A320 Part 1 Flashcards
Flight Maneuvering Load Acceleration limits
-Clean Configuration
-Other Configuration
Clean: - 1G to + 2.5 G
Other: 0G to +2G
Max Alt
39,800 ft NEO and CEO (319, 320 y 321)
Min alt for take off and landing
NEO 14,100 ft and -2000 ft (A320, A321)
CEO 14,100 ft and -1000 ft (A319, A320 ceo)
Runway slope
+ - 2% (All)
Runway altitude
14,100 ft (ALL)
Nominal runway width
45M (ALL)
Minimal runway width
30m (ALL)
Maximum demonstrated crosswind (takeoff and landing)
38kt gust included (ALL)
Maximum tailwind for takeoff and landing
15 KT (ALL)
Note: For landing with a tailwind greater than 10kt, using Flaps Full is recomended
Note. (ALL)
The maximum wind for passenger door operation is:
65 kt
The maximum wind for FWD and AFT cargo door operation is:
40 kt (or 50 kt, if the aircraft nose is into the wind, or if the FWD and AFT cargo doors are on the leeward side)
The FWD and AFT cargo doors must be closed before:
Wind speed exceeds 65 kt
Cockpit window open maximum speed
200 kt
Maximum flaps/slats speed
Flap 0
VMO/MMO
Flaps 1
230 kt Holding
Flaps 1+F
215 kt / Take offf
Flaps 2
200 kt / TAKE OFF/ APPROACH
Flaps 3
185 kt T/O APP LNDG
Flaps FULL
177 kt LANDING
VMO
350 kt
MMO
M0.82
Maximum speed with landing gear extended VLE
280 kt / M 0.67
Maximum speed at wich the landing gear may be extended (VLO extension)
250 kt / M 0.60
Maximum speed at which the landing gear may be retracted (VLO retraction)
220 kt / MMO 0.54
Maximum tire ground speed
195 kt
Minimum control speed VMCL
NEO 116 kt
CEO 109 kt
Minimum control speeds on narrow runways :
30M 35m 40m
+2.5 +1.5 +0
Wipers maximum operating speed
230kt
Maximum taxi weight:
NEO 79,400kg
CEO 78,400kg
Maximum takeoff weight (brake release)
NEO 79,000kg
CEO 78,000kg
Maximum landing weight
NEO 67,400kg
CEO 66,000kg
Maximum zero fuel weight
NEO 64,300kg
CEO 62,500kg
Minimum weight
NEO 40,300 kg
CEO 37,230 kg
Note:
With passengers on board, it is not recommended to exceed 20 min without air conditioning supply. The lack of fresh air supply will significantly reduce the cabin’s air quality
Note: APU BLEED USE WITH HP AIR START UNIT
The flight crew must not use bleed air from the APU bleed and from the HP air star unit at the same time, to prevent any adverse effect on the bleed air system.
Avionics ventilation
OAT < 49 C
No limitation
49C < OAT 55C
2h
55C OAT < 60C
1h
60C OAT < 64C
0.5h
Cabin pressure
Maximum positive differential pressure
9.0 PSI
Maximum negative differential pressure
-1.0 PSI
Safety relief valve setting
8.6 PSI
Maximum cabin alt selection
14,000 ft
Cabin altitude warning
9,550 ft
Maximum normal cabin altitude
8,000 ft
Note: PACK USE WITH LP AIR CONDITIONING UNIT
The flight crew must not use conditioned air from the packs and from the LP air-conditioning unit at the same time, to prevent any adverse effect on the air conditioning system