Limitations Flashcards

1
Q

Flight maneuvering load accelerations limits: Clean configuration

A

-1 g to +2.5 g

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2
Q

Flight maneuvering load accelerations limits: Other configurations

A

0 g to +2 g

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3
Q

Environmental envelope: take off and landing

A

-2000 ft to 9200 ft

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4
Q

Maximum certified crosswind for take off

A

35 kt (gust included) / note: - the maximum certified crosswind value for take of is an airplane flight manual limitation : it it an engine limitation

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5
Q

Maximum demonstrated crosswind for landing

A

38 kt (gust included) / note: - is not an airplane flight manual limitation : it is the maximum crosswind condition experienced during the aircraft certification campaign

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6
Q

Maximum tailwind for takeoff and landing

A

15 kt

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7
Q

Maximum wind for Passenger and cargo doors operations

A

65 kt passenger door / 40 kt cargo door

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8
Q

Cockpit window open maximum speed

A

200 kt

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9
Q

VMO / MMO

A

350 kt / M 0.82

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10
Q

Maximum speeds with the landing gear extended

A

280 kt /M 0.67 (VLE extended)
250 kt /M0.60 (VLO extension)
220 kt /M0.54 (VLO retraction)

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11
Q

Maximum tire speed

A

195 kt

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12
Q

Minimum control speed for landing (VMCL)

A

116

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13
Q

Wipers maximum operating speed

A

230 kt

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14
Q

Maximum take off weight

A

77.000 kg

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15
Q

Maximum landing weight

A

67.400 kg

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16
Q

[321] maximum take off weight

A

89.000 kg

17
Q

[321] maximum landing weight

A

79.200 kg

18
Q

Maximum altitude flaps/slats extended

A

20.000 ft

19
Q

Minimum fuel quantity for takeoff

A

1.500 kg

20
Q

Definition of icing conditions

A

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

21
Q

Maximum brake temperature for takeoff

A

300 degrees Celsius

22
Q

Maximum nosewheel steering angle

A

85 degrees

23
Q

Taxi with deflated or damaged tires

A

If maximum one tire per gear is deflated: 7 kt
if two tires are deflated on the same main gear: 3 kt

24
Q

wingspan value 320 neo

A

35.8 m

25
Q

Length value 320 neo

A

37,57

26
Q

Apu start

A

After 3 consecutive APU start attempts, the flight crew must wait 60 min before a new start attempt

27
Q

Thrust setting/EGT limits

A

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

28
Q

Oil temperature

A

Maximum continuous temperature: 140 graus

Maximum transient (15 min): 155 graus

Minimum starting temperatude: -40 degrees Celsius

Minimum temperature before takeoff: 19 degrees Celsius

29
Q

Minimum oil quantity

A

8.9 qt + estimated consumption. Maximum estimated consumption = 0.45 qt/h

Minimum oil quantity: 10.6 qt

30
Q

Minimum oil pressure

A

17.4 psi

31
Q

Maximum oil pressure

A

Maximum oil pressure (above 50 graus): 130.5 psi

Maximum oil pressure (below 50 graus: 145 psi