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tools kit, the life jackets and the fluid to be injected into the engine.
NOTE 2: Markings and Placards. All markings and placards for passenger information under
normal or emergency conditions must be in English and Portuguese. All markings and
placards for flight attendants information under emergency conditions must be in
English and Portuguese. External markings for emergency operation of doors and
normal ground operations of cargo doors must be in English and Portuguese.
NOTE 3: Continuing Airworthiness. Life limitations are provided in the Chapter 05 of the A300
Maintenance Manual, approved by DGAC.
NOTE 4: The differences of the Brazilian airplanes in relation to the basic DGAC type design are
summarized below:
1. The DGAC approved Brazilian Airplane Flight Manual;
2. Markings and placards in Portuguese language: see Note 2;
3. ADF1 powered by the emergency bus bars;
4. APU fire extinguisher handle “pull and turn” inscription; and
5. Autothrottle control panel identification.
NOTE 5 For model B4-203, the MMO warning selector of modification no. 1688 allows an MMO
switching. MMO is 0.86 for takeoff weights up to 153 000 kg (337 302 lb) and 0.82 for
takeoff weight greater than 153 000 kg (337 302 lb) provided the airplane is operated
in accordance with the corresponding DGAC approved Airplane Flight Manual page
2.03.00 page 1.
NOTE 6 Aircraft identified by the letters FF added to the designation of the model have forward
facing crew cockpit and digital autopilot with associated subsystems.
The definition of FF aircraft is detailed in AI/V-C document 1045/81.
FF aircraft are to be used with a Flight Manual incorporating the FF revision approved
by DGAC.
NOTE 7 If modifications 0904, 1022 and 1023 are embodied, the aircraft has Category IIIa
precision approach capability.
AIRBUS March 1999 EA-8002-01 Sheet 7
IV -Model A310-203 (Transport Category), approved 17 October 1998
Model A310-204 (Transport Category), approved 17 October 1998
Model A310-221 (Transport Category), approved 17 October 1998
Model A310-222 (Transport Category), approved 17 October 1998
ENGINE Model A310-203: Two General Electric model CF6-80A3
Model A310-204: Two General Electric model CF6-80C2A2
Model A310-221: Two Pratt & Whitney model JT9D-7R4D1
Model A310-222: Two Pratt & Whitney model JT9D-7R4E1
MAXIMUM WEIGHT (kg)
A310-203/-221 A310-203/-221/-222 A310-203
VARIANT
Basic
Model
Variant 03
with
mod. 4008
Variant 01
with mod.
3703 *
Variant 04
with mod.
5124 **
Variant 06
with
mod. 6395
Variant 08
with
mod. 7415
Max. Ramp 132 900 125 900 139 500 142 900 135 900 139 500
Max. Take-off 132 000 125 000 138 600 142 000 135 000 138 600
Max. Landing 118 500 118 500 121 500 121 500 118 500 122 000
Max. Zero Fuel 108 500 108 500 111 500 111 500 111 500 112 000
* SB 00-2003
** SB 00-2002
A310-221 A310-204/-222 A310-204 A310-222
VARIANT
Variant 07
with mod.
6764 *
Variant 101
with
mod. 6527
Variant 104
with
mod. 6528
Variant 107
with
mod. 7290
Variant 11
with mod.
10685
Max. Ramp 132 900 139 500 142 900 134 900 144 900
Max. Take-off 132 000 138 600 142 000 134 000 144 000
Max. Landing 119 500 122 000 122 000 122 000 121 500
Max. Zero Fuel 111 500 112 000 112 000 112 000 111 500
* SB 00-2006
FUEL QUANTITY (0.8kg/l) Unusable Usable Fuel (kg)
Tanks Fuel (kg) Variant XX Variant 1XX
Outer 41 5 992 5 920
Inner 40 22 360 22 320
Central 14 15 728 15 728
Total 95 44 080 43 968
AIRBUS March 1999 EA-8002-01 Sheet 8
V - Model A310-304 (Transport Category), approved 17 October 1998
Model A310-308 (Transport Category), approved 17 October 1998
Model A310-322 (Transport Category), approved 17 October 1998
Model A310-324 (Transport Category), approved 24 October 1997
Model A310-325 (Transport Category), approved 24 October 1997
ENGINE Model A310-304: Two General Electric model CF6-80C2A2
Model A310-308: Two General Electric model CF6-80C2A8
or CF6-80C2A2 (See Note 8)
Model A310-322: Two Pratt & Whitney model JT9D-7R4E1
Model A310-324: Two Pratt & Whitney model PW 4152
Model A310-325: Two Pratt & Whitney model PW 4156A
MAXIMUM WEIGHT (kg)
A310-304/-322/-324 A310-304/-308/-324
VARIANT
Basic
Model
Variant 01
with mod.
5616 *
Variant 03
with mod.
8144
Variant 05
with
mod. 7088
Max. Ramp 150 900 153 900 153 900 157 900
Max. Take-off 150 000 153 000 153 000 157 000
　
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