Limitations Flashcards
Wing Span:
- A319, A320
- A320 Sharklet, A321 Sharklet
- 111 Ft 10 In.
- 117 Ft 5 In.
L/G Compressed Ground Clearence
- A319
- A320
- A320 NEO
- A321
- 13.9
- 11.7
- 11.7
- 9.7
Maximum Certified Altitude
FL 398
Runway Slope (mean)
+/- 2%
Runway Altitude
9200 Ft
Nominal Runway Width
45 m (148 Ft)
Maximum Crosswind (Takeoff & Landing)
38 KT’s (Gusts Included)
Maximum Tailwind for Takeoff
15 kts
Maximum Tailwind for Landing
10 Kts
Maximum wind for passenger door operation
65 kts
Cockpit Window open Maximum Speed
200 Kts
Maximum Landing Gear Extended (VLE)
280 Kt/ M. 67
Maximum Landing Gear Extension (VLO)
250 Kt/ M. 60
Maximum Landing Gear Retractions
220 Kt/ M .54
Maximum Wiper Speed
230 Kt
Max Landing Weight A-319 (N502NK - N526NK)
137,788 LBS
Max Landing Weight A-320 (N601NK - N617NK, N697NK, N698NK) Non Sharklet
145,505 LBS
Max Landing Weight A-320 (N618NK - N656NK, N690NK - N696NK) Sharklet
145,505 LBS
Max Landing Weight A-320 NEO (N901NK - N990NK)
148,591 LBS
Max Landing Weight A-321 (N657NK - N687NK) Sharklet
171,519 LBS
Max Landing Weight A-321 NEO (N702NK - N715NK)
174,606 LBS
APU Bleed Use With Air Start
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
Cabin Pressure
Max positive differential pressure
Max negative differential pressure
9.0 PSI
-1.0 PSI
Packs Use With LP Air Conditioning Unit
The Flight Crew must not use conditioned air from the packs and the LP Air Conditioning Unit at the same time, to prevent any adverse effect on the Air Conditioning System.
Minimum Use For Auto Pilot
1. At Takeoff
2. In Approach with F-G/S, FINAL APP, V/S, or FPA mode
3. In Circling Approach
4. ILS Approach when CAT 1 is Displayed on the FMA
5. ILS Approach when CAT 2 or CAT3 (single or dual) is displayed on the FMA
6. After a manual go-around
7. In all other phases
8. 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.
- 100 Ft AGL or at least 5 s after takeoff
- 250 Ft AGL
- 600 Ft AGL
- 160 Ft AGL
- 0 Ft if Autoland
- 100 Ft AGL
- 500 Ft AGL (A319/320)
900 Ft AGL (A321) - Highest Of: MDA/MDh or 500 FT AGL (A319)/ 900 Ft (A321)
Use of NAV Mode in the Terminal Area
- GPS Primary 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
Non Precision Approach with Autopilot (A319 & A321)
If one engine is inoperative, it IS NOT PERMITTED to use the autopilot to perform Non Precision Approaches in the following modes: FINAL APP, NAV V/S, NAV/ FPA.
Only FD use is permitted.
APU Start
After 3 consecutive APU start attempts, the Flight Crew must wait 60 Minutes before a new start attempts
Thrust Settings/ EGT Limits - A319/ A320
1. Takeoff/ Go Around
2. MCT
3. Starting
- 635 C
- 610 C
- 635 C
Thrust Setting/ EGT Limits - A321
1. Take off and Go Around
2. MCT
3. Starting
- 650 C
- 610 C
- 635 C
Thrust Setting/ EGT Limits - A320/ 321 NEO
1. Takeoff and Go Around
2. MCT
3. Starting
- 1083 C
- 1043 C
- 1083 C
Minimum Starting Temperature
(-) 40 C
Minimum temperature before exceeding Idle
(-) 10 C
Minimum Oil Pressure
65 PSI
Starter Limits CEO
- 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 3 failed cycles or 5 min of continuous cranks
- For manual start, observe a two-minute maximum cycle time
- For crank, observe a 5 minute maximum cycle time
- The starter must not be run when N2 is above 10% on ground and 18% in flight
Starter Limits NEO
- A standard automatic start the includes up to two start attempts, is considered one cycle.
- For ground starts (auto or man), a 35s pause is required between successive cycles.
- A 15 min cooling period is required, subsequent to 3 failed cycles, or 15 min of continuous or cumulated crank .
- The start must not be run when N2 is above 20%
Maximum Reverse
Should not be used below 70 kts. Idle reverse is permitted down to aircraft stop
Flex take off
Not permitted on contaminated runways
Max crosswind for engine starts
35 kts
Max altitude for Flaps/ Slats extended
20,000 Ft.
Max Allowed Fuel Imbalance at Takeoff (A319/ A320 CEO&NEO)
Inner Tanks (w/ Outer Tanks Balanced)
1102 LBS
Max Allowed Fuel Imbalance at Landing (A319/ A320 CEO&NEO)
Inner Tanks (w/ Outer Tanks Balanced)
3,306 LBS
Max Allowed Fuel Imbalance at Takeoff (A321 CEO&NEO)
Wing Tanks
882 Lbs
Maximum Brake Temperature for takeoff (brake fans off)
300 C
