A330 Limitations Flashcards
Flight maneuvring load acceleration limits
Clean config -1 g to +2,5 g
Other config 0 g to +2,0 g
Mean RWY slope
+/- 2%
Nominal RWY width
45 meter
Maximum X-wind T/O and Landing
40 kts (gust included)
Maximum tailwind T/O and Landing
T/O 15 kts
Landing at or below 11.000 ft 15 kts
Landing above 11.000 ft 10 kts
Note: for landing with a tailwind greater than 10 kts, FLAPS FULL is recommended
Maximum wind for passenger and cargo doors operation
-Passenger door : 40 kts (50 kts with aircraft nose into the wind)
-FWD and AFT cargo doors : 40 kts (50 kts with aircraft nose into the wind or if the cargo doors are on the downwind side of the aircraft)
-The passenger, FWD and AFT cargo doors must be closed before wind speed exceeds 60 kts
Cockpit window open maximum speed
230 kts
Note: it is not possible to open the cockpit windows with the packs on.
Maximum FLAPS/SLATS speeds
Flaps Lever Position Configuration on Max Speed Flight Phase
Slat/Flap Display
0 VMO / MMO CRUISE 1 1 240 HOLDING 1 1 + F 215 TAKEOFF 2 2 205 APPROACH 2 2 196 TAKEOFF/APPROACH 3 3 186 TAKEOFF/APPR/LDG FULL FULL 180 LANDING
VMO/MMO
330 kts/M0.86
Maximum LG speeds
Maximum speed with landing gear extended (VLE) 250 kts/M0.55
Maximum speed with the LG operating - extension and retraction (VLO) 250 kts/M0.55
Maximum speed for LG gravity extension (VLE/VLO) 200 kts
Maximum tire speed
204 kts
Minimum control speed for landing (VMCL)
126 kts
Weights limitations A330-200
Taxi 233.900
T/O 233.000
Landing 182.000
ZFW 170.000
Minimum weight 116.000
Weight limitations A330-300
Taxi 233.900
T/O 233.000
Landing 187.000
ZFW 175.000
Minimum weight 121.000
Maximum speed for wipers
230 kts
APU Bleed usage not allowed
Together with HP air start unit
Packs usage not allowed
Together with LP air conditioning unit
Autopilot minimum altitudes
At takeoff
In approach with FINAL APP, V/S or FPA mode
In circling approach
ILS approach when CAT1 is displayed on the FMA
ILS approach when CAT2 or CAT3 (single or dual) is displayed on the FMA
After a manual go-around
In all other phases
At takeoff 100 ft AGL and at least 5 s after liftoff
In approach with FINAL APP, V/S or FPA mode 250 ft AGL
In circling approach 500 ft AGL
ILS approach when CAT1 is displayed on the FMA 160 ft AGL
ILS approach when CAT2 or CAT3 (single or dual) is displayed on the FMA 0 ft AGL if autoland
After a manual go-around 100 ft AGL
In all other phases 500 ft AGL
Minimum threshold crossing height
38 ft
N-1 landing capability limitation
CAT III SINGLE in config 3
Maximum wind for autoland
Headwind 35 kts
Crosswind 20 kts
Tailwind 10 kts
Autoland limits
Flaps
Minimum and maximum GS angle
Max airfield elevation
Minimum weight
CONFIG 3 en FULL
-2,5 and -3,25
Below 9200 ft
123.000 kg
APU Operational limitations
Operation and normal start
Elec power online
Bleed and elec power
APU batterij restart limit (elec emer config)
Operation and normal start Hele flight envelope
Elec power only Hele flight envelope
Bleed and elec power 25.000 ft
APU batterij restart limit (elec emer config) 25.000 ft
APU Bleed limitations
Max alt to assist eng start
Max alt for airco and pressurization (single pack)
Max alt for airco and pressurization (dual pack)
Max alt to assist eng start 20.000 ft
Max alt for airco and pressurization (single pack) 22.500 ft
Max alt for airco and pressurization (dual pack) 17.500 ft
APU Bleed not permitted with wing anti ice
Minimum oil quantity
12 qt + estimated consumption (0,56 qt/hr)
Starter
- A standard automatic start that includes up to XXXX start attempts, is considered one cycle
‐ For ground starts (automatic or manual), a XXXX pause per minute of operation is required between
successive cycles
‐ A XXXX cooling period is required, subsequent to two failed cycles, before each subsequent cycle
‐ The starter must not be run when N2 is above XXXX %
- A standard automatic start that includes up to three start attempts, is considered one cycle
‐ For ground starts (automatic or manual), a 30 s pause per minute of operation is required between successive cycles
‐ A 10 min cooling period is required, subsequent to two failed cycles, before each subsequent cycle
‐ The starter must not be run when N2 is above 30 %
Max reverse not below
70 kts
Max altitude for slats/flaps extended
20.000 ft
Maximum brake temp for T/O
300 ‘C
Check table for minimum crew oxygen pressure when bottle pressure shows less then
If OXY pressure is half boxed in Amber (1000 PSI)
Set parking brakes off when one temperature indication is above XXXX degrees
500
Minimum RWY Width for 180’ turn
-A330-200
-A330-300
-44 mtr
-48 mtr
Maximum guaranteed altitude for in-flight engine start
30.000’
Turbulance speed A330-300
Above FL200: M0.78/260 kts
Below FL200: 240 kts
Turbulence speed A330-200
Above FL200: M0.8/260 kts
Below FL200: 240 kts
Procedures only initiatited by PIC
- EMER DESCENT
- ON GROUND EMER/EVACUATION
Items needing PF confirmation (except on ground)
- engine master switches
- reset buttons
- IR switches
- (red) guarded switches
- thrust levers
Minimum temperature for APU battery start
-15’ C
If temp below -15’ C ground power should be used for APU start
Required cabin crew
-A330-200
-A330-300
-6
-7