Limitations Flashcards
Flight maneuvering load accelerations limits: Clean configuration
-1 g to +2.5 g
Flight maneuvering load accelerations limits: Other configurations
0 g to +2 g
Environmental envelope: take off and landing
-2000 ft to 9200 ft
Maximum certified crosswind for take off
35 kt (gust included) / note: - the maximum certified crosswind value for take of is an airplane flight manual limitation : it it an engine limitation
Maximum demonstrated crosswind for landing
38 kt (gust included) / note: - is not an airplane flight manual limitation : it is the maximum crosswind condition experienced during the aircraft certification campaign
Maximum tailwind for takeoff and landing
15 kt
Maximum wind for Passenger and cargo doors operations
65 kt passenger door / 40 kt cargo door
Cockpit window open maximum speed
200 kt
VMO / MMO
350 kt / M 0.82
Maximum speeds with the landing gear extended
280 kt /M 0.67 (VLE extended)
250 kt /M0.60 (VLO extension)
220 kt /M0.54 (VLO retraction)
Maximum tire speed
195 kt
Minimum control speed for landing (VMCL)
116
Wipers maximum operating speed
230 kt
Maximum take off weight
77.000 kg
Maximum landing weight
67.400 kg
[321] maximum take off weight
89.000 kg
[321] maximum landing weight
79.200 kg
Maximum altitude flaps/slats extended
20.000 ft
Minimum fuel quantity for takeoff
1.500 kg
Definition of icing conditions
OAT (ong ground of after takeoff) or TAT (in flight) is at or below 10 degrees celsius and visible moisture in any form is present
Maximum brake temperature for takeoff
300 degrees Celsius
Maximum nosewheel steering angle
85 degrees
Taxi with deflated or damaged tires
If maximum one tire per gear is deflated: 7 kt
if two tires are deflated on the same main gear: 3 kt
wingspan value 320 neo
35.8 m
Length value 320 neo
37,57
Apu start
After 3 consecutive APU start attempts, the flight crew must wait 60 min before a new start attempt
Thrust setting/EGT limits
Takeoff and go around: 1060 degrees Celsius
Maximum continuous thrust (MCT): 1025 degrees Celsius
Starting: on ground 750 degrees Celsius / in flight 875 degrees Celsius
Oil temperature
Maximum continuous temperature: 140 graus
Maximum transient (15 min): 155 graus
Minimum starting temperatude: -40 degrees Celsius
Minimum temperature before takeoff: 19 degrees Celsius
Minimum oil quantity
8.9 qt + estimated consumption. Maximum estimated consumption = 0.45 qt/h
Minimum oil quantity: 10.6 qt
Minimum oil pressure
17.4 psi
Maximum oil pressure
Maximum oil pressure (above 50 graus): 130.5 psi
Maximum oil pressure (below 50 graus: 145 psi
