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