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ATR INDICATIONS AND REPORTING > Reporting > Flashcards

Reporting Flashcards

1
Q

THE MPC UNIT INCLUDES THE FOLLOWING:

A

FLIGHT DATA ACQUISITION UNIT

DATA MANAGEMENT UNIT

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2
Q

THE AIRCRAFT PERFORMANCE MONITORING INPUTS INCLUDE:

A

PRESSURE ALTITUDE, SAT, IAS, ENG TQ

PROP ROTATION SPEED, LANDING GEAR AND FLAPS SENSOR INPUT

AIRCRAFT WEIGHT REQUIRING FLIGHT CREW SELECTION BEFORE EACH TAKE-OFF VIA
THE APM WEIGHT ROTARY SELECTOR

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3
Q

THE FDAU ACQUIRES DATA FROM WHICH OF THE BELOW SYSTEMS:

A

FLIGHT DATA RECORDING

AIRCRAFT PERFORMANCE MONITORING

DATA BROADCAST TO CAC (TO AVIONICS SYSTEM)

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4
Q

THE INDICATION “INCREASED SPEED” AMBER MESSAGE INDICATES:

A

THE AIRCRAFT SPEED IS LOWER THAN THE MINIMUM ICING SPEED +1OKTS

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5
Q

THE INDICATION “DEGRADED PERF” ON THE ALERT WINDOW IN LEVEL FLIGHT MEANS:

A

DRAG ABNORMALLY HIGH & IAS SIGNIFICANT DECREASE COMPARED TO MAXIMUM
CRUISE SPEED

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6
Q

THE MFC SYSTEM CONSISTS OF:

A

2 COMPUTERS, EACH WITH 2 MODULES

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7
Q

THE SELF TEST SEQUENCE OBSERVED DURING POWER UP IS:

A

MFC 1A & MFC 2A FLASH, THEN MFC1B & MFC 2B FLASH

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8
Q

THE INDICATION “MFC 2A” ON THE ALERT WINDOW MEANS:

A

A SINGLE MFC CHANNEL FAILURE

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9
Q

THE INDICATION “MFC 1A + MFC 2B” AMBER MESSAGE ON THE EWD MEANS:

A

A SINGLE CHANNEL FAILURE OF EACH MFC MODULE

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10
Q

THE INDICATION “MFC 1A + MFC 1B” AMBER MESSAGE ON THE EWD MEANS:

A

MULTIPLE MFC CHANNEL FAILURES

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11
Q

THE INTEGRATED MODULAR AVIONIC (IMA) PROVIDES:

A

COMPUTATION AND MEMORY

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12
Q

THE INTEGRATED MODULAR AVIONIC (IMA) IS MAINLY COMPOSED OF

A

A DUAL CORE AVIONICS CABINET

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13
Q

THE CORE AVIONICS CABINET (CAC) EQUIPMENT COMPRISES OF:

A

A RACK AND SET OF CARDS

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14
Q

IN BASIC CONFIGURATION EACH CAC INCLUDES:

A

1 CORE PROCESSING MODULE (CPM)

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15
Q

IN BASIC CONFIGURATION EACH CAC INCLUDES:

A

1 IOM-S (INPUT OUTPUT MODULE)

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16
Q

IN BASIC CONFIGURATION EACH CAC INCLUDES:

A

2 x IOM-DC

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17
Q

THE CORE PROCESSING MODULE PROVIDES:

A

SHARED MEMORY COMPUTATION RESOURCES TO EXECUTE HOSTED AVIONICS
APPLICATIONS

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18
Q

THE SWM (GATEWAY AND SWITCH MODULE) PROVIDES:

A

CONNECTION BETWEEN THE CPM AND OTHER AVIONICS DATA NETWORK SUBSCRIBERS

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19
Q

THE MAIN APPLICATIONS HOSTED BY THE CORE AVIONICS CABINET INCLUDE:

A

FLIGHT WARNING (FWA) AND AUTOFLIGHT (AFCA)

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20
Q

THE CAC 1 AND 2 COMMUNICATE WITH:

A

5 DISPLAY UNITS – DU1, DU2, DU3, DU4, DU5

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21
Q

THE CAC 1 AND 2 COMMUNICATE WITH FIVE DISPLAY UNITS AND SYSTEMS THROUGH
DIFFERENT DATA BUS FORMATS INCLUDING:

A

AFDX: AVIONICS FULL DUPLEX SWITCHED ETHERNET AND A429: ARINC 429

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22
Q

TWO OF THE FIVE DISPLAY UNITS (DUs) ARE DEDICATED TO TWO ADDITIONAL
APPLICATIONS – FMA AND RMA. THESE DUs ARE:

A

DU2 AND DU4

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23
Q

. IF THE CARGO DOOR CONTROL PANEL HAS BEEN OPENED WHICH SELF TEST WILL
COMMENCE:

A

MFC 1A + MFC 2A

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24
Q

ACMS FUNCTIONS ARE:

A

QAR/DAR REPORTING ON A PCMIA DISK

MANAGEMENT OF REPORTS

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25
Q

THE FLIGHT INSTRUMENTS SYSTEM INCLUDES:

A

5 x DUs, 2 x EFCPs, 2 x ICPs, 2 x MCDUs, 2 x MCPs AND 2 x SWITCHING PANELS

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26
Q

THE AUTOFLIGHT CONTROL SYSTEM (AFCS) IS MANAGED BY:

A

TWO AUTOFLIGHT CONTROL APPLICATIONS (AFCA) OF THE CACs

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27
Q

THE AFCAs RECEIVE DATA FROM:

A

A) 2 x ADC
B) 2 x AHRS
C) AIRCRAFT EQUIPMENT SUCH AS NAVIGATION EQUIPMENT AND SENSORS

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28
Q

EACH DU CAN DISPLAY DIFFERENT FORMATS:

A

A) PRIMARY FLIGHT DISPLAY (PFD)
B) MULTI FUNCTION DISPLAY (MFD)
C) THE ENGINE AND WARNING DISPLAY (EWD)

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29
Q

THE MFD SHOWS:

A

NAVIGATION DISPLAY, MEMO DISPLAY, VCP AND SYSTEM DISPLAY (SD)

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30
Q

THE NAVIGATION DISPLAY (ND) CAN BE SET UP IN:

A

ARC MODE, ROSE MODE + PLAN MODE

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31
Q

THE SYSTEM DISPLAY (SD) PAGE CAN SHOW:

A

CABIN PAGE, ELECTRICS PAGE, HYDRAULICS PAGE, ENGINE SECONDARY PAGE

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32
Q

THE EWD INCLUDES:

A

ENGINE PARAMETERS AND ALERT WINDOW

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33
Q

THE EWD INCLUDES:

A

FLIGHT CONTROLS, TRIMS, BRAKES, TEST STATUS AND PRIMARY ENGINE WINDOW

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34
Q

THE MULTI PURPOSE CONTROL (MCP) PANEL ALLOWS ACCESS TO:

A

A) COMM, NAV AND SURVEILLANCE PAGES

B) MULTI DIRECTIONAL PAD AND NUMERIC KEYBOARD

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35
Q

THE STANDBY INSTRUMENTS INCLUDE:

A

AN INTEGRATED ELECTRONIC STANDBY INSTRUMENT

36
Q

THE WEATHER RADAR IS ACCESSED USING:

A

THE SURV PB

37
Q

THE IESI ARCHITECTURE INCLUDES:

A

VOR ILS, VHF, AIRSPEED SCALE AND BAROMETRIC REFERENCE

38
Q

THE SET SWITCH ON THE IESI ALLOWS:

A

A) COURSE ADJUSTMENT WHEN IN VOR MODE
B) VHF NAV TUNING
C) VHF COMM TUNING

39
Q

THE CONTROL AND DISPLAY SYSTEM (CDS) ENABLES THE FLIGHT CREW TO ACCESS:

A

A) FLIGHT INFORMATION
B) AIRCRAFT ENVIRONMENT & AIRCRAFT SYSTEM STATUS
C) AIRCRAFT ALERTS, PROCEDURES, CHECKLISTS

40
Q

CDS MANUAL REVERSION IS CONTROLLED BY:

A

TWO REVERSION PBS

41
Q

ON THE GROUND AIRCRAFT POWERED BY BATTERIES WHICH DUs ARE RESPECTIVELY
CONFIGURED AS EWD AND SD ENGINE PAGE:

A

DU 2 & DU4

42
Q

HOW MANY DUs ARE POWERED ON BATTERIES ONLY:

A

2

43
Q

MANUAL FORMAT RECONFIGURATION IS CONTROLLED BY:

A

A) PFD/EWD/MFD PB ON THE CAPT SIDE
B) PFD/EWD/MFD PB ON THE F/O SIDE

44
Q

ELAPSED TIME ON THE CLOCK CONTROLS THE FOLLOWING FUNCTION:

A

A) WHEN SELECTING THE ET PB THE ET DISPLAY COMES ON

B) WHEN THE ELAPSED TIME COUNTER IS STOPPED, BY STOPPING THE ET PB FOR MORE
THAN 2 SECONDS, THE DISPLAY IS BLANKED AND VALUE IS ZEROED

45
Q

THE CHRONO PB CAN BE USED FOR THE FOLLOWING:

A

A) TO START THE CHRONOMETER

B) TO STOP THE CHRONOMETER

C) TO RESET THE LCD DISPLAY

46
Q

THE AIRCRAFT IS EQUIPPED WITH WHICH OF THE FOLLOWING SOLID STATE RECORDERS:

A

A) COCKPIT VOICE RECORDER

B) FLIGHT DATA RECORDER

47
Q

THE SOLID STATE VOICE RECORDER STARTS AUTOMATICALLY WHEN:

A

WHEN ONE ENGINE IS STARTED

48
Q

THE EFIS CONTROL PANEL LOCATED ON THE CENTRAL PEDESTAL ENABLES CONTROL OF;

A

A) MFD
B) NAV
C) WARNING DISPLAY

49
Q

HOW CAN THE PERFORMANCE PAGE BE DISPLAYED ON THE ND?

A

BY SELECTING “PERF” PB ON THE MFD

50
Q

THE MULTI PURPOSE CONTROL PANEL (MCP) ENABLES:

A

A) COCKPIT CREW TO CONTROL THE VIRTUAL CONTROL PANEL FORMAT ON MFD

B) SELECTION OF THE TCAS

51
Q

WHEN AUTO SPEED IS SELECTED ON THE ICP WHAT COLOUR DOES IT DISPLAY IN:

A

MAGENTA

52
Q

THE FOLLOWING PUSH BUTTONS/SWITCHES ARE CIRCLED IN AMBER TO HELP THE FLIGHT
CREW FIND THEM IN CASE OF SMOKE (FLUORESCENT PAINTING)?

A

A) BTC, DC SVCE/UTLY BUS, ACW GEN 1/2
B) EXHAUST MODE, OVBD VALVE SELECTOR
C) RECIRC FAN ½

53
Q

AN AMBER COLOUR IS USED FOR:

A

A) ICING CONDITION DATA
B) DETECTED MALFUNCTIONS
C) ABNORMAL RANGE DATA

54
Q

A CYAN COLOUR IS ASSOCIATED WITH:

A

MANUAL OPERATION

55
Q

A GREEN COLOUR IS DEDICATED TO:

A

AUTOMATIC NORMAL FUNCTIONING AND COMPUTED DATA IN THE NORMAL RANGE
FOR EACH INTERFACE E.G. CONTROL PANEL DISPLAY UNIT AND MCDU

56
Q

A MAGENTA COLOUR IS USED TO DISPLAY:

A

B) ACTIVE SPEED CONSTRAINTS

C) ALTITUDE CONSTRAINTS

57
Q

HOW ARE INVALID SIGNALS DISPLAYED?

A

AMBER CROSSES OR DASHES

58
Q

What colour is the active or selected emergency procedure title

A

Red

59
Q

A FAILURE DETECTION SEQUENCE FOLLOWS WHICH OF THE BELOW:

A

INFORMATION, IDENTIFICATION, ISOLATION

60
Q

THE CLACKER SOUNDS AT:

A

VMO

61
Q

THE WHOOLER SOUNDS WHEN THE PITCH TRIM IS IN MOTION FOR MORE THAN:

A

1 SECOND

62
Q

WHAT AURAL ALERT IS USED FOR ALTITUDE?

A

C CHORD

63
Q

THE ROLL ATTITUDE ON THE ALTITUDE DISPLAY INDICATOR (ADI) HAS THE FOLLOWING FIX
SCALE REFERENCE MARKS:

A

10, 20, 30, 45 & 60 DEGREES

64
Q

THE HORIZON AND PITCH SCALE ON THE ALTITUDE DISPLAY INDICATOR (ADI) HAS THE
FOLLOWING REFERENCE MARKS:

A

2.5° UP OR DOWN TO 20°, THEN MARKS AT 25°, 30°, 50° & 80°

65
Q

What colour are the flight director command bars

A

Green

66
Q

WHAT IS THE TCAS RANGE WHEN SELECTED ABOVE:

A

-2700FT TO +9900FT

67
Q

WHICH OF THE FOLLOWING DOES THE MEMO PANEL DISPLAY?

A

A) FUEL CROSS FEED CONTROL

B) ANTI-ICING CONTROL

C) DE-ICING CONTROL

68
Q

WHAT IS THE COLOUR CODING FOR A SYSTEM THAT IS SELECTED OFF?

A

WHITE

69
Q

WHEN THE TAKE-OFF INHIBIT IS SELECTED FOR TAKE-OFF WHAT ALERTS ARE INHIBITED:

A

ALL OIL AND SMOKE WARNINGS

70
Q

WHAT IS THE ASSOCIATED AURAL ALERT FOR STALL?

A

CRICKET

71
Q

WHAT IS THE ASSOCIATED AURAL ALERT FOR ENGINE FIRE?

A

CONTINUOUS REPETITIVE CHIME

72
Q

WHAT DOES THE TAKE-OFF CONFIG NOT TEST?

A

BOTH ENGINES ARE RUNNING

73
Q

ON THE ECL WHAT COLOUR CORRESPONDS TO ACTIONS TO BE PERFORMED OR CHOICES TO
BE MADE BY THE FLIGHT CREW:

A

CYAN

74
Q

HOW LONG DOES THE “MAN DEL” PB BE PRESSED FOR IT TO FUNCTION?

A

3 seconds

75
Q

HOW CAN THE TAKE-OFF INHIBIT BE CANCELLED?

A

MANUALLY DEACTIVATED BY PRESSING THE RCL PB

76
Q

HOW LONG IS THE STICK PUSHER ACTIVATION INHIBITED AFTER TAKE-OFF?

A

10 SECONDS AFTER LIFT OFF

77
Q

HOW ARE THE TWO ANGLE OF ATTACK CHANNELS TESTED?

A

MANUALLY TESTED ON THE LATERAL MAINTENANCE PANEL

78
Q

THE MFD MEMO PANEL DISPLAYS THE FOLLOWING INFORMATION:

A

A) FUEL CROSS-FEED AND ANTI-ICING

B) DE-ICING CONTROL, CABIN SEATBELT, NO DEVICE MESSAGE STATUS

79
Q

THE VCP PRESENTS THE FOLLOWING INFORMATION WHICH CAN BE MANAGED THROUGH
THE MCP:

A

VCP NAV, VCP COMM AND SURVEILLANCE PAGES

80
Q

THE FWS IS COMPOSED OF THE FOLLOWING:

A

A) AN ALERTING WINDOW ON THE LEFT PART

B) A PROCEDURE WINDOW ON THE RIGHT PART AND A STATUS AREA DEDICATED TO THE
FWS INFORMATION ON THE BOTTOM PART OF THE PROCEDURAL WINDOW

81
Q

WHAT COLOUR IS THE TAKE-OFF INHIBIT MESSAGE ON THE EWD?

A

GREEN

82
Q

WHAT CAUTIONS ARE NOT INHIBITED FOR TAKE-OFF?

A

ENGINE OIL LO PRESS

83
Q

WHAT COLOUR IS DISPLAYED FOR A TAKE-OFF CONFIG TEST “OK”?

A

CYAN

84
Q

WHERE IS THE TAKE-OFF CONFIG TEST OK DISPLAYED ON THE EWD?

A

ON THE FLIGHT CONTROLS, TRIMS, BRAKE MESSAGE AND TEST STATUS

85
Q

WHICH OF THE FOLLOWING IS CORRECT FOR A STICK PUSHER SHAKER YES TEST?

A

A) STALL CRICKET AND BOTH STICK SHAKERS ARE ACTIVATED

B) AFTER 5 SECONDS GPWS AMBER ALERT MESSAGE IS DISPLAYED ON THE EWD

C) AFTER 10 SECONDS CHANNEL 1, CHANNEL 2 ARE ILLUMINATED, STICK PUSHER IS
ACTIVATED AND STICK PUSHER INDICATION S ILLUMINATE GREEN

86
Q

FOR THE FLIGHT WARNING MANAGEMENT IN ECL WHICH OF THE FOLLOWING IS NOT
CORRECT:

A

PRIORITY CHECKLIST IS BOXED

87
Q

ON THE FLIGHT MANAGEMENT AND ECL NORMAL CHECKLISTS WHEN IS THE AFTER TAKE-
OFF CHECKLIST DISPLAYED?

A

AFTER TAKE-OFF ONCE AIRCRAFT IS AIRBORNE

ATR INDICATIONS AND REPORTING (1 decks)

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