AIRBUS A319/A320 SYSTEMS AND PERFORMANCE INFORMATION 29 OCT 2013

WEIGHT & DIMENSIONS OPERATIONAL LIMITATIONS FUEL

Max Operating Altitude Min Fuel Quantity for Takeoff

Fuel Capacities (Fuel Density 0.785 kg/l)

SPEED LIMITS

Max Operating Limit Speed VMO

Max Operating Limit Mach MMO Max Allowed Wing Fuel Imbalance

Turb Penetration Speed (≤20,000ft) Inner Tanks

Turb Penetration Speed (>20,000ft)

Max Speed, Gear Extended VLE

Max Speed, Gear Extension VLOe

Max Speed, Gear Retraction VLOr

Max Tire Speed No limitations below 2,250kg

Max Windshield Operating Speed Max Imbalance - Outer Tanks

AIRPORT OPERATIONS Max Cockpit Window Open Speed Min Fuel Temperatures

Runway Slope (mean)

Min Runway Elevation ENGINE

Max Runway Elevation Max Starting EGT

Max TOGA EGT (5 or 10min)

MANOEUVRING LOAD ACCEL LIMITS Max MCT EGT

Clean Configuration Engine Stabilized Parameters (ISA) *For JET A, if TAT reaches -34 °C, monitor FUEL

Otherwise N1 SD page that fuel temp remains higher than -36 °C

EGT

WIND LIMITS N2 AUTOLAND LIMITATIONS

Max Demonstrated Crosswind FF Flaps Configuration

Max Tailwind (Takeoff) EPR Autoland Categories

Max Tailwind (Landing) Glideslope Angle Limits

Max Wind for Pax Door Operations LANDING GEAR LIMITS Airport Elevations

Max Wind for Cargo Door Operations Max Altitude, Gear Extension Runway Conditions

Max Crosswind for Engine Start Max Taxi Speed (Straight Line) Landing Weight Limits

Max X-wind, Contaminated Runway (TO/LDG) Max Taxi Speed (Turn)

Damp, Wet (<3mm) Max Steering Angle - Handwheel HYDRAULICS

≤ 3mm Slush, Dry/Wet Snow Max Steering Angle - Tow/Pushback Normal Operating Pressure

Frost Max Steering Angle - Towbarless

Compacted Snow (OAT ≤ -15 ° C) Max Steering Angle - Pedals FLIGHT CONTROLS

Compacted Snow (OAT> -15 ° C) Max Brake Temp (Set Park Brakes) Max Op Alt, Slats/Flaps Extended

>3mm Dry Snow (Max 130mm) Max Brake Temp (Takeoff - Fans Off)

>3mm Wet Snow (Max 30mm) Max Brake Temp (Takeoff - Fans On) NAVIGATION

>3mm Water/Slush (Max 12.7mm) Standard Tire Pressure (A319) Inertial Referene System (IRS)

Ice (Cold & Dry) Standard Tire Pressure (A320) Max Latitude for Ground Alignment

Takeoff not recommended on Wet Ice, Water on In NAV mode, no valid magnetic heading for:

top of Compacted Snow, Dry/Wet Snow over Ice PRESSURIZATION LIMITS Latitude > 82°N

Autoland Wind Limits Max Positive Differential Pressure Latitude > 73°N, between 90° & 120°W

Max Headwind Max Negative Differential Pressure Latitude > 60°S

Max Crosswind Max Cabin Altitude

Max Tailwind REDUCED THRUST TAKEOFF LIMITS

APU LIMITS Thrust Reduction < 25% of Full Rated Thrust

OIL Max EGT for Start - < 25,000ft Flex Temperature not higher than ISA + 55°C

Min Oil Quantity Max EGT for Start - > 25,000ft Flex Temperature not lower than current OAT

Max Oil Quantity Max EGT - 5s for Shutdown Not permitted on Contaminated Runways

Oil Consumption Rate Max EGT - Immediate Shutdown Permitted with any inoperative item affecting

Min Oil Pressure Max Alt for APU Battery Start performance, provided performance shortfall

Min Oil Temp (Starting) Max Alt for APU Bleed (1 Pack) has been applied to meet all performance

Min Oil Temp (Exceeding Idle) Max Alt for APU Bleed (2 Packs) requirements at the takeoff weight, with the

Max Continuous Temperature APU Generator Max Load operating engines at thrust available for the

Max Transient Temperature (15min) "LOW OIL LEVEL" ECAM flex temperature.

A319

70,400 kg

70,000 kg

61,000 kg

57,000 kg

77,400 kg

77,000 kg

64,500 kg

61,000 kg

A320

35,400 kg 37,230 kg

-1g to +2.5g

0g to +2g

20.59 m 22.90 m

Height

Turn Radius

Min Path Width

37.57 m

12.14 m 12.14 m

21.42 m 21.99 m

±2%

-1,000 ft

9,200 ft

34.10 m 34.10 m

33.83 m

MRW

MTOW

MLW

MZFW

Min Weight

Wing Span

Length

155°C

165°C

11 Quarts

25 Quarts

0.3 Qt/hr

60 psi

-40°C

-10°C

25 kt

20 kt

15 kt

38 kt

15 kt

10 kt

65 kt

40 kt

38 kt

10 kt

85°

6°

500°C

300°C

35 kt

350 kt

M 0.82

250 kt

275kt/M.76

280kt/M0.67

250 kt

220 kt

195 kt

230 kt

29 kt

29 kt

29 kt

25 kt

25 kt

75°

95°

350 kg/h

1.01

635°C

635°C

610°C

30 kt

20 kt

15,000 ft

90 kVA

10 hrs

1500 kg

3000±200psi

700 - 742°C

Heavier Tank Fuel Qty Max Imbalance

Full

900°C

982°C

682°C

25,000 ft

20,000 ft

150°C

8.6 psi

-1.0 psi

8,000 ft

209 psi

187 psi

200 kt

25,000 ft

30 kt

20 kt

-54°C

691 kg 5,435 kg 6,476 kg 18,728 kg

JET

A1

/

JP8

/ No3

Jet

JET

A*

JP5

RT

/ T

S-1

JET

B

JP 4

1,500 kg

4,300 kg 1,600 kg

2,250 kg 2,250 kg

690 kg

39,100 ft

21.4%

414°C

57.8%

-43°C -36°C -42°C -45°C -46°C

2x Outer Tk 2x Inner Tk Centre Tk TOTAL

20,000 ft

82°N/S

3 or FULL

CAT II or III

2.5° to 3.15°

≤ 6,500 ft

Dry & Wet

≤ MLW

Max 54°C Max 49°C

LIM SHING KAI