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weight and balance report mentioned in paragraph (6) (b).
(5) The written statement must list any requirements mentioned in
paragraph (4) (d) that are not met.
(6) Each application for export airworthiness approval of a Class I
product must include the following, as applicable:
(a) a statement of conformity mentioned in subregulation 21.130 (2)
for each new product that has not been manufactured under a
production certificate;
(b) unless the importing country does not require it, a weight and
balance report in accordance with subregulations (7), (8), (9) and
(10), as applicable, with a loading schedule when applicable, for
each aircraft in accordance with section 100.7 of the Civil
Aviation Orders;
(c) a maintenance manual for each new product when such a manual
is required under these regulations;
(d) evidence of compliance with the applicable airworthiness
directives, or a suitable notation if any airworthiness directives
are not complied with;
(e) when temporary installations are incorporated in an aircraft for
the purpose of export delivery — a general description of the
installations together with a statement that the installation will be
removed and the aircraft restored to the approved configuration
upon completion of the delivery flight;
(f) historical records such as aircraft and engine log books, repair
and alteration forms, for used aircraft and overhauled products;
(g) for products intended for overseas shipment — a description of
the methods used, if any, for the preservation and packaging of
such products to protect them against corrosion and damage
while in transit or storage. The description must also indicate the
duration of the effectiveness of such methods;
(h) the aircraft’s flight manual required by the applicable
airworthiness regulations for the particular aircraft;
(i) a statement as to the date when title passed or is expected to pass
to a foreign purchaser;
(j) the data required by the special requirements of the importing
country.
Civil Aviation Safety Regulations 1998 (CASR)
Office of Legal Counsel CASR
Civil Aviation Safety Authority 1st Edition – January 2003
Part 21 — 108
Weight and balance reports
(7) A weight and balance report for transport aircraft and commuter
category aeroplanes must be based on an actual weighing of the
aircraft within the period of 12 months preceding the application for
the export airworthiness approval for the aircraft, but after any major
repairs or alteration to the aircraft.
(8) Any changes in equipment that are made after the actual weighing of
the aircraft (except changes classes as major changes) may be
accounted for on a “computed” basis and the report revised
accordingly.
(9) Manufacturers of new non-transport category aeroplanes, normal
category rotorcraft or gliders may include computed weight and
balance data in the report, instead of the results of an actual weighing
of the aircraft, if fleet weight control procedures approved by CASA
have been established for the aircraft. In this case, the following
statement must be included in each report: “The weight and balance
data shown in this report are computed on the basis of CASA’s
approved procedures for establishing fleet weight averages.”.
(10) A weight and balance report must include an equipment list showing
weights and moment arms of all required and optional items of
equipment that are included in the certificated empty weight.
Source FARs section 21.327, modified.
21.329 Issue of export airworthiness approvals for Class I products
(1) An applicant is entitled to an export airworthiness approval for a
Class I product if the applicant shows, at the time the application is
made, that the product meets the requirements of subregulations (2) to
(6) (inclusive), as applicable, except as provided in subregulation (7).
(2) New and used aircraft must meet:
(a) the airworthiness requirements for a standard certificate of
airworthiness under regulation 21.183; or
(b) the airworthiness certification requirements for a special
certificate of airworthiness for an aircraft in the primary,
intermediate or restricted category under regulation 21.184,
21.184A or 21.185 respectively.
Civil Aviation Safety Regulations 1998 (CASR)
CASR Office of Legal Counsel
1st Edition – January 2003 Civil Aviation Safety Authority
Part 21 — 109
(3) Used aircraft must have undergone an annual, or 100 hour, type
inspection in accordance with Part 4A of CAR. The inspection must
have been performed and properly documented within 30 days before
　
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