Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

QF > Test form > Flashcards

Test form Flashcards

1
Q

IAS/ Mach SEL

A

IAS TO MACH .84M

MACH TO IAS 310kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

VNAV activates

A

400’ above RWY elevation

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

TOGA SW FOR GA

A

FIRST PUSH 2000fpm

SECOND PUSH GA THR LIMIT

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

How to disengage approach mode

A

When GS AND LOC CAPTURE

DISENGAGE AP AND BOTH FD OFF

PUSH TOGA

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

AT FMA DURING TAKEOFF

A

THR REF

AT 65kts HOLD

LNAV 50’

VNAV 400’

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Runway align mode

A

500’AGL

STRONGER WINDS ALSO SECOND ALIGNMENT AT 200’

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

AUTOLAND LANDING

A

FLARE AT 50’RA

IDLE AT 25’RA

ROLLOUT 5’RA

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

When is GA ARMED

A

FLAPS OUT OF UP

GS CAPTURE

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

HYD DEMAND PUMPS

A

SYS 1 and 4 AIR DRIVEN DEMAND PUMPS

SYS 2 and 3 ELEC MOTOR DRIVEN DEMAND PUMPS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

AUX HYD PUMPS

A

SYS 1 and 4

OEB ONLY SYS 4

ELECTRIC AUX PUMPS FOR GROUND HANDLING OPS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

HYD FLUID SUPPLY

A

INDEPENDENT RESERVOIR

BLEED AIR SYS PRESSURISES TO PREVENT PUMP CAVITATION AND ENSURE POSITIVE FLOW DURING HIGH DEMAND

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

HYD SYS 1

A

ELEC AUX PUMP

AIR DRIVEN DEMAND

C AP

FLT CONTROLS

TRAILING EDGE FLAP

NOSE GEAR AND STEERING

BODY GEAR AND STEERING

ALTERNATE BRAKES

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

HYD SYS 2

A

ELEC DEMAND PUMP

R AP

FLT CONTROLS

ALTERNATE BRAKES

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

HYD SYS 3

A

ELEC DEMAND PUMP

L AP

FLT CONTROLS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

HYD SYS 4

A

AIR DRIVEN DEMAND PUMP

ELEC AUX PUMP

FLT CONTROLS

OUTBD TRAILING EDGE FLAP

WING GEAR

NORMAL BRAKES

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Antiskid protection

A

Provided in normal and alternate brake SYS

Normal to each individual wheel

Alternate SYS each lateral wheel pair

17
Q

Autobrake SYS

A

RTO MAX BRAKING IF:

AIRPLANE ON GND
GS ABOVE 85kts
ALL THR LEVERS CLOSED

AUTOBRAKE SYS ONLY FOR NORMAL BRAKES AND ANTISKID OP

AIRPLANE DECELERATION RATE IS MAINTAINED THEREFORE AS THRUST REVERSER AND SPOILERS APPLIED THE AUTOBRAKE PRESS IS REDUCED

18
Q

PARKING BRAKE

A

CAN BE SET WITH:

NORMAL BRAKES

ALTN BRAKES

OR BRAKE ACCUMULATOR

19
Q

THR

A

Operates from 400’

For VNAV OR FLCH CHANGES TO CLB

CON FOR OEI

20
Q

STBY PWR - BAT

A

Ground MAINT only

21
Q

LOAD SHEDDING

A

UTIL POWER OFF LTS NOT ILLUMINATED

22
Q

BUS TIE SW

A

AUTO
ARMS AUTO AC BUS CIRCUITRY
CLOSES DCIR

OFF
OPENS BTB AND RELATED DCIR
RESETS FAUKT LOGIC CIRCUITRY

BUS ISLN LT
BTB OPEN
AC ISOLATED FROM SYNCH BUS

23
Q

What does utility busses power

A

FWD MAIN FUEL PUMP 2 and 3

FWD OVERRIDE/JETTISON PUMP 2 and 3

C OVERRIDE/JETTISON PUMP

RECIRC FANS

24
Q

Electrical isolation during AUTOLAND

A

AC AND DC BUSSES 1,2 and 3 are isolated from the synchronous bus to provide independent power sources for all 3 AP.

AC BUS 4 continues to power the synchronous bus

25
Q

What produces DC POWER

A

FOUR TRU

POWERED BY ITS RELATED AC BUS AND PROVIDES DC PWR TO DC BUS

26
Q

When are both outflow valves closed

A

Cabin altitude limiter closes both outflow valves if cabin altitude exceeds 11000’

27
Q

Pressurisation relief

A

Two mechanical positive pressure relief valves prevent overpressurisation

Pack 2 shuts down to assist

Pack 2 resets when both cabin pressure relief valves close

Negative pressure relief valves in forward and aft cargo doors open when the airplane cabin pressure is slightly less than outside air pressure

28
Q

FIRST SEGMENT TAKEOFF PERF

A

ENG FAIL AT V1

CLB WITH GEAR OUT

4 ENG 0.5%

29
Q

SECOND SEGMENT

A

OEI

GEAR UP

CLB AT V2 TO 400’

4 ENG 3%

30
Q

THIRD SEGMENT

A

LEVEL SEGMENT

ACCELERATE AT 400’ FROM V2 TO FINAL TAKEOFF CLB SPD

4 ENG 1.5%

31
Q

FOURTH SEGMENT

A

ENROUTE CONFIG

CLB PAST 400’

4 ENG 1.5%

32
Q

DETERMINING NET FLT PATH

A

4 ENG REDUCE BY 1.0%

33
Q

Approach climb performance

A

OEI AT 1.5Vs

4 ENG 2.4%

34
Q

Landing climb performance

A

3.2% not in excess of 1.3 Vs with AEO

35
Q

Landing distance required

A

DRY 1.67

WET 1.92

36
Q

AUX TANK TRANSFER

A

STAB TANK EMPTY

CWT LESS THAN 36.4T

37
Q

RES TANK 2 and 3 transfer

A

Main tank 2 or 3 less than 18.2T

38
Q

Fuel config for takeoff with CWT

A

Cross feed valves 2 and 3 close when FLAPS EXT TAKEOFF POSN

CWT FUEL FOR ENG 1 and 4

MAIN TANKS FOR ENG 2 and 3

39
Q

Stab fuel transfers

A

CWT LESS THAN 36.4T

OR
AIRBORNE 30 mins

QF (15 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions