A330 Limitations Flashcards
Maximum EGT for APU running?
650 degrees C
Maximum Takeoff/Go-Around EGT/Time Limit - [AEO]?
NOTE: Include TOGA, FLEX and DERATE.
975 degrees C / 5 mins
Minimum Control Speed for Landing - 200 [VMCL]?
118 kts
Engine Out Autoland Configuration?
CONF 3, and if engine out procedures have been completed by 1000 ft AGL.
Maximum Operating Altitude?
41, 450 ft
Outflow Valve CLOSES at what CABIN ALT?
15, 000 ft
Maximum Zero Fuel Weight - 300 [QP*]?
175, 000 kg
Maximum Time for continuous Engine Starter Operation?
Maximum 5 mins ON
Maximum Negative Cabin Differential Pressure - 202 [EBA-EBD]?
- 1.0 psi [+/- .1 psi]
Maximum Positive Cabin Differential Pressure?
9.25 psi
Maximum wind for FWD/AFT cargo door operation?
40 kts / 50kts if nose is into wind or door on the downwind side of the aircraft.
Cargo doors must be closed before the wind exceeds 60 kts.
Maximum Normal Cabin Altitude?
8, 000 ft
Maximum Fuel TEMP JET A/JET A1?
+ 49 degrees C
APU can supply electrical power ONLY up to what altitude?
41, 450 ft
Minimum Weight - 300?
121, 000 kg
Minimum Starting Engine Oil Temperature?
- 40 degrees C
Severe Ice Accretion?
When the ice accumulation on the airframe reaches approximately 5 mm thick or more.
Maximum/Minimum GS Angle: Autoland?
3.25 degrees / 2.5 degrees
Flaps FULL Limit Speed: Landing?
180 kts
Use of APU BLEED for WAI?
Not Permitted
Autopilot Engagement: Takeoff/Go-around?
100 ft (or 5 seconds after takeoff)
Autopilot Disengagement: Approach using FINAL APP, NAV FPA, NAV V/S, TRK FPA, HDG V/S?
250 ft AGL
Flight Manoeuvring Load Limits?
+2.5 G to -1 G : Clean Configuration
+2.0 G to 0 G : Other Configurations
Definition of Icing Conditions?
Icing conditions exist when the OAT (Ground) or TAT (in flight) is AT or BELOW 10 degrees C and visible moisture in any form is present.
Icing conditions also exist when the OAT on the ground is AT or BELOW 10 degrees and whilst operating on ramps, taxiways or runways where snow, standing water or slush may be ingested by the engines, or freeze on engines, nacelles or engine sensor probes.