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& Whitney engines for A310-324 and A310-325:
- S12-FADEC Lightning Protection
- S13-FADEC Engine Isolation
- S14-Thrust Reverser Deletion of Mechanical Interlock
- S15-FADEC
- S16-FADEC - Effect of External Radiation
REQUIRED EQUIPMENT The basic required equipment, as prescribed in the applicable
airworthiness regulations (see Certification Basis) must be
installed in the airplane.
Equipment approved for installation is listed in the following
Certification Standard Equipment List:
- A310-200: AI/V-C N° 5/83;
- A310-200 Variant 100: AI/EA-A N° 251/86; and
- A310-300: AI/EA N° 1901/85;
Cabin furnishings equipment shall be in conformance to the
following frame specifications:
- Galleys : TL 25/1109/74
- Passenger Seats: TL 25/1110/74
NOTES
NOTE 1: Weight and Balance. Current weight balance report, including list of equipment
included in certificate empty weight and loading instructions when necessary, must be
in each aircraft at the time of original certification and at all times thereafter (except in
the case of air carrier operators having an approved weight control system). The
certificate empty weight and the corresponding center of gravity location must include
unusable fuel, engine oil, hydraulic fluid in tanks and in the systems. The certificate
empty weight does not include the lifting jack carried on board, the entrance steps, the
tools kit, the life jackets and the fluid to be injected into the engine.
NOTE 2: Markings and Placards. All placards specified in the approved Brazilian Airplane
Flight Manual must be displayed in the airplane in the appropriate locations. In
addition, all markings and placards for passenger information, external markings for
emergency, load limits in cargo/baggage compartments must be presented in
Portuguese or bilingual (Portuguese/English). The translations acceptable to CTAm
are listed in the CTA Report H.10-0153-02, dated 22 Mar. 1999 or further revisions.
NOTE 3: Continuing Airworthiness. Life limitations are provided in the Chapter 05 of the A310
Maintenance Manual, approved by DGAC.
Structures and Systems Certification Maintenance Requirements are listed in Airbus
Industrie document AI/ST 5/849/85.
AIRBUS March 1999 EA-8002-01 Sheet 14
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 or bilingual (see Note 2);
3. Operational requirements - the following modifications must be installed:
- cabin ozone filter: Mod. 6159;
- cargo/baggage compartment fire protection: Mods. 8265 and 10452;
- DFDR: Mod. 8500 and 8705;
- ELT: TSO C91a;
- Floor emergency escape path marking: Mod. 6515 (MBB System, 6934 (Bruce
System) or 6812 (LSI System);GPWS: Mod. 8960;
- TCAS, if required: Mods. 8616 and 10928 (Bendix System) or Mods. 10664 and
11049 (Honeywell System);
- Windshear detection and guidance system: Mod. 7187; and
- Second ADF: Mod. 4536.
4. MMEL categorized.
NOTE 5: If the modification 4941 is embodied, the aircraft is approved for CAT III Precision
Approach.
NOTE 6: The definition of the aircraft for extended twin engine airplane operations is precised in
the document AI/EA 3000 - “Configuration, Maintenance and Procedures Standards
According to AC 120-42A”, Ref. CMP DGAC.
NOTE 7: Modifications 6920 and 7468 provide for installation in aft cargo compartment of
respectively 1 and 2 Auxiliary Center Tanks with the following characteristics:
Tanks Unusable Fuel Usable Fuel
ACT 1 27 kg (34 l) 5 760 kg (7 200 l)
ACT 2 27 kg (34 l) 5 760 kg (7 200 l)
NOTE 8: On A310-308 model, the engine General Electric CF6-80C2A2 may be used after
embodiment of Service Bulletin A310-71-2003 and with the corresponding revision of
the AFM supplement 11.
NOTE 9: Weight variant 12 to A310-324 model only applies to individual MSN 442, 453, 456
and 467.
NOTE 10: If the modification 11469 (for GE engines) or 11468 (for P&W engines) is installed,
the aircraft is approved in accordance with AC 91-RVSM Reduced Vertical Separation
Minimum operation.
NOTE 11: High density configuration up to 275 passengers can be appreciated by CTA, upon
request and justification provided by Airbus.
LUIZ ALBERTO C. MUNARETTO – Ten.-Cel.-Av. Maj.-Brig.-do-Ar REGINALDO DOS SANTOS
Chefe da Divisão de Homologação Aeronáutica Diretor do Centro Técnico Aeroespacial
(Chief, Divisão de Homologação Aeronáutica) (Director, Centro Técnico Aeroespacial)
　
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