Limitations A319 + A320 OM - B Flashcards by Barack Oberhammer

Flight Maneuvering Load Acceleration Limits

Clean configuration. . . . . . . . . . . . .. . . . . . .-1 g to +2.5 g

Other configurations. . . . . . . . . . . . . . . .. . . . 0 g to +2 g

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Runway Slope

Runway slope (mean). . . . . . . . . . . . . . . . . . . . . . . . .±2 %

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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

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Nominal runway width

45 m

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Minimal runway width

30 m

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Maximum crosswind for takeoff and landing

30 kt gusting up to 38 kt

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Maximum crosswind in LVO for takeoff

10 kt

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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

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Maximum tailwind for landing

10 kt

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Maximum wind for passenger door operation

65 kt

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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

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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

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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

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Maximum Recommended Crosswind on Wet and Contaminated Runways

Compacted Snow

PIREP “Good to Medium”

20 kt

Maximum Crosswind for Take off AND Landing

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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

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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

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Maximum Recommended Crosswind on Wet and Contaminated Runways

Ice (cold & dry)

PIREP “Poor”

5 kt

Maximum Crosswind for Take off AND Landing

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Takeoff is not recommended on the following runway conditions:

–Wet ice

–Water on top of Compacted Snow

–Dry Snow or Wet Snow over Ice

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Cockpit Window Open Maximum Speed

200 kt

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Maximum Flaps/Slats Speeds

FLAPS 1

230 kt

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Maximum Flaps/Slats Speeds

FLAPS 1 + F

215 kt

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Maximum Flaps/Slats Speeds

FLAPS 2

200 kt

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Maximum Flaps/Slats Speeds

FLAPS 3

185 kt

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Maximum Flaps/Slats Speeds

FLAPS FULL

177 kt

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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 °

Limitations A319 + A320 OM - B Flashcards

(88 cards)