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Airbus > Limitations > Flashcards

Limitations Flashcards

0
Q

Runway slope (mean)

A

+- 2%

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1
Q

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS

A

Clean configuration . . . . . . . . . . . . . - 1 g to + 2.5 g

Slats and/or flaps extended . . . . . . . . . . 0 g to + 2 g

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2
Q

Runway altitude

A

9200 ft

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3
Q

Minimum runway width

A

100 ft/30m

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4
Q

Maximum crosswind demonstrated for takeoff

A

38 kt*

*The maximum demonstrated crosswind value is not an Airplane Flight Manual (AFM)
limitation: It is the maximum crosswind condition experienced during the aircraft
certification campaign. Airbus recommends that operators should not intentionally
operate in crosswinds that exceed this value.

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5
Q

Maximum crosswind demonstrated for landing

A

38 kt*

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6
Q

Maximum tailwind for takeoff (319 & 320)

A

15 kts

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7
Q

Maximum tailwind for landing (319, 320 & 321)

A

10 kts

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8
Q

NORMAL & NARROW RUNWAY LENGTHS

A

A normal runway is any runway at least 150 ft/45m wide.

A narrow runway is any runway less than 150 ft/45m wide.

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9
Q

Maximum wind for passenger door operation

A

65 kt

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10
Q

Maximum wind for cargo door operation

A

40 kt/*50 kt

  • If the aircraft nose is oriented into the wind, or if the cargo door is on the leeward
    side of the aircraft, operation of the cargo door is permitted in winds up to 50
    knots. If wind speed begins to exceed these limitations, the cargo door must be
    closed before the wind speed exceeds 65 kts.
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11
Q

Maximum VMO/MMO

A

350 kt/.82 mach

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12
Q

SEVERE TURBULENT AIR PENETRATION

SPEED

A

FL200 and below. . . . . . . . . . . . . . . . . . . . . . . 250 kt

Above FL200 through FL310 . . . . . . . . . . . . . 275 kt

Above FL310 . . . . . . . . . . . . . . . . . . . . . .0.76 mach

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13
Q

Runway altitude

A

9,200 ft

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14
Q

Minimum runway width

A

100 ft/30m

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15
Q

Contaminated Runway

Maximum demonstrated cross wind for takeoff and landing:

A

Wet runway . . . . . . . . . . . . . . . .33 kt (gust included)

Contaminated runway . . . . . . . 10 kt (gust included)

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16
Q

Maximum wind for cargo door operation

A

40 kt/*50 kt

  • If the aircraft nose is oriented into the wind, or if the cargo door is on the leeward
    side of the aircraft, operation of the cargo door is permitted in winds up to 50
    knots. If wind speed begins to exceed these limitations, the cargo door must be
    closed before the wind speed exceeds 65 kts.
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17
Q

SEVERE TURBULENT AIR PENETRATION

SPEED

A

FL200 and below. . . . . . . . . . . . . . . . . . . . . . .250 kt

Above FL200 through FL310 . . . . . . . . . . . . . 275 kt

Above FL310 . . . . . . . . . . . . . . . . . . . . . .0.76 mach

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18
Q

MAXIMUM FLAPS/SLATS SPEEDS

A
  1. 230 Holding
  2. 215 Takeoff
  3. 200 Takeoff / Approach
  4. 185 Takeoff / Approach / Landing
    Full. 177 Landing

It is Frontier’s procedure to extend flaps at a maximum of VFE - 10 knots, except for
Flaps Full, which will be extended at a maximum of VFE - 15 knots.

19
Q

Maximum altitude at which the landing gear may be extended

A

25,000 ft

20
Q

Maximum Tire Speed (ground speed)

A

195 kt

21
Q

Maximum speed for use of windshield wipers

A

230 kt

22
Q

Maximum speed for opening cockpit window

A

200 kt

23
Q

TAXI SPEED (A320)

A

When the taxi weight is higher than 167,550 lbs do not exceed a taxi speed of 20
kt during a turn.

24
Q

Max operating altitude with slats and/or flaps extended

A

20000 feet

25
Q

AUTOPILOT ENGAGEMENT

A

After Takeoff/Go-Around (If SRS is indicated) 100 AGL

Non-Autoland ILS Approach with CAT 1 displayed on FMA 160 AGL
Non-Autoland ILS Approach with CAT 2/3 displayed on FMA 80 AGL
Autoland ILS Approach (one or two autopilots) Rollout/Taxi Speed

26
Q

AUTOLAND WIND RESTRICTIONS

A

For autolanding, the surface wind conditions are limited to the following:

– 30 knots of headwind
– 15 knots of crosswind
– 10 knots of tailwind

27
Q

Autobrakes (if available) are required when….

A

Autobrakes (if available) are required for all CAT III approaches.
– Runways less than 8000 ft – Medium
– Runways 8000 ft or longer – Low or Medium

28
Q

Autolands are prohibited if…

A

braking action is reported less than fair.

29
Q

The minimum fuel quantity for takeoff is

A

3300 lbs

30
Q

Maximum brake temperature for takeoff

A

300 C

31
Q

GEAR DOWN SPEEDS

A

Maximum speed with landing gear extended (VLE) . . . . . . . . . . . . . . . .280 kt/.67 mach

Maximum speed at which the landing gear may be extended . . . . . . . . . . . . . . . 250 kt
(VLO extension)

Maximum speed at which the landing gear may be retracted . . . . . . . . . . . . . . . 220 kt
(VLO retraction)

32
Q

APU LOW OIL LEVEL ECAM

A

10 hours

33
Q

APU Maximum altitude for APU electrical and start

A

39,000 ft

34
Q

Maximum altitude for APU battery start

A

25,000 ft

35
Q

The APU automatically shuts down at

A

107 %

36
Q

APU starter cycles

A

After three starter motor duty cycles, each separated by a one minute cool down, wait
60 minutes before attempting three more cycles.

37
Q

APU Maximum EGT

A

675 C

38
Q

APU Maximum EGT for start (below 35,000 feet)

A

1090 C

39
Q

APU Maximum EGT for start (above 35,000 feet)

A

1120 C

40
Q

Maximum altitude for APU pneumatics (1 pack w/electrical)

A

22,500 ft

41
Q

Maximum altitude for APU pneumatics (2 packs w/electrical)

A

15,000 ft

42
Q

Maximum altitude for APU assisted engine start

A

20,000 ft

43
Q

MAX hydraulic pressure

A

3200 psi

44
Q

Maximum brake temperature for takeoff

A

300 C

Airbus (2 decks)

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