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ATR INDICATIONS AND REPORTING > Reporting > Flashcards

Reporting Flashcards

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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
THE FLIGHT INSTRUMENTS SYSTEM INCLUDES:
5 x DUs, 2 x EFCPs, 2 x ICPs, 2 x MCDUs, 2 x MCPs AND 2 x SWITCHING PANELS
26
THE AUTOFLIGHT CONTROL SYSTEM (AFCS) IS MANAGED BY:
TWO AUTOFLIGHT CONTROL APPLICATIONS (AFCA) OF THE CACs
27
THE AFCAs RECEIVE DATA FROM:
A) 2 x ADC B) 2 x AHRS C) AIRCRAFT EQUIPMENT SUCH AS NAVIGATION EQUIPMENT AND SENSORS
28
EACH DU CAN DISPLAY DIFFERENT FORMATS:
A) PRIMARY FLIGHT DISPLAY (PFD) B) MULTI FUNCTION DISPLAY (MFD) C) THE ENGINE AND WARNING DISPLAY (EWD)
29
THE MFD SHOWS:
NAVIGATION DISPLAY, MEMO DISPLAY, VCP AND SYSTEM DISPLAY (SD)
30
THE NAVIGATION DISPLAY (ND) CAN BE SET UP IN:
ARC MODE, ROSE MODE + PLAN MODE
31
THE SYSTEM DISPLAY (SD) PAGE CAN SHOW:
CABIN PAGE, ELECTRICS PAGE, HYDRAULICS PAGE, ENGINE SECONDARY PAGE
32
THE EWD INCLUDES:
ENGINE PARAMETERS AND ALERT WINDOW
33
THE EWD INCLUDES:
FLIGHT CONTROLS, TRIMS, BRAKES, TEST STATUS AND PRIMARY ENGINE WINDOW
34
THE MULTI PURPOSE CONTROL (MCP) PANEL ALLOWS ACCESS TO:
A) COMM, NAV AND SURVEILLANCE PAGES B) MULTI DIRECTIONAL PAD AND NUMERIC KEYBOARD
35
THE STANDBY INSTRUMENTS INCLUDE:
AN INTEGRATED ELECTRONIC STANDBY INSTRUMENT
36
THE WEATHER RADAR IS ACCESSED USING:
THE SURV PB
37
THE IESI ARCHITECTURE INCLUDES:
VOR ILS, VHF, AIRSPEED SCALE AND BAROMETRIC REFERENCE
38
THE SET SWITCH ON THE IESI ALLOWS:
A) COURSE ADJUSTMENT WHEN IN VOR MODE B) VHF NAV TUNING C) VHF COMM TUNING
39
THE CONTROL AND DISPLAY SYSTEM (CDS) ENABLES THE FLIGHT CREW TO ACCESS:
A) FLIGHT INFORMATION B) AIRCRAFT ENVIRONMENT & AIRCRAFT SYSTEM STATUS C) AIRCRAFT ALERTS, PROCEDURES, CHECKLISTS
40
CDS MANUAL REVERSION IS CONTROLLED BY:
TWO REVERSION PBS
41
ON THE GROUND AIRCRAFT POWERED BY BATTERIES WHICH DUs ARE RESPECTIVELY CONFIGURED AS EWD AND SD ENGINE PAGE:
DU 2 & DU4
42
HOW MANY DUs ARE POWERED ON BATTERIES ONLY:
2
43
MANUAL FORMAT RECONFIGURATION IS CONTROLLED BY:
A) PFD/EWD/MFD PB ON THE CAPT SIDE B) PFD/EWD/MFD PB ON THE F/O SIDE
44
ELAPSED TIME ON THE CLOCK CONTROLS THE FOLLOWING FUNCTION:
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
THE CHRONO PB CAN BE USED FOR THE FOLLOWING:
A) TO START THE CHRONOMETER B) TO STOP THE CHRONOMETER C) TO RESET THE LCD DISPLAY
46
THE AIRCRAFT IS EQUIPPED WITH WHICH OF THE FOLLOWING SOLID STATE RECORDERS:
A) COCKPIT VOICE RECORDER B) FLIGHT DATA RECORDER
47
THE SOLID STATE VOICE RECORDER STARTS AUTOMATICALLY WHEN:
WHEN ONE ENGINE IS STARTED
48
THE EFIS CONTROL PANEL LOCATED ON THE CENTRAL PEDESTAL ENABLES CONTROL OF;
A) MFD B) NAV C) WARNING DISPLAY
49
HOW CAN THE PERFORMANCE PAGE BE DISPLAYED ON THE ND?
BY SELECTING “PERF” PB ON THE MFD
50
THE MULTI PURPOSE CONTROL PANEL (MCP) ENABLES:
A) COCKPIT CREW TO CONTROL THE VIRTUAL CONTROL PANEL FORMAT ON MFD B) SELECTION OF THE TCAS
51
WHEN AUTO SPEED IS SELECTED ON THE ICP WHAT COLOUR DOES IT DISPLAY IN:
MAGENTA
52
THE FOLLOWING PUSH BUTTONS/SWITCHES ARE CIRCLED IN AMBER TO HELP THE FLIGHT CREW FIND THEM IN CASE OF SMOKE (FLUORESCENT PAINTING)?
A) BTC, DC SVCE/UTLY BUS, ACW GEN 1/2 B) EXHAUST MODE, OVBD VALVE SELECTOR C) RECIRC FAN ½
53
AN AMBER COLOUR IS USED FOR:
A) ICING CONDITION DATA B) DETECTED MALFUNCTIONS C) ABNORMAL RANGE DATA
54
A CYAN COLOUR IS ASSOCIATED WITH:
MANUAL OPERATION
55
A GREEN COLOUR IS DEDICATED TO:
AUTOMATIC NORMAL FUNCTIONING AND COMPUTED DATA IN THE NORMAL RANGE FOR EACH INTERFACE E.G. CONTROL PANEL DISPLAY UNIT AND MCDU
56
A MAGENTA COLOUR IS USED TO DISPLAY:
B) ACTIVE SPEED CONSTRAINTS C) ALTITUDE CONSTRAINTS
57
HOW ARE INVALID SIGNALS DISPLAYED?
AMBER CROSSES OR DASHES
58
What colour is the active or selected emergency procedure title
Red
59
A FAILURE DETECTION SEQUENCE FOLLOWS WHICH OF THE BELOW:
INFORMATION, IDENTIFICATION, ISOLATION
60
THE CLACKER SOUNDS AT:
VMO
61
THE WHOOLER SOUNDS WHEN THE PITCH TRIM IS IN MOTION FOR MORE THAN:
1 SECOND
62
WHAT AURAL ALERT IS USED FOR ALTITUDE?
C CHORD
63
THE ROLL ATTITUDE ON THE ALTITUDE DISPLAY INDICATOR (ADI) HAS THE FOLLOWING FIX SCALE REFERENCE MARKS:
10, 20, 30, 45 & 60 DEGREES
64
THE HORIZON AND PITCH SCALE ON THE ALTITUDE DISPLAY INDICATOR (ADI) HAS THE FOLLOWING REFERENCE MARKS:
2.5° UP OR DOWN TO 20°, THEN MARKS AT 25°, 30°, 50° & 80°
65
What colour are the flight director command bars
Green
66
WHAT IS THE TCAS RANGE WHEN SELECTED ABOVE:
-2700FT TO +9900FT
67
WHICH OF THE FOLLOWING DOES THE MEMO PANEL DISPLAY?
A) FUEL CROSS FEED CONTROL B) ANTI-ICING CONTROL C) DE-ICING CONTROL
68
WHAT IS THE COLOUR CODING FOR A SYSTEM THAT IS SELECTED OFF?
WHITE
69
WHEN THE TAKE-OFF INHIBIT IS SELECTED FOR TAKE-OFF WHAT ALERTS ARE INHIBITED:
ALL OIL AND SMOKE WARNINGS
70
WHAT IS THE ASSOCIATED AURAL ALERT FOR STALL?
CRICKET
71
WHAT IS THE ASSOCIATED AURAL ALERT FOR ENGINE FIRE?
CONTINUOUS REPETITIVE CHIME
72
WHAT DOES THE TAKE-OFF CONFIG NOT TEST?
BOTH ENGINES ARE RUNNING
73
ON THE ECL WHAT COLOUR CORRESPONDS TO ACTIONS TO BE PERFORMED OR CHOICES TO BE MADE BY THE FLIGHT CREW:
CYAN
74
HOW LONG DOES THE “MAN DEL” PB BE PRESSED FOR IT TO FUNCTION?
3 seconds
75
HOW CAN THE TAKE-OFF INHIBIT BE CANCELLED?
MANUALLY DEACTIVATED BY PRESSING THE RCL PB
76
HOW LONG IS THE STICK PUSHER ACTIVATION INHIBITED AFTER TAKE-OFF?
10 SECONDS AFTER LIFT OFF
77
HOW ARE THE TWO ANGLE OF ATTACK CHANNELS TESTED?
MANUALLY TESTED ON THE LATERAL MAINTENANCE PANEL
78
THE MFD MEMO PANEL DISPLAYS THE FOLLOWING INFORMATION:
A) FUEL CROSS-FEED AND ANTI-ICING B) DE-ICING CONTROL, CABIN SEATBELT, NO DEVICE MESSAGE STATUS
79
THE VCP PRESENTS THE FOLLOWING INFORMATION WHICH CAN BE MANAGED THROUGH THE MCP:
VCP NAV, VCP COMM AND SURVEILLANCE PAGES
80
THE FWS IS COMPOSED OF THE FOLLOWING:
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
WHAT COLOUR IS THE TAKE-OFF INHIBIT MESSAGE ON THE EWD?
GREEN
82
WHAT CAUTIONS ARE NOT INHIBITED FOR TAKE-OFF?
ENGINE OIL LO PRESS
83
WHAT COLOUR IS DISPLAYED FOR A TAKE-OFF CONFIG TEST “OK”?
CYAN
84
WHERE IS THE TAKE-OFF CONFIG TEST OK DISPLAYED ON THE EWD?
ON THE FLIGHT CONTROLS, TRIMS, BRAKE MESSAGE AND TEST STATUS
85
WHICH OF THE FOLLOWING IS CORRECT FOR A STICK PUSHER SHAKER YES TEST?
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
FOR THE FLIGHT WARNING MANAGEMENT IN ECL WHICH OF THE FOLLOWING IS NOT CORRECT:
PRIORITY CHECKLIST IS BOXED
87
ON THE FLIGHT MANAGEMENT AND ECL NORMAL CHECKLISTS WHEN IS THE AFTER TAKE- OFF CHECKLIST DISPLAYED?
AFTER TAKE-OFF ONCE AIRCRAFT IS AIRBORNE

ATR INDICATIONS AND REPORTING (1 decks)

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