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j)  compliance with structural integrity programmes  for aeroplanes.
4.1.3 The structural integrity programme for aeroplanes (sometimes referred to as the ageing aeroplane programme) may include the following, dependent on the structural design criteria:
a)  supplementary structural inspection programme,
b)  corrosion prevention and control programme;
c)  service bulletin review and mandatory modification programme;
d)  repairs review for damage tolerance; and/or
e)  widespread fatigue damage (WFD) review.
4.2. Organization responsible for the type design
4.2.1  Type certificate holder
4.2.1.1 Annex 8, Part II, Chapter 4 refers to the transmittal of information relating to the continuing airworthiness of the aircraft to the type design organization of that aircraft. Normally, this organization will be the holder of the Type Certificate for the aircraft type; in some cases (prior to Amendment 98 of Annex 8), it will be the holder of an equivalent document certifying approval of the type design by the certificating authority.
4.2.1.2 The reference to transmittal of this information to such an organization necessitates that:
a)  for aeroplane over 5 700 kg maximum certificated take-off mass and helicopters over 3 175 kg certificated take-off mass engaged in international civil aviation, an organization holding the Type Certificate (or equivalent document) will exist throughout the operational life of the aircraft type; and
b)  the holder of the Type Certificate (or equivalent document) will be in possession of the type design and type certification data and have the competence to use that data as necessary for the continuing airworthiness of the aircraft.
Note 1.— Throughout the remainder of this Chapter 4, the “organization responsible for the type design” will be referred to as the “Type Design Organization” for ease of reading.
 Note 2.—  When appropriate, States should also update their information concerning design
organizations responsible for type design under their jurisdiction that is listed in ICAO Circular 95 —
The Continuing Airworthiness of Aircraft in Service.
4.2.2 Transfer of the Type Certificate to a new holder
4.2.2.1 Cases can be envisaged where the holder of a Type Certificate (or equivalent document) may transfer legal ownership of a type design to a new owner, for business purposes. If the new owner remains located within the same geographical jurisdiction as the previous owner, then the State of Design remains unchanged. However, if the new owner is located under the geographical jurisdiction of another Contracting State, then there is also a change in the designation of the State of Design. The activities involving the transfer of a Type Certificate should be regulated by the appropriate CAA to ensure that the continuing airworthiness responsibilities under Annex 8, for the affected type design, are maintained or retained by the new holder and/or State of Design.
4.2.2.2 The CAA responsible for the new holder will need to be satisfied that all necessary background data, including the type design data and type certification data, have been transferred to the new holder and that the new holder is able to support the continuing airworthiness of the aircraft type. Where the transfer involves another Contracting State, the CAAs of the previous and new State of Design will need to resolve any problems arising from any different requirements and procedures for type certification in the new State of Design. In addition, if the aircraft is manufactured under the jurisdiction of another Contracting State, Annex 8, Part II, Chapter 4 requires that both the State of Design and the State of Manufacture establish an agreement that ensures the manufacturing organization cooperates with the type design organization in assessing information received on service experiences. 
　
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