starts if flight number inserted
a- before takeoff roll + 3 minutes.
b- before Taxi
c- before first engine start + 3 minutes
25. PFR recording stops after when aircraft decelerate below
a- 80 knots +5 seconds.
b- 60 knots +30 seconds.
c- 80 knots +30 seconds.
26. an Angle-Of-Attack (AOA) sensor failure has been detected and that systems A, B and C are affected
by this failure. The Air Data System (ADS) will transmit
a- an internal failure
b- an external failure
c- an internal failure with independent fault.
27. What type of systems can memorize failures, which occurred in the last 64 flight legs?
a- Type 3 (CFDS)
b- Type 1 (CFDS)
c- ECAM computer
28. Previous leg report can store up to 200 failures over the last
a- 64 flight legs.
b- 60 flight legs
c- 20 days of flights
29. If the failure occurred intermittently, the PFR will have ______against fault details.
a- INHIBT
b- Asterisk
c- INTM
30. Class 3 faults can be traced in avionics status page of
a- MDDU
b- MCDU
c- AIDS
31. Troubleshooting data is presented on MCDU in
a- hexadecimal language.
b- Binary language
c- Dual languages
32. Type 2 systems don’t have
a- BITE system
b- default memory
c- menu mode.
33. PFR filter database is adapted from ______under diskette form.
a- Service bulletin SB
b- Service Information Letter (SIL)
c- Fleet enhancement program (FEP)
34. Only primary failures, INDEPENDENT failures and CLASS 2 failure messages (Maintenance status) are
received from
a- FWC
b- LRUs
c- SDAC
35. The CFDIU receives the engine serial number from the
a- (SDAC)
b- CFDIU
c- (DMC)
36. When the CFDIU is affected by an internal failure, the message CFDIU is displayed on the ECAM
a- Engine warning page
b- MAINTENANCE STATUS page.
c- CFDIU Bite on LRU
37. PFR filtering program, Each filter is identified by
a- a 15-character data base number.
b- part number
c- filter floppy number
38. Data to printer is transmitted via Low Speed (LS) ARINC 429 buses, one at a time using a
a- Avionics protocol.
b- ARINIC protocol.
c- handshake protocol.
39. 12 inputs are available on the printer,
a- but only 1 is allocated.
b- but only 6 are allocated.
c- And all are allocated.
40. Input 1 in printer has
a- the highest priority; input 12 has the lowest one.
b- the lowest priority; input 12 has the highest one.
c- the same priority as of input 12
