Signature of AID Inspector Date
For complete aircraft, list applicable specification or Type Certificate Data Sheet numbers for the aircraft, engine and propeller. Applicable specifications or Type Certificate data sheet, if not attached to this Export Certificate, will have been forwarded to the appropriate governmental office of the importing country.
AID Form No. A/W . . . . . .
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CHAPTER 4.— CONTINUING AIRWORTHINESS OF AIRCRAFT
Note.— General information on the continuing airworthiness procedures followed in individual ICAO Contracting States is published in ICAO Circular 95 — The Continuing Airworthiness of Aircraft in Service.
4.1 Introduction to the concept of continuing airworthiness
4.1.1 Continuing airworthiness covers the processes that require all aircraft to comply with the airworthiness requirements in their type certification basis or imposed as part of the State of Registry’s requirements and are in a condition for safe operation, at any time during their operating life.
4.1.2 Under the control of the respective CAAs of the State of Design, the State of Registry and, when appropriate, the State of the Operator, continuing airworthiness includes the following:
a) design criteria which provide the necessary accessibility for inspection and permit the use of established processes and practices for the accomplishment of maintenance;
b) information that identifies the specifications, methods, and procedures necessary to perform the continuing airworthiness tasks identified for the aircraft and the tasks necessary to maintain the aircraft, as developed, by the type design organization; and publication of this information in a format that can be readily adapted for use by an operator;
c) adoption by the operator into its maintenance programme, the specifications, methods, and procedures necessary to perform the continuing airworthiness tasks identified for the aircraft and the tasks necessary to maintain the aircraft, using the information provided by the type design organization;
d) the reporting of faults, malfunctions, and defects and other significant maintenance and operational information by the operator to the type design organization in accordance with the requirements of the State of Registry and the State of the Operator;
e) the reporting of faults, malfunctions, and defects and other significant maintenance information by the maintenance organization to the type design organization in accordance with the requirements of the State having jurisdiction on the maintenance organization;
f) the analysis of faults, malfunctions, defects, accidents and other significant maintenance and operational information by the type design organization, the State of Design and the State of Registry and the initiation and transmission of information and recommended or mandatory action to be taken in response to that analysis;
g) consideration of the information provided by the type design organization and action on the information as deemed appropriate by the operator or the State of Registry, with particular emphasis on action designated as “mandatory”;
h) adoption and accomplishment by the operator of all mandatory requirements with particular emphasis on fatigue life limits and any special tests or inspections required by the airworthiness requirements of the type design of the aircraft or subsequently found necessary to ensure structural integrity;
i) adoption by the operator into its maintenance programme, supplemental structural inspection programmes and subsequent structural integrity programme requirements, taking into consideration the structural integrity programme for aeroplanes recommended by the type design organization; and
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