Fcom Flashcards
minimum height for AP
100ft or 5 sec after liftoff
normal hyd pressure
3000 PSI
max wiper speed
230 kt
MAX TYRE SPEED
195 kt
what do you do at touchdown in an overweight landing
max reverse and brake fan once stopped
high speed protection: max bank
40°(positive static stability)
PWS envelope
RA below 1800ft. at take off, inhibited above 100kt up to 50 ft.
During landing alerts are inhibited below 50 ft.
what do you avoid doing on landing after a fuel leak?
selecting reversers
actions for engine tail pipe fire
engine master off, dry crank.
Don’t press the fire pb
Ptu activates when differential pressure between yellow and green reaches
500 psi Inhibited during first engine start, self.tests during second engine start
GPWS MODE 1
excessive rate of descent
Sink RATE….. PULL UP
GPWS MODE 2
excessive terrain closure rate
terrain terrain…… pull up
GPWS MODE 3
altitude loss after take off
dont sink
GPWS MODE 4
unsafe terrain clearance when not in landing configuration
too low terrain….. too low gear/flaps
GPWS MODE 5
descent below glideslope
glideslope
AP disconnection in overspeed
VM0+15 or MM0+0.04
engine start cycles limitations
3 starts attempts are one cycle
20 sec between cycles
15 min cooling after 4 failed cycles
Don’t run starter when N2 》20%
minimum altitudes for AP in ILS and rnp app
160 ft ILS and 250 ft FIN APP
minimum altitude for AP in ILS and
FINAL APP
160 ft ILS cat 1
250 ft final app, v/s or fpa
Max altitude to assist engine start with
APU bleed
20000 ft
In a flap or slat locked failure,
overspeed and VFE are computed out of?
VFE and VFE NEXT are computed out of
flap lever position
VLS and overspeed out of actual surface position
when does the system deliver high flow for the packs?
In single pack operations and when APU is supplying bleed air
Order of hyd system powering spoilers, inboard to outboard
G Y B Y G
Ailerons are controlled by (computer and hyd)
Elac 1 primarily and G/B hyd
Elevators are controlled by what (computers and hyd)
Left elev: B/G
Right elev Y/B
Primarily by elac2. Then elac 1, then SECs
The THS is controlled by which computer and hyd?
G/Y and Elac 2.
Elac 1 takes over in case of failure, followed by sec 2 and sec1
How many start attempts consist of 1 cycle? How much do you need to wait between cycles?
3 start attempts. 20 second wait between successive cycles. After 4 failed cycles you need 15 min waiting
When does the DFDR records?
-5 min after first electric power up, or when GND CTL pushed
-Otherwise After 1st engine start
-In flight always
-5 min after 2nd engine shut down
What generates amber cautions? And what red warnings?
SDAC
FWC
Fuel temp limitations
+ 55 deg
-43 deg
Why is TCAS blue sometimes not enough to comply with a climb RA?
Because it is limited to VLS-5 and Vmax.
To override select AP/FD off and fly the green up to V alpha max
What are the 3 levels of failure?
Level 1 requires only crew monitoring, no procedure required
Level 2 it’s amber caution, with single chime
Level 3 is master warning, with CRC
How long does DFDR stores data for?
25 h
Do we have load factor protection in altn law?
Yes
How is roll rate in altn law?
It is like direct law. It’s 30 deg/sec (25 with slats), and to limit it only roll spoiler 4 and 5 are used