Document ID: chunk:federal_register_of_legislation:F2024C01027:reg:15:p105
Version: federal_register_of_legislation:F2024C01027
Segment Type: reg
Provision Reference: reg 15 (pt 105/182)
Character Range: 414753–417671

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.

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