T05 Flashcards
Study
1
Q
Wing span
A
60.1 M
2
Q
180 turn min width
A
42.0 m
3
Q
MTOW
A
227,930
4
Q
MZFW
A
161025
5
Q
MAX CRZ ALT
A
43,100
6
Q
NUMBER OF FUEL TANKS 787
A
3
7
Q
NGS SYS
A
REDUCES FUMES AND EXPLOSIONS
8
Q
OUTBOARD DISPLAY
A
PFD
9
Q
M.C RESET…REMOVE EICAS MESSAGE
A
FALSE
10
Q
M.C INHIBITED ON GRD WHEN
A
F..C.S. CUTOFF
11
Q
TCAS OFF
A
ADVISORY MESSAGE
12
Q
EICAS PAGE NUMBERS MEAN
A
MORE PAGES
13
Q
NORMAL BRK TEMP
A
0-4.9
14
Q
RTO MAX BRK
A
> 85 KTS
15
Q
RED ENG FIRE WARNING MEANS
A
FIRE NOT STOPPED
16
Q
NORMAL MENU USED FOR ON ECL
A
ALL NORMAL C/L COMPLETE
17
Q
TAXI C/L INCOMPLETE
A
UNDER OWN PWR
18
Q
INCOMP APP C/L WILL OCCUR
A
FMC TRANSITION LVL
19
Q
AUTO FLT SYS INCLUDE
A
AFDS, 3 AP, ATT
20
Q
FMA SHOWS WT?
A
ENGAGED OR ARM
21
Q
USE FMA FOR ?
A
MODE ENGAGE
22
Q
FMA CHANGE..GREEN BOX SHOWN FOR
A
10 SECS
23
Q
LNAV ENGAGE BANK SELECTOR HAS NO EFFECT
A
TRUE
24
Q
MCP ALT SELECTOR SELECTING AUTO
A
ALT CHANGE 100FT INCREMENTS
25
LNAV ARMED ON TOF, LNAV WILL ENGAGE AT
50' AGL
26
ENG FAIL INTIAL CLIMB TARGET SPD
V2 TO MAX V2+15
27
IF VNAV IS ARMED FOR TOF IT ENGAGES AT 400'
TRUE
28
PRESSING TOGA TWICE
DISARMS LNAV/VNAVE
29
IF FD'S OFF THEY ARE SHOWN AUTOMATICALLY IF
TOGA ENGAGES
30
WHEN LOCALIZER IS CAPTURED THE INBND CRS IS AUTOMATICALLY SET
TRUE
31
ON ILS BELOW 1500 RA TO DISARM APP MODE
DIS CONNECT AP, FD'S
32
PREAUTO LAND TEST ON ILS OCCURS AT
1500' RA
33
787 AUTO ALIGN WITH RWY AT
500-200'
34
FLARE MODE ENGAGES
60-40'
35
ROLLOUT OCCURS AT
2 FT
36
TOGA STW BECOME ARMED IN FIGHT
FLPS NOT UP AND G/S CAPTURE
37
AFTER PUSHING TOGA FOR GA THE THRUST FMA WILL READ
THR
38
LNAV ENGAGES AUTO ON A MISS APP
200 FT AP ENGAGED OR 50' NO AP
39
AP DISC PUSHED TWICE WILL
STOP THE WARNING
40
EFB HAS CONNECTION WITH
FMC, FD PRINTER, [ DATALINK SYS] AND OTHER EFB
41
IF COPY FMC DATA IS USED THE RECIEVED DATA WILL SHOW WITH GREEN HIGHLIGHTS
TRUE
42
ELECTRICAL CAN BE SUPPLIED BY 1 APU GEN ON GRD OR INFLIGHT
FALSE, CAN NOT
43
HOW DOES THE FIRST EXT PWR CONNECTED SHOW ON THE SYNOPTIC PG
GREEN FLOW LINE AND ENERGIZED AC SYMBOL
44
HOW MANY START GEN'S ON EACH ENGINE
2
45
WHEN WILL ENG STARTER GENS START SUPPING PWR TO THERE AC BUSES
AFTER THE ENG STARTED
46
WT DOES MAIN BAT SUPPLY ON GRD
INTIAL START UP AND HELP WT APU START
47
APU SUPPLIED FUEL FROM WHICH MAIN TANK
LEFT MAIN TANK
48
WHEN CAN APU BE STARTED
EXT PWR AVAILABLE, MAIN ENG GENS OR APU BAT
49
BAT STW MUST BE ON TO START APU
TRUE
50
APU LIMIT SHOW ON EICAS
HIGH EGT [LOW OR HIGH O. TEMP LIMIT MORE THAN NORMAL]
51
WHEN WOULD APU CONT TO OPERATE AFTER APU LIMIT IS SHOWN
INFLT/ GRD WITH ENG RUNNING OR DURING ENG START
52
WHEN WOULD APU SHUTDOWN ADVISAORY BE SHOWN
FAULT OR FIRE... AUTO SHUT DOWN
53
WHICH CONDITION WOULD INDICATE [APU SHUT DWN]
APU SHUT DWN AUTOMATICALLY
54
WT DOES VIDEO CAB IN USE MEAN
VIDEO ENTERTAINMENT SYS IS IN USE
55
PA SYS HAS ITS ON PTT ON ACP
YES
56
DASHES ON TCP SHOW
RADIO INOP
57
ON GRD WT ENG SHUT DN, RADIOS AUTO DE-ENERGIZE IF TRANSMIT..
35 SECS
58
ACT WPT ON LEGS
MAGENTA
59
ACTIVE WPT ON ND
MAGENTA
60
MODIFIED RTE IS SHOWN
BLUE LINE NOT DASH MAGENTA
61
CAN CONDITIONAL WPT BE ENTERED BY CREW
NO --FALSE
62
ACTIVE WPT CLEARANCE CHANGES THE
ACTIVE WPT
63
HOLDING PATTERN BECOMES ACTIVE
AT FIX
64
HOW MAY VNAV PHASES OF FLT
5
65
VNAV CLB STARTS
THR REDUCTION TO TOP OF CLB
66
VNAV APP PHASE CONTINUES UNTIL LAND, GA OR PAST LAST WPT
TRUE.
67
WT DOES PHASE OF FLIGHT CONTROLS
HOW VNAV OPERATES
68
HEIGHT ABV ORGIN IS SHOWN ON
TOF REF PG 2
69
VNAV ALT MEANS
AC LVL AT MCP ALT
70
VNAV CRZV PG WHEN WILL STEP FIELD WILL GO BLANK
WITH IN 200 TOD OR 500 NM FROM DESTINATION
71
WHICH INCORRECT DATA CAN CAUSE PROBLEMS DURING DES
INCORRECT WINDS / ALTITUDE/AIRSPEED CONSTRAINTS
72
STRONGER TAIL WIND IN DES
DECREASE PITCH, DRAG REQUIRED
73
DES DIR SHOWS
IF ONE OR MORE WPTS BTW WAY POINT AND END OF DESCENT
74
MAGENTA SPD BAND ON PFD
RANGE OF SPD...STAY ON PATH
75
IF AIRSPD INCREASE ABV TARGET SPD IN VNAV PATH...
FMC...THRUST IDLE....TRY KEEP IN THE BAND
76
IF AIRSPD DECREASE MORE THAN 15KTS BELOW TARGET DES SPD
FMC ADDS THRUST
77
HYD PRESS IS REMOVED AFTER LANDING GR AND DOORS ARE UP AND LOCKED
TRUE
78
GEAR OPS SPD
270 KTS-0.82M
79
RUDDER PEDAL TURN NOSE WHEEL MAX
8 DEG
80
PURPOSE OF RUDDER PEDAL DISCONNECT STW?
DOESN'T LET NOSE WHEEL MOVE DURING FLIGHT CONTROL CHECK
81
IF NOSE GEAR ISOLATION VALVE IS CLOSED ..NOSE WHEEL IS UNAVAILABLE..
FALSE
82
RUDDER PEDALS CONTROLS
NOSE WHEEL STEERING AND RUDDER
83
WHAT KEEPS REV THR FRM GOING BEYOND REV IDLE ON FIRST PULL
SOLENOID OPERATED INTERLOCK BLOCKS REV THR UNTIL REVERSER DEPLOYED
84
WHEN DOES AURAL CANCEL RESETS
GRD + ENG SHUT DOWN
85
WHEN CAN G/S INHIBIT BE SET
DES BELOW 1500 AGL
86
IF GLIDE SLOPE ALERT IT STOPSS
IF AIRPLANE MOVES BACK TO GLIDE SLOPE
87
TERR DATA IS SHOWN
ND, VSD, MINI MAP
88
ONLY TER WITHIN 2000' OF AIRPLANE ALT IS SHOWN ON ND AND MINI MAP
TRUE
89
PWS STARTS ON GRD
ONE ENG SET TO TOF THRUST
90
IN-FLIGHT WIND SHEAR WARNING AREA IS
0.5 TO 1.5 MILES
91
PWS BLIND SPOT IS FROM NOSE TO
0.5 MILE
92
PWS ALERTS ONLY OCCUR BELOW
1200' RA
93
TOO LOW TERR IS CAUSED BY
A/C NT IN LND CONFIG AND LOW RADIO ALT
94
TRAFFIC ADV CAUTION GIVEN
48-20 SEC BEFORE NPA
95
TCAS ND IS SELECTED TO 80 NM
3 MIL RING SHOWS AROUND AIRPLANE SYMBOL
96
BELOW 1000 FT RA TCAS AUTO SWT
TA ONLY
97
ARE TCAS DES RA ARE INHIBITED BELOW 1650 ON TOF
FALSE
98
TCAS DES RA ARE INHIBITED FROM
1200 RA
99
DURING APP ALL TCAS RA'S ARE INHIBITED BELOW
1000
