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Takeoff 18% MAC 33% MAC
Landing 15% below 120 500 kg
18% above 125 500 kg
35%
Linear variation between 120 500 kg and 125 500 kg.
FUEL QUANTITY (0.782kg/l) Usable Fuel
Tanks Unusable
Fuel
Normal preselected
refueling
Refueling with
high level shut off
(kg) (kg) (kg) (liters)
Outer 12 7 000 7 218 9 230
Inner 40 27 000 27 190 34 770
Total 52 34 000 34 408 44 000
AIRBUS March 1999 EA-8002-01 Sheet 2
II - Model A300B4-203 (Transport Category), approved 16 June 1980.
ENGINE Two General Electric model CF6-50C2. turbojet engines.
MAXIMUM WEIGHT (kg) Max. Ramp 165 900
Max. Take-off 165 000
Max. Landing 134 000
Max. Zero Fuel 124 000
CG RANGE Forward Aft
Takeoff 18% MAC 33% MAC
Landing 15% below 124 000 kg
18% above 130 000 kg
35%
Linear variation between 124 000 kg and 130 000 kg.
FUEL QUANTITY (0.782kg/l)
Usable Fuel
Unusable
Without SB N° 28.021
(Mod. 1664)
With SB N° 28.021
(Mod. 1664)
Tanks fuel Normal
preselected
refueling
Refueling with
high level
shut off
Normal
preselected
refueling
Refueling with
high level
shut off
(kg) (kg) (kg) (liters) (kg) (kg) (liters)
Outer 12 7 000 7 202 9 210 7 000 7 241 9 260
Inner 130 27 000 27 026 34 560 27 000 27 480 35 140
Center 48 11 000 11 206 14 330 13 500 13 763 17 600
Total 190 45 000 45 434 58 100 47 500 48 484 62 000
III - DATA PERTINENT TO ALL A300 SERIES
FUEL See General Electric Specification D50 TF2. This specification
is also applicable to the APU.
Additives:
- anti-icing: PHILLIPS PFA-55MB to MIL I 27686
specification, 0,15% by volume maximum concentration
- biocide: SOHI0 BIOBOR JF at 270 PPM maximum
concentration;
- anti-static: SHELL ASA-3 at 1 PPM maximum concentration.
For operating conditions specific to each fuel, refer to
corresponding Flight Manual.
ENGINE LIMITS (2.2482 lb/daN)
Static thrust at sea level:
Take-off (5min.)* (Up to 30°C)
Maximum continuous (Up to 30ºC)
23 050 daN (51 800 lb)
20 600 daN (46 300 lb)
AIRBUS March 1999 EA-8002-01 Sheet 3
ENGINE LIMITS (2.2482 lb/daN)
(Cont.) Maximum engine speed:
N1 rpm (%)
N2 rpm (%)
4 068 (118.5%)
10 761 (109.5%)
Maximum gas temperature:
Take-off (5min.)*
Maximum continuous
Maximum acceleration (2 min)
Starting
945oC
910oC
960oC
900/750oC
Maximum oil temperature
(supply pump inlet):
Take-off, stabilized
Transient (15 mn max.)
160oC
175oC
Approved oils See Specification GE D50TF1
called for in SB GE N° 79-1
* 10 minutes at take-off thrust allowed only in case of engine failure
(at take-off or during go-around).
** Up to 40 sec/above 40 sec.
AUXILIARY POWER UNIT Airesearch TS CP 700-5 (Specification SC 6203).
Operating limitations:
- Maximum power rating at sea level: 105.8 kW (142 hp)
- Maximum operating speed - N1: 30 910 rpm (110%)
- N2: 38 845 rpm (110%)
- Maximum gas temperature at turbine: 585oC
Approved oils: see AIRESEARCH maintenance manual TSCP
700 49.20.00 table 303.
AIRSPEED LIMITS Maximum Operating Mach (MMO)
(IAS, unless otherwise stated) At and over 12 700 m (28 000 ft) : 0.86/0.82 (see Note 5)
Maximum Operating Speed (VMO)
Up to 12 882 m (28 400 ft) : 345 kt:
Maneuvering Speed (VA): see DGAC approved Brazilian Flight
Manual.
Extended Flaps/Slats Speed (VFE): see table below:
Slats/Flaps (°) VFE (kt)
Take-off 16/0 250
Take-off 16/8 215
Approach 16/15 205
Landing 25/25 180
Enroute 16/0 210 (M=0.47)
Minimum Control Speed: - In flight (VMCA): 112 kt
- Takeoff/Landing (VMCG): 107 kt
Landing gear: (VLE) - Extended: 270 kt/ Mach 0.59
(VLO) - Extension 270 kt
(VLO) - Retraction 240 kt
Tyres Limit Speed (Ground Speed): 195.5 kcas
AIRBUS March 1999 EA-8002-01 Sheet 4
DATUM Station 0 - 6.38 m (251.26 in) forward of the fuselage nose.
MEAN AERODYNAMIC
CHORD
6.6080 m (250.15 in); leading edge of MAC: Sta. 1116.
LEVELING MEANS Clinometer on the cabin rails.
MINIMUM FLIGHT CREW 2 pilots and 1 flight engineer.
2 pilots for aircraft identified FF (See Note 6).
MAXIMUM PASSENGERS 345 in compliance with the requirements of FAR 25 Amdt. 32,
covering emergency exits. Emergency evacuation demonstration
in compliance with FAR 25 para. 25.803 (c) was conducted with
330 passengers. For the number of passengers authorized for
each aircraft, see the corresponding interior arrangement
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