GM 21.A.93(c) Period of validity for the application.GM No 2 to 21.A.93(b)(1)(iii) Interaction of changes to the type design and changes to the master minimum equipment list (MMEL).GM No 1 to 21.A.93(b)(1)(iii) Interaction of changes to the type design and changes to operational suitability data (OSD).AMC 21.A.93(b) Certification programme for a change to a TC or an STC.Appendix A to GM 21.A.91 Examples of Major Changes per discipline.GM 21.A.91 Classification of changes to a type certificate (TC).21.A.91 Classification of changes to a type-certificate.21.A.90C Stand-alone changes to the Instructions for Continued Airworthiness.GM 21.A.90B Standard changes - Certification Specifications.SUBPART D - CHANGES TO TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES.AMC1 21.A.65 Continuing structural integrity programme for aeroplane structures.21.A.65 Continuing structural integrity for aeroplanes structures.GM to 21.A.62, 21.A.108 and 21.A.120B Availability of Operational Suitability Data.21.A.62 Availability of operational suitability data.21.A.51 Duration and continued validity.GM 21.A.35(f)(2) Flying Time for Function and Reliability Testing.GM 21.A.35(f)(1) Flying Time for Function and Reliability Testing.GM 21.A.35(b)(2) Objective and Content of Function and Reliability Testing.GM 21.A.21(a)(3)(i) Clarification of the term ‘determined’.21.A.21 Requirements for the issuance of a type certificate or restricted type certificate.AMC 21.A.20(c) Compliance documentation.GM 21.A.20(b) Reporting on the compliance demonstration process.GM 21.A.20 Compliance demonstration process.21.A.20 Demonstration of compliance with the type certification basis, operational suitability data certification basis and environmental protection requirements.21.A.19 Changes requiring a new type-certificate.GM 21.A.15(e) and (f) Period of validity for the application for a type certificate (TC) or restricted type certificate (RTC).GM 21.A.15(c) Updates to the certification programme.GM No 2 to 21.A.15(d) Determination of type or variant.GM No 1 to 21.A.15(d) Application for the approval of operational suitability data – MMEL for ELA1 and ELA2.AMC 21.A.15(b)(5) Breakdown of the certification programme into compliance demonstration items (CDIs).Appendix A to AMC 21.A.15(b) Means of compliance codes.AMC 21.A.15(b) Content of the certification programme.GM 21.A.14(b) Eligibility for alternative procedures.AMC1 21.A.14(b) Demonstration of capability.SUBPART B - TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES.AMC1 21.A.7(c) Completeness and timely availability of the ICA.GM4 21.A.7(b) Integration of ICA between products (aircraft, engines, propellers).GM3 21.A.7(b) Approval status of the manual for a component or article.GM1 21.A.7(b) Other persons required to comply.AMC1 21.A.7(b) Identification of a complete set of instructions for continued airworthiness (ICA).GM3 21.A.7(a) Non-ICA supplier data (e.g.GM2 21.A.7(a) Determination of which supplier data is part of the ICA.GM1 21.A.7(a) Scope of ICA, their publication format and typical ICA data.AMC3 21.A.7(a) DAH responsibility to check the supplier data which is part of the ICA or referenced with the ICA.21.A.7 Instructions for continued airworthiness.GM1 21.A.5 Repair designs and record keeping. ![]()
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