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MZFW
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Runway slope + ou -...
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Limitations A320
a few A320 limitations
| Question | Answer | ||
|---|---|---|---|
| MZFW | 64.3 | ||
| Runway slope + ou -... | 2% | ||
| Runway altitude max | 9 200ft | ||
| Maximum X-wind T/O | 35kt LDG —> | 38kt | |
| Maxi tail wind for take off | 15kt | ||
| Maxi tail wind for landing | 15kt | ||
| Maximum wind for passenger door operation ? | 65kt | ||
| Maximum wind for cargo door operation ? | 40kt or ... ? --> | 50kt si nose into the wind or cargo door on the leeward side | |
| Max wind to close cargo doors ? | 65kt | ||
| VMO | 350kt | ||
| MMO | M0.82 | ||
| VLE | 280kt value in Mach ? --> | 0.67 | |
| VLO extension | 250kt Valut in Mach ? | 0.60 | |
| VLO retraction | 220kt Valeur in Mach ? | 0.54 | |
| Maximum altitude at which landing gear can be extended | 25 000ft | ||
| Maximum tire ground speed | 195kt | ||
| Maximum windshield wipers in use | 230kt | ||
| Maximum cockpit window opening | 200kt | ||
| RAM ok to open if differential pressure below... | 1 PSI | ||
| is it ok to use LP ground unit and packs at the same time ? | no | ||
| is it ok to use HP ground unit when APU supplies bleed air ? | no | ||
| Minimum height of use of autopilot on T/O | 100ft AGL or 5s after liftoff | ||
| Minimum height of use of autopilot with FINAL APP, V/S or FPA mode | 250ft | ||
| Minimum height of use of autopilot on circling app | 500ft for cat C | ||
| Minimum height of use of autopilot on ILS Cat 1 | 160ft AGL | ||
| Minimum height of use of autopilot on PAR app | 250ft | ||
| Minimum height of use of autopilot on go around | 100ft AGL | ||
| Minimum height of use of autopilot (all other phases) | 500ft AGL | ||
| Use of the AP or FD in OPEN DES or DES mode is not permitted in approach, unless the FCU altitude is set to, or above | MDA (MDH) or 500 ft, whichever is the highest | ||
| Automatic Landings : max Headwind | 30kt | ||
| Automatic Landings : max Tailwind | 10kt | ||
| Automatic Landings : max Crosswind | 20kt (or 15kt in rollout One Engine Inop) | ||
| CAT II and CAT III autoland are approved in CONF ... | 3 or Full | ||
| Automatic landing is demonstrated with glide path angle within... | -2.5 °, -3.25 ° | ||
| Automatic landing is demonstrated with weight... | At or below MLW | ||
| Automatic landing is demonstrated for airport elevation at or below... | 9200 ft but not below XXX ft altitude pressure ? | - 2000 ft | |
| Automatic landing is demonstrated at which speed ? | approach speed (VAPP) = VLS + wind correction (Minimum wind correction 5 kt, maximum wind correction 15 kt) | ||
| Automatic rollout performance has been approved on ..... or ..... runways (type of contamination) | dry or wet | ||
| Maximum operating altitude with flaps and/or slats extended is | 20 000 ft | ||
| Maximum brake temperature for takeoff (brake fans off) = | 300 °C | ||
| APU Inflight battery start jusqu’à .... ft | 25 000 ft | ||
| APU Bleed up to ... ft | 22500ft. 2 packs up to... | 15000ft. Eng start up to... | 20000ft |
| Oil Minimum starting temperature | -40 °C | ||
| Oil Minimum temperature for takeoff | -10 °C | ||
| Starter : .... consecutive cycles, with …. s between each cycle | Starter : 3 consecutive cycles, with 60s between each cycle Cooling period, after 3 start attempts: ... min | 15 min | |
| Maximum reverse should not be used below ... kt | 70 kt | ||
| Takeoff at reduced thrust is permitted on contaminated runways ? | no | ||
| Maximum takeoff alternate distance | 405 NM | ||
| Maximum distance from an adequate aerodrome | 405 NM | ||
| minimum oil quantity for the flight | 8,9 qt + 0,45 qt / hdv | ||
| Minimum battery voltage at power-up if a/c not electrically supplied for more than 6h | 25.5V if below ? --> | after 20 min, check above 25.5V | |
| Maximum X-wind for ENG start | 45kt | ||
| Fuel temp min …., max …. | -43°C / 55°C | ||
| Oxygène cockpit au sol | > 550 psi pour CDB / > 780 si obsv 2 > 550 psi pour OPL / > 780 si obsv 1 |
Created by:
niklas320