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

18
Q

Level change minimum height

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
Maximum altitude with flaps extended
FL 200
26
Holding in icing conditions
use of flaps is prohibited
27
Speedbrake in flight
Do not exceed flight detention And Do not use below 1,000' RA
28
Large and rapid control inputs
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
Usage of weather radar
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
Fuel temps
Maximum - 49* | Minimum - -43* or fuel freeze plus 3*
31
Fuel imbalance
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
When is takeoff prohibited
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
Company descent speed limits
250kt below 10,000' (unless approved by ATC) 250kt below 5,000' 210kt below 2,000' AAL
34
What is the stable approach criteria?
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
Severe turbulence penetration speed
280 KIAS | M0.76
36
``` Instrument approach limits NDB VOR XTK LOC GS Distance Alt check height ```
``` NDB: 5* VOR: 5* or half scale XTK: 0.3nm LOC: 1/2 scale GS: 1/2 Scale Check height: +-200’ ```
37
Mayday call inclusions
Mayday X 3 - Station addressed - Aircraft ID - Nature of call eg. Fire/fuel etc - intentions - Position - other info if reqd
38
Minimum Fuel Quantity for operation of Electric hydraulic pumps
760kg per side