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a) master minimum equipment list – comprising information relating to the permissibility of dispatching aircraft with a known component or system inoperative, [For additional information, see 1.8.3 of this Part];
b) continuing airworthiness maintenance information (sometimes issued as a maintenance planning document) – is the basis for the initial recommended maintenance programme for newly certified aircraft; and
c) configuration deviation list – comprising information relating to the operation of an aeroplane without certain secondary airframe or engine parts.
1.3.6 Post-type certification activities
1.3.6.1 General
A State of Design that issues a Type Certificate for an aircraft has responsibilities under Annex 8 to provide continuing airworthiness services to States of Registry. The CAA and the Type Certificate holder fulfill this responsibility through a system of receiving and exchanging of information, surveillance, assessment of service difficulty experiences, and development of the necessary airworthiness actions. The organization responsible for the approved type design (holder) is an integral part of this process.
1.3.6.2 Retention of type design data
The type design data are contained in records, reports, drawings, and other documents that describe collectively the exact configuration of the type design when it was approved. The type design data must be maintained by the CAA or the Type Certificate holder, or both. The CAA should determine the eligibility and type of data to be maintained by the Type Certificate holder. In either case, it should be recognized that the type design records are permanent and may not be destroyed as long as an aircraft remains in service. Data maintained by the Type Certificate holder must be made available to the CAA for such routine activities as production inspection, surveillance, design change reviews, development of corrective actions, or for any other reasons deemed necessary by the CAA. The record-keeping should consist of at least the following:
a) the drawings and specifications, and a listing of those drawings and specifications necessary to define the configuration and design features of the product as it was shown to comply with the requirements applicable to the product;
b) reports on analysis and tests undertaken to substantiate compliance with the applicable requirements;
c) information, materials and processes used in the construction of the aircraft, engine or propeller;
d) an approved flight manual or its equivalent (type-related document), including the master minimum equipment list and configuration deviation list (if applicable);
e) an approved maintenance review board (MRB) report, maintenance programme or equivalent document, and aircraft maintenance manual with details of manufacturer’s-recommended and CAA-accepted scheduled maintenance plan and procedures guidelines;
f) any other data necessary to allow, by comparison, the determination of airworthiness and noise characteristics (where applicable) of later products of the same type; and
g) in the case of revalidation of Type Certificates issued by other States only:
1) a statement from the airworthiness authority of the State of Design detailing the deviations or differences permitted between the national airworthiness Standards and those of the aircraft, engine(s) and propeller(s) as approved;
2) the Type Certificate/design approval or equivalent for the aircraft, engine(s) and propellers, issued by the airworthiness authority of the State of Design; and
3) a listing and complete set of all mandatory airworthiness directives or their equivalent.
1.3.6.3 Responsibility of Type Certificate holder
The Type Certificate holder remains responsible for the continued integrity of the approved type design and it or its representative must continue to be the CAA’s contact point for resolving issues that may require corrective action. To fulfill this responsibility, the holder of a Type Certificate should have the continued capability, or access to a capability, of providing appropriate technical solutions for service difficulties when service experience warrants it, or when the CAA requires mandatory corrective action. If the holder is no longer capable or if the Type Certificate is transferred to another holder, the CAA should take action in accordance with the guidance material provided under Part III, Sub-Chapter 4.2, Interpretation of the Organization Responsible for the Type Design. In the case of the Type Certificate being transferred to another holder, the CAA should ensure that the new holder is capable of fulfilling the minimum responsibilities described herein.
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适航手册 AIRWORTHINESS MANUAL(30)
