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g)  the date of issuance, the original signature and seal (as applicable) of the issuing CAA.
1.3.5.3.2 The holder of the Type Certificate is the organization that has responsibility for the design of the aircraft. In the case of jointly designed aircraft, or in the case where design work is subcontracted to other organizations, the certificating authority will require one organization to be responsible for the type design.
1.3.5.3.3 A Type Certificate is effective until surrendered, suspended or revoked, or until a termination date is otherwise established by the issuing CAA.
1.3.5.4  Type Certificate data sheet
The Type Certificate data sheet is an integral part of, and issued at the same time as, the Type Certificate. The data sheet is prepared by the ACD and identifies in detail the certification basis, the operating conditions, limitations, and maintenance requirements that have been specified as mandatory in the approval of the type design. When several models are included in the same Type Certificate, information should be repeated for each model, except for such common data as reference datum, mean aerodynamic chord, levelling means, control surface movements, etc. An example of a Type Certificate Data Sheet is shown in Appendix B to this Chapter.
1.3.5.5  Documents necessary for approved type design
The conditions and limitations of the approved type design are specified in the CAA-approved Type Certificate data sheet. This information is part of the Type Certificate and is mandatory for the safe operation and continued airworthiness of the aircraft. The Type Certificate data sheet also references other information that is necessary for the proper operation and maintenance of the aircraft in service. This other information may be developed concurrently during the type certification process and approved after the issuance of the Type Certificate. The following information should be documented in a form and manner prescribed by the CAA, and subsequently made available to operators of the aircraft:
a)  limitations and procedures necessary for a safe flight operation because of design, operating, or handling characteristics, including those necessary to maintain compliance with the approved noise limits, if applicable. This information is usually provided in the aircraft flight manual, mass and balance manual, and master minimum equipment list;
b) limitations and procedures necessary for a safe ground operation and maintenance such as:
1)  mandatory replacement times for structural parts, structural inspection intervals, and related structural inspection procedures (usually identified in an airworthiness limitations document);
2)  mandatory maintenance tasks to be performed at pre-determined intervals, as established during the type certification process (usually identified as certification maintenance requirements); and
3)  instructions for continued airworthiness of the aircraft, engine and propeller (usually contained in maintenance review board report), descriptive data and accomplishment instructions for the maintenance, servicing, inspection and repair (usually contained in the aircraft/engine/propeller maintenance manuals, engine installation manual, and structural repair manual).
c)  a continuing structural integrity programme, including specific information concerning corrosion prevention and control, necessary for the continued airworthiness of aeroplanes over 5 700 kg maximum certificated take-off mass (as required in Annex 8, Part II).
Note.— The publication of CAA-approved data in any document furnished to aircraft operators should provide for the clear identification or distinction of such approval when such document also contains other data or information accepted or not approved by the CAA. 
1.3.5.6 Other information necessary for operation of aircraft
Other information necessary for the operation of the aircraft under Annex 6 are typically developed concurrently with the type certification process, although this information or data are not requirements for the issuance of a Type Certificate. As with airworthiness-related data, this operation-related information should also be provided to operators of the aircraft. This information includes the:
　
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