Limitations Flashcards

(73 cards)

1
Q

Load Acceleration Limits

A
  • Clean Configuration: -1.0g to +2.5g
  • Other Configuration: 0g to +2.0g
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2
Q

A319/A320 Wingspan

A

111 ft
10 in.

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3
Q

A320 Sharklet,
A321 Sharklet Wingspan

A

117 ft.
5 in.

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4
Q

A319 Tailstrike Pitch Attitude

A

L/G Struts Compressed:
13.9 degrees

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5
Q

A320/A320 NEO Tailstrike Pitch Attitude

A

L/G Struts Compressed:
11.7 degrees

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6
Q

A321 Tailstrike Pitch Attitude

A

L/G Struts Compressed:
9.7 degrees

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7
Q

Maximum Certified Altitude

A

FL398

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8
Q

Runway Slope

A

+/- 2%

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9
Q

Max Runway Altitude

A

9,200 ft

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10
Q

Nominal Runway Width

A

45 m (148 ft)

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11
Q

Max Crosswind (takeoff and landing)

A

38 knots (gust included)

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12
Q

Max Tailwind - Takeoff

A

15 knots

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13
Q

Max Tailwind - Landing

A

10 knots

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14
Q

Max Wind for PAX Door Operation

A

65 knots

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15
Q

Cockpit Window Open Maximum Speed

A

200 knots

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16
Q

Maximum Operating Speed
Vmo Mmo

A

350 knots/M.82

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17
Q

Max speed with landing gear extended
(VLE)

A

280 knots/M.67

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18
Q

Max landing gear extension speed
(VLO Extension)

A

250 knots/M.60

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19
Q

Max landing gear retraction speed
(VLO Retraction)

A

220 knots/M.54

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20
Q

Max Taxi Speed (A320)

A

Takeoff weight higher than 167,550 lbs:
20 knots in a turn

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21
Q

Wipers Maximum Operating Speed

A

230 knots

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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.

Why? B/c causes overpressure issues (two sources)

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23
Q

Cabin Pressure:
Max Positive Differential Pressure

A

9 PSI

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24
Q

Cabin Pressure:
Max Negative Differential Pressure

A

-1.0 PSI

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25
Packs Use With LP Air Conditioning Unit
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. Why? B/c causes overpressure issues (two sources)
26
Min Height for AP - At Takeoff
100 ft AGL and at least 5 seconds after takeoff
27
Min Height for AP - In approach with F-G/S, FINAL APP, V/S, or FPA mode
250 ft AGL
28
Min Height for AP - In Circling Approach
600 ft AGL
29
Min Height for AP - ILS approach when CAT 1 is displayed on the FMA
160 ft AGL
30
Min Height for AP - ILS approach when CAT 2 or 3 displayed on the FMA
0 ft AGL if Autoland
31
Min Height for AP - After a Manual Go-Around
100 ft AGL
32
Min Height for AP - In All Other Phases
500 ft AGL (A319/A320) 900 ft AGL (A321)
33
The use of AP or FD in OPEN DES or DES mode is only permitted in approach, when the FCU altitude is set at or above, the higher of the two:
Highest of: MDA/MDH or 500 ft (A319/A320) MDA/MDH or 900 ft (A321) Why? b/c in OPEN DES, you'll be at THR IDLE, speed is controlled by pitch, thrust won't be able to spooled up
34
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 cross-checked with navaid raw data.
35
A319/A321: If one engine is inoperative, it is not permitted to use the autopilot to perform NPAs (non-precision approaches) in the following modes:
* FINAL APP * NAV V/S * NAV/FPA * *Only FD use is permitted.
36
APU Start
After **three consecutive APU start attempts**, the Flight Crew must wait **60 min** before a new start attempt.
37
Thrust Setting/EGT Limits: A319/320 CEO EGT Limit for T/O & Go-Around
****635 C (Time Limit: All engines op - 5 mins One engine inop - 10 mins)
38
Thrust Setting/EGT Limits: A321 CEO EGT Limit for T/O & Go-Around
****650 C (Time Limit: All engines op - 5 mins One engine inop - 10 mins)
39
Thrust Setting/EGT Limits: A320/A321 NEO EGT Limit for T/O & Go-Around
****1,083 C (Time Limit: All engines op - 5 mins One engine inop - 10 mins)
40
Thrust Setting/EGT Limits: A319/320 CEO Max. Continuous Thrust (MCT)
610 C
41
Thrust Setting/EGT Limits: A321 CEO Max. Continuous Thrust (MCT)
610 C
42
Thrust Setting/EGT Limits: A320/A321 NEO Max. Continuous Thrust (MCT)
1,043 C
43
Thrust Setting/EGT Limits: A319/320 CEO Starting
635 C
44
Thrust Setting/EGT Limits: A321 CEO Starting
635 C
45
Thrust Setting/EGT Limits: A320/A321 NEO Starting
1,083 C
46
Minimum Oil Temperature for Starting (All CEO/NEO)
-40 C
47
Minimum Oil Temperature Before IDLE is exceeded (CEO)
-10 C
48
Minimum Oil Temperature Before Takeoff (CEO)
50 C
49
Minimum Oil Temperature Before Takeoff (NEO)
52 C
50
Minimum Oil Pressure (CEO)
60 PSI
51
Minimum Oil Pressure (NEO)
65 PSI
52
Engine Starter (CEO)
* - 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 two-minute maximum cycle time * - For crank, observe 5 min maximum cycle time * - The starter must not be run when N2 is above 10% on-ground and 18% in-flight
53
Engine Starter (NEO)
* - 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 cumulative crank * - The starter must not be run when N2 is above 20%
54
Max Reverse Thrust should not be used below:
70 knots (Idle reverse is permitted down to aircraft stop.) Other: max reverse is most effective at high speeds
55
FLEX takeoff is not permitted:
On contaminated runways.
56
Max Crosswind for Engine Start
35 knots
57
Max Altitude for Flaps and/or Slats
20,000 ft
58
For JET A only, if TAT reaches ____, monitor on FUEL SD page that fuel temperature remains higher than _____.
-34 C/ -36 C
59
Max Fuel Imbalance - Takeoff (A319/A320-all)
Inner tanks: (Heavier tank full) 1,102 lbs
60
Max Fuel Imbalance - In Flight and at Landing (A319/A320-all)
Inner tanks: (Heavier tank full) 3,306 lbs
61
Max Fuel Imbalance - Takeoff (A321-S)
Wing tanks: (Heavier tank full) 882 lbs
62
Max Brake Temp for Takeoff (brake fans off)
300 C Other: - Cannot take off w/ brake fans on - If over 300, get down to 150 with fans and then fans come off
63
Max Altitude for APU Start on Battery Power
25,000 ft
64
Max Altitude for APU Start (on A/C power) and Operation
FL410
65
A319 Max Landing Weight
137,788 lbs
66
A320 (CEO) Max Landing Weight
145,505 lbs
67
A320-S Max Landing Weight
145,505 lbs
68
A320 (NEO) Max Landing Weight
148,591 lbs
69
A321-S Max Landing Weight
171,519 lbs
70
A321 (NEO) Max Landing Weight
174,606 lbs
71
Max Tire Speed
Ground Speed 195 Kts
72
Min. Oil Quantity (CEO)
11 qts + 0.3 for every hr of flight
73
Min. Oil Quantity (NEO)
14 qts