Limitations Flashcards
After TAKE OFF, pilot can engage AP :
100 ft
5s
What is the maximum speed for the landing gear extension, retraction, extended ?
Extension 250
Retraction 220
Extended 280
The maximum altitude to extend the speed brakes is :
No limits
AP ON down to (ILS CAT1)
160 ft AGL
AP ON down to (FINAL APP, V/S or FPA mode)
250 ft AGL
AP ON down to (circling)
500 ft AGL
Use of AP or FD in OPEN DES or DES MODES is not permitted in
approach unless the FCU altitude is set at or above :
MDA or 500 ft AGL
X wind limitation
Tail wind limitation
X wind 38 kts
Tail wind Takeoff 15 kts
Tail wind Landing 10 kts
on dry runways only
The maximun brake temperature for TAKE-OFF is (with and without FANS)
300 °C without FANS
150 °C with FANS
APU STARTER CYCLES:
max number in a row
cool down time between each start
Waiting time after 1 full cycle
3 starts
1 min cool down
60 min waiting time
APU start in flight:
Max altitude
Max altitude on batteries only
No max altitude
FL250 on batteries only
APU supply in flight:
ELEC
BLEED
ELEC on all flight envelope
BLEED for engine start assist up to FL200
BLEED for AC and PRESSU up to FL200 (1 pack)
BLEED for AC and PRESSU up to FL150 (2 packs)
Engines start cycles (1 cycle = up to 3 starts)
Max number of consecutive cycles
Pause between 2 cycles
Cool down time after Max number of consecutive cycles
4 consecutive cycles
20s
15 min to cool down starter
Min OIL temp before
Start up
Take Off
- 40 °C for start up
- 10 °C for take-off
Définition of icing conditions
OAT (on ground) or TAT (in flight) < 10°C and visible moisture is present (fog, clouds, visibility less than 1600 or rains, ice…)
OAT < 10°C and water patches or slush on runway, taxiways
Takeoff max fuel imbalance
Inner tanks
Outer Tanks
In flight and landing max fuel imbalance
Inner tanks
Outer Tanks
Takeoff max fuel imbalance
Inner tanks if full 500 kg then >1000 kg
Outer Tanks 370 kg
In flight and landing max fuel imbalance
Inner tanks if full 1500 kg then >1600 kg
Outer Tanks 690 kg
The maximum speed to use the windshield wipers is
230 kts
MAX TIRE speed
195 kts
Max alternate distance for :
Take OFF
Adequate airport in flight
1h de vol N-1 sans vent
395 NM for both
Minima ILS (MDH and RVR)
CAT II
CAT III fail passive
CAT III fail operationel
CAT II 100 ft AGL 300m
CAT III fail passive 50 ft AGL 200m
CAT III fail operationel 20 ft 200m CAT IIIA 75m CATIIIB
MAX / MIN altitude for Take Off and Landing
-1000 ft
+8000 ft
Airport Limitations:
Nominal runway width
Minimal runway width
Max wind for passenger door
Max wind for cargo doors
Nominal runway width 45 m
Minimal runway width 30 m
Max wind for passenger door 65 kts
Max wind cargo doors 40 kts (50 kts if A/C face into the wind)
Cockpit windows open max speed
Cockpit wipers max speed
Windows 200 kts
Wipers 230 kts
Max Flaps / Slats speeds 1 1+F 2 3 FULL
1 230 1+F 215 2 200 3 185 FULL 177
MTOW
MLW
MZFW
MTOW 73 500 kg
MLW 64 500 kg
MZFW 60 500 kg
Cabin Pressure
MAX positive delta P
MAX negative delta P
Safety valve setting
MAX positive delta P 9.0 PSI
MAX negative delta P -1.0 PSI
Safety valve setting 8.6 PSI
Thrust Setting time limit
TOGA AEO
TOGA OEI
MCT
TOGA AEO 5 min
TOGA OEI 10 min
MCT No limit
Vitesse en turbulence
< FL200 250 kts
FL200 < Alt < FL310 275 kts
> FL310 0.76 M
Minimum OIL quantity
9.5 qts + estimated consumption of A/C endurance (0.5 qt/h)
Max altitude for Slats/Flaps
20 000 ft
JET A1 min TEMP
-43 °C
Definition of severe ice accretion
> 5 mm
Taxi with deflated or damaged tires
one tyre per gear deflated : max turn speed
two tyre per gear deflated : max turn speed
NWS max angle
one tyre per gear deflated : max turn speed 7 kt
two tyre per gear deflated : max turn speed 3kt
NWS max angle 30°
Max latitude for IRS alignment
Max possible latitude flights with IRS
Max latitude for IRS alignment 73°North/South
Max possible latitude flights with IRS 73° North / 60° South
Min height for PAPI use
200 ft
EGT max start-up
725 °C
Flight Envelope
-2000 ft –> 39800 ft
VMO / MMO
350
M0.82
Cabin Altitude warning
9550 ft
Cab alt max selectable
14 000 ft
APU max N1
107%
APU envelope (air)
-1000ft to 41000ft
APU envelope (gnd)
-1000ft to 9200ft
MCT EGT
915 °C
N1 max
N2 max
104%
105%
Fuel min / max Temp
-36°C
54°C
Min T/O fuel
1500 kg
180 turn on runway
24m
