Test form

Question 1

IAS/ Mach SEL

Answer 1

IAS TO MACH .84M

MACH TO IAS 310kts

Question 2

VNAV activates

Answer 2

400’ above RWY elevation

Question 3

TOGA SW FOR GA

Answer 3

FIRST PUSH 2000fpm

SECOND PUSH GA THR LIMIT

Question 4

How to disengage approach mode

Answer 4

When GS AND LOC CAPTURE

DISENGAGE AP AND BOTH FD OFF

PUSH TOGA

Question 5

AT FMA DURING TAKEOFF

Answer 5

THR REF

AT 65kts HOLD

LNAV 50’

VNAV 400’

Question 6

Runway align mode

Answer 6

500’AGL

STRONGER WINDS ALSO SECOND ALIGNMENT AT 200’

Question 7

AUTOLAND LANDING

Answer 7

FLARE AT 50’RA

IDLE AT 25’RA

ROLLOUT 5’RA

Question 8

When is GA ARMED

Answer 8

FLAPS OUT OF UP

GS CAPTURE

Question 9

HYD DEMAND PUMPS

Answer 9

SYS 1 and 4 AIR DRIVEN DEMAND PUMPS

SYS 2 and 3 ELEC MOTOR DRIVEN DEMAND PUMPS

Question 10

AUX HYD PUMPS

Answer 10

SYS 1 and 4

OEB ONLY SYS 4

ELECTRIC AUX PUMPS FOR GROUND HANDLING OPS

Question 11

HYD FLUID SUPPLY

Answer 11

INDEPENDENT RESERVOIR

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

Question 12

HYD SYS 1

Answer 12

ELEC AUX PUMP

AIR DRIVEN DEMAND

C AP

FLT CONTROLS

TRAILING EDGE FLAP

NOSE GEAR AND STEERING

BODY GEAR AND STEERING

ALTERNATE BRAKES

Question 13

HYD SYS 2

Answer 13

ELEC DEMAND PUMP

R AP

FLT CONTROLS

ALTERNATE BRAKES

Question 14

HYD SYS 3

Answer 14

ELEC DEMAND PUMP

L AP

FLT CONTROLS

Question 15

HYD SYS 4

Answer 15

AIR DRIVEN DEMAND PUMP

ELEC AUX PUMP

FLT CONTROLS

OUTBD TRAILING EDGE FLAP

WING GEAR

NORMAL BRAKES

Question 16

Antiskid protection

Answer 16

Provided in normal and alternate brake SYS

Normal to each individual wheel

Alternate SYS each lateral wheel pair

Question 17

Autobrake SYS

Answer 17

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

Question 18

PARKING BRAKE

Answer 18

CAN BE SET WITH:

NORMAL BRAKES

ALTN BRAKES

OR BRAKE ACCUMULATOR

Question 19

THR

Answer 19

Operates from 400’

For VNAV OR FLCH CHANGES TO CLB

CON FOR OEI

Question 20

STBY PWR - BAT

Answer 20

Ground MAINT only

Question 21

LOAD SHEDDING

Answer 21

UTIL POWER OFF LTS NOT ILLUMINATED

Question 22

BUS TIE SW

Answer 22

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

Question 23

What does utility busses power

Answer 23

FWD MAIN FUEL PUMP 2 and 3

FWD OVERRIDE/JETTISON PUMP 2 and 3

C OVERRIDE/JETTISON PUMP

RECIRC FANS

Question 24

Electrical isolation during AUTOLAND

Answer 24

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

Question 25

What produces DC POWER

Answer 25

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

Question 26

When are both outflow valves closed

Answer 26

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

Question 27

Pressurisation relief

Answer 27

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

Question 28

FIRST SEGMENT TAKEOFF PERF

Answer 28

ENG FAIL AT V1 CLB WITH GEAR OUT 4 ENG 0.5%

Question 29

SECOND SEGMENT

Answer 29

OEI GEAR UP CLB AT V2 TO 400' 4 ENG 3%

Question 30

THIRD SEGMENT

Answer 30

LEVEL SEGMENT ACCELERATE AT 400' FROM V2 TO FINAL TAKEOFF CLB SPD 4 ENG 1.5%

Question 31

FOURTH SEGMENT

Answer 31

ENROUTE CONFIG CLB PAST 400' 4 ENG 1.5%

Question 32

DETERMINING NET FLT PATH

Answer 32

4 ENG REDUCE BY 1.0%

Question 33

Approach climb performance

Answer 33

OEI AT 1.5Vs 4 ENG 2.4%

Question 34

Landing climb performance

Answer 34

3.2% not in excess of 1.3 Vs with AEO

Question 35

Landing distance required

Answer 35

DRY 1.67 WET 1.92

Question 36

AUX TANK TRANSFER

Answer 36

STAB TANK EMPTY CWT LESS THAN 36.4T

Question 37

RES TANK 2 and 3 transfer

Answer 37

Main tank 2 or 3 less than 18.2T

Question 38

Fuel config for takeoff with CWT

Answer 38

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

Question 39

Stab fuel transfers

Answer 39

CWT LESS THAN 36.4T OR AIRBORNE 30 mins