A320 Limitations Flashcards Preview

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Flashcards in A320 Limitations Deck (59)
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1
Q

319, 320, 321 Wingspan

A

111 ft. 10 in.

2
Q

320 Sharklet, 321 Sharklet Wingspan

A

117 ft. 5 in.

3
Q

319 Tailstrike Pitch Attitude

A

13.9 Compressed

4
Q

A320 (IAE and NEO) Tailstrike Pitch Attitude

A

11.7 Compressed

5
Q

A321 Tailstrike Pitch Attitude

A

9.7 Compressed

6
Q

Max certified altitude

A

FL398

7
Q

Runway slope

A

+- 2%

8
Q

Max runway altitude

A

9,200 ft

9
Q

Nominal runway width

A

148 ft (45 meters)

10
Q

Max crosswind (takeoff AND landing)

A

38 kts (gust included)

11
Q

Max tailwind for takeoff

A

15 kts

12
Q

Max tailwind for landing

A

10 kts

13
Q

Max wind for pax door operation

A

65 kts

14
Q

Max with landing gear extended (Vle)

A

280 kt/M.67

15
Q

Max landing gear extension (Vlo Extension)

A

250 kt/M.60

16
Q

Max landing gear retraction (Vlo Retraction)

A

220 kt/M.54

17
Q

Max speed for windshield wiper use

A

230 kts

18
Q

ONLY the A320/A321; when taxi weight is higher than___________, do not exceed a taxi speed of ____ kts during a turn.

A

167,550 lbs, 20 kts

19
Q

A319 Max Landing Weight

A

137,788 lbs

20
Q

A320 (IAE) Max Landing Weight

A

145,505 lbs

21
Q

A320 (NEO) Max Landing Weight

A

148,591 lbs

22
Q

A321 (IAE) Max Landing Weight

A

171,519 lbs

23
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.

24
Q

Max positive pressure differential

A

9.0 psi

25
Q

Max negative differential pressure

A

-1.0 psi

26
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.

27
Q

Min use height for AP at Takeoff

A

100 ft AGL and at least 5 s after T/O

28
Q

Min use height for AP in approach with F-G/S, FINAL APP, V/S, or FPA mode

A

250 AGL

29
Q

Min use height for AP in circling approach

A

600 ft AGL

30
Q

Min use height for AP use on ILS approach when CAT 2 or CAT 3 (single or dual) is displayed on the FMA

A

0 ft AGL if Autoland

31
Q

Min use height for AP after a manual Go-Around

A

100 ft AGL

32
Q

Min use height for AP in all other phases

A

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

33
Q

Min use height for AP or FD in OPEN DES or DES mode is 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)

34
Q

NAV mode may be used in terminal area if

A
  1. GPS primary is available, or
  2. HIGH accuracy is displayed, and the appropriate RNP is checked or entered on the MCDU, or
  3. FMS navigation is cross-checked with navaid raw data.
35
Q

If one engine is inop on 319/321, you cannot use AP to perform NPAs in the following modes.

A

FINAL APP, NAV V/S, NAV/FPA.

Only FD use is permitted.

36
Q

APU Start Limits

A

3 consecutive start attempts, then 60 min cool down.

37
Q

EGT limit for Takeoff or GA (319 and 320 Classic)

A

635 C for 5 min, 10 min if engine failure

38
Q

EGT limit for MCT (319, 320 Classic, 321)

A

610 C, Unlimited time

39
Q

EGT limit for start, ground or flight (319, 320 Classic, 321)

A

635 C

40
Q

EGT limit for Takeoff or GA (A321)

A

650 C for 5 min, 10 min if engine failure

41
Q

EGT limit for TO or GA (320/321 NEO)

A

1083 C for 5 min, 10 min if engine failure

42
Q

EGT limit for start, ground or flight (320/321 NEO)

A

1083 C

43
Q

EGT limit for MCT (320/321 NEO)

A

1043 C, Unlimited time

44
Q

Minimum oil temp for engine start (IAE)

A

-40 C

45
Q

Minimum oil temp prior to exceeding idle (IAE)

A

-10 C

46
Q

Minimum oil pressure (320/321 NEO)

A

65 PSI

47
Q

Starter Limitations (IAE)

A
  • 1 auto start attempt = 1 cycle
  • Ground starts (auto or man) 15 seconds between cycles
  • 3 failed cycles or 5 min of continuous cranking: 30 minutes cooling period
  • For manual start, observe a 2 min max cycle time
  • For crank, observe a 5 min max cycle time
  • Starter must not run when N2 above 10% on ground, or 18% in flight
48
Q

Starter Limitations (NEO)

A
  • 2 auto start attempts = 1 cycle
  • Ground starts (auto or manual ) 35 seconds between each cycle
  • 3 failed cycles or 15 minutes of continuous or cumulative cranking; 15 minute cooling period
  • Starter must not run when N2 is above 20%
49
Q
  • Max reverse thrust should not be used below…
  • Idle reverse permitted down to…
A
  • 70 kts
  • Aircraft stop
50
Q

Flex TO is not permitted on (IAE and NEO)

A

Contaminated runways

51
Q

Engine Start Crosswind Limit

A

35 kts

52
Q

Max Altitude with slats/flaps extended

A

20,000 ft.

53
Q

Jet A only, if TAT reaches ____, monitor on Fuel SD page that fuel temperature remains higher than _____.

A

-34C, -36C

54
Q

Max INNER tank fuel imbalance at TAKEOFF (319, 320)

A

If heavier tank FULL, then 1102 lbs.

55
Q

Max INNER tank fuel imbalance IN-FLIGHT and LANDING (319, 320)

A

If heavier tank FULL, then 3306 lbs.

56
Q

Max WING tank fuel imbalance at TAKEOFF (321 Sharklet)

A

If heavier tank FULL, then 882 lbs.

57
Q

Max brake temp for takeoff (brake fans off)

A

300 C

58
Q

Min use height for A/P on ILS approach when CAT 1 displayed on the FMA

A

160 ft AGL

59
Q

A321 (NEO) Max Landing Weight

A

174,606 lbs