Limitations Flashcards

1
Q

Wingspan

A319, A320

A

111 feet, 10 inches

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2
Q

Wingspan

A320 Sharklet, A321 Sharklet

A

117 feet, 5 inches

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3
Q

Aircraft Geometry
Tailstrike Pitch Attitude
(L/G Struts Compressed)

A

A-319……13.9
A-320……11.7
A-321…….9.7

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4
Q

Max Certified Altitude

A

FL398

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5
Q

Runway Slope

All A/C

A

+/-2%

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6
Q

Runway Altitude

All A/C

A

9,200 ft

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7
Q

Nominal Runway Width

All A/C

A

45 m (148ft)

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8
Q

Max Demonstrated X-wind (take-off and landing)

All A/C

A

38 kt (gust included)

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9
Q

Max tailwind for takeoff

All A/C

A

15 kt

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10
Q

Max tailwind for Landing

All A/C

A

10 kt

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11
Q

Max wind for passenger door operation

All A/C

A

65 kt

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12
Q

Max with 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/.54M

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15
Q

Max altitude landing gear may be extended

A

25,000 ft

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16
Q

When taxi weight is higher than _________ lb, do not exceed a taxi speed of _____ durning a turn.

A

167,550 lb, 20 kt

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17
Q

Windshield wipers in use max speed

A

230 kt

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18
Q

Max Landing Weight A319

A

137,788 lb

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19
Q

Max Landing Weight A320

A

145,505 lb

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20
Q

Max Landing Weight A320 NEO

A

148,591 lb

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21
Q

Max Landing Weight A321

A

171,519 lb

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

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23
Q

Cabin Pressure

Max positive differential pressure

A

9.0 PSI

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24
Q

Cabin Pressure

Max negative differential pressure

25
Packs Use With LP Air Conditioning Unit
The Flight Crew must not use conditioned air from the packs and from the LP Conditioning Unit at the same time, to prevent any adverse effects on the Air Conditioning system.
26
Min height for autopilot At takeoff
100ft AGL and at least 5 s after takeoff
27
Autopilot limit when in APPH with F-G/S, FINAL APP, V/S, or FPA mode
250 ft AGL
28
Min height for autopilot | Circling Approach
600 ft AGL
29
Min height for autopilot ILS approach when CAT 1 is displayed on the FMA
160 ft. AGL
30
Min height for autopilot ILS approach when CAT 2 or CAT 3 (single or dual) is displayed on the FMA
0 ft AGL if autoland
31
Min height for autopilot | All other phases
500 ft AGL (A319/A320) | 900 ft AGL (A321)
32
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:
Highest of MDA/MDH or 500 ft (A319/A320) MDA/MDH or 900 ft (A321)
33
NAV mode may be used in the terminal area, provided:
-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.
34
APU starter limits
After three consecutive APU start attempts, the Flight Crew must wait 60 min before a new start attempt.
35
Thrust setting/EGT Limits Takeoff and go-around (N502NK-N654NK)
635C 5 min both engines | 635C 10 min one engine inop
36
Thrust setting/EGT Limits MCT (N502NK-N654NK)
610C not limited
37
Thrust setting/EGT Limits Starting (N502NK-N654NK)
635C
38
Thrust setting/EGT Limits Takeoff and go-around (N657NK-N687NK)
650C 5 min both engines | 650C 10 min one engine inop
39
Thrust setting/EGT Limits MCT (N657NK-N687NK)
610C not limited
40
Thrust setting/EGT Limits Starting (N657NK-N687NK)
635C
41
Thrust setting/EGT Limits Takeoff and go-around (A320NEO/A321NEO)
1,083C 5 min both engines | 1,083C 10 min one engine inop
42
Thrust setting/EGT Limits MCT (A320NEO/A321NEO)
1,043C not limited
43
Thrust setting/EGT Limits Starting (A320NEO/A321NEO)
1,083C
44
Minimum starting oil temperature | N502NK-N687NK
-40C
46
Minimum oil temperature before IDLE is exceeded | N502NK-N687NK
-10C
47
Min oil pressure | N901NK-N990NK
65 PSI
48
Starter limits | N502NK-N687NK
- A standard automatic start that includes only one start attempt, is considered one cycle - For ground starts (automatic or manual), a 15 s 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 2 min maximum cycle time - For crank, observe a 5 min maximum cycle time - The starter must not be run when N2 is above 10% on-ground and 18% in-flight.
49
Start limits A320NEO/A321NEO
- A standard automatic start that includes up to two start attempts, is considered one cycle - For ground starts (automatic or manual), a 35 s 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%.
49
Reverse thrust limits
Maximum reverse should not be used below 70 kt. | Idle reverse is permitted to aircraft stop
50
Reduced thrust | All A/C
Takeoff at reduced thrust is not permitted on contaminated runways, when wind shear advisories or alerts are in effect, OAT is within 10 degrees of FLEX temp, or MEL
51
Engine starting crosswind limit | All-Aircraft
Up to 35 kt
52
For Jet-A only, if TAT reaches -34C
Monitor on FUEL SD page that fuel temperature remains higher than -36C
53
Max altitude for flaps and slats
20,000
54
Max allowed fuel imbalance at takeoff Inner tanks full (outer tanks balanced) (N618NK-N654NK, N901NK-N990NK)
1,102 lb
55
Max allowed fuel imbalance in flight and at landing Inner tanks (Outer tanks balanced) (N601NK-N654NK, N901NK-N990NK)
3,306 lb
55
Max allowed fuel imbalance at takeoff | N657NK-N687NK
882 lb
56
Max brake temp for takeoff | Brake fans (if installed) off
300F
57
Max Landing Weight A321NEO
174,606
58
Min height for autopilot After a manual go-around
100 ft AGL