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c)  Engineering inspection – any aspect of the type design, for which compliance with the certification item cannot be determined through review of drawings or reports, should receive an engineering compliance inspection. An engineering compliance inspection is to assure that an installation, and its relationship to other installations on a product, complies with the design requirements.
d)  Flight Test – for aircraft, an actual demonstration of flight capabilities and characteristics in accordance with an approved flight test plan.
1.3.4.4  Non-compliance
The ACD should notify the applicant in writing of any non-compliance found during the process of data review, inspections, ground and flight tests and, if it becomes necessary, the discontinuance of official type certification tests. The applicant should advise the ACD when the non-compliance finding has been resolved or when the cause of the discontinuance of the tests has been corrected and a resumption of the type certification tests is requested. The identification and resolution of non-compliance items should be properly documented and kept part of the record for the type certification project.
1.3.5  Certifying the type design
1.3.5.1  General
All findings of compliance made by the ACD, or its delegate, should be recorded or annotated in the certification compliance plan. When the applicant has demonstrated compliance and the ACD has found full compliance on all certification items, including the resolution of outstanding items, the plan is signed off and becomes the official certification compliance record for the type certification project. The certification compliance record serves as the satisfactory evidence specified under Annex 8, Part II, Section 1.4, Type Certificate, for the issuance of a Type Certificate. The approval of the type design, and subsequent issuance of a Type Certificate, means that:
a)  the type design meets all the relevant requirements specified in the certification basis, including special conditions issued by the CAA,
b)  all engineering and conformity inspections have been completed and the prototype product has been found to meet all pertinent requirements; and
c)  in the case of aircraft, the prototype has been test flown and found to comply with all the performance requirements of the pertinent airworthiness Standards.
1.3.5.2  Withholding approval of type design
There may exist a situation, although rare, where an applicant successfully demonstrated, and the ACD found, compliance with the certification basis but a known or suspected feature makes the aeronautical product unsafe, taking into account the category in which certification was requested. Notwithstanding the entitlement of the applicant for a Type Certificate, the ACD has a responsibility under Annex 8, Part II, 1.3.3 to withhold the approval or issuance of a Type Certificate for an aircraft if it is known or suspected to have unsafe features that are not specifically guarded against by the certification basis. The Type Certificate shall be denied if the applicant fails to correct the unsafe feature.
1.3.5.3 Issuance of a Type Certificate
1.3.5.3.1 A Type Certificate is issued by the CAA under Annex 8, Part II, Section 1.4, as evidence of approval of a type design. An example of a Type Certificate is shown in Appendix A to this Chapter. A Type Certificate usually contains the following information:
a)  the approval or Type Certificate number;
b)  the Type Certificate holder’s name and address;
c)  the aeronautical product identification (aircraft, engine, propeller model designation);
d)  the applicable airworthiness requirements, 
e)  a statement attesting compliance of the product with the applicable airworthiness requirements;
f)  a statement incorporating or referencing the Type Certificate Data Sheet, which defines the type design, as part of the approval; and
　
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