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

A310-200/300 NAV DME

DME

1. DME TR IS INTROGATOR WORK IN 63MHZ CONT BY VOR CONT PNL
2. DISTANCES SHOWN IN RMI TOP AND PFD
3. DME ANT AND ATC ARE I/W EACH OTHERS
4. ON RMI IF NCD SHOWN WITH --- ,IF FAULT IT BECOME BLANK
5. FMS CAN AUTO TUNE THE DME
6. LOC TUNE SO G/S AND DME AUTO TUNE

A310-200/300 NAV R/A

R/A

1. R/A #1 GOES TO EGPWC

2. BOTH R/A UNIT LOST IN SMOKE PROCEDURE

3.  R/A TR POWERED FROM 301XP

4. DH SHOWN ON PFD

A310-200/300 NAV ILS

 

ILS

1. LOC FRQ IS 108.10 TO 111.95MHZ PAIRED WITH G/S FRQ
2. G/S FRQ IS 329.15 TO 335 MHZ
3. ILS DEV CAN BE SEEN IN ROSE AND ARC
4. ILS#1 SHOWN ON CAPT PFD AND F/O ND
5. LOC TUNE SO G/S AND DME AUTO TUNED

A310-200/300 NAV VOR

VOR

1.FRQ IS 108 TO 118MHZ


2.VOR UNIT IS IN 85 AND 86VU
3.VOR DEV AND TO/FROM COMPUTED IN EFIS SGU
4.VOR SHOWN ON ND AND RMI

B747-200/300 NAV-ATC

ATC

1.       A SUPPRESSION LINE SENT TO DME TO PREVENT INTERFERANCE

2.       FRQ IS 960 TO 1220MHZ

3.       ANT IS BLADE TYPE BOTH LOWER CAN I/W DME ANT              

4.       TCAS AND ATC’S ARE IN 500VU(FRONT OF W/R TR)

5.       ATC EMR CODES IS 7500,7600,7700

6.       CONT PNL POWERED BY 401XP THEN ATC#1 ALSO NORM BUS THEN TO ATC#2

7.       WARN PRIORITY:   1.STALL        2. WINSHEAR      3. EGPWS     4. TCAS

8.       TCAS HAS 2 ANT TOP AND DOWN

9.       TCAS POWERED FROM AC EMR BUS

10.   TCAS IS INTROGATOR BUT ATC IS TRANSPONDER

A310-200/300 NAV W/R

W/R
1.W/R MAP ON ND AVAIL IN ARC AND MAP

2.ANT AND CONT PNL POWERED FROM TR
3.GAIN CAN ADJUSTED IN MAP MODE OF W/R ONLY
4.ANT CAN TILT 40DEG PITCH AND 90DEG LAT(15 TIMES PER MIN) ALSO MANUALLY IS 15DEG
5.OVER TEMP FAULT LIT ON FACE OF TR IN 130°C
6.W/R MODES:
               MAP: GREEN FOR GND,YELLOW FOR TERRAIN , BLACK FOR WATER
              WX: RED IS FOR HEAVY PRESCRIPTION
              TEST: A PATTERN SHOWN

A310-200/300 NAV ADC

ADC

1.ALFA PROBE #3 USED ONLY FOR FAC FOR AOA PROTECTION AND ALFA TRIM

2.2 STBY ASI AND ONE STBY ALTEMETER

3.A/S SHOWN ON PFD AND TAS AND GS ON ND WHEN >100KT

4.TAT SHOWN ON L/H ECAM AND TRP FROM TCC

5.THERE ARE 2 TAT PROBE TO ADC’S

6.IF TCC’S FAIL ADC CAN SEND TAT TO TRP

7.SAT SHOWN IN CRUISE PAGE

8.BARO REF ON ALTEMETER SENT TO ADC’S AND CPC’S BUT STD(STANDARD) GOES TO FWC,FCC AND SGU’S

9.MACH <0.5 ON PFD SHOWN BY ---

10.ADC#1 IN 96VU AND #2 IN 86VU

11.STBY AND CAPT  PITOT PROBES ARE IN L/H BUT STATIC PROBE CAPT HAS BOTH ON L/H AND R/H ALSO F/O AND STBY

12.THERE ARE 2 TAT PROBE GOES TO ADC’S

13.TCC#1 AND SGU#1 GET TAT DATA FROM BOTH ADC

14.STBY STATIC PROBE CONNECTED TO PRESSURIZED SYS

15.STALL WARN INHIB ON GND EXCEPT TEST

16.AOA SENT TO SFCC FOR ALFA LOCK WHEN AOA>9DEG SLAT RET INHIB

17.EGPWS GET A/S SIG FROM ADC#1

18.ADC TEST DONE FROM MTP OR FRONT FACE OF UNIT

19.DURING TEST OVER SPD CAN BE TEST BY INHIB OVRD SW ON ECAM MTP

A310-200/300 NAV IRS

IRS

1. EACH IRU HAS 3 GYRO AND 3 ACC 
2. ALIGN FLASH IF ENTERED POS DIFFER FROM LAST POS

3. WHEN IRU WORKS WITH BAT ON GND, BATT OP LIT + HORN

4. IRS SW:

OFF

NAV: IN NOMAL OPERATION HDG , POS AND ATT IS AVAIL

ATT: WHEN POS LOST FROM IRU ONLY HDG AND ATT AVAIL

5. STBY HORIZON SUPP BY 303PP BUT ITS GYRO MOTOR FROM 3PHASE INVERTOR

6. IRU#1 SUPP BY BATT AND 402XP

7. INRTIAL V/S COMPUTES IN IRU

8. IRS FAIL AUTO SW FOR IVS TO BARO V/S IN VSI IF ADC FAIL ALSO MAN SW TO ADC#2

A310-200/300 NAV EFIS

EFIS
1. SGU# 1 SUPP L/H AND SGU#2 FOR R/H BUT SGU#3 SUPP BOTH SIDE BUT #1 HAS PRIORITY

2. EFIS COMPLEMENTARY PNL:
FD/FPV ON / OFF
VOR
ILS
NAV: WAY POINT SHOWN FROM FMC

3. SGU INPUTS: W/R TR, FWC’S, SDAC
4. YAW BAR APEAR IN:
LAND
T/O
ROLL OUT
DECRAB
5. R/A DATA SHOWN IF ALT<1800FT
6. ADC OR FAC FAIL CAN SW BY INST SW

7. SPD LIM FLASHES IF FAC FAIL
8. SPD FLASHES IF ADC FAIL
9. ATT FLASHED IF IRS FAIL ALSO NO SEPHERE
10. CHECK ATT FLASHES IF DESCREPANCY BETWEEN IRU’S DET BY FWC

11. PLAN MODE : MAP IS FIXED A/C SYMBOL MOVING BUT IN MAP MODE A/C IS FIXED

12. IRS FAILURE ON ND CAZ NO COMPASS ROSE ALSO HDG FLAG
13. IF FMC FAIL MAP NOT AVAIL FLAG , ROSE OR ARC MUST SEL
14. IF SGU#3 FAIL ON ECAM EFIS SGU FAULT+SSC
15. SGU#1 PFD#1 AND CAPT CONT PNL POWERED FROM AC EMER BUS (404XP)
16. ND#1 FROM AC ESS BUS

A310-200/300 IND REC AIDS

AIDS

1. DFDAU IN 90VU HAS 2 FAULT LIT ON FACE : DFDR AND DFDAU
2. DFDR POWERED WHEN GND CONT SW ON OR BOTH ENG RUN(SW NOT HELD ANY MORE)
3. DFDR FAULT LIT ON O/H PNL INHIBITED IN FLT IFF DFDAU FAILED
4. AN ACCELEROMETER UNDER CABIN NEAR CG GIVES 3 AXLE ACCELRATION TO DFDAU
5. ACC POWERED BY 28VDC

A310-200/300 IND REC FWS

FWS

1.    ALL WARN PRODUCED IN FWC EXCEPT EGPWS WARN

2.    ALL CRT CAN I/W EACH OTHER

3.    SDAC(SYS DATA ANALOGE CONVERTOR) PRODUCES THE SYS PAGES

4.    FWC#1 POWERED FROM (401XP) EMR AND NORM AC BUS, FWC#2 JUST FROM NORM BUS

5.    WARN LEVELS:

                                      3: EMR RED +CRC

                                      2: ABNORMAL AMBER +SC

                                      1: NO CHIME

                                      0: INFORMS THE SITUATION

6.       LEVEL 3 GENEREATED IN BOTH FWC BUT OTHER WARN DIVIDED TO HALF FOR EACH ECAM:

                      L/H: WARN AND STATUS AND MEMO

                      R/H: IS SYS PAGES

7.       CLR P/B WILL BE ON WHEN WARN PAGE OR STATUS PAGE DISPLAYED

8.       SYS PAGE ARE 14 BUT 12 CAN BE SEL+ CRUISE PAGE AND ENG START PAGE  AUTO

10.   AUTO CALL OUT PRODUCED IN FWC FROM 400FT TO 3FT

11.   LAND CONFIG FAIL AND FIRE NOT INHIBITED IN ANY PHASE OF FLT

12.   FWC PRODUCES 12 FLT PHASE TO INHIBT MANY WARN

13.   CHIMES IN FWC:

                        SC (SINGLE CHIME): AMBER

                        CRC (CONTINUOUS REPEATITIVE CHIME): RED

                        CLICK: LAND CAPIBILITY CHANG

                        CAVALRY CHARGE: A/P DISCONNECT

                        C CHORD: ALT ALERT

                        BUZZER: SELCAL AND CABIN

                        KETTLE: DECISION HEIGHT

                        CRICKET: STALL WARN

14.   SDAC PRODUCES ALL AMBER AND WHITE AND MEMO

15.   IF SDAC FAIL ECAM SHOWS ONLY FUEL QTY (NO MEMO)

16.   ONE FWC FAIL: HALF OF AMBER LIT LOST

17.   FWC CIRCUIT:

                        ACQUIRE: ACQ#1 SENDS TO PROC#2, IF ACQ FAIL HALF AMBER FAULT LOST

                        PROCESS: IF FAIL OTHER ONE DONE, FWC FAULT ON MTP

18.   BOTH FWC FAIL: CRUISE PAGE DISPLAYED(ENG PARAMETER AND AIR COND IF ENG P/B PRESS)

19.   ONE CRT FAIL SHOWS BLACK WITH WHITE LINE IT MUST BE OFF (SGU CAN SHOW ALL SYS PAGE AND WARN IN ONE CRT

20.SGU (SYMBOL GEN UNIT) INPUTS: FWS, SDAC, FQIC, ADC

21.   RCL P/B MUST HELD FOR 3SEC TO RECALL FAULTS

22.   EMR CANCEL P/B CAN CANCEL THE EGPWS AUDIO

23.   ECAM TEST POSSIBLE IN GND ONLY

24.   IN NORMAL CONFIG L/H DU FEED BY SGU#1 AND FWC’S AND R/H DU BY SGU#2 AND SDAC

25.   CB MONITOR NOT AVAIL WHEN ENG RUN (OIL PRESS SW GIVE THIS SIG)

26.   CRUISE AVAIL IF BOTH DU HEALTHY

27.   AMBER LIT CLEARED DON’T COMING BACK BUT RED’S DO IF FAULT  STILL EXIST