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airbus > LIMITATIONS > Flashcards

LIMITATIONS Flashcards

1
Q

WINGSPAN, Non-Sharklet

A319, A320

A

111 feet, 10 inches

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2
Q

WINGSPAN, Sharklet

A320, A321

A

117 feet, 5 inches

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3
Q

GROUND CLEARANCE TABLE
Tailstrike Pitch Attitude.

L/G Struts Compressed

A319
A320
A320 NEO
A321

A

A319 - 13.9

A320 - 11.7

A320 NEO - 11.7

A321 - 9.7

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4
Q

MAXIMUM CERTIFIED ALTITUDE

A

FL398

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5
Q

RUNWAY SLOPE (mean)

A

+- 2%

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6
Q

RUNWAY ALTITUDE

A

9,200 ft

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7
Q

NOMINAL RUNWAY WIDTH

A

45 m (148 ft)

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8
Q

MAXIMUM DEMONSTRATED CROSSWIND (takeoff and landing)

A

38 kt (gust included)

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9
Q

MAXIMUM TAILWIND FOR TAKEOFF

A

15 kt

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10
Q

MAXIMUM TAILWIND FOR LANDING

A

10 kt

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11
Q

MAXIMUM WIND FOR PASSENGER DOOR OPERATION

A

65 kt

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12
Q

MAX W/ LANDING GEAR EXTENDED (VLE)

A

280 kt/M.67

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13
Q

MAX LANDING GEAR EXTENSION (VLO Extension)

A

250 kt/M.60

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14
Q

MAX LANDING GEAR RETRACTION (VLO Retraction)

A

220 kt/M.54

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15
Q

MAX ALTITUDE LANDING GEAR MAY BE EXTENDED

A

25,000 ft

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16
Q

WIPERS MAXIMUM OPERATING SPEED

A

230 kt

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17
Q

APPLICABLE TO 601NK THRU N696NK

When the taxi weight is higher than___________:
Caution: Do not exceed a taxi speed of ____kt during a turn

A

167,550

20

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18
Q

APPLICABLE TO N502NK THRU N536NK

MAX LANDING

A

137,788

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19
Q

APPLICABLE TO N601NK THRU N656NK, N690NK THRU N696NK

MAX LANDING

A

145,505 lb

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20
Q

APPLICABLE TO N901NK THRU N915NK

MAX LANDING

A

148,591

21
Q

APPLICABLE TO N657NK THRU N687NK

MAX LANDING

A

171,519

22
Q

APU BLEED USE WITH AIR START UNIT

A

The flight crew must not use bleed air from the APU BLEED and from the HP Air Unit at the same time, to prevent any adverse effect on the Bleed Air System.

23
Q

CABIN PRESSURE

MAX POSITIVE DIFFERENTIAL

MAX NEGATIVE DIFFERENTIAL

A
  1. 0 PSI

- 1.0 PSI

24
Q

PACKS USE WITH LP AIR CONDITIONING UNIT

A

The flight crew must not use conditioned air from the packs and from the LP Air Conditioning Unit at the same time, to prevent any adverse effect on the Air Conditioning System.

25
Q

MINIMUM HEIGHT FOR USE OF AUTOPILOT

TAKEOFF WITH SRS MODE

A

100 ft AGL

26
Q

MINIMUM HEIGHT FOR USE OF AUTOPILOT

STRAIGHT-IN NON-PRECISION APPROACH

A

Applicable Minimum

27
Q

MINIMUM HEIGHT FOR USE OF AUTOPILOT

CIRCLING APPROACH

A

Applicable Minimum -100 ft

28
Q

MINIMUM HEIGHT FOR USE OF AUTOPILOT

ILS APPR WHEN CAT 2 OR CAT 3 IS NOT DISPLAYED ON THE FMA

A

160 ft AGL

29
Q

MINIMUM HEIGHT FOR USE OF AUTOPILOT

GO-AROUND (AP OR FD ENGAGEMENT)

A

100 ft AGL

30
Q

MINIMUM HEIGHT FOR USE OF AUTOPILOT

ALL OTHER PHASES

A

500 ft AGL (319/320)

900 ft AGL (321)

31
Q

MINIMUM HEIGHT FOR USE OF AUTOPILOT

USE OF THE AP OR FD IN OPEN DES OR DES MODE IS NOT PERMITTED IN APPROACH, UNLESS THE FCU ALTITUDE IS SET AT OR ABOVE

A

Highest of:

Minimum or 500 ft (319/320)
Minimum or 900 ft (321)

32
Q

USE OF NAV MODE:

IN THE TERMINAL AREA

A

NAV mode may be used in the terminal area provided that:

  • GPS Primary is available, or
  • The appropriate RNP is checked or entered on the MCDU, and HIGH accuracy is displayed, or
  • FMS navigation is crosschecked with navaid raw data
33
Q

APPLICABLE TO N502NK THRU N536, N657NK THRU N687NK

Non-Precision Approaches with Engine-Out

A

If one engine is inoperative, it is not permitted to use the autopilot to perform NPAs in the following modes: FINAL APP, NAV V/S, NAV/FPA

Only FD use is permitted

34
Q

APU START

A

After three consecutive APU start attempts, the Flight Crew must wait 60 min before a new start attempt

35
Q

POWER PLANT
Thrust Setting/EGT Limits
Applicable to N502NK THRU N656NK, N690NK THRU N696NK

A

Takeoff and Go-around
All engines operative 5 min
One engine inoperative 10 min
635C

MCT 610C

Starting, On Ground
In Flight
635C

36
Q

POWER PLANT
Thrust Setting/EGT Limits
APPLICABLE TO N657NK THRU N687NK

A

Takeoff and Go-around
All engines operative 5 min
One engine inoperative 10 min
650C

MCT 610C

Starting, On ground
In flight
635C

37
Q

POWER PLANT
Thrust Setting/EGT Limits
APPLICABLE TO N901NK THRU N915NK

A

Takeoff and Go-around
All engines operative 5 min
One engine inoperative 10 min
1083C

MCT 1043C

Starting, On ground
In flight
1083C

38
Q

OIL
APPLICABLE TO N502NK THRU N696NK

Minimum starting temp:

Minimum temperature before IDLE is exceeded

A
  • 40

- 10

39
Q

OIL
APPLICABLE TO N901NK THRU N915NK

Minimum Oil Pressure

A

65 PSI

40
Q

STARTER

APPLICABLE TO N502NK THRU N696NK

A
  • A standard automatic start that includes only one start attempt, is considered one cycle
  • For ground starts (automatic or manual), a 15s pause is required between successive cycles
  • A 30 min cooling period is required, subsequent to three failed cycles or 5 min of continuous crank
  • For manual start, observe a two-minute max cycle time
  • For crank, observe a 5 min max cycle time
  • The starter must not be run when N2 is above 10% on-ground and 18% in-flight.
41
Q

STARTER

APPLICABLE TO N901NK THRU N915NK

A
  • A standard automatic start that includes up to three start attempts, is considered one cycle
  • For ground starts (automatic or manual), a 35s pause is required between successive cycles.
  • A 15 min cooling period is required, subsequent to three failed cycles, or 15 min of continuous or cumulated crank.
  • The starter must not be run when N2 is above 20%
42
Q

Reverse Thrust

APPLICABLE TO N901NK THRU N915NK

A

Maximum reverse should not be used below 70kt. Idle reverse is permitted down to aircraft stop.

43
Q

Reduced Thrust Takeoff

Applicable to all A/C

A

FLEX takeoff is not permitted on contaminated runways

44
Q

Crosswind operation On Ground

Engine Start

A

The engine is able to start in crosswind up to 35 kt.

45
Q

Flight Controls
Maximum altitude Flaps/Slats Extended
Maximum operating altitude with slats and/or flaps extended

A

20,000 ft

46
Q

Fuel Temperature

A

For Jet A only, if TAT reaches -34 C, monitor on FUEL SD page that fuel temperature remains higher than -36C.

47
Q

Maximum Allowed Wing Fuel Imbalance
APPLICABLE TO N618NK THRU N656NK, N690NK THRU N696NK, N901NK THRU N915NK (320 SHARKLET)

Fuel Imbalance at takeoff, maximum asymmetry

Fuel imbalance In Flight and At Landing, maximum asymmetry

A

1102 lb

3306 Ib

48
Q

Maximum Allowed Wing Fuel Imbalance
APPLICABLE TO N657NK THRU N687NK (A321 SHARKLET)

Fuel Imbalance at takeoff, maximum asymmetry

A

882 Ib

49
Q

BRAKE TEMPERATURE

Maximum brake temperature for takeoff

A

300C

airbus (1 decks)

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