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Bulk: 2 770 kg (1 442 kg with mod. 3656).
For the positions and the loading conditions authorized in each
position (references of containers, pallets and associated
weights) see Weight and Balance Manual Chapter 1.10.05.
HYDRAULIC FLUIDS Specification NSA 30-7110.
TYRES See SB A310-32-2006
MAXIMUM OPERATING
ALTITUDE
12 530 m (41 100 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.
S/N’S 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.
IMPORT ELEGIBILITY 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”.
AIRBUS March 1999 EA-8002-01 Sheet 12
IMPORT ELEGIBILITY (Cont.) The CTA Report H.10-0153-02, dated 22 Mar. 1999 or further
revisions, contains the Brazilian requirements for the acceptance
of these airplanes. (See Note 4)
CERTIFICATION BASIS RBHA 25 [corresponding to: FAR Part 25 - including
Amendments 1 thru 19 (initial A300 certification basis);
Amendments 20 thru 41; Amendment 42 except paragraph
25.109; Amendment 43 except paragraph 25.1326;
Amendment 44 except paragraph 25.1413; Amendment 45
except paragraph 25.571, 25.573; Amendment 46 except
paragraph 25.803(c), 25.803(d), 25.809(f) (1)(iv),
25.809(f)(1)(v); Amendment 47 except paragraph
25.809(f)(1)(iii); Amendment 49 except paragraph 25.733; and
Amendment 54 except paragraph 25.365(e)(1) and 25.365(e)(2)
- plus RBHA 25 special paragraph 25.729(e)(7)].
RBHA 36 [corresponding to ICAO Annex 16 Vol. I], plus any
addition or deletion established in paragraphs 6, 8 and 9 of this
report and including the following special requirements listed in
DGAC certification basis and endorsed by CTA:
01. French-German technical complementary conditions:
- CB2-Minimum Stalling Speed
- CB7-1-Flight in Rough Air
- CC4-1-“En Route” Design Conditions with High Lift
Devices Extended
- CC5-1-Design Manoeuvre Conditions
- CC6-1-Design Gust Conditions (except for A310-300
variant 08)
- CC6-3-Design Gust Conditions (for A310-300 variant 08
only)
- CC8-1-Bird Impact
- CC9-1-Asymmetric Load on the Horizontal Stabilizers
- CC10-1-Ground Loads
- CC11-Jacking Loads
- CC12-1-Crash Design Conditions
- CD1-1-General Design of Systems
- CD8-1-Operation of Landing Gear
- CD9-2-Protection of Equipment installed on LG and LG
Wheel Wells
- CE0-Engine Installation - Application JAR E
- CE2-1-Windmilling without Oil
- CE4-1-Engine Vibration Levels
- CE10-1-Auxiliary Power Unit (APU) and its installation on
the Aircraft
- CF3-1-Functioning of the Systems under Negative
Acceleration
- CF7-1-Electrics
--Endurance demonstration
02. Special condition applicable to A310-300 Series related to
Center of Gravity Control Systems.
03. Discrete gust requirements for A310-308 variants 08 and 09
approved in accordance with JAR NPA 25C-205.
04. Extended Range Twin Engine Airplane Operations approval
in accordance with AC 120-42.
AIRBUS March 1999 EA-8002-01 Sheet 13
CERTIFICATION BASIS
(Cont.)
05. Precision Approach and Landing requirements
complemented by CTC 25-2 for category II and category I
approach, JAR AWO Section III NPA no 25G-142 (June
83) for category III precision approach with and without
decision height (fail operational system); the Automatic
Flight Control System complies with AC 25.1329-1A for
cruise and AC 20-57A for automatic landing.
06. Special conditions related to the use of FADEC on the Pratt
　
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