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drawing approved by the DGAC.
MAXIMUM BAGGAGE Cargo compartment maximum load:
Forward: 16 620 kg
Mid: 10 280 kg
Aft (bulk): 2 500 kg
For the positions and the loading conditions authorized in each
position (references of containers, pallets and associated
weights) see Approved Flight Manual (chapter 6 - Annex 02).
The aircraft must be loaded according to instructions included in
the Weight and Balance Manual
HYDRAULIC FLUIDS Specification NSA 30-7110.
TYRES See SB A300-32-002.
MAX. OPERATING ALTITUDE 12 200 m (40 000 ft)
TEMPERATURE OPERATING See DGAC approved Brazilian AFM.
LIMITS
CONTROL SURFACE
MOVEMENTS
The movement of the various control surfaces must be carefully
controlled by proper rigging of the flight control systems. The
airplane must therefore be rigged in accordance with the
following DGAC-approved information and data:
Control surface movement inspection: Airbus Industrie Reports
A300B 8.27.010, .011, .012, .013, .014 and .015.
Rigging procedure: Airbus Industrie Reports A007-10.063,
-10.094, -10.095, -10.100, -10.102, -10.103, -10.105 and -
10.123.
SERIAL NUMBERS ELIGIBLE A Certificate of Airworthiness for Export endorsed as Noted
under "Import Requirements" must be submitted for each
individual aircraft for which application for a Brazilian
Certificate of Airworthiness is made.
AIRBUS March 1999 EA-8002-01 Sheet 5
IMPORT ELIGIBILITY A Brazilian Certificate of Airworthiness may be issued on the
basis of on a DGAC Export Certificate on Airworthiness (or a
third country Export Certificate on Airworthiness, in case of
used aircraft imported from such country), including the
following statement:
“The aircraft covered by this certificate has been inspected,
tested and found to be in conformity with the Brazilian
approved type design as defined by the Brazilian Type
Certificate no. 8002 and in condition of safe operation”.
The CTA Report H.10-015-01, dated 19 May 80 or further
revisions, contains the Brazilian requirements for the acceptance
of these airplanes. (See Note 4)
CERTIFICATION BASIS RBHA 25 (corresponding to Franco/German requirements of
FAR Part 25 including Amdts. 1 thru 19).
FAR 25 Amdt. 23 for the following paragraphs : 25.145,
25.1305, 25.1321, 23.1331, and 25.1333.
FAR 25 Amdt. 24 for paragraph 25.1303.
FAR 25 Amdt. 32 for paragraphs 25.785, 25.787, 25.789,
25.791, 25.809, 25.811, 25.812, 25.853, 25.855, 25.857,
25.1557, and Appendix F.
Franco/German “Conditions Techniques Complémentaires” as
listed in DGAC documents 4080 DTA/M dated 6 August 1970,
and 2060 DTA/M dated 30 March 1973.
Operation at take-off thrust extended to 10 minutes in case of
engine failure, as per SGAC letter 16233 DTA/SDT/M of
7 March 1974.
Endurance flight campaign called for as per paragraph 6.4 of
SGAC/LBA document on the organization of the A300 B
Certification, dated 6 October 1970.
For the Automatic Flight Control System, the applicable
technical requirements are complemented by:
- AC.25 1329-1A for category 1 cruise and approach;
- Circulars DTA/M 3938 and AC 20-57A for category II
approach and automatic landing;
- AC 120-28 A for category III a precision approach;
The requirements are established in SGAC letter 3904 DTA/M;
dated 20 July 1972.
Use of flexible take-off thrust as per SGAC letter 1694, dated
12 March 1974.
Noise Standard: ICAO Annex 16.
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:
- A300B2-203: AI/V-C N° 149/ 80; and
- A300B4-203: AI/V-C N° 13/79.
AIRBUS March 1999 EA-8002-01 Sheet 6
REQUIRED EQUIPMENT
(Cont.)
Cabin furnishings equipment shall be in conformance to the
following frame specifications:
- For Galleys: TL 25/1109/74; and
- For 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
　
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