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