Limitations Flashcards

1
Q

Max operating alt

A

410

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2
Q

Max takeoff and landing alt

A

10000 except for 800 and 900 which is 8400

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3
Q

Max crosswind for takeoff or landing including gusts

A

33 kts

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4
Q

Sever turbulence speed

A

.76 or 280 kias

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5
Q

Max taxi weight

A

700 155,000
800 174,900
900 182,200

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6
Q

Max takeoff weight

A

154500
174200
187700

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7
Q

Max landing weight

A

129200
146300
157300

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8
Q

Max zero fuel weight

A

149300

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9
Q

Max differential cabin pressure

A

9.1

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10
Q

Limitations on packs with engine bleeds on

A

Do not operate the packs on high

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11
Q

Autopilot limitations

A

Use of aileron trim is prohibited
Not below 400 feet on takeoff
Single channel operation during approach no autopilot below 50 feet
Don’t use autopilot below 100 ra when pressure alt is 8400

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12
Q

Auto land wind speeds

A

Headwind 25 kts
Crosswind 25 kts
Tailwind 10 kts

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13
Q

Engine ignition

A

On for takeoff landing heavy rain and anti ice operation

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14
Q

Engine start duty cycle

A

Each start attempt to 2 minutes

Min of 10 seconds is required between

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15
Q

Apu loads in flight

A

Bleed plus electrical load 10000 feet

Bleed is 17000

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16
Q

Max flap extension altitude

A

20,000

17
Q

Speed brakes

A

Don’t use below 1000

18
Q

Max winds for heads up display

A

25 hw
15 xw
10 tw

19
Q

Hud limitations

A

May not be used above 8400 pressure
For manual approaches aIII mode is selected and ap and at must be detected prior to 500 tdze
Landing must be flaps 30 or 40 both engines
Landing flaps 15 one engine

20
Q

Max tank fuel temp

A

49

21
Q

Min in flight fuel tank temp

A

3 degrees above freezing point of fuel or -43

22
Q

Max fuel imbalance

A

Between tank 1 and 2 must be scheduled to 0

Random imbalance must not exceed 1000

23
Q

Max tailwind component for takeoff and landing

A

10 kts

24
Q

What are the 6 displays called

A

Primary flight displays
Navigation displays
Upper display unit
Lower display unit

25
Q

What are the displays controlled by

A

Display source panel
Efis control panels
Display select panel

26
Q

What standby instruments are available

A

Standby magnetic compass
Standby attitude indicator
Standby airspeed/altitude

27
Q

Air data reference system

A

Two computers
Adiru L. Captain pitot probe tat probe capt static port and alpha vane

Adiru R fo pitot probe alpha vane fo static port and tat probe
Info is sent to flight displays by two display electronic units

28
Q

Deu 1 and 2

A

Deu supply’s info from various systems number 1 sends info to capt du inboard and out board and upper du
Number 2 is same for fo but Lower du

If either fails the other deu controls all six
Each pilot contains info from separate sources