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737 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max ramp weight

A

79,242

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2
Q

Max Take off weight

A

79,015

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3
Q

Max landing weight

A

66,360

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4
Q

Max zero fuel weight

A

62,731

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5
Q

Runway greater than 45m crosswind limits

A

Takeoff;

Dry: 34kts
Wet: 25kts

Landing;

Dry: 40kts
Wet: 40kts

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6
Q

Runways less than 45m crosswind limits

A

Takeoff;

Dry: 25kts
Wet: 25kts

Landing;

Dry: 25kts
Wet: 25kts

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7
Q

Flap limitations settings 1 - 5

A

250kts

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8
Q

Flap limitation settings 10 & 15

A

210kts

200kts

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9
Q

Flap limitations settings 25 & 30

A

190kts

175kts

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10
Q

Flap limitations setting 40 and alternate extension

A

162kts

230kts

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11
Q

Gear limitations

Extend

Retract

Extended

A

270kts or .82M

235kts

320kts or .82M

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12
Q

T/O and LDG tailwind limits

A

15kts demonstrated

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13
Q

Max altitude

A

FL410

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14
Q

Maximum T/O and LDG altitudes

A

8,400’

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15
Q

Max runway slope

A

2%

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16
Q

HF refuelling

A

Prohibited

17
Q

Max cabin differential

A

9.1 PSI

18
Q

Level change minimum height

A

1,000’

19
Q

Aileron trim with autopilot

A

Prohibited

20
Q

Autopilot minimum altitude

A

400’AGL for engaging

21
Q

Minimum and maximum G/S

A

2.5* to 3.25*

22
Q

Autoland limitations

A

H/W - 25kts
X/W - 20kts
T/W - 15kts
Flap settings 30 and 40 and two engine only

23
Q

Reverse thrust in flight

A

Prohibited

24
Q

APU bleed and electric heights

A

Bleed only - 17,000’
Elec only - 41,000’

FAA
Bleed and electric air - 10,000’
Bleed and electric ground - 15,000’

25
Q

Maximum altitude with flaps extended

A

FL 200

26
Q

Holding in icing conditions

A

use of flaps is prohibited

27
Q

Speedbrake in flight

A

Do not exceed flight detention

And

Do not use below 1,000’ RA

28
Q

Large and rapid control inputs

A

Avoid rapid and large control inputs, especially in combination with large changes in pitch roll or yaw, (large side slip angles) as they may result in structural failure at any speed even below VA.

29
Q

Usage of weather radar

A

Avoid using in a hangar or within 50’ of refuelling or a fuel spill.

Avoid using when people are within the normally enclosed radome area.

30
Q

Fuel temps

A

Maximum - 49*

Minimum - -43* or fuel freeze plus 3*

31
Q

Fuel imbalance

A

Should be 0kg

Can be a maximum of 453kg for taxi, takeoff, Flight or landing.

Main tanks 1 & 2 must be full if centre tank is above 453kg

32
Q

When is takeoff prohibited

A

The requirements of the standard takeoff minima aren’t met.
Snow, ice or frost on the aircrafts critical surfaces.
Falling snow or freezing precipitation since last inspection.
Runway braking reported as poor.
Runway is contaminated.

33
Q

Company descent speed limits

A

250kt below 10,000’ (unless approved by ATC)

250kt below 5,000’

210kt below 2,000’ AAL

34
Q

What is the stable approach criteria?

A

Speed +10 / -5kts of Vapp or magenta target.
Descent rate of 1,000’pm or as briefed
Wings level with small corrections to maintain intended flight path
Pitch attitude between -2.5* and 10*
PAPI - 3 whites or reds
TVASIS - 2 whites high or low.

Note: when circling or offset approach must be satisfied by 500’AGL or Go Around.

35
Q

Severe turbulence penetration speed

A

280 KIAS

M0.76

36
Q 
Instrument approach limits
NDB
VOR
XTK
LOC
GS
Distance Alt check height
A 
NDB: 5*
VOR: 5* or half scale
XTK: 0.3nm
LOC: 1/2 scale
GS: 1/2 Scale
Check height: +-200’
37
Q

Mayday call inclusions

A

Mayday X 3

  • Station addressed
  • Aircraft ID
  • Nature of call eg. Fire/fuel etc
  • intentions
  • Position
  • other info if reqd
38
Q

Minimum Fuel Quantity for operation of Electric hydraulic pumps

A

760kg per side

737 (17 decks)

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