ElectronicBasicKeshvari

ElectronicBasicKeshvari

A 320 کشوری الکتریک

1.   IN CLASSIC VER WHAT CONTROLS TAV?                             ZC

2.   PACK CONTROLLER ELECTRICALLY CONTROLS?     BYPASS VALVE , RAI

3.  WHERE GALLEY AND LAV AIR EXIT FROM?                       OFV

4.   LAND LIGHT SW MUST AT..... TO ILLUMINATE THE LIGHT?   ON

5.   WHAT TAXI AND T/O LIGHT NEED TO ILLUMINATE? NOSE L/G  D/L

6.   WHERE IS LOGO LIGHT?                          HORIZONTAL STAB

7.   WHICH  HAS 4 LIGHT ( PAX,LAV,CAPT AND ATT) CALL?  AREA CALL PNL

8.   AFT AND FWD PRESSURIZED BULKHEAD?        FRAME 1 AND 70

9.   WHERE IS ZONE 243?                         UPPER HALF FUSELAGE

10.  WHICH ONE IS CORRECT?                  TAIL ZONE:  300

11.  TR OVERHEAT TEMP?                                                           171

12.  TR OVER CURRENT?                              50A±10   IN 60 MILISECOND

13.  WHICH BUSES ARE SUPP

14.  NORMAL SUPPLY OF AC ESS?              AC 1

15.  IF ONE TR FAIL OTHER TR REPLACED?        AUTO OR MAN

16.  IF ONE GEN SUPP BOTH AC BUS?       BOTH BTC AND RELATED GLC CLOSE

17.  AVAIL LIGHT MEANS?     EXT PWR MAY BE ON 

18.  BOTH GALLEY POWERED IN FLIGHT?           2 GEN RUN

19.    WHEN RAT REPLACED BY STATIC INV?     CLASSIC<100KNT,    ENH<50

20.    DEF VALVE AMBER LIGHT IS FOR?        CONFIRM OPENING OF DEF VLV

21.  WHAT IS SEQ OF TANK IN 321 & 320?

22.    AMBER BOX AROUND QUANTITY ON ECAM MEANS?    UNUSABLE FUEL

23.  WHEN LOW LEVEL COMES? 750KG

24.    IF ALL PUMPS STOPED FUEL CAN GOES TO ENG FROM?     SUCTION LINE

25.  HOW REF ENABLED?                        REF/FED DOOR OPEN

26.  WHEN SEQ VALVE OPEN?

27.    IDG SHUTDOWN THE ENG IN?                                             185

28.    ECU CONTROLS….. FOR IDG COOLING?                 FUEL RETURN VALVE

29.    IN FLIGHT BRK USES?                   GREEN

30.   CLASSIC AND ENH VER FOR NOSE STEERING USES?   GREEN & YELLOW

31.   HOW MANY FADEC?          2 FADEC , ONE EACH ENG WORK SEPARATE

32.   EIU CB PULLING CAUSES?                  WINDOWS AND PROB HEATIN

33.   WHERE IS OXYGEN FIXED BOTTLE?                      FWD L/H

34.          OVERHEAD OXY P/B IS FOR?                         SUPPLY ON/OFF

35.          VALVES OF POTABLE WATER SYS?      DRAIN + OVERFLOW+FILL/DRAIN

36.          WHEN VACUUM GEN OPERATE?      BELOW 16000FT & FLUSH SW PRESS

37.          ENG COOLING SHROUD COOLED BY?         STAGE 4 & 9

38.          WHAT IS PS3?                     METERES COMPRESSOR DISCH PRESS

39.          APU DESIGN?                  ONE STAGE CENTRIFUGAL COMPRESSOR

40.          APU BLEED VALVE OPEN & XFEED VALVE AUTO?

41.          WHICH ONE IS DOUBLE LOOP DET?                     WING

42.          EACH FDU RECIEVES?            ONLY OWN SIDE LOOP SIG

43.          A/C ON GND EXT FAN & VALVE?

44.          NO GO ITEMS? FAC1,ELAC2,SFCC1

45.          WHICH SURFACE CAN MECH CONT?         RUDD & THS

46.          WHAT IS ACTIVE PROTECTION IN DIRECT LAW?       NO PROTECTION

47.          IF ROLL FAIL WHICH LAW?              ALTERNAT PITCH

48.          IF THS SERVO JAM?                 DEACTIVED

49.          HOW MANY DETENTS IN THR LEVER?                          6

50.          WHAT TRIPLE IND SHOW?                   BRK ACCUM PRESS+L/H R/H MODULATED BRK PRESS

51.          BLUE ELEC PUMP IN FLT OPERATE?

52.          WHEN RED ARROW  LIGHT IS

53.          WHEN AUTO BRAKE ACTIVED?   GND ,PUSH/B PRESS,BSCU 

54.          REVERSE LOGIC?

55.          AFTER FREE FALL IS STEERING AVAIL?              NO
56. EMER DOOR CAN OPEN ?          ONLY FROM INSIDE
57. HOW MANY DOOR  A320 HAVE?     2EMER DOOR AND ONE SLIDE EACH SIDE 

  

A320 ELECTRONIC EXAMPLE QUESTION

EXAMPLE Q

1. PURPOSE OF AMU IS FOR NAV AND COMM AUDIO INTEGRATING

2. FMGC CAN TUNE ALL NAV SYS

3. SECAL IS INSIDE AMU

4. SELCAL CODE CAN INSERTED ON SELCAL PNL IN 80VU

5. PRINTER CAN PRINT ATSU CFDS AND AIDS

6. SELCAL IND ON ACP

7. A/P COMPUTERS ARE FMGC AND FAC

8. MCDU NORMAL MODE AVAIL IN FLT AND MENU MODE IN GND

9. SIDE STICK AND PEDAL DONOT MOVE AUTO

10. FD CAN ENGAGE IF POWER UP TEST OK

11. BOTH RMP FAIL REMAIN RMP CAN TUNE HF1 HF2 VHF3

12. ADR CAN DISCONN FROM ADIRU PNL

13. ATT AND ALT COMES FROM ADIRU

14. INDEPENDENT UNITS ARE: W/R TR, TCAS, R/A, GPWS

15. A/P SENDS IN THRUST REDUCED TO SET LEVER TO RETARD GATE

16. MCDU USED FOR LONG TERM AND FCU FOR SHORT TERM

17. FAILURES SHOWN ON LOWER PART OF EWD

18. WARNINGS INL/H AND MEMO AND SEC FAIL ARE R/H LOWER

19. STBY COMPASS HAS SW TO CALIBRATE

20. DFDR GET DATA FROM FDIU

21. PROBES CONN TO ADM AND STBY IND

22. MCDU FUNC IS: ALIGN IRS, TEST AND TUNE

23. ATC MODE C CAN BE SEEN WITH ALTITUDE

24. ATC HAS 2 ANT TOP AND 2 BOTTOM

25. FWC GENERATE TA WARN

26. TCAS SHOWN ON PDF SPEED SCALE AND ND

27. MECH AND ATT LIT AUTO OFF AFTER 60 SEC

28. DME SHOWN ON CAPT PFD, F/O ND, DDRMI

29. DFDR REC 25 HOUR

30. RA UNIT ARE AFT PART OF AFT CARGO DOOR

31. JACK CONN TO…

32. SYS PAGE AUTO APEAR IF FLAP >20

33. VOR ANT IS TOP OF VERT STAB

34. MARKER ANT BOTTOM NEAR FWD CARGO

35. PERMENANT DATA ON SD ( LOWER ECAM) IS: SAT, TAT , ISA,GW, HOUR

36. DME SHOWS DASH IF NONE COMPUTED DATA

37. RMP MAIN FUNCTION?

38. DOES FMGC USE ADF AS NAV SOURCE IN AUTO TUNING?

39. RMP FAIL SAME SIDE NAV MANUAL TUNING LOST

40. 4-EXTERNAL SENSORS OF ADIRU

41. FAC FUNCTIONS

42. A/P WARNINGS WHERE IS INDICATED?

43. STATUS PAGE MANUAL DISPLAY AND AUTOMATIC DISPLAY

44. MODES OF AFCS THAT CAN BE SELECTED ON FCU?SPD-MACH-ALT-V/S

45. WHAT CAN BE SEEN ON DDRMI?

46. WHERE IS DME INDICATED? PFD-ND-DDRMI

47. PERMANENT INDICATION ON LOWER PART OF STATUS PAGE

48. INDICATION OF RA? <2500FT+GROUND BAR UNDER300FT+RED RIBBON UNDER 500FT

49. WHAT DO WE HAVE ON CFDS BACK UP MODE?

50. ADIRU HOW MANY ACCELEROMETER AND GYROS?

51. WHEN MANUAL TUNING ON RMP? BOTH FMGC FAIL +NAV RED LIT P.B PRESSED ON RMP

52. ENGINE PARAMETERS INDICATED WHERE?

53. CLASS II FAILURE? IMMEDIATE ACTION OR NEXT PROPER TIME FOR RECTIFICATION

54. TCAS ON ND AND V/S ON R/H PFD

B747 ELECTIC QUESTION EXAMPLE

B747 ELECTRIC QUESTION EXAMPLE

1. AIRCRAFT BATTERY AMPERAGE AND VOLTAGE? 24V, 34A

2. TR AMPERE? 75A

3. EXT POWER TR RATE? 20A

4. WHAT’S THE AMPERE OF BAT CHARGER? 40A

5. IF OPEN PHASE DETECTED WHICH ONE TRIPS? BTB TRIP

6. TR INPUTS? 115VAC, 3PHASE

7. MAX ALLOWED CSD TEMP RISE? 15 DEG

8. WHERE’S GND SERVICE RELAY? P14

9. WHERE’S BATT THERMOSTAT? UP IN ONE OF CELLS

10. HOW CAN CSD CONNECT? ON GND WITH ENG S/D

11. CSD OIL TEMP SHOWS? OIL LEAVING CSD

12. ENG S/D WHICH RELAY TRIP? GCB

13. WHICH CONDITION FOR FUELING? STBY SW MUST OFF, BATT ON

14. WHICH UNIT CONTROL SSB? BOTH CAN OPEN BUT CLOSING BY BPCU2 ONLY

15. APU MECH FAULTS WHAT HAPPEN? APB TRIP

16. APU ELEC FAILURE? GCR TRIP

17. HOW CAN CONNECT BTB? MAN OR AUTO

18. BAT BOOSTER OUTPUT? 23V

19. WHERE PMG AC VOLTAGE CONVERTED TO DC? INSIDE GEN OR GCU?

20. FOR MEASURING REACTIVE POWER?CURRENT FROM PHASE B, VOLT FROM PHASE A,C

21. WHEN BEARING FAILURE? DISCONNECT CSD

22. HOW CAN POWER THE GND HAND BUS? GND ONLY, EXT PWR CONNECTED

23. EXT POWER AND APU ARE CONNECTED WHAT’S PRIORITY? EXT (FOR HAND BUS)

24. SSB GREEN LIT IS ON MEANS? SSB OPEN

25. NORM SOURCE OF DC BUS? TR

26. RADIO BUS SW AND MASTER RADIO SW LOCATION? P5

27. WHERE ARE DC ISO SW’S? P4

28. NORM SOURCE OF AC ESS? AC4

29. CSD IS A? HYDROMECHANICAL

30. APU BAT CHARGER LOCATION? E8 IN AFT

31. ELCU CONTROL SWITCH SYS? GALLY

32. IF BOTH EXT POWER OR BOTH APU CONNECTED? SSB TRIP

33. OUTPUT POWER OF ENG’S? 60KVA

34. OUTPUT POWER OF APU? 90KVA

35. WHICH BUS POWERS F/O RADIO BUS? AC2

36. DIFF OF APU AND ENG GEN’S? APU HASN’T CSD

37. CSD SPEED? 8000RPM

38. WHICH ONE CONTROLS APU RPM? ETC

39. WHAT KIND OF WIRE USED IN A/C? ALUMINUM

40. CSD HAS CAPABILITY OF? UNDERDRIVE(NO OVERDRIVE)

41. HOW CAN READ GEN FAULTS? PUSH READ P/B ON ANN PNL

42. HOW ERASE FAULTS? READ AND ERASE AT THE SAME TIME

43. DC STBY NORM POWERED BY? DC ESS

44. WHICH BAT NEED FOR APU STARTING? BOTH BAT

45. MAN ON POS OF INV? FOR TEST

46. BAT BOOSTER USED FOR? VHF1, VOR1, G/S1

47. BAT BOOSTER LOCATION? UPPER EQUIP CENTER

48. INV LOCATION? UPPER EQUIP CENTER

49. BAT CHARGING MODES? PULSING, CONSTANT POTENCIAL, NORMAL

50. PULSING USED FOR? WHEN BAT IS FULLY CHARGED

51. FAULT IN SYNC BUS? LOAD LIT ON

52. GND HAND BUS CAN POWER BY? APU1 AND EXT1

53. WHEN BAT CHARGING HOT BAT BUS POWERED BY? BAT

54. TEMP FOR STOP BAT CHARGING? 58DEG

55. APU BAT CHARGER POWERED BY? GND SRVC BUS

56. IF CSD DISCONN WHICH ONE TRIP? GCB

A310 ELECTRONIC QUESTION EXAMPLE

A310 ELECTRONIC QUESTION  EXAMPLE

1.       WHICH SYS’S ARE FAIL OP?   Y/D & P/T

2.       VM SHOWN BY A? GREEN DOT IN CLEAN CONFIG

3.       Y/D FUNC? DAMP THE  DUTCH ROLL 

4.       PITCH SERVO LOCATION? L/H ELEV

5.       EACH A/P SEVO? 1 SERVO AND 2 FU(FOLLOW UP)

6.       ROLL SERVO IS IN R/H WING

7.       DUTCH ROLL GAIN?  DECREASED IF SPD INCREASE

8.       V2 CLEARED? AFTER T/O

9.       FAC LOCATION? #1 IN 83VU, #2 IN 84VU

10.   TURN COORD FUNC AVAIL IF?  A/P NOT IN CMD

11.   ATH FUNC: THR LIMIT, AUTO THR, SPD HOLD,THR HOLD

12.   THIRD ALFA PROBE USED FOR #1 AND #2 FAC

13.   A/P ENG ON GND? IN CWS

14.   A/P ENG ON FLT? IN CMD

15.   COMM BETWEEN MTP AND AFCS? IS ARINC429

16.   A/P LEVER IS? DISCRET

17.   A/P ENG ON GND? HYD IS NESSARY (BUT FOR Y/D CAN REPLACE WITH L/G COMPRESS)

18.   IN A/P ENG BANK ANGLE MUST LESS THAN 45

19.   YES, NO, DISPLAY PUSH AT SAME TIME FOR READ SEVERAL PREVIOUS FAULTS

20.   MTP MEMORIZE  64 PREVIOUS LEG FAILUIRE

21.   EACH COMPUTER IN AFCS HAS COMMAND AND MONITOR?  FAIL PASSIVE

22.   A/P#1 USE G HYD AND #2 USE Y

23.   ATS ARM? THRUST LIMIT COMPUTED

24.   THR LIM SHOWN ON? TRP

25.   TEMP OF FLX T/O MUST BE … THAN TAT? GREATER

26.   BASIC MODE FOR A/P OR FD? V/S AND HDG HOLD  

27.   ATS LEVER ARM WHAT ON FMA? AMBER MAN THR

28.   ATH MFA? IN ZONE 1

29.   CWS/CMD IN? ZONE 5

30.   LAND CAT IN ZONE 4

31.   WHICH SERVOMOTOR HAS 2 MOTOR IN ONE PACKAGE? P/T

32.   PTW MOVE MANUALLY? BOTH P/T DESENGAGED THEN Y/D THEN A/P TRIP

33.   P/T ELEC STOP BEFOR MECH STOP

34.   LAND CAPIBILITY CHANGE? TRIPLE CLICK

35.   TRP TO TCC IS (BI-DIRECTIONAL ) 2 WAY BUS

36.   PROFILE IS LONG MODE

37.   VOR IS LAT MODE

38.   COMM MODED: T/O,LAND,G/A

39.   Y/D PRIORITY IS BECAUSE? SERVO#1 HAS A BIGGER CYLENDER

40.   AFS/LAND TEST AND GND SCAN NOT AVAIL IN FLT

41.   WHICH AFCS TEST PNL P/B AVAIL IN FLT? DISPLAY,CLEAR

42.   Y/D HAS FEED BACK TO PEDAL? NO

43.   FAC SEND TO TCC? SPD LIM( VMAX, VMIN) ,AFS DISCRET 2, ALFA FLOOR PROTECTION

44.    IN LAND MODE IF ONE G/S FAIL?  G/S FLAG AND AUTO LAND FLASHE

45.  CVR LOCATION? PRESSURIZED AREA

46.  CVR TEST FROM? PNL AND UNIT

47.  VHF LOCATION? #1 IN 96VU, #2 IN 86VU, #3 IN 85VU

48.   HF PNL LOCATION? BOTH IN PEDESTAL

49.  HF HAVE ONE ANT AND 2 COUPLER

50.  COUPLER IS BETWEEN ANT AND UNIT

51.  VHF AND VOR TEST ON UNIT,LRU STATUS REMAIN OFF WHAT’S THE FAULT? LRU FAULTY

52.  SQL/LAMP TEST? SQUELTCH DISABLED

53.  PA SELECTOR ON UNIT POS TO OPERAT PANORMALLY ? MUST IN OPERATE

54.  PA LOAD POS? SHOWS MAIN AMP LOAD MUST>30

55.  HF#1 AND #2 WORK TOGETHER? ONLY IN RECEPTION MODE

56.  ATC GIVE SIG TO DME FOR? PREVENT INTERFERENCE

57.  COUPLER MA ON MTP? IF PRESS DROP OR ANY FAULT IN COUPLER

 58.  DFDR POWER? 115VAC ESS

59.  LA (LINEAR ACC) LOCATION? CABIN FLOOR NEAR CG

60.  LA POWERED FROM? DFDAU

61.  LA OUTPUT TO? DFDAU

62.  SGU INPUTS ARE? ARINC AND DISCRET

63.  EFIS INPUTS ARE? DIGITAL AND ANALOGE

64.  EFIS DU’S INPUTS? ALL VIA SGU ONLY

65.  WHICH STATEMENT IS CORRECT? EACH FRAM HAS 4 SUB,256 WORD,768 BIT/S, 768 BIT

66.  DFDAU OUTPUTS TO DFDAU? HARVARD BI-PHASE

67.  DFDR RECORDS? 25HOUR

68.  WHICH CLOCK FOR DFDR? CLOCK#2 ALSO FOR FMC2

69.  WHITE MSG ON L/H ECAM MEANS?  ACTION PERFORMED

70.  INPUTS OF SDAC?150 ANALOGE ,200DISCRET

71.  SAT IN CRUISE PAGE AND TAT IN MEMO

72.  LEVEL 2 WARN? NO IMMIDATE ACTION NEED

73.  STATUS PAGE? SHOWN AFTER CLEAR THE FAULT OR ACTION PERFORMED

74.  ALL INFORMATIO TO SGU FROM? MEMO FROM SDAC AND WARN FROM FWC

75.  STATUS PAGE CAN SELECT? FROM ECP AND AUTO

76.  EFIS FAULT? LOAD LIT ON ECAM BITE P/B

77.  FWC PROCESS FAIL? NOTHING HAPPEN

78.  DFDAU FAIL IN FLT WHAT IS IND? NOTHING

79.  CRUISE PAGE ON GND? FWC CB 1 AND 2 OUT

80.   NAV/VOR/ILS SW LOCATED? IN COMPLEMENTARY PNL

81.   FPA SEL FROM? EFIC COMPLEMANTARY PNL

82.   ILS#1 SHOWN ON? CAPT PFD AND F/O ND

83.   R/A #1 SENDS TO EGPWS

84.   W/R SHOWN ON? ND IN ARC AND MAP

85.   W/R CAN DISABLE FROM? ITS PNL AND EFIS PNL ALL MODE EXCEPT ARC AND MAP

86.   W/R GAIN MANUALL INCREASE? MAP MODE ONLY

87.   WHICH MODE RECEIVES INFORMATION FROM FMC? MAP

88.   DH SHOWN ON? PFD

89.   TA SHOWN ON VSI BY? FILLED CIRCLE

90.   MACH VALUE SHOWN IN PFD AT LOWER L/H? MORE THAN 0.5

91.   EACH ENVIRONMENT A/C SYS COSIST OF? 1 TAT 1 PITOT 2 STATIC PROBE

92.   R/A#1 FAIL? AUTO TRANSFER TO R/A#2

93.   ADF FAIL WHAT SHOWN ON ND? POINTER CLEARD (FLAG IS ON RMI)

94.   ADF SHOWN IN ND? ARC AND ROSE MODE

95.   ADC#1 FAILS FOR TAT? EFIS AUTO TRANSFER TO ADC #2

96.   F/O USING SGU#3, IF CAPT SELECT SGU#3? SGU#3 USED FOR CAPT AND F/O BACK TO SGU#2

97.   COMMAND SIG IN PROFILE MODE COME FROM? FMC

98.   COMMAND SIG FOR NAV? FMC

99.   HECK ATT, CHECK HDG COMES FROM? FWC

100.            IRS CAN ALIGN FROM? FMS CDU AND ISDU

101.            IRS ALIGNED FROM FMS CDU? ENTER TO FROM OR ENTER LONG AND LAT

102.            IF IRU FAIL? VSI/TCAS RANGE FLAG

103.            HOW MANY GYROS IN IRU? 3

104.            IRU TEST FROM? ASTP(AV SYS TEST PNL) (  MTP)

105.            IRS CONT DISPLAY SEGMENTS CAN CHECK? ANN LIT TEST AND TEST POS IN IRS CDU

106.            GPWS WARN INHIBIT WHEN? STALL WARN

107.            ADF SHOWS? RELATIVE BEARING AND MAG BEARING  IF HDG AVAIL

108.            ADF HAS? 2 ANT WHICH EACH HAS 3 PART  IN 1 HOUSING

109.            R/A UNIT LOCATION? AFT CARGO IN DOOR

110.            ADC SW? FMC  AUTO SW , BUT FOR FAC AND IRU MAN MUST SEL ADC INST SW

111.            ADC LOCATION? 96 AND 86VU

112.            EGPWS SELF TEST INHIB? BELOW 1000FT

113.            FMS DATA SHOWN? MAP AND PLAN

114.            W/R AVAIL IN? MAP AND ARC

115.            A/C SYMBOL SHOWS? MAG TRACK