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24 Cards in this Set
- Front
- Back
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MTOW -321 |
93T |
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MRW - 321 |
93.4T |
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MLW -321 |
77.8T |
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MZFW - 321 |
73.8T |
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Type of flaps |
Double slotted Fouler Flaps |
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VMCA - 321 Clean |
114 kts |
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Max EGT |
TOGA- 650° EF 10mins - 650° Startup - 635° MCT - 610°
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VFE all |
Config 1 - 235 Config 1+F - 225 Config 2 - 215 Config 3 - 195 Config Full - 190 |
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Autoflight |
No AP use below 900ft outside of TO/LDG |
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30m Runway Ops |
Permitted only if runway has turning nodes Min turn radius 32m EFA - not permitted |
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Max Pax |
220/230 - upgraded cabin config |
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Slide and raft config |
Slide Rafts - LR 1+4 Escape Slide LR 2+3
FO operates R1 slide raft FO takes Survival Kit from R1 Galley |
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Packs operation |
ECON - less than 168 pax ECON OFF - Normal APU or Single pack - auto high flow |
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Speed brake use |
Full spd brake can be used in Auto or manual flight
Full spd brake is equal to 1/2 on a320
SPD brake is inhibited from Config 3 |
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Fuel tanks |
Single large fuel tank in each wing
Centre tank
Jet pumps transfer fuel from centre tank to wing tanks through Venturi effect
Fuel for engine taken from wing tanks only
Max capacity w/o ACT 18605kg |
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Max flex |
Flex ISA+ 42° |
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Fuel burn |
3T per hour 50kg/min 6.5kg/nm |
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Turbulence penetration speeds |
275 below FL200 305/M0.76 above FL200 |
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ETOPs calculation |
60mins - 405nm 120mins - 774nn Profile Used 0.78M/320kts FL120 MCT |
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Can an Airbus stall in normal conditions? |
Yes. On transition from NORMAL LAW to DIRECT LAW and vice versa on T/O and landing. |
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Max tank imbalance 321 at TO |
Full tanks - 300kg, allowance increases with reduction in fuel. |
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Fuel gravity feeding |
2T centre tank fuel unusable ALWAYS |
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T/O alternate / Return Airport Requirements |
Required when conditions are below lowest usable landing minima available for a return. Plan for SE ops. (Cat IIIA, 50ft 175m) Within 405nm Adequate (SE 60mins 321) |
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Basic Empty Weight - ULD |
46T |
