Limitations A319 + A320 OM - B Flashcards
Flight Maneuvering Load Acceleration Limits
Clean configuration. . . . . . . . . . . . .. . . . . . .-1 g to +2.5 g
Other configurations. . . . . . . . . . . . . . . .. . . . 0 g to +2 g
Runway Slope
Runway slope (mean). . . . . . . . . . . . . . . . . . . . . . . . .±2 %
Runway Altitude
A320-214 (-BHA, -BHC)
A319-132 / A320-214 (all ex. -BHA, -BHC) / A320-216
A320-214 (-BHA, -BHC)
Runway altitude. . . . . . . . . . . . . . . . . . . . . . .. . . . . 14 100 ft
A319-132 / A320-214 (all ex. -BHA, -BHC) / A320-216
Runway altitude. . . . . . . . . . . . . . . . . . . . . . . . . 9200 ft
Nominal runway width
45 m
Minimal runway width
30 m
Maximum crosswind for takeoff and landing
30 kt gusting up to 38 kt
Maximum crosswind in LVO for takeoff
10 kt
Maximum tailwind for takeoff
10 kt
A319-132 / A320-214 (all ex. -BNK, -BNL)
Note: Maximum for takeoff — 15 kt on selected runways. Refer to OM-C (AAL) for runways with
15 kt maximum tailwind component for takeoff
Maximum tailwind for landing
10 kt
Maximum wind for passenger door operation
65 kt
Maximum wind for FWD and AFT cargo door operation
40 kt
or 50 kt, if the aircraft nose is into the wind, or if the FWD and aft cargo doors are on the leeward side
Maximum Recommended Crosswind on Wet and Contaminated Runways
Damp / Wet / Up to 3 mm (1/8”) of water
30 kt gusting up to 38 kt
Maximum Crosswind for Take off AND Landing
Maximum Recommended Crosswind on Wet and Contaminated Runways
Slush Up to 3 mm (1/8”)
Dry Snow Up to 3 mm (1/8”)
Wet Snow Up to 3 mm (1/8”)
Frost
PIREP “GOOD”
25 kt
Maximum Crosswind for Take off AND Landing
Maximum Recommended Crosswind on Wet and Contaminated Runways
Compacted Snow
PIREP “Good to Medium”
20 kt
Maximum Crosswind for Take off AND Landing
Maximum Recommended Crosswind on Wet and Contaminated Runways
Dry Snow More than 3 mm (1/8”), up to 100 mm (4”)
Wet Snow More than 3 mm (1/8”),
- for takeoff up to 25 mm (1”)
- for landing up to 30 mm (6/5”)
Compacted Snow
OAT above -15°C
Slippery when wet
PIREP “Medium”
15 kt
Maximum Crosswind for Take off AND Landing
Maximum Recommended Crosswind on Wet and Contaminated Runways
Water More than 3 mm (1/8”), up to 12.7 mm (1/2”)
Slush More than 3 mm (1/8”), up to 12.7 mm (1/2”)
PIREP “Medium to poor”
10 kt
Maximum Crosswind for Take off AND Landing
Maximum Recommended Crosswind on Wet and Contaminated Runways
Ice (cold & dry)
PIREP “Poor”
5 kt
Maximum Crosswind for Take off AND Landing
Takeoff is not recommended on the following runway conditions:
–Wet ice
–Water on top of Compacted Snow
–Dry Snow or Wet Snow over Ice
Cockpit Window Open Maximum Speed
200 kt
Maximum Flaps/Slats Speeds
FLAPS 1
230 kt
Maximum Flaps/Slats Speeds
FLAPS 1 + F
215 kt
Maximum Flaps/Slats Speeds
FLAPS 2
200 kt
Maximum Flaps/Slats Speeds
FLAPS 3
185 kt
Maximum Flaps/Slats Speeds
FLAPS FULL
177 kt
Maximum Operating Speed VMO/MMO
VMO. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 350 kt
MMO. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .0.82 M
Maximum speed with the landing gear extended (VLE)
280 kt /0.67 M
Maximum speed at which the landing gear may be extended (VLO extension)
250 kt /0.60
Maximum speed at which the landing gear may be retracted (VLO retraction)
220 kt /0.54
Maximum Tire Speed
195 kt
Minimum Control Speed for Landing (VMCL)
A319-132
A319-132
109 kt
Minimum Control Speed for Landing (VMCL)
A320-214
A320-214
113 kt
Minimum Control Speed for Landing (VMCL)
A320-216
A320-216
108 kt
Taxi Speed
When the taxi weight is higher than 76000 kg
(during a turn)
20 kt during a turn
Wipers Maximum Operating Speed
230 kt
RAT deployment during flight test, the airspeed must be limited to?
250 kt
AVIONICS VENTILATION
During ground operations and depending on the Outside Air Temperature (OAT), the flight crew
must limit the time that the aircraft electric power supply is used, in normal avionics ventilation
system configuration, as follows:
OAT ≤ 49 °C ?
49 °C < OAT ≤ 55 °C ?
55 °C < OAT ≤ 60 °C ?
60 °C < OAT ≤ 64 °C ?
OAT ≤ 49 °C No limitation
49 °C < OAT ≤ 55 °C 2 h
55 °C < OAT ≤ 60 °C 1 h
60 °C < OAT ≤ 64 °C 0.5 h
CABIN PRESSURE
Maximum positive differential pressure?
9.0 PSI
CABIN PRESSURE
Maximum negative differential pressure ?
-1.0 PSI
CABIN PRESSURE
Safety relief valve Setting PSI?
8.6 PSI
Autopilot Function
The autopilot can be used with the following minimum values:
At takeoff?
100 ft AGL or 5 s after liftoff
Autopilot Function
The autopilot can be used with the following minimum values:
In non-precision approach using F-LOC◄ or FG/
S◄ (FLS◄ function)
200 ft AGL
Autopilot Function
The autopilot can be used with the following minimum values:
In non-precision approach using FINAL APP◄,
NAV FPA, NAV V/S, TRK FPA, HDG V/S, LOC
V/S, LOC FPA
250 ft AGL
Autopilot Function
The autopilot can be used with the following minimum values:
In circling approach
500 ft AGL for aircraft category C
600 ft AGL for aircraft category D
Autopilot Function
The autopilot can be used with the following minimum values:
ILS/MLS◄ approach when CAT1 is displayed
on the FMA
160 ft AGL
Autopilot Function
The autopilot can be used with the following minimum values:
GLS◄ approach when AUTOLAND is not displayed
on the FMA
160 ft AGL
Autopilot Function
The autopilot can be used with the following minimum values:
ILS/MLS◄ approach when CAT2 or CAT3
(single or dual) is displayed on the FMA
0 ft AGL if autoland
Autopilot Function
The autopilot can be used with the following minimum values:
PAR approach (Precision Approach Radar)
250 ft AGL
Autopilot Function
The autopilot can be used with the following minimum values:
After a manual go-around
100 ft AGL
Autopilot Function
The autopilot can be used with the following minimum values:
In all other phases
500 ft AGL
Takeoff in GPS Primary ◄
For certain airports, where the difference between the local coordinate system and WGS 84
(geodesic standard used by GPS, FMS) is not negligible, a map shift may occur after takeoff.
The flight crew must………………………………. for takeoff from these airports, until a safe altitude is
reached.
deselect the GPS
RNP accuracy with GPS PRIMARY◄ is
En route
1 NM
RNP accuracy with GPS PRIMARY◄ is
In terminal area
0.5 NM
RNP accuracy with GPS PRIMARY◄ is
In approach
0.3 NM
Use of NAV Mode
After Takeoff
NAV mode may be used after takeoff provided that:
NAV mode may be used after takeoff provided that:
–GPS PRIMARY◄ is available, or
–The flight crew checked the FMGS takeoff updating
Use of NAV Mode
In Terminal Area
NAV mode may be used in terminal area provided that:
–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.
APU Start
After…………… consecutive APU start attempts, the flight crew must wait …….. min before a new start
attempt.
After three consecutive APU start attempts, the flight crew must wait 60 min before a new start
attempt
A P U
Maximum N Speed?
107%
APU EGT
Maximum EGT for APU start (below 35 000 ft)?
Maximum EGT for APU start (above 35 000 ft)?
Maximum EGT for APU running ?
Maximum EGT for APU start
(below 35 000 ft). . . . . . . . . . . . . . . . . . . . . . 1 090 °C
Maximum EGT for APU start
(above 35 000 ft). . . . . . . . . . . . . . . . . . . . 1 120 °C
Maximum EGT for APU running. . . . . . . . . . . .675 °C
Electrical Power
Maximum continuous load per generator ?
(100 %): 90 KVA
Electrical Power
Maximum continuous load per TRU ?
200 A
THRUST SETTING/EGT LIMITS
A319-132
Takeoff(1) and Go around
All engines operative
One engine inoperative
Time Limits and EGT Limits?
All engines operative 5 min
One engine inoperative 10 Min
with max 635 °C
THRUST SETTING/EGT LIMITS
A320-214 / A320-216
Takeoff(1) and Go around
All engines operative
One engine inoperative
Time Limits and EGT Limits?
All engines operative 5 min
One engine inoperative 10 Min
with max 950 °C
THRUST SETTING/EGT LIMITS
A319-132
Maximum Continuous Thrust (MCT)
Time Limits and EGT Limits?
Not time limited
max 610 °C
THRUST SETTING/EGT LIMITS
A320-214 / A320-216
Maximum Continuous Thrust (MCT)
Time Limits and EGT Limits?
Not time limited
max 915 °C
THRUST SETTING/EGT LIMITS
A319-132
Starting EGT?
max 635 °C
THRUST SETTING/EGT LIMITS
A320-214 / A320-216
Starting EGT?
max 725 °C
Engine Shaft Speeds
A320-214 / A320-216
Maximum N1 ?
Maximum N2 ?
Maximum N1 104 %
Maximum N2 105 %
Engine Shaft Speeds
A319-132
Maximum N1 ?
Maximum N2 ?
Maximum N1 100 %
Maximum N2 100 %
Oil Temperature
A319-132
Maximum continuous temperature. ? Maximum transient temperature (15 min) ? Minimum starting temperature ? Minimum temperature before IDLE is exceeded ? Minimum temperature before takeoff ?
Maximum continuous temperature. . . . . . . . . . 155 °C
Maximum transient temperature (15 min). . . . . 165 °C
Minimum starting temperature. . . . . . . . . . . . . . -40 °C
Minimum temperature before IDLE is exceeded.. . -10 °C
Minimum temperature before takeoff. . . . . . . . . . 50 °C
Oil Temperature
A320-214 / A320-216
Maximum continuous temperature. ?
Maximum transient temperature (15 min) ?
Minimum starting temperature ?
Minimum temperature before takeoff ?
Maximum continuous temperature. . . . . . . . . . 140 °C
Maximum transient temperature (15 min). . . . . 155 °C
Minimum starting temperature. . . . . . . . . . . . . . -40 °C
Minimum temperature before takeoff. . . . . . . . - 10 °C
Minimum Oil Pressure
A319-132
60 PSI
Minimum oil pressure
A320-214 / A320-216
13 PSI
Flex Takeoff
FLEX takeoff is not permitted on ……………………?
Contaminated RWYs
Flex Takeoff A319-132
TFLEX cannot be:
–Higher than TMAXFLEX, equal to ISA ……… °C.
Note: When engine anti-ice is on, the flexible temperature is limited to ISA ……….. °C
A319-132
–Higher than TMAXFLEX, equal to ISA + 65 °C
Note: When engine anti-ice is on, the flexible temperature is limited to ISA + 60 °C
Flex Takeoff
A320-216
TFLEX cannot be:
–Higher than TMAXFLEX, equal to ISA ……… °C.
A320-216
Higher than TMAXFLEX, equal to ISA + 70 °C.
TFLEX cannot be:
A320-214
Higher than TMAXFLEX, equal to ISA……… °C. TMAXFLEX corresponds to a reduction of………. % from the full rated takeoff thrust.
A320-214
Higher than TMAXFLEX, equal to ISA + 53 °C. TMAXFLEX corresponds to a reduction of
25 % from the full rated takeoff thrust.
A319-132
CROSSWIND OPERATION ON GROUND
This engine is able to start in crosswind up to……. kt ?
A319-132 Only
This engine is able to start in crosswind up to 35 kt
Maximum operating altitude with slats and/or flaps extended?
Maximum operating altitude with slats and/or flaps extended
20000 ft
FUEL TEMPERATURE JET A1
MIN ?
MAX?
MIN -43 °C
MAX +54 °C
FUEL TEMPERATURE JET A
MIN ?
MAX?
MIN -36 °C
MAX +54 °C
Fuel Imbalance at Takeoff
Inner Tanks (Outer Tanks Balanced)
Full ——————–? kg max imbalance
3000 kg ————? kg max imbalance
1450 kg ————-? kg max imbalance
Full ——————–500 kg
3000 kg ————1050 kg
1450 kg ————-1450 kg
Fuel Imbalance at Takeoff
Outer Tanks (Inner Tanks Balanced)
? kg max imbalance
370 kg
Fuel Imbalance in Flight and at Landing
Inner Tanks (Outer Tanks Balanced)
Full ——————-? kg max imbalance
4300 kg ———–? kg max imbalance
2250 kg ———–? kg max imbalance
Full ——————-1500 kg
4300 kg ———–1600 kg
2250 kg ———– 2250 kg
Fuel Imbalance in Flight and at Landing
Outer Tanks
Maximum Asymmetry?
Maximum Asymmetry
690 kg
Minimum fuel quantity for takeoff?
1500 kg
Hydraulic
MAX OPERATING PRESSURE (AT ZERO DELIVERY) ?
3 000 PSI ± 200 PSI
Maximum brake temperature for takeoff (brake fans ◄ off) ?
300 °C
Maximum NWS angle ?
85 °
