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
1
Q
A319 A320 WINGSPAN
A
111’ 10”
2
Q
A320 SHARKLET A321 SHARKLET WINGSPAN
A
117’ 5”
3
Q
TAILSTRIKE ATTITUDE 319
A
13.9
4
Q
TAILSTRIKE ATTITUDE 320 and A320 NEO
A
11.7
5
Q
TAILSTRIKE ATTITUDE 321
A
9.7
6
Q
MAX certified altitude
A
FL 398
7
Q
Runway Slope
A
+/- 2%
8
Q
Runway Altitude
A
9,200ft
9
Q
Nominal Runway Width
A
148 ft (45m)
10
Q
Max Crosswind Takeoff and Landing
A
38 kt (gust included)
11
Q
Max tailwind takeoff
A
15 kt
12
Q
Max tailwind landing
A
10 kt
13
Q
Max wind for passenger door operation
A
65 kt
14
Q
Max Landing Gear Extended V Le
A
280 kt /.67M
15
Q
Max Landing Gear Extension (V Lo Extension)
A
250 kt /.60M
16
Q
Max Landing Gear Retraction (V Lo Retraction)
A
220 kt /.54M
17
Q
Max altitude landing gear may be extended
A
25,000 ft
18
Q
MAX Weight and Speed Limit in taxi turn
A
When Higher than 167550 lb Max speed in turn 20 kt
19
Q
Windshield Wiper Use Max Speed
A
230 kt
20
Q
A319 MAX LANDING
A
137,788
21
Q
A320 MAX LANDING
A
145,505
22
Q
A320 NEO MAX LANDING
A
148,591
23
Q
A321 MAX LANDING
A
171,519
24
Q
APU with HP Ground Unit
A
Do not use HP ground unit when APU supplies bleed air to avoid system damageto prevent any adverse effect on the Air Conditioning system.
25
MAX Positive differential cabin Pressure
9.0 PSI
26
MAX Negative differential cabin Pressure
-1.0 PSI
27
Air Conditioning with LP Ground Unit
Do not use conditioned air simultaneously from PACKS and LP ground unit to prevent any adverse effect on the Air Conditioning system.
28
Minimum Height for use of Autopilot Takeoff with SRS mode
100 ft AGL TAKEOFF WITH SRS MODE-AN INTERNAL FMGS LOGIC PREVENTS THE AUTOPILOT FROM ENGAGING DURING THE 5 SECONDS AFTER LIFTOFF
29
Minimum Height for use of AutopilotStraight-in Non-Precision approach
Applicable Minimum
30
Minimum Height for use of AutopilotCircling Approach
Applicable Circling Minimum -100ft
31
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)
32
Minimum Height for use of AutopilotGo- Around (AP or FD engagement)
100ft AGL
33
Minimum Height for use of Autopilot All other Phases
500 ft AGL (A319/A320)900 ft AGL (A321)
34
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)
35
NAV mode may be used in 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.
36
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
```
37
APU starter motor duty cycles
After 3 cycles wait 60 minutes before attempting 3 more cycles
38
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
39
THRUST/EGT LIMITSA319, A320 (not NEO), A321Starting
635 C
40
THRUST/EGT LIMITSA320 NEOSTARTING
1018 C EGT
41
THRUST/EGT LIMITSA319, A320 (not NEO), A321MCT
Unlimited time 610
42
THRUST/EGT LIMITSA320 NEOMCT
unlimited time1043 C EGT
43
THRUST/EGT LIMITSA319 A320 (not NEO)Takeoff and Go Around
5 minutes 2 engines10 minutes 1 engine 635 C EGT
44
THRUST/EGT LIMITSA321Takeoff and Go Around
5 minutes 2 engines10 minutes 1 engine650 C EGT
45
THRUST/EGT LIMITSA320 NEOTakeoff and Go Around
5 minutes 2 engines10 minutes 1 engine1083 C EGT
46
OIL Temp minimum starting temp
-40 C
47
OIL Temp minimum prior to exceeding idle
-10 C (min temp for oil for takeoff is +50 C ecam will alert if below)
48
OIL A320 NEO Minimum Oil Pressure
65 PSI
49
Min OIL QUANTITY
11 qts. + Est. Consumption (~0.3 qt/hr) (not in limitations but need to know)
50
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
51
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 %.
52
REVERSE THRUST
Maximum reverse should not be used below 70 kt (Idle reverse is permitted down to aircraft stop)
53
REDUCED THRUST (FLEX)
Takeoff at reduced thrust is not permitted on contaminated runways or into known windshear
54
MAX CROSSWIND DURING START
35 Kts
55
FLAPS and SLATS MAX operating altitude with slats and/or flaps extended
20,000 ft
56
For JET A only, if TAT reaches:
-34 °C, monitor on FUEL SD page that fuel temperature remains higher than -36 °C.
57
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
58
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
59
A321 Sharklet MAX allowed wing tank fuel imbalance at TAKEOFF
Tank fuel quantity heavier tank FULL- MAX imbalance= 882 lb
60
MAX brake temperature for takeoff (brake fans off)
300 C
