| 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 | | |
