Limitations Flashcards

1
Q

Autopilot engagement for takeoff

A

Not below 400 ft

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2
Q

Fuel loading

A

Main tank 1 and 2 must be full if the center tank contains more than 453kg

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3
Q

Single channel autopilot on approach

A

Not below 50ft

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4
Q

Autoland wind limits

A

Headwind 25kts
Crosswind 20kts
Tailwind 15kts

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5
Q

Severe Turbulence Air Penetration speed

A

Climb 280 KIAS/ .76 Mach, whichever is lower.

Cruise FMC recommended thrust setting.

Descent .76 Mach/ 280/ 250kts (below 150/ MLW)

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6
Q

Ground wind limits for all doors

A
  • 40kts while opening or closing
  • 65kts while open
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7
Q

Holding

A

Holding in icing conditions with flaps extended is prohibited.

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8
Q

Maximum fuel tank temperature

A

49 degrees

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9
Q

Minimum fuel tank temerature

A

-43 degrees or 3 degrees above the fuel freezing temperature, whichever is higher

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10
Q

Maximum flap extention altitude

A

20,000ft

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11
Q

Autoland capability

A

Flaps 30 or 40

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12
Q

LVL CHG

A

Do not use below 1000ft AFE

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13
Q

Maximum and minimum glideslope angles for Autoland

A

3.25 and 2.5 degrees

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14
Q

Engine Limits

A

Maximum and minimum limits are RED

Caution limits are AMBER

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15
Q

Engine Ignition must be on for

A
  • Takeoff
  • Landing
  • Operation in heavy rain
  • Anti ice operation
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16
Q

Reverse Thrust

A

Intentional selection of reverse thrust in flight is prohibited.

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17
Q

ATM takeoff thrust restrictions

A

Not permitted with antiskid inoperative or contaminated RWY.

18
Q

Inflight APU Bleed + electrical load

A

10,000ft

19
Q

APU bleed limitation

A

17,000ft

20
Q

APU electrical load

A

41,000ft

21
Q

After 3 consecutive aborted start attemps

A

15 minute cooling period is required

22
Q

Before using APU bleed air

A

Run the APU for 2 full minutes

23
Q

Flight control limitations

A

Avoid rapid and large alternating control inputs

24
Q

Do not deploy speedbrakes

A

below 1,000ft RA

25
Q

Alternate flap duty cycle

A

When extending or retracting flaps with the ALTERNATE FLAPS position switch, allow 15 seconds between movements to avoid clutch damage.

After a complete extend/ retract cycle allow 5 minutes for cooling

26
Q

Avoid weather radar operation

A
  • In hanger
  • When personnel are within the area normally enclosed by the airplane nose radome
27
Q

HGS AIII Demonstrated Conditions

A

Headwind 25kts
Crosswind 15kts
Tailwind 10kts
Field Elevation 5,500ft

28
Q

RVSM Altimeter on ground discrepancy

A

Max difference between Capt & FO 50ft (up to 5,000ft)

Max difference between Capt of FO and field elev 75ft

29
Q

HF radios

A

Do not operate HF radio while refuelling

30
Q

Runway slo/-pe

A

+/- 2%

31
Q

Landing Gear (extend) Limit

A

270kts

32
Q

Landing gear (retract) Limit

A

235kts

33
Q

Landing gear (extended) Limit

A

320kts/.82M

34
Q

Flap limit 1-5

A

250kts

35
Q

Flap limit 10

A

210kts

36
Q

Flap limit 15

A

200kts

37
Q

Flap limit 25

A

190kts

38
Q

Flap limit 30

A

175kts

39
Q

Flap limit 40

A

162kts

40
Q

Alternate flap extension limit

A

230kts