General Limitations Flashcards
Approach Category 320/321/321 NEO
320/321 NEO Category C
321 CEO Category D
Flight Maneuvering Load Limit:
Clean-
Other Configurations (Slats and/or Flaps Extended) -
-1.0g to +2.5g
0.0g to +2.0g
Max Crosswind TO and landing
TO - 35kts
Landing - 38kts
Max Tailwind Takeoff
A320/320neo/321neo - 15kts
A321 - 10kts
Max Runway Slope
-/+ 2%
Max Tailwind Landing
All AC - 10kts
Minimum Runway Width Limitations
Minimum Runway Width - 148 ft / 45 m
AC 227-229 and 321 NEOs 100 ft / 30 m
Max and Min Pressure Alt for TO & LNDG
9200ft
-2000ft
Narrow Runway Width
Less than 148 ft. / 45 m
Max Wind for Passenger Door Operation
65kts
Max wind for Cargo Door Operations
40kts / 50kts
50kts if nose of plane is oriented into the wind or cargo door is leeward of wind.
VMO/MMO
350KIAS / .82 Mach
VLO (Retraction)
220kts / 0.54 Mach
VLO (Extension)
250kts / 0.60 Mach
VLE (Extended)
280kts / 0.67 Mach
Max Tire Speed
195kts Groundspeed
Max Windshield Wiper Operation Speed
230 KIAS
Max Cockpit Window Speed
200 KIAS
Max Taxi Speed (greater than 167,550 lbs)
A320 CEO - 20kts during a turn
Maximum Flaps/Slats Extended Altitude
20,000ft MSL
Stabilized Approach Policy
1000ft:
1. Rate of Descent 1200FPM or less
2. One dot ILS/LOC, 1/2 for VOR, 0.30 NM RNAV (Lateral) RNP
3. Glidepath ONE DOT (Vertical)
4. Final Configuration
5. NO GPWS Warnings and Cautions
500 FT:
1. Rate of Descent 1000FPM or less
2. Speed -5 to +15 KTS.
3. Thrust Stabilized, usually above idle, commensurate with power required to maintain speed
4. Landing checklist completed
T.O Inhibit duration?
1500 ft or 2 min after liftoff
LDG Inhibit duration?
Below 800ft till 80kts
Max Operational Pressure Altitude
39,800ft
Speed Brake Limitation 320 NEO
Use of speed brakes at or below 240kts is not permitted if:
- GWCG is above 35% or
- In overweight landing conditions.
Landing on Narrow Runways 227-229 and 602-699
Autoland is not authorized
Dispatch from/to narrow runways not allowed in case of: NWS inop, one or more brake inop.
Diversion to normal width runways recommended in case of:
Rudder Jam, rudder pedal jam, yaw damper system fault, rudder travel limit system fault, all failures leading to loss of NWS(yellow sys loss, double hydraulic/BSCU/LGCIU faults)
Minimum oil quantity
320 CEO - 9.5 qt + 0.5 qt for each hour of flight
320 NEO - 9.0 qt + 0.5 qt for each hour of flight or 10.6 qt, whichever is higher
321 NEO - OAT at or above -30C 14 qt below -30C 16.5 qt
Minimum oil temp for takeoff
19 degrees c
321 NEO 52 degrees C
At what temp do we leave the flaps at 1 after landing
30 degrees C
Minimum oil temp for engine start
-40 degrees C
When is an autoland required
When below cat I minimums
Furthermore when visibility is at or below 1/2 mile or 2400 RVR the approach will be set up and briefed as an autoland
What is the minimum runway width for an autoland
148ft/45m
Max altitude for a APU battery restart
25000 ft
Autoflight altitude limitations
* After TO
* Enroute
* RNAV visual
* Non-precision approach
* Non-autoland with Cat I FMA
* Non-autoland with CAT II/III FMA
* Autoland approach
* Go-around
- After TO - 100’ and 5 sec after TO
- Enroute - 900’
- RNAV visual - 500’
- Non-precision approach - DDA/DA
- Non-autoland with Cat I FMA - 160’
- Non-autoland with CAT II/III FMA - 80’
- Autoland approach - Taxi rollout speed
- Go-around - 100’
Which decent modes are not permitted inside the FAF or below 1000’ AGL
OPEN DES
DES
Autoland authorizations
Must be flown by captains
Not less than a 148’/45m wide runway
Braking action must not be less than MED
Autoland brake selection requirements
Less than 8000’ - MED
8000’ or greater - LOW or MED
Engine thrust time limitations
Takeoff go around
* all engine 5min
* one engine 10 min
When is a reduced thrust TO prohibited
- On a slippery or wet runway
- When suspected, reported, or known windshear is present
- When a special Dept procedure specifies full thrust for TO
Is TO with the center tanks supplying fuel prohibited?
Yes
What is the minimum fuel amount for TO?
3300 lbs and absent of low fuel ECAM
