Test form Flashcards
IAS/ Mach SEL
IAS TO MACH .84M
MACH TO IAS 310kts
VNAV activates
400’ above RWY elevation
TOGA SW FOR GA
FIRST PUSH 2000fpm
SECOND PUSH GA THR LIMIT
How to disengage approach mode
When GS AND LOC CAPTURE
DISENGAGE AP AND BOTH FD OFF
PUSH TOGA
AT FMA DURING TAKEOFF
THR REF
AT 65kts HOLD
LNAV 50’
VNAV 400’
Runway align mode
500’AGL
STRONGER WINDS ALSO SECOND ALIGNMENT AT 200’
AUTOLAND LANDING
FLARE AT 50’RA
IDLE AT 25’RA
ROLLOUT 5’RA
When is GA ARMED
FLAPS OUT OF UP
GS CAPTURE
HYD DEMAND PUMPS
SYS 1 and 4 AIR DRIVEN DEMAND PUMPS
SYS 2 and 3 ELEC MOTOR DRIVEN DEMAND PUMPS
AUX HYD PUMPS
SYS 1 and 4
OEB ONLY SYS 4
ELECTRIC AUX PUMPS FOR GROUND HANDLING OPS
HYD FLUID SUPPLY
INDEPENDENT RESERVOIR
BLEED AIR SYS PRESSURISES TO PREVENT PUMP CAVITATION AND ENSURE POSITIVE FLOW DURING HIGH DEMAND
HYD SYS 1
ELEC AUX PUMP
AIR DRIVEN DEMAND
C AP
FLT CONTROLS
TRAILING EDGE FLAP
NOSE GEAR AND STEERING
BODY GEAR AND STEERING
ALTERNATE BRAKES
HYD SYS 2
ELEC DEMAND PUMP
R AP
FLT CONTROLS
ALTERNATE BRAKES
HYD SYS 3
ELEC DEMAND PUMP
L AP
FLT CONTROLS
HYD SYS 4
AIR DRIVEN DEMAND PUMP
ELEC AUX PUMP
FLT CONTROLS
OUTBD TRAILING EDGE FLAP
WING GEAR
NORMAL BRAKES
Antiskid protection
Provided in normal and alternate brake SYS
Normal to each individual wheel
Alternate SYS each lateral wheel pair
Autobrake SYS
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
PARKING BRAKE
CAN BE SET WITH:
NORMAL BRAKES
ALTN BRAKES
OR BRAKE ACCUMULATOR
THR
Operates from 400’
For VNAV OR FLCH CHANGES TO CLB
CON FOR OEI
STBY PWR - BAT
Ground MAINT only
LOAD SHEDDING
UTIL POWER OFF LTS NOT ILLUMINATED
BUS TIE SW
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
What does utility busses power
FWD MAIN FUEL PUMP 2 and 3
FWD OVERRIDE/JETTISON PUMP 2 and 3
C OVERRIDE/JETTISON PUMP
RECIRC FANS
Electrical isolation during AUTOLAND
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
What produces DC POWER
FOUR TRU
POWERED BY ITS RELATED AC BUS AND PROVIDES DC PWR TO DC BUS
When are both outflow valves closed
Cabin altitude limiter closes both outflow valves if cabin altitude exceeds 11000’
Pressurisation relief
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
FIRST SEGMENT TAKEOFF PERF
ENG FAIL AT V1
CLB WITH GEAR OUT
4 ENG 0.5%
SECOND SEGMENT
OEI
GEAR UP
CLB AT V2 TO 400’
4 ENG 3%
THIRD SEGMENT
LEVEL SEGMENT
ACCELERATE AT 400’ FROM V2 TO FINAL TAKEOFF CLB SPD
4 ENG 1.5%
FOURTH SEGMENT
ENROUTE CONFIG
CLB PAST 400’
4 ENG 1.5%
DETERMINING NET FLT PATH
4 ENG REDUCE BY 1.0%
Approach climb performance
OEI AT 1.5Vs
4 ENG 2.4%
Landing climb performance
3.2% not in excess of 1.3 Vs with AEO
Landing distance required
DRY 1.67
WET 1.92
AUX TANK TRANSFER
STAB TANK EMPTY
CWT LESS THAN 36.4T
RES TANK 2 and 3 transfer
Main tank 2 or 3 less than 18.2T
Fuel config for takeoff with CWT
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
Stab fuel transfers
CWT LESS THAN 36.4T
OR
AIRBORNE 30 mins
