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c)  Final Phase – is usually initiated by conducting a final TCB meeting. The timing of the final TCB meeting is commonly scheduled either near the completion, or following completion, of the demonstration of compliance with the certification basis and successful performance of all ground and flight testing. The final TCB meeting should provide for the:
1)  review of all outstanding items on which there may be some question of compliance with the agreed certification basis; 
2)  establishment of the type certification data sheet items and aeroplane flight manual or equivalent document items; 
3)  determination of the status of any outstanding technical data; and
4)  establishment of a TCB position on their readiness, which may be contingent on the disposition or full completion of all outstanding items, to recommend to the DCA the issuance of a Type Certificate for the aeronautical product for which an application was submitted,
1.2.5.3.2. As stated in 1.2.5.3.1 a) 5), the TCB may require the formation of special compliance teams for the purpose of conducting special certification reviews of potential problem areas. The special certification review normally involves an in-depth, comprehensive study of complex, controversial or troublesome aircraft design features, or aircraft component problems associated with airworthiness determination of an aircraft, engine, propeller or aircraft component. Examples of potential safety problem areas for which such a special review may be appropriate include the following:
a)  complex or unique design features;
b)  advanced state-of-the-art concepts in design, quality or manufacturing processes;
c)  features that may require special conditions;
d)  troublesome features used in similar previous designs requiring further analysis or evaluation;
e)  compliance areas critical to safety and requiring judgment evaluations;
f)  undesirable maintainability characteristics;
g)  equivalent safety proposals with potential for major effects on safety; or
h)  complicated interrelationships of unusual features.
1.2.5.3.3 Special certification reviews are normally conducted with the assistance of specialists groups composed of members of the concerned divisions of the CAA. The groups may seek assistance from other governmental agencies, outside consulting firms and industry, as necessary, to obtain technical expertise for conducting a thorough evaluation. The group’s findings and recommendations are submitted to the Chairman of the TCB.
1.2.5.4 Record-keeping of TCB activities
Records should be made and kept for each TCB meeting that clearly identify, among other things, all decisions taken, the certification basis, agreements reached, status of action items, tasking and deliverables of persons, and commitments on schedules. Copies of such records should be distributed promptly to the meeting attendees and to all affected and concerned persons. Each item or subject discussed should be summarized under a separate heading and the problem stated clearly, followed by any conclusions and recommendations. Persons required to take action on specific matters by a critical due date should be identified clearly. Based on the knowledge of the design features or potential safety problems obtained from the TCB meetings, those certification areas for which a special certification review is required should also be identified in the records.
1.3 Type Certification activities: State of Design
1.3.1 General
1.3.1.1 The main objective of the type certification process is for a State to determine for itself the overall compliance of the type design of an aeronautical product with their applicable airworthiness requirements. This objective applies to both the State of Design and State of Registry. The State of Design has prime responsibility for the original or initial approval of the aeronautical product. A State of Registry has a responsibility to establish that there is satisfactory evidence of design approval of an aircraft being issued a Certificate of Airworthiness under Annex 8. While Annex 8 sets the minimum international airworthiness Standards in the form of general design objectives, it is not sufficient by itself to be the sole basis for the approval of a type design and issuance of a Type Certificate. The ability to issue the Type Certificate referred to in Annex 8 is conditioned upon States having comprehensive and detailed airworthiness (design) standards for the aircraft, engine and/or propeller that include or implement the design objectives of Annex 8.
　
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