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70 Cards in this Set
- Front
- Back
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Flight maneuvering load acceleration limits |
Clean: -1g to +2.5g Other: 0g to 2.0 g |
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Flight altitude envelope and takeoff and landing envelope |
Max altitude: 39,800 Lowest altitude: -2,000' T/o and landing range: 9,200' to -2,000' |
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Runway slope limit (mean) |
+/- 2% |
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Max runway altitude |
9,200' |
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Nominal runway width |
45m (148') Minimal runway width: 35m |
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Max demonstrated crosswind |
38 kts (gust included) |
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Max tailwind for takeoff and landing |
15 kts Note: for landing in tailwinds greater than 10 kts use flaps full |
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Max wind for passenger door operations |
Pax door operation: 65 kts |
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Max wind for cargo door operations |
Cargo doors operation: 40 kts (50 if the nose is into the wind or if the cargo doors are on the leeward side of the wind) |
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Maximum wind speed before cargo door must be closed |
65 kts |
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Takeoff limitations on contaminated runways |
Not recommended on the following conditions: -Wet Ice -Water on top of compacted snow -Dry snow or wet snow over ice |
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Max flap/slat speeds |
Flap lever 1 in flight: 230 kts Flap lever 1 on the ground: 215 Flaps 2: 200 kts Flaps 3: 185 kts Flaps Full: 177 kts Note: flaps 1 in the air only puts out slats, no flaps are lowered |
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Max Landing Gear Speeds |
Max speed with gear extended (VLE): 280 kt Max speed to extend gear (VLO): 250 kts Max speed to retract gear (VLO): 220 kts |
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Max operating speeds |
MMO: .82 (at max alt - steadily decreases to vmo at FL250) VMO: 350 kts (FL250 and below) |
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Max tire speed |
195 kts |
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Minimum control speed for landing (VMCL) |
113 kts |
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Max wiper operating speed |
230 kts |
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Max speed for cockpit window open |
200kts |
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Taxi turn speed limit |
When weight is over 76,000 kg (167,550 lbs), do not exceed a taxi speed of 20 kts during a turn |
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Max Taxi Weight |
73,900 kg (162,921 lb) |
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Max Takeoff Weight (at breaks release) |
73,500 kg (162,039 lbs) |
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Max Landing Weight |
64,500 kg (142,198 lbs) In exceptional cases, an immediate landing at weight above max landing weight is permitted, providing the pilot follows the overweight landing procedure. |
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Max Zero Fuel Weight |
61,000 kg (134,481 lbs) |
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Minimum Weight |
36,230 kg (82,079 lbs) |
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Limitation on RAM AIR INLET |
Only open if differential pressure is lower than 1 PSI |
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Limitation on air conditioning with low pressure ground unit |
Do not use conditioned air simultaneously from packs and the LP ground unit. Airflow supplied by the ground cart shall not exceed 1.2 kg/s (2.60 lb/s). |
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Limitation on air conditioning with high pressure ground unit |
Do not use HP ground unit when APU supplies bleed air to avoid bleed system damage. |
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Maximum positive differential pressure |
+8.6 PSI differential pressure |
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Maximum negative differential pressure |
-1 PSI differential pressure |
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Temperature/Time limitation on avionics ventillation system |
OAT=49*c no limitation OAT=55*c time limit 2 hours OAT=60*c time limit 1 hour OAT=64*c time limit .5 hour |
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Minimum height for use of autopilot on takeoff with SRS mode |
100' AGL or 5 seconds after takeoff |
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Minimum height for use of the autopilot on a straight-in non precision approach |
Approach minimums |
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Minimum height for use of autopilot on a circling approach |
Circling minimums -100 ft |
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Minimum height for use of the autopilot on an ILS approach when CAT2 or CAT3 is not displayed in the FMA |
160' AGL |
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Minimum height for use of the autopilot on a Precision Approach Radar (PAR appraoch) |
250' AGL The use of AP and/or the FD is authorized in PAR approach, with the HDG V/S or TRK FPA |
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Minimum height for the use of autopilot during a Go-Around (AP or FD engagement) |
100' AGL |
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Minimum heigh for use of the autopilot on a visual approach |
500' AGL |
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Limitation on the AP or FD in OPEN DES or DES mode |
The use of AP or FD in OPEN DES or DES mode is not permitted on approach, unless the FCU altitude is set to (or above) MDA or 500', whichever is highest. |
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Limitation on use of NAV and FINAL APP modes for non-precision approaches |
NAV and FINAL APP mode may be used for VOR, VOR/DME, NDB, NDB/DME, or RNAV (GPS) approaches, but not for ILS, LOC, LOC-BC, LDA, or SDF. |
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Limitation on VOR, VOR/DME, NDB or NDB/DME approaches in NAV or NAV and FINAL APP mode |
If GPS PRIMARY is not available: -The reference NAVAID and the corresponding airborne equipment is serviceable, tuned, and monitored during the approach, or -The radio NAVAID coverage supports the RNP value, specified for the approach procedure. |
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Limitation on a GPS appraoch |
GPS PRIMARY must be available. RNAV approaches without GPS PRIMARY may be performed only if: 1) The radio NAVAID coverage supports the RNP value, and 2) HIGH accuracy is displayed on the MCDU with the specified RNP, and 3) Operational approval is obtained |
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Approved configuration for CAT II or III landing |
CAT II and CAT III autoland are approved in CONF 3 or CONF FULL |
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Maximum wind conditions for CAT II or CAT II automatic approach and landing and roll out |
Headwind: 30kts Tailwind: 10 kts Crosswind: 20 kts |
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Max load per generator |
100% (90KvA) |
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Max load per TR |
200 amps |
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Max operating altitude with slats/flaps retracted |
20,000' |
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Minimum fuel temperature for JET A |
If TAT reaches -34*c, monitor the FUEL SD page that fuel temperature remains higher than -36*c. |
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Minimum fuel quantity for takeoff |
1,500 kg (3,307 lb) and WING TK LO LVL warning must not be displayed on ECAM for takeoff. |
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Limitation on fuel management |
Center tank must be emptied before the wing tanks. |
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Normal operating pressure for hydraulic system |
3,000 PSI |
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Maximum brake temperature for takeoff (brake fans off) |
300*c |
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Maximum allowed fuel imbalance |
INNER TANKS (OUTER TANKS BALANCED) Tank Fuel Quantity (heavier tank): FULL Maximum allowable imbalance: 1,500 kg (3,306 lb) |
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Inertial Reference System - Latitude Limits |
In NAV mode, the IRS will not provide a valid magnetic heading for latitude greater than 73*N and 60*S. Flight outside these limits is prohibited. |
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Limitation on ISIS |
When both PFDs are lost, the ISIS bugs function must not be used. |
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Limitation on the APU starter |
After 3 start motor duty cycles, wait 60 minutes before attempting 3 more cycles. |
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APU max rotor speed |
107% |
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APU max EGT |
657*C |
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Limitation on APU bleed air |
Air bleed extraction for wing anti-icing is not permitted. |
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Engine-Time limit on operating in TOGA setting. |
5 minutes (10 minutes in case of engine failure) |
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Engine-Maximum engine EGT in TOGA setting |
950*C |
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Engine-Max engine EGT in MCT setting |
915*C |
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Engine-Max engine EGT during engine start |
725*C |
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Engine-Max N1 and N2 |
N1 104% N2 105% |
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Minimum oil temperature prior to takeoff |
-10*C |
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Max Continuous Oil Temperature |
140*C |
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Max transient oil temperature |
155*C (15 minutes) |
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Minimum starting oil temperature |
-40*c |
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Engine starter limitation |
1. 4 consecutive cycles: each lasts a max of 2 minutes 2. Pause between start attempts: 20s 3. Cooling period, after 4 start attempts: 15 min 4. No running engagement of the starter, when N2 is above 20% |
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Limitation on thrust reverser usage |
1. It is not permitted to select reverse thrust in flight. 2. It is not permitted to back up the aircraft with reverse thrust. 3. Maximum revers should not be used below 70 kts (or when airspeed starts to fluctuate). 4. Idle reverse is permitted down to aircraft stop. |
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Max crosswind for engine starting |
35 kts |
