LIMITATIONS BOLD 2-27-19 (date indicates when updated) If you find an error or need an update on any card in this class text 563-564-9569 Flashcards
A319 A320 WINGSPAN
111’ 10”
A320 SHARKLET A321 SHARKLET WINGSPAN
117’ 5”
TAILSTRIKE ATTITUDE 319
13.9
TAILSTRIKE ATTITUDE 320 and A320 NEO
11.7
TAILSTRIKE ATTITUDE 321
9.7
MAX certified altitude
FL 398
Runway Slope
+/- 2%
Runway Altitude
9,200ft
Nominal Runway Width
148 ft (45m)
Max Crosswind Takeoff and Landing
38 kt (gust included)
Max tailwind takeoff
15 kt
Max tailwind landing
10 kt
Max wind for passenger door operation
65 kt
Max Landing Gear Extended V Le
280 kt /.67M
Max Landing Gear Extension (V Lo Extension)
250 kt /.60M
Max Landing Gear Retraction (V Lo Retraction)
220 kt /.54M
Max altitude landing gear may be extended
25,000 ft
MAX Weight and Speed Limit in taxi turn
When Higher than 167550 lb Max speed in turn 20 kt
Windshield Wiper Use Max Speed
230 kt
A319 MAX LANDING
137,788
A320 MAX LANDING
145,505
A320 NEO MAX LANDING
148,591
A321 MAX LANDING
171,519
APU with HP Ground Unit
Do not use HP ground unit when APU supplies bleed air to avoid system damageto prevent any adverse effect on the Air Conditioning system.
MAX Positive differential cabin Pressure
9.0 PSI
MAX Negative differential cabin Pressure
-1.0 PSI
Air Conditioning with LP Ground Unit
Do not use conditioned air simultaneously from PACKS and LP ground unitto prevent anyadverse effect on the Air Conditioning system.
Minimum Height for use of Autopilot Takeoff with SRS mode
100 ft AGLTAKEOFF WITH SRS MODE-AN INTERNAL FMGS LOGIC PREVENTS THE AUTOPILOT FROM ENGAGING DURING THE 5 SECONDS AFTER LIFTOFF
Minimum Height for use of AutopilotStraight-in Non-Precision approach
Applicable Minimum
Minimum Height for use of AutopilotCircling Approach
Applicable Circling Minimum -100ft
Minimum Height for use of Autopilot ILS Approach when CAT 2 or CAT 3 is not displayed on FMA
160 FT AGL(80 ft if displayed)
Minimum Height for use of AutopilotGo- Around (AP or FD engagement)
100ft AGL
Minimum Height for use of Autopilot All other Phases
500 ft AGL (A319/A320)900 ft AGL (A321)
Minimum Height for use of Autopilot AP OR FD in OPEN DES or DES mode
not permitted in approach, unless FCU altitude is set at or above highest of:Minimums or 500 ft (A319/320)Minimums or 900 ft (A321)
NAV mode may be used in terminal area provided:
- GPS PRIMARY is available, or
- The appropriate RNP is checked or entered on the MCDU, andHIGH accuracy is displayed, or
- FMS navigation is crosschecked with navaid raw data.
Non-Precision Approaches With Engine Out A319 and A321 only
If one engine is inoperative it IS NOT PERMITTED to use the autopilot to perform NPAs in the following modes: * FINAL APP * NAV V/S * NAV/FPA ONLY FD use is permitted
APU starter motor duty cycles
After 3 cycles wait 60 minutes before attempting 3 more cycles
APU ALTITUDE LIMITS
APU BLEEDMax altitude to assist engine start . . . . .. . . . . . . . . 20,000 ftMax altitude for air conditioning and pressurization(single pack operation) . . . . . . . . . . . . . . . . . . . . . . 20,000 ftMax altitude for air conditioning and pressurization(dual pack operation) . . . . . . . . . . . . . . . . . . . . . . . . . 15,000 ftUse of APU bleed air for wing anti-ice is not permitted.Max Alt for electric …………………………………………. 25000ft
THRUST/EGT LIMITSA319, A320 (not NEO), A321Starting
635 C
THRUST/EGT LIMITSA320 NEOSTARTING
1018 C EGT
THRUST/EGT LIMITSA319, A320 (not NEO), A321MCT
Unlimited time 610
THRUST/EGT LIMITSA320 NEOMCT
unlimited time1043 C EGT
THRUST/EGT LIMITSA319 A320 (not NEO)Takeoff and Go Around
5 minutes 2 engines10 minutes 1 engine 635 C EGT
THRUST/EGT LIMITSA321Takeoff and Go Around
5 minutes 2 engines10 minutes 1 engine650 C EGT
THRUST/EGT LIMITSA320 NEOTakeoff and Go Around
5 minutes 2 engines10 minutes 1 engine1083 C EGT
OIL Temp minimum starting temp
-40 C
OIL Temp minimum prior to exceeding idle
-10 C(min temp for oil for takeoff is +50 C ecam will alert if below)
OIL A320 NEO Minimum Oil Pressure
65 PSI
Min OIL QUANTITY
11 qts. + Est. Consumption (~0.3 qt/hr)(not in limitations but need to know)
STARTER A319,A320.A321 (not NEO)
STARTER A319,A320.A321 (not NEO)-a standard automatic start that includes only one start attempt is considered one cycle-For ground starts (automatic or manual) a 15 sec pause is required between successive cycles -A 30 min cooling period is required, subsequent to the three failed cycles or 5 min of continuous crank-For Manual start, observe a 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
STARTER A320 NEO
STARTER A320 NEO-3 consecutive start attempts is one cycle -For ground starts (auto or manual)35 s between each cycle -After 3 cycles, or after 15 min of continuous or cumulative cranking: A 15 min cooling period is necessary before a new start motoring cycle is attempted.-No starter, engagement when N2 is above 20 %.
REVERSE THRUST
Maximum reverse should not be used below 70 kt (Idle reverse is permitted down to aircraft stop)
REDUCED THRUST (FLEX)
Takeoff at reduced thrust is not permitted on contaminated runways or into known windshear
MAX CROSSWIND DURING START
35 Kts
FLAPS and SLATS MAX operating altitude with slats and/or flaps extended
20,000 ft
For JET A only, if TAT reaches:
-34 °C, monitor on FUEL SD page that fuel temperature remains higher than -36 °C.
A320 Sharklet And A320 NEO MAX allowed wing fuel imbalance at TAKEOFF
Outer tank balanced Tank fuel quantity heavier tank FULL- MAX inner tank imbalance= 1102 lb
A320 Sharklet And A320 NEO MAX allowed wing fuel imbalance at landing
Outer tank balanced Tank fuel quantity heavier tank FULL- MAX inner tank imbalance=3306lbs
A321 Sharklet MAX allowed wing tank fuel imbalance at TAKEOFF
Tank fuel quantity heavier tank FULL- MAX imbalance= 882 lb
MAX brake temperature for takeoff (brake fans off)
300 C
