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Other 87 Materials > T05 > Flashcards

T05 Flashcards

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1
Q

Wing span

A

60.1 M

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2
Q

180 turn min width

A

42.0 m

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3
Q

MTOW

A

227,930

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4
Q

MZFW

A

161025

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5
Q

MAX CRZ ALT

A

43,100

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6
Q

NUMBER OF FUEL TANKS 787

A

3

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7
Q

NGS SYS

A

REDUCES FUMES AND EXPLOSIONS

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8
Q

OUTBOARD DISPLAY

A

PFD

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9
Q

M.C RESET…REMOVE EICAS MESSAGE

A

FALSE

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10
Q

M.C INHIBITED ON GRD WHEN

A

F..C.S. CUTOFF

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11
Q

TCAS OFF

A

ADVISORY MESSAGE

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12
Q

EICAS PAGE NUMBERS MEAN

A

MORE PAGES

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13
Q

NORMAL BRK TEMP

A

0-4.9

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14
Q

RTO MAX BRK

A

> 85 KTS

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15
Q

RED ENG FIRE WARNING MEANS

A

FIRE NOT STOPPED

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16
Q

NORMAL MENU USED FOR ON ECL

A

ALL NORMAL C/L COMPLETE

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17
Q

TAXI C/L INCOMPLETE

A

UNDER OWN PWR

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18
Q

INCOMP APP C/L WILL OCCUR

A

FMC TRANSITION LVL

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19
Q

AUTO FLT SYS INCLUDE

A

AFDS, 3 AP, ATT

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20
Q

FMA SHOWS WT?

A

ENGAGED OR ARM

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21
Q

USE FMA FOR ?

A

MODE ENGAGE

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22
Q

FMA CHANGE..GREEN BOX SHOWN FOR

A

10 SECS

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23
Q

LNAV ENGAGE BANK SELECTOR HAS NO EFFECT

A

TRUE

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24
Q

MCP ALT SELECTOR SELECTING AUTO

A

ALT CHANGE 100FT INCREMENTS

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25
Q

LNAV ARMED ON TOF, LNAV WILL ENGAGE AT

A

50’ AGL

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26
Q

ENG FAIL INTIAL CLIMB TARGET SPD

A

V2 TO MAX V2+15

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27
Q

IF VNAV IS ARMED FOR TOF IT ENGAGES AT 400’

A

TRUE

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28
Q

PRESSING TOGA TWICE

A

DISARMS LNAV/VNAVE

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29
Q

IF FD’S OFF THEY ARE SHOWN AUTOMATICALLY IF

A

TOGA ENGAGES

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30
Q

WHEN LOCALIZER IS CAPTURED THE INBND CRS IS AUTOMATICALLY SET

A

TRUE

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31
Q

ON ILS BELOW 1500 RA TO DISARM APP MODE

A

DIS CONNECT AP, FD’S

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32
Q

PREAUTO LAND TEST ON ILS OCCURS AT

A

1500’ RA

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33
Q

787 AUTO ALIGN WITH RWY AT

A

500-200’

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34
Q

FLARE MODE ENGAGES

A

60-40’

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35
Q

ROLLOUT OCCURS AT

A

2 FT

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36
Q

TOGA STW BECOME ARMED IN FIGHT

A

FLPS NOT UP AND G/S CAPTURE

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37
Q

AFTER PUSHING TOGA FOR GA THE THRUST FMA WILL READ

A

THR

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38
Q

LNAV ENGAGES AUTO ON A MISS APP

A

200 FT AP ENGAGED OR 50’ NO AP

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39
Q

AP DISC PUSHED TWICE WILL

A

STOP THE WARNING

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40
Q

EFB HAS CONNECTION WITH

A

FMC, FD PRINTER, [ DATALINK SYS] AND OTHER EFB

41
Q

IF COPY FMC DATA IS USED THE RECIEVED DATA WILL SHOW WITH GREEN HIGHLIGHTS

A

TRUE

42
Q

ELECTRICAL CAN BE SUPPLIED BY 1 APU GEN ON GRD OR INFLIGHT

A

FALSE, CAN NOT

43
Q

HOW DOES THE FIRST EXT PWR CONNECTED SHOW ON THE SYNOPTIC PG

A

GREEN FLOW LINE AND ENERGIZED AC SYMBOL

44
Q

HOW MANY START GEN’S ON EACH ENGINE

A

2

45
Q

WHEN WILL ENG STARTER GENS START SUPPING PWR TO THERE AC BUSES

A

AFTER THE ENG STARTED

46
Q

WT DOES MAIN BAT SUPPLY ON GRD

A

INTIAL START UP AND HELP WT APU START

47
Q

APU SUPPLIED FUEL FROM WHICH MAIN TANK

A

LEFT MAIN TANK

48
Q

WHEN CAN APU BE STARTED

A

EXT PWR AVAILABLE, MAIN ENG GENS OR APU BAT

49
Q

BAT STW MUST BE ON TO START APU

A

TRUE

50
Q

APU LIMIT SHOW ON EICAS

A

HIGH EGT [LOW OR HIGH O. TEMP LIMIT MORE THAN NORMAL]

51
Q

WHEN WOULD APU CONT TO OPERATE AFTER APU LIMIT IS SHOWN

A

INFLT/ GRD WITH ENG RUNNING OR DURING ENG START

52
Q

WHEN WOULD APU SHUTDOWN ADVISAORY BE SHOWN

A

FAULT OR FIRE… AUTO SHUT DOWN

53
Q

WHICH CONDITION WOULD INDICATE [APU SHUT DWN]

A

APU SHUT DWN AUTOMATICALLY

54
Q

WT DOES VIDEO CAB IN USE MEAN

A

VIDEO ENTERTAINMENT SYS IS IN USE

55
Q

PA SYS HAS ITS ON PTT ON ACP

A

YES

56
Q

DASHES ON TCP SHOW

A

RADIO INOP

57
Q

ON GRD WT ENG SHUT DN, RADIOS AUTO DE-ENERGIZE IF TRANSMIT..

A

35 SECS

58
Q

ACT WPT ON LEGS

A

MAGENTA

59
Q

ACTIVE WPT ON ND

A

MAGENTA

60
Q

MODIFIED RTE IS SHOWN

A

BLUE LINE NOT DASH MAGENTA

61
Q

CAN CONDITIONAL WPT BE ENTERED BY CREW

A

NO –FALSE

62
Q

ACTIVE WPT CLEARANCE CHANGES THE

A

ACTIVE WPT

63
Q

HOLDING PATTERN BECOMES ACTIVE

A

AT FIX

64
Q

HOW MAY VNAV PHASES OF FLT

A

5

65
Q

VNAV CLB STARTS

A

THR REDUCTION TO TOP OF CLB

66
Q

VNAV APP PHASE CONTINUES UNTIL LAND, GA OR PAST LAST WPT

A

TRUE.

67
Q

WT DOES PHASE OF FLIGHT CONTROLS

A

HOW VNAV OPERATES

68
Q

HEIGHT ABV ORGIN IS SHOWN ON

A

TOF REF PG 2

69
Q

VNAV ALT MEANS

A

AC LVL AT MCP ALT

70
Q

VNAV CRZV PG WHEN WILL STEP FIELD WILL GO BLANK

A

WITH IN 200 TOD OR 500 NM FROM DESTINATION

71
Q

WHICH INCORRECT DATA CAN CAUSE PROBLEMS DURING DES

A

INCORRECT WINDS / ALTITUDE/AIRSPEED CONSTRAINTS

72
Q

STRONGER TAIL WIND IN DES

A

DECREASE PITCH, DRAG REQUIRED

73
Q

DES DIR SHOWS

A

IF ONE OR MORE WPTS BTW WAY POINT AND END OF DESCENT

74
Q

MAGENTA SPD BAND ON PFD

A

RANGE OF SPD…STAY ON PATH

75
Q

IF AIRSPD INCREASE ABV TARGET SPD IN VNAV PATH…

A

FMC…THRUST IDLE….TRY KEEP IN THE BAND

76
Q

IF AIRSPD DECREASE MORE THAN 15KTS BELOW TARGET DES SPD

A

FMC ADDS THRUST

77
Q

HYD PRESS IS REMOVED AFTER LANDING GR AND DOORS ARE UP AND LOCKED

A

TRUE

78
Q

GEAR OPS SPD

A

270 KTS-0.82M

79
Q

RUDDER PEDAL TURN NOSE WHEEL MAX

A

8 DEG

80
Q

PURPOSE OF RUDDER PEDAL DISCONNECT STW?

A

DOESN’T LET NOSE WHEEL MOVE DURING FLIGHT CONTROL CHECK

81
Q

IF NOSE GEAR ISOLATION VALVE IS CLOSED ..NOSE WHEEL IS UNAVAILABLE..

A

FALSE

82
Q

RUDDER PEDALS CONTROLS

A

NOSE WHEEL STEERING AND RUDDER

83
Q

WHAT KEEPS REV THR FRM GOING BEYOND REV IDLE ON FIRST PULL

A

SOLENOID OPERATED INTERLOCK BLOCKS REV THR UNTIL REVERSER DEPLOYED

84
Q

WHEN DOES AURAL CANCEL RESETS

A

GRD + ENG SHUT DOWN

85
Q

WHEN CAN G/S INHIBIT BE SET

A

DES BELOW 1500 AGL

86
Q

IF GLIDE SLOPE ALERT IT STOPSS

A

IF AIRPLANE MOVES BACK TO GLIDE SLOPE

87
Q

TERR DATA IS SHOWN

A

ND, VSD, MINI MAP

88
Q

ONLY TER WITHIN 2000’ OF AIRPLANE ALT IS SHOWN ON ND AND MINI MAP

A

TRUE

89
Q

PWS STARTS ON GRD

A

ONE ENG SET TO TOF THRUST

90
Q

IN-FLIGHT WIND SHEAR WARNING AREA IS

A

0.5 TO 1.5 MILES

91
Q

PWS BLIND SPOT IS FROM NOSE TO

A

0.5 MILE

92
Q

PWS ALERTS ONLY OCCUR BELOW

A

1200’ RA

93
Q

TOO LOW TERR IS CAUSED BY

A

A/C NT IN LND CONFIG AND LOW RADIO ALT

94
Q

TRAFFIC ADV CAUTION GIVEN

A

48-20 SEC BEFORE NPA

95
Q

TCAS ND IS SELECTED TO 80 NM

A

3 MIL RING SHOWS AROUND AIRPLANE SYMBOL

96
Q

BELOW 1000 FT RA TCAS AUTO SWT

A

TA ONLY

97
Q

ARE TCAS DES RA ARE INHIBITED BELOW 1650 ON TOF

A

FALSE

98
Q

TCAS DES RA ARE INHIBITED FROM

A

1200 RA

99
Q

DURING APP ALL TCAS RA’S ARE INHIBITED BELOW

A

1000

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