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.
Vmo/Mmo?
330 kts/M.86
Maximum Engine Oil Temperature?
160 degrees C
Maximum LDG Tailwind < 11, 000 ft?
15 kts
If the APU needs to be started off the aircraft batteries - Ground:
What is the minimum BAT1, BAT2 or APU V?
23.5V
Minimum Oxygen Pressure Pre-Flight?
1,330 psi
Maximum Start EGT - In Flight?
975 degrees C
Maximum speed for Idle Reverse Thrust?
Until Stop
Autopilot Disengagement: ILS approach when CATII/CATIII (single or dual) is displayed on the FMA?
0 ft AGL if autoland
Minimum Fuel Quantity for Takeoff?
5, 200 kg
Maximum Cockpit Window Open Speed?
230 kts
Maximum Runway Altitude?
12, 500 ft
Flaps 2 Limit Speed: Takeoff/Approach?
196 kts
Maximum N2?
113 %
Positive Safety Relief Valve Setting?
8.85 psi [+/- .1 psi]
Maximum Wipers Operating Speed?
230 kts
Autopilot Disengagement: All other phases of flight?
500 ft AGL
NOTE: The AP or FD in OP DES or DES mode is not permitted in approach, unless the FCU altitude is set to, or above, the MDA or 500ft AGL, whichever is higher.
Maximum N1?
115.5 %
Maximum Flap/Slats Extension Altitude?
20, 000 ft
Minimum Engine Oil Quantity?
12 qt + estimated consumption (+/- 0.56 qt/hr)
Maximum Takeoff/Go-Around EGT/Time Limit - [OEI]?
975 degrees C / 10 mins
Engine Starter Cooling Cycle?
30 seconds OFF per minute ON
Selection of Reverse Thrust inflight?
PROHIBITED
Maximum Landing Gear Operating/Extended Speed? [VLO/VLE]
250 kts/M.55
Flaps 1 Limit Speed: Takeoff? [1 + F]
215 kts
Autopilot Disengagement: ILS CATII - Manual Landing
[CAT2/CAT3 SINGLE or CAT3 DUAL - FMA]
80 ft AGL
Autopilot Disengagement: ILS Approach when CAT 1 is displayed on the FMA?
160 ft AGL
Autopilot Disengagement: Circling Approach?
500 ft AGL
Turbulence penetration speed: A330-200?
Below FL200 : 240 kts
At or above FL200 : 260kts/M.80
Flaps 2 Limit Speed: Approach? [CONF 1]
205 kts
Maximum Start EGT - On Ground?
750 degrees C
Maximum TO Tailwind?
15 kts
Maximum Altitude for APU to provide Air Conditioning and Pressurization (Dual Pack)?
17, 500 ft
Flaps 1 Limit Speed: Holding?
240 kts
ENGINES: After 2x consecutive 5 min duty cycles, wait…?
10 mins to allow starter to cool
A330 Wingspan?
60.3 m
A/C has NOT been electrically supplied for 6hrs or more - Preflight.
If Battery voltage is < 25.5 V preflight, how long does a charging cycle take?
20 mins
Flaps 3 Limit Speed: Takeoff/Landing?
186 kts
Maximum Landing Weight - 202 [EBA-EBD]?
180, 000 kg
Minimum Control Speed for Landing - 300 [VMCL]?
123 kts
Max Speed Landing Gear Gravity Extension?
200 kts
Maximum Landing Weight - 300 [QP*]?
187, 000 kg
Maximum altitude for APU BLEED to assist engine start?
20, 000 ft
Maximum APU N speed?
107 %
Maximum Landing Weight - 202/203 [EBE-G, J-S, V]?
182, 000 kg
Maximum Brake Temperature for Takeoff?
300 degrees C
Don’t engage Engine Starter with N2 >?
> 30 %
Maximum Continuous Thrust EGT Limit?
940 degrees C
Maximum Taxi Weight - ALL?
233, 900 kg
Autopilot Disengagement: Approach using F-LOC or F-G/S?
200 ft AGL
APU START?
Maximum 3 x consecutive starts attempts, then wait 60 mins before new start attempt.
Maximum Tire Speed?
204 kts
Nominal Runway Width?
45 m
Minimum Inflight TAT?
-53 degrees C
Minimum Weight - 202-203?
116, 000 kg
A/C has not been electrically supplied for 6hrs or more - Preflight.
Minimum BAT1, BAT2 and APU V?
25.5V
Maximum Crosswind TO/LDG - WET RWY?
32 kts
APU Battery Restart Limit Altitude?
[ELEC EMER CONFIG]
25, 000 ft
Maximum Crosswind TO/LDG - DRY RWY?
40 kts
Maximum LDG Tailwind - Autoland (CATII/III)?
10 kts
During refuelling/defuelling procedures, APU starts or shutdowns are permitted with the following restriction:
- If the APU failed to start or following and automatic shutdown, do not start the APU
- If a fuel spill occurs, perform and APU shutdown.
Maximum Negative Cabin Differential Pressure? [EBE-G, J-S, V, QP*]?
- 0.73 psi [+/- .1 psi]
Maximum Headwind: ILS CAT II/III Autoland?
35 kts
Turbulence penetration speed: A330-300?
Below FL200 : 240 kts
At or above FL200 : 260kts/M.78
Maximum LDG Tailwind > 11, 000 ft?
10 kts
Minimum Fuel TEMP?
INNER TANK: Freezing Point +3 degrees C or -54 degrees C [whichever is higher]
Note: JETA1 FP = -47 + 3 = -44 degreesC
OUTER or TRIM TANK: Freezing Point
Maximum Altitude for APU to provide Air Conditioning and Pressurization (Single Pack)?
22, 500 ft
Maximum EGT for APU start?
1, 250 degrees C
Maximum Takeoff Weight - ALL?
233, 000 kg
Maximum wind for passenger door operation?
40 kts / 50kts if nose is into wind.
Passenger doors must be closed before wind exceeds 60 kts.
With passengers on board, how long before air conditioning must be supplied?
20 mins
APU can supply both bleed air and electrical power up to what altitude?
22, 500 ft
Maximum Brake Temperature for Takeoff? [with FANS]
150 degrees C
Maximum APU operating altitude?
41, 450 ft
Maximum Speed for Max Reverse Thrust?
> 70 kts
Maximum Runway Slope?
+/-2%
Maximum Engine Oil Transient Temperature? (15 mins)
175 degrees C
Minimum Engine Oil Pressure?
10 psi
Maximum Crosswind: ILS CAT II/III Autoland?
20 kts
Maximum Zero Fuel Weight - 202 [EBA-EBD]?
168, 000 kg
Maximum Zero Fuel Weight - 202/203 [EBE-G, J-S, V]?
170, 000 kg