Limitations Flashcards

1
Q

N502NK THRU N536NK

A

A319

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2
Q

N601NK THRU N617NK, N697NK, N698NK– Non Sharklet
* N618NK THRU N656NK, N690NK THRU N696NK – Sharklet
* N629NK THRU N656NK, N690NK THRU N696NK – “Jet Pump”
Fuel System
* N901NK THRU N990NK – NEO

A

A320

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3
Q

N657NK THRU N687NK – Sharklet
N702NK THRU N715NK - NEO

A

A321

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4
Q

Wingspan- A320Sharklet/NEO A321 Sharklet/NEO

A

117’ 5”

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5
Q

Tail strike pitch attitude

A319

A

13.9 degrees

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6
Q

Tail strike pitch attitude

A320/320NEO

A

11.7 Degrees

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7
Q

Tail strike pitch attitude

A321/NEO

A

9.7 degree’s

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8
Q

Maximum Certified Altitude

A

FL398

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9
Q

Maximum crosswind (takeoff and landing)

A

38 kt (gust included)

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10
Q

Maximum tailwind for takeoff

A

15 kt

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11
Q

Maximum tailwind for landing

A

10 kt

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12
Q

Wipers Maximum Operating Speed

A

230 kt

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13
Q

When the takeoff weight is higher than _________ Do not exceed a taxi speed of _________

A

167,550 lb

20 kt

N601NK THRU N656NK, N690NK
THRU N698NK

(A320)

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14
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 Start Unit at the same time, to prevent any adverse effect
on the Bleed Air System.

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15
Q

Minimum Use Height For Autopilot

At takeoff

A

100 ft AGL and at least 5 s after
takeoff

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16
Q

Minimum Use Height For Autopilot

In approach with F-G/S, FINAL APP,
V/S, or FPA mode

A

250 ft AGL

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17
Q

Minimum Use Height For Autopilot

In Circling Approach

A

600 ft AGL

18
Q

Minimum Use Height For Autopilot

ILS approach when CAT 1 is
displayed on the FMA

A

160 ft AGL

19
Q

Minimum Use Height For Autopilot

ILS approach when CAT 2 or CAT 3
(single or dual) is displayed on the
FMA

A

0 ft AGL if autoland

20
Q

Minimum Use Height For Autopilot

After a manual go-around

A

100 ft AGL

21
Q

Minimum Use Height For Autopilot

In all other phases

A

500 ft AGL (A319/A320)
900 ft AGL (A321)

22
Q

Minimum Use Height For Autopilot

The AP or FD in OP DES or DES
mode can be used in approach.
However, its use is only permitted if
the FCU selected altitude is set to,
or above, the higher of the two:

A

Highest of:
MDA/MDH or 500 ft AGL (A319/
A320)
MDA/MDH or 900 ft AGL (A321)

23
Q

After three consecutive APU start attempts, the Flight Crew must wait

A

60 min before a new start attempt.

24
Q

A319/A320
N502NK THRU N656NK, N690NK
THRU N698NK

Takeoff go around
Time/EGT Limit

A

All engines operative
5 min
One engine inoperative
10 min

635 °C MAX EGT

25
Q

A321
N657NK THRU N687NK

Takeoff go around
Time/EGT Limit

A

All engines operative
5 min
One engine inoperative
10 min

650 °C MAX EGT

26
Q

A320NEO/A321NEO

Takeoff go around
Time/EGT Limit

A

All engines operative
5 min
One engine inoperative
10 min

1083 °C MAX EGT

27
Q

A319/A320
N502NK THRU N656NK, N690NK
THRU N698NK

MCT
Time/EGT Limit

A

Not limited

610 °C

28
Q

A321
N657NK THRU N687NK

MCT
Time/EGT Limit

A

Not limited
610 °C

29
Q

A320NEO/A32NEO

MCT
Time/EGT Limit

A

Not limited

1,043 °C

30
Q

Starting EGT Limits

A

A319/A320/A321 - 635 EGT

A320/A321 NEO - 1083 EGT

31
Q

A319/A320/A321

Minimum starting temperature
Minimum temperature before IDLE is exceeded

A

-40 C
-10 C

32
Q

Thrust reverser limits

A

Maximum reverse should not be used below 70 kt.

Idle reverse is permitted down to aircraft stop.

33
Q

FLEX takeoff limits

A

FLEX takeoff is not permitted on contaminated runways.

34
Q

ENGINE START crosswind limit

A

up to 35 kt.

35
Q

Maximum operating altitude with slats and/or flaps extended

A

20,000 ft

36
Q

JET A Temp limits

A

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

37
Q

A319/A320/A320NEO

Max Fuel Imbalance at Takeoff inner tanks

A

1,102 lb

38
Q

A321/A321NEO

Max Fuel Imbalance at Takeoff wing tanks

A

882 lb

39
Q

Maximum brake temperature for takeoff (brake fans (if installed) off)

A

300 °C

40
Q

LP air and Packs

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.

41
Q

Minimum AP alt.
LPV approach (with SLS ) when APPR1 is displayed on the
FMA

A

160 ft AGL