Limitations (Rev 11) Flashcards
Max wind for takeoff and landing
50 kts (U)
(Non-memory item)
What are the max landing weights?
137/142/171
A319 137,788
A320 142,198
A321 171,519
Max XW for takeoff and landing
29G35 kts (U)
Max XW for landing with vis <4000 or 3/4
15 kts (U)
Max XW (including gust) for Autoland
20 kts
Max TW for takeoff (A320/321 with IAE engines)
10 kts
Max TW for takeoff (All A319 and A320/321 with CFM engines)
15 kts
Max operating altitude
39,000’ (U)
Max TW for landing (Non-Sharklet)
10 kts
Sharklet is 15 kts
Max flap and/or slat extension altitude
20,000’
Max gear extension altitude
25,000’
Max operating airspeed (SL to FL246)
350 KIAS
Max operating Mach number (>FL246)
.82M (Mmo)
Icing conditions exist when OAT (on ground) or TAT (inflight) is __________ and visible moisture is present
10°C or below
Engine anti-ice must be on during all ground and flight ops when icing conditions exist or are anticipated, except during climb and cruise when the temp is ________
Below -40°C SAT
Engine anti-ice must be on prior to and during descent in icing conditions, including temperatures __________
Below -40°C SAT
(Non-memory item)
Open the Ram Air Inlet only if differential pressure is less than ________
+1.0 psi
(Non-memory item)
Max brake temp for takeoff
300°C
(Non-memory item)
Max taxi speed
30 kts (U)
(Non-memory item)
Max taxi speed for 90° turn
10 kts (U)
(Non-memory item)
Min Jet A fuel temp
-36°C
(Non-memory item)
If one tire is deflated on one or more gears, the speed should be limited to ________ when turning
7 kts
(Non-memory item)
If two tires are deflated on the same main gear, speed should be limited to ________ and the NWS angle limited to ________
3 kts; 30°
Min height for Autopilot use after takeoff in SRS mode
100’ AGL
(Non-memory item)
Min height for Autopilot use on an ILS (non-Autoland with CAT 2, CAT 3 SINGLE, or CAT 3 DUAL on FMA)
80’ AGL
(Non-memory item)
Min height for Autopilot use on an ILS (non-Autoland with CAT 1 on FMA)
160’ AGL
(Non-memory item)
Min height for Autopilot use after manual Go Around in SRS mode
100’ AGL
(Non-memory item)
The use of OPEN DES is prohibited ______
Inside FAF or below 1000’ AGL during visual approach
Max HW for Automatic Approach, Landing, and Roll Out (including gusts) (except A319 Sharklet)
30 kts
A319 Sharklet: 2E 20 kts, 1E 15 kts
Max TW for Automatic Approach, Landing, and Roll Out (including gusts) (except A319 Sharklet)
10 kts
A319 Sharklet 5 kts
(Non-memory item)
The aircraft is certified for an engine-out CAT III Single approach and autoland provided _________
Engine-out procedures are completed prior to 1000’ AFL
Max XW for Automatic Approach, Landing, and Roll Out (including gusts) with vis 4000 or 3/4 or greater (except A319 Sharklet)
20 kts
A319 Sharklet: 2E 20 kts, 1E 10 kts
(Non-memory item)
A320 engine-out autolands are authorized in CONF ______ only
FULL
(Non-memory item)
A319 and A321 engine-out autolands are authorized in CONF ______
3 or FULL
(Non-memory item)
With one engine inop, the use of the remaining thrust reverser is permitted provided _______
Not more than idle reverse thrust is used
XW is not more than 15 kts
(Non-memory item)
Time limit for TOGA thrust
5 mins (2E)
10 mins (1E)
(Non-memory item)
Start limits for CFM engines
4 consecutive cycles w/2 minute max duration
15 min cooling period after 4 start attempts
(Non-memory item)
Start limits for IAE engines
3 consecutive cycles w/2 minute max duration on first two starts followed by 1 minute max duration on third
Pause 15 sec between start attempts
30 min cooling period after 3 start attempts or 4 min continuous cranking
Reverse Thrust is for ______ use only
Ground
(Non-memory item)
Max reverse thrust should not be used below _____
70 KIAS or when IAS starts to fluctuate
Idle reverse is permitted to aircraft stop
(Non-memory item)
Min oil quantity for dispatch is ________
13 quarts (U)
(Non-memory item)
The ____ tank fuel must be emptied before ______ are emptied unless the ______ tank fuel is treated as ballast
Center; wing; center (U)
(Non-memory item)
Takeoff using ______ fuel is prohibited
Center tank
(Non-memory item)
On the A321, if center tank is not full, dispatch with more than ______ lbs total fuel in both ACTs is prohibited, unless directed by an MEL
200 (U)
(Non-memory item)
Min height for use of the Autopilot on a non-ILS approach
DA, DDA, or MDA
(Non-memory item)
After ___ APU starter motor duty cycles, wait ____ before attempting ________
3; 60 minutes; 3 more cycles
(Non-memory item)
In flight, the APU gen is limited to an AC load of _____ for flight altitudes ___________ with temps of ISA +20 and below
90 kVA; below 25,000’
(Non-memory item)
Max altitude for APU bleed operation
20,000’
use for wing AI is not permitted
(Non-memory item)
The APU may be started and operated even if the _________ ECAM advisory is displayed. MX action is required within the next ________ of APU operation
LOW OIL LEVEL; 10 hours
(Non-memory item)
Resetting a tripped ________ or ________ CB is prohibited
Fuel boost pump or Fuel indicating system
(Non-memory item)
Max continuous load per generator
100% (90 kVA)
(Non-memory item)
Max continuous load per TRU
200 A
(Non-memory item)
Max difference between altimeters and a known airport altitude
+/- 75’
(Non-memory item)
Max difference between altimeters on PFD 1 and 2
20’
Max allowable inflight difference between CA and FO PFD altitude displays for RVSM operations
200’
Undue Activation of Alpha Protection
3 conditions:
- Continuous nose down pitch above Vls
- Alpha Max hides Alpha Prot strip while wings level
- Alpha Prot strip rapidly moves 30+ kts during maneuvers with AP on and speed brakes retracted
One ADR pb - KEEP ON
Two ADR pbs - OFF
