a/c lenght
63.69m
distance from center of a/c to center of inner engine
9.37m
distance from center of a/c to center of outer engine
19.6m
a/c height
16.83m
distance from nose gear to main gear
25.37m
distance between outer main gears
10.68m
wingspan
60.3m
minimum turning radius on dry runway
47m
tailstrike pitch angle with gear compressed
10.1°
tailstrike pitch angle with gear not compressed
14.2°
flight maneuvering load acceleration limits clean
-1.0g to 2.5g
flight maneuvering load acceleration limits not clean
0g to 2g
min. & max. pressure altitudes for takeoff and landing
-2000ft to 12’500ft
max. pressure altitude
41’100ft
minimum TAT
-53°C
max. mean RWY slope
±2 %
nominal RWY width
45m
max. crosswind for takeoff
37.5kts
max. crosswind for landing
41kts
max. tailwind for takeoff
10kts
max. tailwind for landing
15kts for landing at or below 10’000ft
10kts for landing above 10’000ft
for landing above 10kts, Flaps FULL recommended
max. windspeed for passanger door operation
40kts (50kts if a/c nose is into the wind)
doors must be closed before windspeed exceeds 60kts
max. windspeed for cargo door operation
40kts (50kts if a/c nose is into the wind or cargo doors on downwind side)
takeoff limitations on contaminated runways
Takeoff is not recommended on the following runway conditions:
Wet ice,
Water on top of Compacted Snow,
Dry Snow or Wet Snow over Ice.
cockpit window open max. speed
230kts
Vmo
330kts
Mmo
0.86
max. speed Flaps 1
255kts
max. speed Flaps 1+F
215kts
max. speed Flaps 2
196kts (205 if ECAM when actual slats/flaps position is 1+F)
max. speed Flaps 3
186kts
max. speed Flaps FULL
180kts
max. speed with landing gear extended
250kts/M0.55
max. speed with landing gear extending or retracting
max. speed for landing gear gravity extension
200kts
max. tire speed
204kts
Vmcl
125kts
Vmcl-2
157kts
Vmca
112-124kts depending on altitude
Vmcg
114-127kts (depending mainly on altitude and slightly on configuration)
wipers max. operating speed
max. taxi weight
275’900kg
max. takeoff weight
275’000kg
max. landing weight
192’000kg
max. zero fuel weight
181’000kg
min. weight
130’000kg
max. time without air conditioning with PAX on board
20min (recommended)
APU bleed air with HP air start unit
not allowed
max. positive differential pressure
9.25 PSI
max. negative differential pressure
-1.0 PSI
safety relief valve setting
8.85 PSI
packs use with LP air conditioning unit
AP after takeoff
100ft AGL and at least 5s after liftoff
AP in approach with FINAL APP, V/S or FPA mode
250ft AGL
AP in circling approach
500ft AGL
AP in ILS approach when CAT1 is displayed on the FMA
160ft AGL
DH in ILS approach when CAT2 or CAT3 (single or dual) is displayed on the FMA
0ft if autoland
AP after a manual go-around
100ft AGL
AP in all other phases
minimum DH for CAT 2
+ prerequisites for the use
100ft
one AP engaged and min. CAT 2 in FMA
for manual landing, disconnect AP no later than 80ft
minimum DH for CAT 3 Single
50ft
A/THR and one AP engaged and min. CAT 3 Single on FMA
Alert height for CAT 3 Dual
200ft
A/THR and both AP engaged, CAT 3 Dual on FMA
minimum RVR for CAT 3 without DH
75m
OEI LVO restrictions
Conf 3 for Cat 2 or 3 approaches
Cat 3 Single if single inner engine out
Cat 3 Dual if single outer engine out
wind limitations for Cat 2 + 3
HW: 35 kts
XW: 20 kts
TW: 10 kts
limitations for Cat 2+3 ops
glide angle 2.5 - 3.25°
airfield elevation 9200ft (pressure altitude!)
weight below MLW (in case of EMER, autoland can be performed up to 270t)
APU and refueling/defueling restrictions
If the APU failed to start or following an automatic APU shutdown, do not start the APU
If a fuel spill occurs, perform a normal APU shutdown.
APU bleed max. ALT to assist ENG start
20’000ft
APU bleed max. ALT for single pack operation
22’500ft
APU bleed max. ALT for dual pack operation
17’500ft
APU bleed for wing anti-ice
not permitted
time limit for TOGA/FLEX thrust AEO
5 min
time limit for TOGA/FLEX thrust OEI
10 min
minimum oil quantity
10 qts + 0.6qts/flt hr
starter limitations
A standard automatic start that includes up to three start attempts, is considered one cycle
For ground starts (automatic or manual), a 20 s pause is required between successive cycles
A 15 min cooling period is required, subsequent to four failed cycles
The starter must not be run when N2 is above 20 %
Usable Fuel Outer Tanks (kg)
ca. 2900kg x2
Usable Fuel Inner Tanks (kg)
ca. 33600kg x2
Usable Fuel Center Tank (kg)
ca. 32600kg
Usable Fuel Trim Tank (kg)
ca. 4900kg
Usable Fuel Total (kg)
ca. 110’400kg
minimum and maximum Flex Temperature
min: ISA+15 & / actual OAT
max: ISA+40
max. altitude with flaps/slats extended
max. temperature with Jet A1/A
+60°C
min. temperature with Jet A1
-47°C in outer & trim tank (=freezing point)
-42°C in inner tank (=freezing point +5°C)
min. temperature with Jet A
-40°C in outer & trim tank (=freezing point)
-35°C in inner tank (=freezing point +5°C)
max. allowed fuel imbalance in inner tanks
2300kg if heavier tank full, more if not
(given outer tanks balanced)
max. allowed fuel imbalance in outer tanks
1100 kg if heavier tank full, more if not
(given inner tanks balanced)
max. break temperature for takeoff
300°C
PM callout airspeed
“Speed” if speed -5/+10kts
PM callout ROD during approach
“sink rate” when ROD > 1200ft/min
PM callout bank angle during approach
“Bank” when bank angle > 7°
PM callout pitch attitude on approach
“Pitch” when pitch < 0° or pitch > 10°
PM callout approach tracking ILS
“Loc” if localizer deviation > 1/2 dot
“Glide” if glide slope deviation > 1/2 dot
PM callout crosstrack
“Crosstrack” when crosstrack > 0.1 NM
PM callout vertical deviation
“Vdev” when vertical deviation > 1/2 dot
PM callout approach tracking VOR/NDB
“Course” when 1/2 dot/2.5° deviation on VOR or 5° on ADF
PM callout pitch attitude during landing
“Pitch pitch” when pitch attitude approaches the tail strike pitch limit indicator or reaches 7.5°
PM callout bank angle during landing
“Bank bank” if the bank angle reaches 7°
PM callout bank angle during go-around
“Bank” if bank angle > 7°
PM callout pitch attitude during go-around
“Pitch” if pitch attitude < 10° up or pitch attitude > 20° up
PM callout ROD during go-around
“sink rate” if there is no climb rate
Zuletzt geändertvor 8 Monaten