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Other 87 Materials > Test 35 > Flashcards

Test 35 Flashcards

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1
Q

2 Transponder and TCAS are controlled from

A

ATP & TCP

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2
Q

Enable Boom mic after using O2 mask?

A

Left O2 Stowage box close= Reset

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3
Q

CAC (Cabin Air Compressor) inFlight starter assist eng start:

A

1 CAC run to maintain pack

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4
Q

Automatic Ice detection..inhibited

A

Grd Below 75kts

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5
Q

Can you change Autobrake Deaceleration level

A

yes,

Rotate the selector

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6
Q

App Idle is selected by EEC if

A

Auto + Valves commanded open or ON

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7
Q

Min Alt to engage AP?

A

200 Ft

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8
Q

Simultaneous Eng Start allowed…

A

Apu running + both starter Gen are operational

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9
Q

FWD Cargo Flow..High flow

A

live animals or odorous goods

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10
Q

Inflight Wing Ant-Ice selector on

A

WAI operates without input from automatic ice detection system (with TAT 10C or below)

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11
Q

Activate O2 Mask mic…

A

O2 Mask door open

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12
Q

IAS to Mach

A

.84/310 Kts

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13
Q

If Pax O2 deploys

A

Return to Seat, extinguish

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14
Q

During Grd start autostart monitors and ….attempt to correct for?

A

[compressor stall, High residual egt], hot start, loss of one starter, no egt rise, start time exceed

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15
Q

On hud , Runway edge lines …in delcuttered mode…enable at?

A

300 ft 60 feet

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16
Q

Antice and rain sys include

A

Auto ice detection, EAI, WAI, [pack inlet anti-ice] ,fd window heat, windshield wipers and washers, probe heat

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17
Q

VSD terrain color on gpws lateral map, green means

A

> 250 ft + gear down

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18
Q

Manual trim auto trim…to zero …TOF

A

30kts

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19
Q

Stuck mike on grd

A

Both eng shut down…>35 secs , dashes (—-) on TCP

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20
Q

Primary Flight Comp stw…Disc

A

Direct mode

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21
Q

Each Fuel Tank contains

A

2 AC pwr fuel pumps

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22
Q

An Apu fire cause Autoshutdown

A

Grd + Inflight

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23
Q

Rat provides

A

Hyd Pwr –> cent hyd + elec pwr …flight envelope

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24
Q

Auto wing Anti-ice avail

A

FLT + Grd > 80kts

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25
Q

SLATS ext midrange

A

FLPS 1

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26
Q

Pecs (pwer electric cooling sys)

A

no FD control

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27
Q

787 Eng fire ext bottles?

A

two

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28
Q

How many fuel x-feed valves

A

one

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29
Q

Excessive bank angle..amber ..PFD

A

> 35D

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30
Q

Gen drive disconnect mechanism allows

A

Auto disconnect or manual

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31
Q

Four electr brk pwr supply units….receive two separate inputs

A

28 Vdc + Main battery

32
Q

EICAS CONFIG GEAR…

A

800 FT

33
Q

LNAV MAINTAINS CURRENT HDG

A

PASSING LAST ACTIVE WPT

34
Q

LOC/FAC CAPTURE CAN OCCUR WITH IN

A

120 D

35
Q

MIN EXT PWR SOURCE FOR ENG START

A

2 FWD

36
Q

EICAS …EGT AMBER BAND MEANS

A

MAX CONT EGT LIMIT

37
Q

787 BRAKE SYSTEM IS

A

ELEC-MECHANICAL

38
Q

CORRECT RWY SLOPE 787

A

+- 2 %

39
Q

HOW DO YOU KNOW CCS ( FIRE DETECTION & MANG) APP …AVAIL DURING BAT ONLY APU START?

A

CDU…VISIBLE ON LOWER DISPLAY

40
Q

ON GRD WARNING HORN…

A

IRS DELETING BATTERY

41
Q

…LOCKED OUT AT HIGH SPD?

A

AILERONS

42
Q

FLT ENVELOPE PROTECTIONS?

A

STALL, OVER SPD, ROLL/BANK ANGLE + TAIL STRIKE

43
Q

DURING HUD TOF, DEVIATION BECOMES ACTIVE

A

45D, 2D, 75FT

45D RWY HDG
2D OF CENTER ILS LOC BEAM
75 FT GLS LOC CENTER LINE

44
Q

F/D OFF…NO STEERING INDICATIONS UNLESS

A

TO/GA PUSHED > 80KTS & FLAPS OUT OF UP

45
Q

TRIM AIR FAULT LIGHT ON

A

TRIM AIR VALVE COMMANDED CLS….ZONE SUPPLY DUCT OVERHEAT

46
Q

WHEN APU STARTS AUTO IN FLIGHT

A

LOSS THREE OR MORE GENERATORS

47
Q

SCAVENGE SYS OPS….FUEL TRANSFER…EITHER MAIN TANK QTY LESS…

A

16,000 KG

48
Q

TAMS [THRUST ASS MIN SPD] …ALWAYS BE …VMCG OR VMCA FOR TOF & GA

A

10 KTS

49
Q

CABIN/ UTILITY STW OFF?

A

[GALLEY], MOST CABIN LTS, OTHER NON- ESSENTIAL CAN UTILITY LOADS

50
Q

DOES IRU ….ALIGN IN FLT?

A

YES

51
Q

MAX ALT APU START?

A

STARTED AND OPERATED TO AIRPLANE MAX CERT ALT

52
Q

REASON FOR X-START (MAGENTA)…

A

CURRENT ALT & OR AIRSPD OUTSIDE WINDMILLING START ENVELOPE

53
Q

ENG FIRS SWT AUTO UNLOCK

A

FIRE WARNING OR FC STW…CUT OFF

54
Q

WHICH HYD PWR NOSE GEAR STEERING

A

CENTER

55
Q

ANP EQUAL OR EXCEED RNP

A

NAV UNABLE RNP

56
Q

LNAV ENGAGES @> 50FT …LATERALLY WITH IN

A

2.5 NM

57
Q

ALTN MODE FLAP AND SLAT EXT IS LIMITED TO

A

SLATS MID POS & FLPS 20

58
Q

PRIMARY ENGINE INDICATIONS DISPLAYED FULL TIME

A

N1, EGT

59
Q

TOF PWS ..INHIBITIED

A

100 KTS ->400 RA

60
Q

CAB TRANSMIT SELECT STW …PUSHED TWICE

A

PRIORITY CALL TO CAB STATION

61
Q

NOT CORRECT STATEMENT…PULLING ENG FIR SWT OUT

A

CLOSES ..ENG BLEED AIR VALVE

62
Q

APP IDLE IN FLIGHT

A

[FLAPS 25 OR GREATER] OR LND GEAR DN

63
Q

RTO SELECTION…MAX BRK PRESS…ABV IDLE

A

ABOVE 85 KTS

64
Q

CRITICAL WARNINGS…ENG FAIL….DISPLAYED

A

PFD

65
Q

THREE INDEPENDENT …HYD SYS

A

5000 PSI

66
Q

ITNERACTIVE CDU CAN BE DISPLAYED ON ANY MFD…BY PUSHING CDU SWT

A

TRUE

67
Q

FOR APU START WITH APU BATT AS PWR SOURCE, …START/GEN IS ALWAYS USED

A

RIGHT

68
Q

FMC DOESN’T SEQUENCE ACTIVE WPT MORE… NM OF ACTIVE RTE AND NOT ON AN OFFSET

A

21 NM

69
Q

HOW DOES PECS DISPLY ON GRD

A

A SINGLE LOOP DISPLAYED WHEN ONLY ONE FWD WXT PWR IS CONNECTED AND SELECTED ON

70
Q

FREQUENCIES CAN BE ENTERED IN ACT OR STBY ON TCP

A

TRUE

71
Q

HYD QTY IS DISPLAYED

A

AS PERCENTAGE OF NORMAL SERVICE LEVEL [1.00 IS NORMAL SERVICE LVL]

72
Q

DURING DES AND APP WHAT ARM GO AROUND MODE

A

EXT FLAPS FROM UP TO 1

73
Q

SPD TREND VECTOR ON PFD INDICATES

A

10 SECONDS BASED ON CURRENT ACC OR DECELERATION

74
Q

AUTOMATIC ICE DETECTION IS INHIBITED

A

ON GRD <75 KTS

75
Q

PUSHING BOTH TRIM STW ON GRD

A

DIRECTLY MOVES STABILIZER

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