Browse all sections of Initial Airworthiness and Environmental Protection (748/2012) (Nov 2025)

• 21L.A.85 Demonstration of compliance
• GM3 21L.A.9(b) Instructions for continued airworthiness
• GM1 21L.B.12 Exchange of information
• 21.A.108 Availability of operational suitability data
• 21.B.433 Findings and corrective actions
• GM1 21L.A.223(a) Classification of repairs designs to an aircraft for which design compliance has been declared
• GM1 21L.B.24(b)
• AMC1 21L.A.227(a) Compliance activities for declaring compliance of a major repair design
• GM2 21L.A.9(a) Instructions for continued airworthiness
• 21.B.420 Investigation
• 21L.B.15 Immediate reaction to a safety problem
• AMC1 21.A.130(b)(4)(i) Statement of conformity
• AMC1 21L.A.25(a)
• AMC1 21.A.804(b) Identification of parts and appliances
• 21L.A.193 Release of parts for installation
• AMC1 21L.A.27(d) Requirements for the issuance of a type certificate
• AMC1 21.A.709(b) Application for the approval of flight conditions
• AMC 21L.B.241(a)(1) and 21L.B.242(a)(1) Critical design review of the design and physical inspection and assessment of the aircraft
• SUBPART M -- DESIGN OF REPAIRS TO TYPE-CERTIFIED PRODUCTS
• SUBPART J -- DECLARED DESIGN ORGANISATIONS
• 21L.B.63 Registration of a declaration of design compliance
• 21L.A.26 Type design
• 21L.B.171 Investigation
• 21.A.727 Obligations of the holder of a permit to fly
• GM 21.A.708(d) Control of aircraft configuration
• (SUBPART C -- NOT APPLICABLE)
• GM1 21L.A.83(b) Demonstration of design capability
• AMC2 21.B.25 Management system
• GM1 to 21L.A.127(c) Obligations of the declared production organisation
• GM No 1 to 21.A.101(g) Establishment of the operational suitability data (OSD) certification basis for changes to type certificates (TCs)
• 21L.A.123 Declaration of production capability
• 21.A.127 Tests: aircraft
• AMC1 21L.A.107(e) Declaration of design compliance for a major change
• 21L.A.22 Eligibility
• 21L.A.272 Eligibility
• 21.B.432 Oversight programme
• AMC1 21.B.120(a) Initial certification procedure
• 21.A.139A Information security management system
• 21.B.431 Oversight principles
• GM2 21L.A.273(a)
• 21L.B.46 Investigation
• AMC No 1 to 21.B.100(b) Level of involvement (LoI) in projects for minor changes and minor repairs
• 21.A.151 Terms of approval
• 21L.B.223 Continuing airworthiness oversight of a repair design for which design compliance has been declared
• 21.A.51 Duration and continued validity
• GM 21.A.126(b)(2) Production inspection system - Suitable storage and protection
• GM1 21L.A.164(b) Transferability and re-issuance of noise certificates and restricted noise certificates within Member States
• GM 21.B.107 and 21.B.111 Operational suitability data (OSD) considerations for the approval of changes to type certificates (TCs) or supplemental type certificates (STCs)
• AMC1 21.A.265(a) Obligations of the holder
• GM1 21.1 Competent authority
• 21.B.435A Changes to the information security management system
• AMC 21L.B.241(a)(1) and 21L.B.242(a)(1) Critical design review of the design and physical inspection and assessment of the aircraft
• 21.B.105 Type-certification basis, environmental protection requirements and operational suitability data certification basis for a major change to a type certificate
• 21.A.606 Requirements for the issuance of an ETSO authorisation
• AMC2 21.A.3A(a) Reporting system
• AMC1 21L.A.65(b) Application for a change to a type certificate
• AMC1 21L.A.44(a) Compliance activities for a declaration of design compliance
• GM No 3 to 21.A.15(d) OSD content
• AMC1 21.A.3A(e) Reporting system
• 21L.A.29 Transferability of a type certificate
• AMC1 21L.A.227(c)
• AMC1 21L.A.44(c)
• AMC1 21.B.115(b),(c) and 21.B.215(b),(c) Means of compliance
• SUBPART H -- CERTIFICATES OF AIRWORTHINESS AND RESTRICTED CERTIFICATES OF AIRWORTHINESS
• SUBPART P -- PERMIT TO FLY
• AMC1 21.A.139(d)(2) Production management system
• Appendix A to AMC1 21L.A.85 Demonstration of compliance
• AMC 21.A.608 Declaration of Design and Performance
• GM 21.B.225(a) Objective evidence
• AMC1 21L.A.25(e)(1) Demonstration of compliance
• AMC1 21L.B.16(d) Management system
• SUBPART C -- DECLARATIONS OF DESIGN COMPLIANCE
• 21.A.181 Duration and continued validity
• GM1 21L.A.175(d) Resources of the declared design organisation
• SUBPART B -- TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES
• GM1 21.B.85(a) Applicable environmental protection requirements for a type certificate or restricted type certificate
• AMC1 21L.A.9(d) Completeness and timely availability of the Instructions for Continued Airworthiness
• 21.A.90B Standard changes
• 21L.B.186 Changes to declarations
• SUBPART K -- PARTS (Reserved)
• 21L.A.65 Application for a change to a type certificate
• 21L.A.145 Transferability and re-issuance of a certificate of airworthiness and of a restricted certificate of airworthiness within Member States
• Instructions for the use of EASA Form 1
• GM1 21L.A.208 Requirements for the approval of a major repair design
• GM1 21L.B.162(d) Issuance or amendment of a certificate of airworthiness or a restricted certificate of airworthiness
• GM 21.A.15(e) and (f) Period of validity for the application for a type certificate (TC) or restricted type certificate (RTC)
• GM1 21.B.115 and 21.B.215 Means of compliance
• AMC1 21.A.139(c)(4)(ii) Production management system
• AMC No 2 to Appendix XII - Conditions for appointment of Lead Flight Test Engineers (LFTEs) - Medical fitness
• GM1 21.A.130, 21.A.163 and 21.A.165 Performance of tasks in real time for the issuance of an 'EASA Form 1' for prototype and new parts, appliances and products other than complete aircraft, using information and communication technologies (ICT)
• AMC1 21L.A.226(e) Declaration of design compliance of major repair designs
• GM1 21.B.225(b) Findings and corrective actions
• 21L.A.12 Means of compliance
• 21.A.145 Resources
• 21.A.247 Changes in the design management system
• 21.A.203 Eligibility
• GM1 21.A.147 Changes to the production management system
• Appendix XII -- Categories of flight tests and associated flight test crew qualifications
• AMC2 21L.B.144(a) and 21L.B.184(a) Oversight programme
• 21L.B.161 Investigation
• GM 21.A.708(b)(6) Continuing airworthiness
• 21.A.723 Duration and continued validity
• 21L.B.206 Unrepaired damage
• 21L.B.141 Initial oversight investigation
• AMC1 21L.B.21(c) Findings and corrective actions
• GM1 21L.A.125(a) Resources of the declared production organisation
• 21.B.100 Level of involvement
• SUBPART I -- NOISE CERTIFICATES AND RESTRICTED NOISE CERTIFICATES
• GM1 21L.B.43(a) Type-certification basis for a type certificate
• AMC1 21.A.145(c)(2) Resources
• GM1 21L.A.173(b) Declaration of design capability
• SUBPART A -- GENERAL PROVISIONS
• 21.B.10 Oversight documentation
• 21L.A.64 Eligibility
• 21.A.131 Scope
• GM1 21.A.3B(b) Failures, malfunctions and defects
• AMC1 21.A.245(a) Resources
• GM No 2 to 21.A.121 Applicability - Applicable design data
• 21L.B.41 Certification specifications
• AMC to 21.A.143, 21.A.243, 21.A.14(b), 21.A.112B(b) and 21.A.432B(b) Flight Test Operations Manual (FTOM)
• GM 21.A.126(a)(4) Production inspection system - Applicable design/production data procedures
• GM1 21L.A.252(b)(2) Identification of parts
• AMC1 21.A.145(a) Resources
• GM1 21L.A.226(c) Declaration of design compliance of major repair designs
• 21L.B.202 Investigation and issuance of an approval for a minor repair design
• GM No 2 to 21.A.165(c) Obligations of holder - Conformity with type design
• AMC 21.B.100(a) and 21.A.15(b)(6) Level of involvement (LoI) in a certification project for a type certificate (TC), a major change to a TC, a supplemental type certificate (STC), a major repair design or European technical standard order (ETSO) authorisation for an auxiliary power unit (APU)
• 21L.B.221 Initial oversight investigation of a declaration of design compliance of a major repair design to an aircraft for which design compliance has been declared
• GM No 1 to 21.A.128 Acceptable functional test - Engines
• 21.A.3A Reporting system
• AMC1 21L.A.125(d)(1) Resources of the declared production organisation
• GM 21.A.711(e) Additional conditions and restrictions
• SUBPART B -- TYPE CERTIFICATES
• Appendix A to GM1 21L.A.63 Classification of changes to a type certificate
• 21L.B.22 Enforcement measures
• GM1 21L.A.174(b)(1) Management system for design
• GM1 21.A.139, 21.A.239, 21.B.120, 21.B.140, 21.B.220, and 21.B.240 The use of information and communication technologies (ICT) for performing remote audits
• 21.A.710 Approval of flight conditions
• GM1 21.A.165(c)(3)(i) Obligations of the holder
• AMC1 21.B.222(b)(1) Oversight programme
• AMC1 21.A.139(d) Production management system
• Appendix A to AMC1 21L.A.108(a) Compliance activities for declaring compliance of a major change
• 21.A.435 Classification and approval of repair designs
• GM1 21L.A.125(b) Resources of the declared production organisation
• Article 2 Certification of products, parts, appliances, control and monitoring unit and control and monitoring unit components
• 21L.B.185 Oversight activities
• GM1 21.B.220(a) Initial certification procedure
• 21L.B.62 Initial oversight investigation
• AMC1 21.B.25(a)(1) Management system
• SUBPART K -- PARTS
• GM1 21L.A.66(f) Demonstration of compliance
• AMC1 21.B.220 Initial certification procedure
• AMC1 21L.B.83(c) Investigation of a major change to a type certificate
• AMC1 21L.B.144(a) and 21L.B.184(a) Oversight programme
• SUBPART J -- DESIGN ORGANISATION APPROVAL
• 21L.A.253 Identification of products
• GM1 21.A.5(a) and (b) Record-keeping
• AMC1 21L.A.7 Record-keeping
• 21L.A.108 Compliance activities for declaring compliance of a major change
• AMC1 21.A.124 Application
• GM 21.A.431A(e) Repairs to European technical standard order (ETSO) articles other than auxiliary power units (APUs)
• AMC1 21L.A.3(e) Reporting system
• GM1 21L.A.174(d) Management system for design
• GM to 21.A.62, 21.A.108 and 21.A.120B Availability of Operational Suitability Data
• GM2 21L.A.9(b) Instructions for continued airworthiness
• GM1 21L.A.61 Scope
• 21.A.135 Issuance of production organisation approval
• AMC1 21.A.239(d) Design management system
• 21.A.804 Identification of parts, appliances, and control and monitoring unit (CMU) components
• GM 21.A.126(b)(1) Production inspection system - Inspection of parts in process
• AMC 21.A.15(a) Form and manner
• 21L.B.18 Changes in the management system
• 21.A.147 Changes in the production management system
• GM 21.B.107 and 21.B.111 Operational suitability data (OSD) considerations for the approval of changes to type certificates (TCs) or supplemental type certificates (STCs)
• 21.A.251 Terms of approval
• 21.B.125 Findings and corrective actions
• AMC1 21L.A.192(a)(4) Showing of compliance
• 21.A.163 Privileges
• 21L.1 Scope
• 21.A.14 Demonstration of capability
• Transitional provisions from regulations amending Regulation (EU) No 748/2012
• 21.B.325 Issuance of airworthiness certificates
• GM2 21.B.15(b) Information to the Agency
• SUBPART P - PERMIT TO FLY
• Appendix I to GM 21.A.101 Related documents
• GM1 21L.A.163(b)(2) Application
• 21L.B.20 Record-keeping
• AMC1 21L.B.13(b) Information to the Agency
• AMC1 21L.B.141 Initial oversight investigation
• GM3 21L.B.13(b) Information to the Agency
• 21L.A.1 Scope
• Article 6 Continued validity of parts and appliances certificates
• AMC1 21.B.432(a) and (b) Oversight programme
• Note from the editor
• GM1 21.B.75 Special conditions
• GM1 21L.A.67(c) Requirements for the approval of a minor change to a type certificate
• AMC1 21L.A.105(a) Declaration of design compliance for minor changes
• GM2 21.A.3A(a)(1) and (b)(1) Reporting system
• Appendix C to GM 21.A.101 A method to determine the changed and affected areas
• GM1 21L.A.203(a) Classification of repair designs to a type-certified product
• Appendix XI - EASA Form 65 - Letter of Agreement for production without a production organisation approval
• Appendix IV -- EASA Form 53B -- Certificate of release to service
• AMC1 21.A.609(c) and (d) Obligations of holders of ETSO authorisations
• 21.B.109 Type-certification basis, environmental protection requirements and operational suitability data certification basis for a supplemental type certificate
• GM 21.A.97(b) Requirements for the approval of a major change
• 21.A.725 Renewal of permit to fly
• GM1 21L.A.143(c)(1)(ii) Application for a certificate of airworthiness or a restricted certificate of airworthiness
• 21.A.35 Flight Tests
• AMC No 1 to 21.A.263(c)(5), (8) and (9) Scope and criteria
• GM1 21L.2 Competent authority
• GM 21.A.91 Classification of changes to a type certificate
• 21L.A.24 Application for a type certificate
• AMC1 21.A.239(d)(2) Design management system
• 21L.A.161 Scope
• AMC1 21L.A.24(b)(4) Application for a type certificate
• 21.A.112A Eligibility
• AMC1 21L.B.16(a)(5) Management system
• GM 21.A.20(b) Reporting on the compliance demonstration process
• Appendix A to AMC 21.A.15(b) Means of compliance codes
• GM 21.A.14(b) Eligibility for alternative procedures
• Annex III
• GM1 21L.A.7 Record-keeping
• 21.A.713 Changes
• GM1 21L.A.25(f) Demonstration of compliance
• 21L.A.165 Continued validity of a noise certificate and of a restricted noise certificate
• GM1 21L.A.273(c) Production control system
• GM1 21L.B.161(a)(6) Investigation
• Annex II
• AMC1 21L.A.128 Notification of changes and cessation of activities
• 21.A.703 Eligibility
• AMC1 21L.A.208(c) Requirements for the approval of a major repair design
• AMC4 21.B.431 Oversight principles
• GM1 21L.B.161(c) Investigation
• GM2 21.A.139(d)(1) Production management system
• AMC1 21L.B.20(a) Record-keeping
• 21L.B.64 Continuing airworthiness oversight of aircraft for which design compliance has been declared
• AMC1 21.A.263(c)(6) Privileges
• GM1 21.B.125(b) Findings and corrective actions
• AMC 21.A.93(b) Certification programme for a change to a TC or an STC
• AMC1 21L.A.9(a) Instructions for continued airworthiness
• 21L.A.67 Requirements for the approval of a minor change to a type certificate
• AMC1 21L.A.85(e)(3) Demonstration of compliance
• AMC1 21.A.139(c)(1) Production management system
• 21L.A.205 Application for the approval of a repair design to a type-certified product
• GM 21.A.124(b)(1)(ii) Certification or approval needed in advance of the issue of a POA
• GM2 21.B.125(b) and 21.B.225(b) Findings and corrective actions
• GM1 21L.A.124(b)(2)(xiii) Management system for production
• AMC1 21L.A.84(b)(1) Application for a supplemental type certificate
• Article 3 Continued validity of type-certificates and related certificates of airworthiness
• 21L.B.16 Management system
• GM1 21.B.55 Record-keeping
• 21.A.134A Means of compliance
• 21L.A.84 Application for a supplemental type certificate
• GM1 21L.A.101 Scope
• SUBPART Q -- IDENTIFICATION OF PRODUCTS, PARTS, APPLIANCES, CONTROL AND MONITORING UNITS (CMUs) AND CMU COMPONENTS
• SUBPART P -- PERMIT TO FLY
• Appendix F to GM 21.A.101 The use of service experience in the exception process
• 21L.A.8 Manuals
• 21.A.11 Scope
• 21L.A.252 Design of markings
• GM1 21L.A.43(b)(10) Declaration of design compliance
• GM1 21.A.239(d) Design management system
• 21L.B.122 Registration of a declaration of design compliance for a major change to an aircraft design
• SUBPART D -- CHANGES TO TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES
• GM1 21L.A.125(c)(4) Resources of the declared production organisation
• GM1 21L.A.275(g) Obligations of a natural or legal person issuing a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1)
• AMC No 3 to Appendix XII - Demonstration of compliance with competence level 1 or level 2 requirements
• AMC1 21L.A.208 Requirements for the approval of a major repair design
• 21L.A.204 Eligibility
• AMC 21.A.15(b) Content of the certification programme
• 21L.B.204 Issuance of an approval of a major repair design
• SUBPART A -- GENERAL PROVISIONS
• 21L.B.85 Continuing airworthiness oversight of changed products for which a type certificate has been issued
• AMC3 21L.A.9(a) Instructions for continued airworthiness
• Article 7a Operational suitability data
• AMC3 21.B.25(a)(3) Management system
• 21.A.92 Eligibility
• 21L.A.91 Changes to a part of a product covered by a supplemental type certificate
• GM2 21L.A.44(g) Compliance activities for a declaration of design compliance
• 21.A.443 Limitations
• SUBPART A -- GENERAL PROVISIONS
• SUBPART F -- PRODUCTION WITHOUT PRODUCTION ORGANISATION APPROVAL
• 21.B.425 Issuance of noise certificates
• AMC No 1 to 21.A.129(c) Obligations of the manufacturer - Conformity of prototype models and test specimens
• GM1 21.B.326(a)(3) and (b)(3) Certificate of airworthiness
• AMC to 21.A.143, 21.A.243, 21.A.14(b), 21.A.112B(b) and 21.A.432B(b) Flight Test Operations Manual (FTOM)
• GM1 21L.A.192(a)(4) Showing of compliance
• GM1 21L.A.274(b) Issuance of a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1)
• 21L.A.101 Scope
• 21L.A.122 Eligibility
• AMC2 21.B.431 Oversight principles
• 21L.A.23 Demonstration of design capability
• AMC1 21L.A.24(a) Application for a type certificate
• 21.A.611 Design changes
• 21.A.172 Eligibility
• 21L.A.207 Requirements for the approval of a minor repair design
• AMC 21.A.606(d) Declaration
• GM1 21.A.149 and 21.A.249 Transferability
• AMC 21L.B.241(a)(2) and 21L.B.242(a)(2) Physical inspection and assessment of the aircraft in order to ensure that the aircraft is capable of safe flight, and that flight testing can be conducted safely (physical inspection and safety review)
• 21L.B.183 Oversight
• 21.A.15 Application
• 21.B.222 Oversight programme
• GM1 21L.A.202 Standard repairs
• AMC1 21.A.239(c) Design management system
• 21.B.240A Changes to the information security management system
• SUBPART G - DECLARED PRODCUTION ORGANISATIONS
• AMC1 21L.A.241(b)(2)
• 21.A.95 Requirements for approval of a minor change
• GM No 1 to 21.A.121 Applicability - Individual product, part or appliance
• AMC3 21.B.431 Oversight principles
• Appendices to ANNEX Ib (Part 21 Light)
• 21.A.91 Classification of changes to a type certificate
• GM1 21L.A.124(b)(2)(viii) Management system for production
• GM1 21L.A.44(f) Compliance activities for a declaration of design compliance
• GM1 21L.A.124(b)(2)(vi) Management system for production
• GM1 21L.A.174(b)(3)
• (SUBPART L -- NOT APPLICABLE)
• GM1 21L.B.61(b) Detailed technical specifications for declarations of design compliance
• 21L.B.253 Oversight activities
• 21.B.320 Investigation
• AMC1 21.B.55(a) Record-keeping
• AMC1 21L.A.207 Requirements for the approval of a minor repair design
• AMC No 2 to 21.A.133(b) and (c) Eligibility - Link between design and production organisations
• 21.A.265 Obligations of the holder
• SUBPART E -- SUPPLEMENTAL TYPE-CERTIFICATES
• SUBPART C -- DECLARATIONS OF AIRCRAFT DESIGN COMPLIANCE
• 21L.A.273 Production control system
• GM1 21.B.85 Applicable environmental protection requirements for a type certificate or restricted type certificate
• 21L.A.69 Approval of a change to a type certificate under a privilege
• AMC1 21L.B.252 Oversight programme
• 21L.A.223 Classification of repair designs to an aircraft for which design compliance has been declared
• AMC1 21.A.433(a)(5) Requirements for the approval of repairs to large aeroplanes subject to point 26.302 of Part-26
• GM2 21L.B.12 Exchange of information
• GM 21.A.165(a) Obligations of the holder - Basic working document
• 21.A.207 Amendment or modification
• GM1 21L.A.163(c)(1)(ii) Application
• GM 21.A.431B Standard repairs - Certification Specifications
• GM1 21L.A.176 Scope of work
• AMC1 21.A.5 (d) & (e) Record-keeping
• GM 21.A.20(d) Final statement
• AMC1 21.B.430 Initial certification procedure
• GM 21.A.21(b), 21.A.95(c), 21.A.97(c), 21.A.115(c), 21.B.103(b), 21.B.107(b) and 21.B.111(b) Approval of operational suitability data (OSD)
• 21.A.5 Record-keeping
• 21L.A.25 Demonstration of compliance
• 21L.A.171 Scope
• AMC1 21L.B.83(d) Investigation of a major change to a type certificate
• GM2 21L.B.13(b) Information to the Agency
• 21L.A.11 Findings and observations
• Appendix E to GM 21.A.101 Procedure for evaluating material contribution to safety or impracticality of applying latest certification specifications to a changed product
• 21L.B.47 Issuance of a type certificate
• Appendix I -- EASA Form 1 -- Authorised Release Certificate
• 21.B.65 Suspension, limitation and revocation
• AMC1 21.B.222 Oversight programme
• GM2 21.B.125(b) and 21.B.225(b) Findings and corrective actions
• (SUBPART C -- NOT APPLICABLE)
• 21L.A.62 Standard changes
• Appendix J to GM 21.A.101 Definitions and terminology
• AMC 21L.B.62(b) Physical inspection and assessment of the first article of a given aircraft in the final configuration (first-article inspection) prior to the registration of a declaration of design compliance
• AMC1 21L.A.66 Demonstration of compliance
• GM 21.A.804(a)(1) Identification of parts and appliances
• SUBPART D -- CHANGES TO TYPE CERTIFICATES
• AMC 21.A.148 Changes of location - Management during change of location
• GM 21.A.127 Approved production ground and flight tests
• GM1 21L.A.3(a)(1)
• GM1 21.A.139, 21.A.239, 21.B.120, 21.B.140, 21.B.220, and 21.B.240 The use of information and communication technologies (ICT) for performing remote audits
• GM No 1 to 21.A.125B(a) Uncontrolled non-compliance with applicable design data
• 21L.A.173 Declaration of design capability
• SUBPART I -- NOISE CERTIFICATES
• GM1 21.A.239(d)(3) Design management system
• AMC1 21.A.7(b) Identification of a complete set of instructions for continued airworthiness (ICA)
• 21L.A.210 Obligations of a holder of a repair design approval
• 21L.2 Competent authority
• GM 21.A.126(a)(1) Production inspection system - Conformity of supplied parts, appliances and material
• GM 21.A.713 Changes
• 21L.A.82 Eligibility
• AMC1 21L.B.121 Initial oversight investigation of a declaration of design compliance of a major change to the design of an aircraft for which design compliance has been declared
• 21L.A.5 Collaboration between design and production
• 21L.A.206 Demonstration of compliance
• GM 21.A.90A Scope
• 21L.B.24 Means of compliance
• 21L.B.123 Continuing airworthiness oversight of a changed aircraft for which design compliance has been declared
• 21L.A.228 Obligations of the declarant of a declaration of design compliance of a repair design
• 21L.A.227 Compliance activities for declaring compliance of a major repair design
• GM1 21.A.125B(a), 21.A.158(a) and 21.A.258(a) Findings and observations
• Article 12 Entry into force
• Cover regulation
• AMC1 21L.A.108(c)
• GM1 21.A.804(a)(3) Identification of parts and appliances
• GM1 21L.B.16(a)(2) Management system
• GM1 21L.A.21 Scope
• 21.B.82 Operational suitability data certification basis for an aircraft type-certificate or restricted type-certificate
• AMC1 21.B.433(d) Findings and corrective actions
• AMC 21.A.130(c)(1) Initial transfer of ownership
• GM 21.A.445 Unrepaired damage
• GM 21.B.82 Operational suitability data (OSD) certification basis for an aircraft type certificate (TC) or restricted type certificate (RTC)
• GM No 2 to 21.A.708(c) Substantiations
• AMC 21.A.4 Transferring of information on eligibility and approval status from the design holder to production organisations
• AMC1 21L.B.143(b) Oversight
• GM 21.A.432B(b) Alternative procedures
• GM 21.B.325(a) Airworthiness certificates
• AMC1 21L.A.178 Notification of changes and cessation of activities
• 21.A.7 Instructions for continued airworthiness
• 21L.B.12 Exchange of information
• Article 7 Permit to fly
• 21.B.70 Certification specifications
• 21L.A.144 Obligations of the applicant for a certificate of airworthiness or a restricted certificate of airworthiness
• 21.B.115 Means of compliance
• GM No 1 to 21.A.125A(b) Letter of agreement - Contents of the Manual
• AMC2 21.A.122 Eligibility
• GM1 21L.A.44 Compliance activities for a declaration of design compliance
• GM1 21L.A.11(a) Findings and observations
• GM1 21.A.90C Stand-alone changes
• AMC1 21L.A.66(e)(3) Demonstration of compliance
• 21.A.604 ETSO authorisation for an auxiliary power unit (APU)
• AMC1 21.A.239(c)(5) Design management system
• GM1 21L.A.44(a) Compliance activities for a declaration of design compliance
• 21L.A.172 Eligibility
• SUBPART B -- TYPE CERTIFICATES
• 21.A.122 Eligibility
• 21L.A.70 Obligations for minor changes to a type certificate
• Appendix II -- EASA Form 15a, 15c and 15d -- Airworthiness Review Certificate
• AMC1 21.A.239(c)(3) and (4) Design management system
• SUBPART D -- CHANGES TO TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES
• 21.B.327 Restricted certificate of airworthiness
• AMC1 21.A.243(d) Handbook
• 21.A.9 Access and investigation
• GM1 21L.A.201 Scope
• 21.A.97 Requirements for approval of a major change
• AMC3 21.A.3A(a) Reporting system
• GM1 21.A.249 Transferability
• Appendix A to AMC1 21L.A.24(b) Means-of-compliance codes
• AMC1 21L.A.227(b) Compliance activities for declaring compliance of a major repair design
• GM1 21L.A.273(f) Production control system
• AMC to 21.A.143, 21.A.243, 21.A.14(b), 21.A.112B(b) and 21.A.432B(b) Flight Test Operations Manual (FTOM)
• Article 11 Repeal
• AMC1 21L.B.181 Initial oversight investigation
• 21.A.209 Transferability and re-issuance within Member States
• GM 21.A.125A(c) Letter of agreement - Assistance
• GM1 21L.A.23(a) Demonstration of design capability
• SUBPART M -- REPAIRS
• 21.B.25 Management system
• 21.A.431A Scope
• 21L.B.83 Investigation of a major change to a type certificate
• 21L.A.121 Scope
• 21L.A.68 Requirements for the approval of a major change to a type certificate
• AMC1 21L.A.108(f) Compliance activities for declaring compliance of a major change
• 21L.A.192 Showing of compliance
• 21.A.41 Type-certificate
• AMC1 21L.A.43(c) Declaration of design compliance
• 21.1. Competent authority
• GM 21.A.126 Production inspection system
• 21.A.432C Application for a repair design approval
• GM No 2 to 21.A.128 Acceptable functional test - Variable pitch propellers
• GM1 21L.A.44(g) Compliance activities for a declaration of design compliance
• GM2 21.B.85 Applicable environmental protection requirements for a type certificate or restricted type certificate
• 21L.A.126 Scope of work
• AMC2 21.B.25(a)(3) Management system
• GM2 21L.A.3(a)
• AMC 21.A.115 Requirements for the approval of major changes in the form of a supplemental type certificate (STC)
• 21.A.259 Duration and continued validity
• AMC1 21L.A.175(d) Resources of the declared design organisation
• 21.A.175 Language
• 21L.A.66 Demonstration of compliance
• SUBPART G -- PRODUCTION ORGANISATION APPROVAL
• GM1 21.B.120(c) Initial certification procedure
• Article 2a - Transitional arrangements for certificates previously issued under Annex I (Part 21)
• GM No 2 to 21.A.125A(b) Letter of agreement - Production Inspection System: Functional Tests
• AMC1 21L.A.173(c) Declaration of design capability
• GM 21.2 Scope
• AMC1 21.B.222(a) and (b) Oversight programme
• SUBPART G -- PRODUCTION ORGANISATION APPROVAL
• AMC1 21L.A.127(b) Obligations of the declared production organisation and AMC1 21L.A.177(b) Obligations of the declared design organisation
• AMC1 21.A.125B(c), 21.A.158(c), 21.A.258(c) Findings and observations
• GM No 4 to 21.A.165(c) Airworthiness Release or Conformity Certificate
• SUBPART H -- CERTIFICATES OF AIRWORTHINESS AND RESTRICTED CERTIFICATES OF AIRWORTHINESS
• GM1 21L.B.22 Enforcement measures
• AMC2 21.B.222(b) Oversight programme
• AMC1 21.B.432(b) Oversight programme
• GM No 1 to 21.A.125A Letter of agreement - Meaning of individual
• 21.A.6 Manuals
• 21.A.109 Obligations and EPA marking
• SUBPART H -- CERTIFICATES OF AIRWORTHINESS AND RESTRICTED CERTIFICATES OF AIRWORTHINESS
• GM1 21L.A.252(b)(2)(iii) Identification of critical parts
• AMC1 21.B.430(e) Initial certification procedure
• AMC 21.B.100(a) and 21.A.15(b)(6) Level of involvement (LoI) in a certification project for a type certificate (TC), a major change to a TC, a supplemental type certificate (STC), a major repair design or European technical standard order (ETSO) authorisation for an auxiliary power unit (APU)
• 21.A.708 Flight conditions
• AMC1 21L.B.144(d)
• GM1 21L.A.273(h) Production control system and 21L.A.275(e) Obligations of a natural or legal person issuing a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1)
• SUBPART R - STATEMENT OF CONFORMITY FOR AIRCRAFT AND AUTHORISED RELEASE CERTIFICATES (EASA FORM 1) FOR ENGINES AND PROPELLERS, AND PARTS THEREOF, WHICH CONFORM TO A DECLARATION OF DESIGN COMPLIANCE
• AMC2 21.A.145(a) Resources
• 21L.B.102 Investigation
• AMC1 21L.B.142 Registration of a declaration of production capability
• 21.A.116 Transferability
• AMC1 21.A.7(a) ICA contents
• AMC 21L.B.241(a)(2) and 21L.B.242(a)(2) Physical inspection and assessment of the aircraft in order to ensure that the aircraft is capable of safe flight, and that flight testing can be conducted safely (physical inspection and safety review)
• AMC1 21L.A.108(b) Compliance activities for declaring compliance of a major change
• 21.A.719 Transferability
• 21.A.112B Demonstration of capability
• AMC1 21L.A.44(b) Compliance activities for a declaration of design compliance
• AMC1 21.A.125B(a)(3), 21.A.158(a)(3) and 21.A.258(a)(3) Findings and observations
• AMC2 21.B.221 Oversight principles
• AMC2 21.A.265(a) Obligations of the holder
• AMC1 21L.B.46(c) Investigation
• SUBPART K -- PARTS, APPLIANCES, AND CONTROL AND MONITORING UNIT (CMU) COMPONENTS
• 21L.B.181 Initial oversight investigation
• AMC1 21.A.243(a) Handbook
• 21.A.20 Demonstration of compliance with the type certification basis, operational suitability data certification basis and environmental protection requirements
• AMC1 21L.B.20(a)(1)
• GM 21.A.129(a) Availability for inspection by the competent authority
• 21.A.610 Approval for deviation
• AMC1 21.B.120(d) Initial certification procedure
• AMC 21.A.432C(b) Certification programme for a repair design approval
• 21.A.124 Application
• GM1 21L.B.24 Means of compliance
• GM 21.A.21(b), 21.A.95(c), 21.A.97(c), 21.A.115(c), 21.B.103(b), 21.B.107(b) and 21.B.111(b) Approval of operational suitability data (OSD)
• GM1 21.B.55(e) Record-keeping
• 21L.A.203 Classification of repair designs to a type-certified product
• GM 21.A.35 Flight Tests
• 21L.A.177 Obligations of the declared design organisation
• AMC1 21.A.307(b)(3) and (b)(4) Verification activities to be conducted on the part or appliance or release documentation prior to installation
• 21.A.451 Obligations and EPA marking
• AMC2 21.A.239(d) Design management system
• 21L.A.83 Demonstration of design capability
• GM 21.A.21(b), 21.A.95(c), 21.A.97(c), 21.A.115(c), 21.B.103(b), 21.B.107(b) and 21.B.111(b) Approval of operational suitability data (OSD)
• AMC 21.A.97 Requirements for the approval of a major change
• Article 5
• AMC1 21L.A.43(b)(11) Declaration of design compliance
• GM1 21.1(e) Competent authority
• AMC1 21.A.263(c)(1) Privileges
• AMC 21.A.113(a) Form and manner
• AMC1 21L.A.85(e)(2) Demonstration of compliance
• 21.A.807 Identification of ETSO articles
• Appendix B to GM 21.A.101 Application charts for changed product rule
• 21.A.433 Requirements for approval of a repair design
• 21L.A.222 Standard repairs
• 21.A.2 Undertaking by a person other than the applicant for, or holder of, a certificate
• 21L.A.255 Identification of parts
• AMC1 21.A.163(d) Privileges
• GM1 21L.A.122(a)
• 21.B.35 Changes in the management system
• 21.B.220 Initial certification procedure
• GM1 21L.A.9(b) Instructions for continued airworthiness
• GM1 21L.A.10 Access and investigation
• GM1 21.A.145(a) Resources
• 21L.A.274 Issuance of a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1)
• GM No 2 to 21.A.126(a)(3) Production inspection system - Means of checking of the production processes
• 21L.A.27 Requirements for the issuance of a type certificate
• Incorporated amendments
• GM1 21.A.239(c) Design management system
• 21.A.231 Scope
• 21.A.609 Obligations of holders of ETSO authorisations
• GM4 21L.A.9(b) Instructions for continued airworthiness
• AMC No 2 to 21.A.263(c)(5), (8) and (9) Procedure for the approval of a major repair, a major change to a type certificate (TC), or a supplemental type certificate (STC) by a design organisation approval (DOA) holder under their privileges
• 21L.B.81 Type-certification basis and applicable environmental protection requirements for a major change to a type certificate
• AMC2 21L.A.9(a) Instructions for continued airworthiness
• 21L.A.104 Eligibility
• GM1 21.A.3A(a) and 21.A.3A(b) Reporting system
• AMC2 21.A.163(c) Completion of EASA Form 1
• AMC1 21L.A.3(a)(3)
• 21.B.103 Issuance of a type-certificate or a restricted type-certificate
• EASA FORMS
• AMC 21.A.95 Requirements for the approval of a minor change
• AMC1 21.A.5 Record-keeping
• AMC1 21L.A.43(b) Declaration of design compliance
• GM 21.A.21(b), 21.A.95(c), 21.A.97(c), 21.A.115(c), 21.B.103(b), 21.B.107(b) and 21.B.111(b) Approval of operational suitability data (OSD)
• SUBPART E -- SUPPLEMENTAL TYPE CERTIFICATES
• AMC1 21L.A.63(c) Classification of changes to a type certificate
• AMC1 21L.A.206(e)(2) Demonstration of compliance
• 21.B.15 Information to the Agency
• GM1 21L.A.3(a)(3)
• 21L.A.178 Notification of changes and cessation of activities
• 21.A.125B Findings and observations
• GM 21.A.435(b) Repair design approval
• 21.A.432B Demonstration of capability
• 21.A.201 Scope
• AMC1 21.A.239(c)(5)(i) Design management system
• GM1 21.A.805 Identification of critical parts
• GM1 21L.A.7(a)
• GM1 21.B.433(e) Findings and corrective actions
• GM No 3 to 21.A.165(c) Obligations of the holder - Condition for safe operation
• GM2 21L.A.12 Means of compliance
• AMC1 21.A.143(a)(1) Production organisation exposition
• SUBPART O -- EUROPEAN TECHNICAL STANDARD ORDER AUTHORISATIONS
• SUBPART Q -- IDENTIFICATION OF PRODUCTS AND PARTS
• AMC1 21.B.25(a)(5) Management system
• GM1 21L.A.124(c) Management system for production
• 21.A.701 Scope
• GM1 21.B.15(b) Information to the Agency
• GM2 21L.A.127(c) Obligations of the declared production organisation
• GM1 21L.A.102 Standard changes
• 21.A.608 Declaration of Design and Performance (DDP)
• 21.A.165 Obligations of the holder
• 21L.A.174 Management system for design
• GM1 21L.A.222 Standard repairs
• Appendix V -- EASA Form 24 -- Restricted Certificate of Airworthiness
• AMC1 21L.A.25(e)(3) Demonstration of compliance
• 21.A.126 Production inspection system
• GM3 21.B.15(b) Information to the Agency
• AMC1 21.A.239(c)(2) Design management system
• GM1 21L.A.63 Classification of changes to a type certificate
• SUBPART Q -- IDENTIFICATION OF PRODUCTS AND PARTS (Reserved)
• AMC2 21.B.15(b) Information to the Agency
• AMC1 21L.B.144(d)
• GM to 21.A.62, 21.A.108 and 21.A.120B Availability of Operational Suitability Data
• AMC to 21.A.143, 21.A.243, 21.A.14(b), 21.A.112B(b) and 21.A.432B(b) Flight Test Operations Manual (FTOM)
• 21.A.171 Scope
• AMC1 21.B.222(d) and (e) Oversight programme
• GM1 21.A.139(c)(5) Production management system
• GM3 21.A.7(b) Approval status of the manual for a component or article
• GM2 21.A.124A and 21.A.134A Means of compliance
• GM1 21L.B.21(f) Findings and observations
• Disclaimer
• GM1 21.A.5 Record-keeping
• 21L.A.229 Unrepaired damage
• 21L.B.184 Oversight programme
• 21L.A.42 Eligibility
• GM1 21L.A.124(b)(1)
• 21L.A.46 Aircraft design data
• 21.A.602A Eligibility
• 21.A.21 Requirements for the issuance of a type certificate or restricted type certificate
• AMC1 21.B.125(d) and 21.B.225(d) Findings and corrective actions
• 21L.A.125 Resources of the declared production organisation
• SUBPART M -- REPAIRS
• GM 21.A.126(b)(3) Production inspection system - Use of derived data instead of original design data
• GM1 21L.A.83(a) Demonstration of design capability
• 21L.B.19 Resolution of disputes
• GM1 21L.A.209(b) Approval of a repair design under a privilege
• AMC1 21L.A.3(a) Reporting system
• SUBPART F -- PRODUCTION WITHOUT PRODUCTION ORGANISATION APPROVAL
• GM1 21.A.139, 21.A.239, 21.B.120, 21.B.140, 21.B.220, and 21.B.240 The use of information and communication technologies (ICT) for performing remote audits
• GM1 21.B.25(a)(2) Management system
• 21.A.258 Findings and observations
• AMC 21.A.20(c) Compliance documentation
• GM1 21L.A.124(b)(2)(vi) Management system for production
• GM2 21L.A.3(a)(1)
• GM1 21L.A.124(b) Management system for production
• GM1 21.A.239(c)(4)(ii) Design management system
• AMC1 21L.A.85(b) Demonstration of compliance
• GM1 21.B.433(b) Findings and corrective actions
• AMC1 21L.A.68(c) Requirements for the approval of a major change to a type certificate
• AMC1 21.A.3A(a)(3), 21.A.3A(b)(3), 21.A.3A(d) Reporting system
• 21L.A.128 Notification of changes and cessation of activities
• GM2 21.B.65 Suspension, limitation and revocation
• GM1 21L.A.27(c)(1) Requirements for the issuance of a type certificate
• GM3 21.A.7(a) Non-ICA supplier data (e.g. component maintenance manuals (CMMs))
• AMC1 21.A.139(d)(2)(ii) Production management system
• Appendix D to GM 21.A.101 Other guidance for affected areas
• AMC1 21.B.20A Immediate reaction to an information security incident or vulnerability with an impact on aviation safety
• AMC 21L.A.47(a) Physical inspection and flight tests of the first article of that aircraft (first-article inspection) prior to registration of a declaration of design compliance
• 21L.A.175 Resources of the declared design organisation
• 21.A.158 Findings and observations
• Appendix IX -- EASA Form 53 -- Certificate of Release to Service
• GM1 21L.A.252(c) Identification of parts produced under Subpart R
• AMC1 21L.A.5 Collaboration between design and production
• 21.A.90C Stand-alone changes to the Instructions for Continued Airworthiness
• 21L.B.163 Oversight
• AMC1 21L.A.65 Application for a change to a type certificate
• AMC 21.A.432C(a) Form and manner
• GM1 21.B.222(b)(1)(ii) Oversight programme
• AMC No 1 to 21.A.163(c) Computer generated signature and electronic exchange of the EASA Form 1
• AMC1 21L.B.144 and 221L.B.184 Oversight programme
• GM3 21L.A.9(a) Instructions for continued airworthiness
• 21.A.133 Eligibility
• GM1 21L.A.62 Standard changes
• 21.A.173 Classification
• GM1 21.B.125(b) and 21.B.225(b) Findings and corrective actions
• 21.A.47 Transferability
• 21L.A.221 Scope
• AMC2 21.B.120(a) Initial certification procedure
• GM 21.A.151 Terms of approval - Scope and categories
• AMC1 21.A.239(c)(4)(ii) Design management system
• AMC1 21L.A.25(e)(2) Demonstration of compliance
• 21.A.128 Tests: engines, propellers, and control and monitoring units (CMUs)
• 21.A.174 Application
• GM1 21.B.125(e) and 21.B.225(e) Findings and corrective actions
• GM 21.A.133(a) Eligibility - Approval appropriate for showing conformity
• GM1 21L.A.126(a) Scope of work
• GM No 2 to Appendix XII - Competence and experience of pilots for Category 3 and Category 4 flight tests and of Lead Flight Test Engineers (LFTEs)
• AMC1 21.A.139(c) Production management system
• 21L.B.101 Type-certification basis and applicable environmental protection requirements for a supplemental type certificate
• 21L.B.205 Continuing airworthiness oversight of products for which a repair design has been approved
• 21.B.120 Initial certification procedure
• GM2 21.A.7(a) Determination of which supplier data is part of the ICA
• 21L.A.103 Classification of changes to the design of an aircraft for which design compliance has been declared
• 21.A.118B Duration and continued validity
• 21L.A.2 Obligations and actions performed by a person other than the applicant for, or holder of, a certificate or the declarant of a declaration of design compliance
• 21L.B.182 Registration of a declaration of design capability
• AMC1 21.A.139(c)(5)(i) Production management system
• AMC1 21L.A.225(b) Declaration of design compliance for minor repair designs
• GM1 21.A.139(d)(1) Production management system
• AMC1 21.A.145(d)(2) Resources
• AMC No 2 to 21.A.129(c) Obligations of the manufacturer - Conformity with Applicable Design Data
• AMC3 21.B.220 Initial certification procedure
• AMC1 21L.A.225(a) Declaration of design compliance for minor repair designs
• 21L.A.201 Scope
• 21L.A.90 Continued validity of a supplemental type certificate
• GM1 21.A.139, 21.A.239, 21.B.120, 21.B.140, 21.B.220, and 21.B.240 The use of information and communication technologies (ICT) for performing remote audits
• GM 21.A.21(a)(3)(i) Clarification of the term 'determined'
• AMC1 21.A.139(c)(5) Production management system
• 21.B.215 Means of compliance
• 21.A.93 Application
• GM 21.A.719 Transfer of a permit to fly
• AMC1 21L.A.85(a)
• 21.A.111 Scope
• 21.A.432A Eligibility
• AMC1 21.B.15(b) Information to the Agency
• 21.A.182 Aircraft identification
• AMC1 21L.A.272 Eligibility
• GM1 21L.A.207(c) Requirements for the approval of a minor repair design
• AMC1 21.B.220(e) Initial certification procedure
• 21.B.450 Amendments to the type-certification basis for a repair design approval
• Appendix VI -- EASA Form 25 -- Certificate of Airworthiness
• AMC1 21.A.139(e) and 21.A.139(d)(2)(xiv) Production management system
• AMC No 1 to Appendix XII - Training courses for Lead Flight Test Engineers (LFTEs)
• GM1 21.A.3A(a)(3), 21.A.3A(b)(3) and 21.A.3A(d) Reporting system
• Article 9 Production organisations
• GM1 Annex I Definitions
• Appendix B to point 21L.A.103 Classification of changes to the design of an aircraft for which design compliance has been declared
• 21.A.33 Inspections and tests
• AMC2 21L.B.144(a) and 21L.B.184(a) Oversight programme
• 21L.A.30 Continued validity of a type certificate
• 21L.A.211 Unrepaired damage
• 21L.B.44 Special conditions
• 21.B.140 Amendment of a letter of agreement
• GM No 2 to 21.A.15(d) Determination of type or variant
• GM1 21.B.65 Suspension, limitation and revocation
• 21.A.303 Compliance with the applicable requirements
• AMC1 21L.A.66(e)(2) Demonstration of compliance
• 21L.A.162 Eligibility
• AMC1 21.A.239(c)(1) Design management system
• AMC1 21.A.245(b) Resources
• GM1 21.A.130, 21.A.163 and 21.A.165 Performance of tasks in real time for the issuance of an 'EASA Form 1' for prototype and new parts, appliances and products other than complete aircraft, using information and communication technologies (ICT)
• GM1 21.B.222(c) Oversight programme
• 21.B.20 Immediate reaction to a safety problem
• GM 21.A.701(a) Permit to fly when a certificate of airworthiness or a restricted certificate of airworthiness is not appropriate
• EASA eRules
• GM No 1 to 21.A.15(d) Application for the approval of operational suitability data - MMEL for ELA1 and ELA2
• AMC2 21L.B.16(a)(3) Management system
• GM1 21L.A.124(e) Management system for production and 21L.A.126(e) Scope of work
• GM1 21L.A.43(b)(4)
• GM1 21.A.307(b)(4) Certification specifications referred to in point 21.A.307(b)(4)
• 21.A.204 Application
• 21.B.520 Investigation
• GM1 21L.A.127(l) Obligations of the declared production organisation
• GM1 21L.A.66(d) Demonstration of compliance
• 21L.A.48 Non-transferability of a declaration of aircraft design compliance
• 21.A.3B Airworthiness directives
• 21.B.20A Immediate reaction to an information security incident or vulnerability with an impact on aviation safety
• GM1 21L.B.13(b) Information to the Agency
• 21L.A.275 Obligations of a natural or legal person issuing a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1)
• SUBPART O -- EUROPEAN TECHNICAL STANDARD ORDER AUTHORISATIONS (Reserved)
• GM1 21.A.139(d)(2)(ii) Production management system
• 21L.A.141 Scope
• Annex I
• GM 21.A.126(b)(4) Production inspection system - Segregation of rejected material
• GM to Subpart P
• 21.A.13 Eligibility
• AMC1 21L.A.206(c) Demonstration of compliance
• Article 4 Continued validity of supplemental type-certificates
• AMC1 21.A.245(d) Resources
• GM1 21L.A.124(d) Management system for production
• 21.A.31 Type design
• GM 21.A.701 Scope
• Article 1 Scope and definitions
• AMC1 21L.A.241(b)(1)
• GM 21.A.35(f)(1) Flying Time for Function and Reliability Testing
• GM 21.B.80 Type-certification basis for a type certificate (TC) or restricted type certificate (RTC)
• AMC1 21L.B.16(a)(1) Management system
• GM1 21.B.30 Allocation of tasks to qualified entities
• GM 21.B.325(b) Completion of the Airworthiness Review Certificate by a Member State
• AMC2 21.A.243(d) Handbook
• 21.A.148 Changes of location
• GM1 21.B.115(b) and (c) and 21.B.215(b) and (c) Means of Compliance
• AMC1 21L.A.67 Requirements for the approval of a minor change to a type certificate
• 21.B.225 Findings and corrective actions
• AMC1 21.A.134 Application
• SUBPART J -- DECLARED DESIGN ORGANISATIONS
• SUBPART N -- DESIGN OF REPAIRS TO AIRCRAFT FOR WHICH DESIGN COMPLIANCE HAS BEEN DECLARED
• 21.A.177 Amendment or modification
• AMC1 21.B.221(f) Oversight principles
• Appendices
• AMC 21.A.605(a)(1) Certification programme
• 21.A.243 Handbook
• SUBPART N -- DESIGN OF REPAIRS TO AIRCRAFT FOR WHICH DESIGN COMPLIANCE HAS BEEN DECLARED
• GM No 3 to 21.A.128 Acceptable functional test - Engines and Propellers
• 21.A.803 Handling of identification data
• GM1 21.A.159(a)(3) Duration and continued validity
• GM1 21L.B.44 Special conditions
• AMC 21.A.303(c) Standard Parts
• AMC1 21.A.263(c)(2) Privileges
• 21L.A.61 Scope
• 21L.A.106 Obligations of the person making a declaration of compliance of the design of a minor change
• AMC1 21.B.125(d) and 21.B.225(d) Findings and corrective actions
• AMC1 21L.A.7(d) Record-keeping
• AMC1 21.B.221 Oversight principles
• 21L.B.241 Investigation prior to the issuance of a permit to fly
• AMC1 21L.A.107(b) Declaration of design compliance for a major change
• GM1 21L.A.121(a) Scope
• Appendix VII -- EASA Form 45 -- Noise Certificate
• GM1 21.A.265(b) Obligations of the holder
• GM1 21L.B.22 Enforcement measures
• GM No 2 to 21.A.125B(a) Examples for level one findings
• GM1 21.A.125B(a), 21.A.158(a) and 21.A.258(a) Findings and observations
• Article 2 Transitional provisions (Regulation (EU) 2015/1039)
• AMC1 21L.A.25(c) Demonstration of compliance
• AMC1 21L.A.122(c) Eligibility
• 21L.A.47 Obligations of the declarant of a declaration of design compliance
• GM1 21L.A.193(b)(5) Equipment exempted from an airworthiness approval in accordance with Commission Regulation (EU) No 965/2012
• GM1 21L.B.184(a) Oversight programme
• 21L.A.224 Eligibility
• 21.A.619 Duration and continued validity
• GM1 21.A.139, 21.A.239, 21.B.120, 21.B.140, 21.B.220, and 21.B.240 The use of information and communication technologies (ICT) for performing remote audits
• GM1 21L.B.252(d)
• 21.B.221 Oversight principles
• AMC2 21L.A.24(b)(4) Application for a type certificate
• GM 21.A.126(a)(2) Production inspection system - Identification of incoming materials and parts
• 21L.B.84 Issuance of an approval of a major change to a type certificate
• AMC 21.B.225(a) Notification of findings
• GM1 21L.A.85(d) Demonstration of compliance
• 21L.A.142 Eligibility
• GM1 21.A.124A and 21.A.134A Means of compliance
• 21.B.55 Record-keeping
• GM1 21L.B.171(c) Investigation
• GM1 21.A.126(b)(5) Production inspection system -- Engineering and manufacturing review procedure
• AMC2 21L.B.16 Management system
• Article 10 Agency measures
• AMC2 21.A.139(d)(2)(ii) Production management system
• GM 21.A.35(b)(2) Objective and Content of Function and Reliability Testing
• GM1 21.A.3A(a)(1) and (b)(1) Reporting system
• Appendix III -- EASA Form 20a -- Permit to Fly
• AMC1 21.B.240 Changes in production management system
• SECTION B - PROCEDURES FOR COMPETENT AUTHORITIES
• GM1 21L.A.227 Compliance activities for declaring compliance of a major repair design
• SUBPART D -- CHANGES TO TYPE CERTIFICATES
• 21L.B.201 Type-certification basis and applicable environmental protection requirements for a repair design approval
• GM1 21L.A.126(d) Scope of work
• 21L.B.17 Allocation of tasks to qualified entities
• 21L.A.89 Transferability of a supplemental type certificate
• AMC1 21L.A.66(e)(1) Demonstration of compliance
• GM1 21L.A.85(f) Demonstration of compliance
• AMC1 21L.B.23(b) Airworthiness directives
• AMC1 21L.A.86 Requirements for approval of a supplemental type certificate
• GM1 21.B.222(d)(2) Oversight programme
• GM1 21L.A.3(a)
• GM1 21L.B.162(b) Issuance or amendment of a certificate of airworthiness or a restricted certificate of airworthiness
• 21L.B.242 Investigation prior to issuance of the flight conditions
• AMC1 21L.B.251(b) Oversight
• AMC2 21.B.430 Initial certification procedure
• GM2 21.A.239(d)(3) Design management system
• AMC1 21L.A.275(a) Obligations of a natural or legal person issuing a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1)
• 21L.A.254 Handling of identification data
• GM1 21L.B.183(b) Oversight
• SECTION B -- PROCEDURES FOR COMPETENT AUTHORITIES
• GM1 21L.A.229 Unrepaired damage
• AMC1 21L.A.193(b)(3)
• AMC 21.A.153 Changes to the terms of approval -- Application for a change to the terms of approval
• GM1 21L.A.174(b) Management system for design
• GM2 21.A.7(b) ICA -- format
• 21.A.129 Obligations of the production organisation
• GM1 21.B.25 Management system
• 21L.B.14 Airworthiness directives received from non-Member States
• GM No 2 to 21.A.303(c) Officially recognised Standards
• AMC2 21.A.243(a) Handbook
• 21L.B.61 Detailed technical specifications and applicable environmental protection requirements for declarations of product design compliance
• 21L.A.105 Declaration of design compliance for minor changes
• AMC1 21.A.130(b)(4)(ii) Statement of conformity
• GM1 21L.A.193(b)(4) Certification specifications referred to in point 21L.A.193(b)(4)
• SUBPART F -- CHANGES TO AIRCRAFT FOR WHICH DESIGN COMPLIANCE HAS BEEN DECLARED
• GM 21.A.21(b), 21.A.95(c), 21.A.97(c), 21.A.115(c), 21.B.103(b), 21.B.107(b) and 21.B.111(b) Approval of operational suitability data (OSD)
• AMC1 21L.A.125(d)(2) Resources of the declared production organisation
• GM1 21.B.20A Immediate reaction to an information security incident or vulnerability with an impact on aviation safety
• 21.A.245 Resources
• 21.B.453 Issuance of a repair design approval
• AMC1 21.A.245(e) Resources
• GM1 21.A.139(c)(5)(i) Production management system
• 21.A.153 Changes to the terms of approval
• AMC1 21.A.125B(a)(3), 21.A.158(a)(3) and 21.A.258(a)(3) Findings and observations
• GM1 21.A.245(c)(2) Resources
• AMC1 21L.A.68 Requirements for the approval of a major change to a type certificate
• 21.A.1 Scope
• GM 21.A.35(f)(2) Flying Time for Function and Reliability Testing
• AMC1 21L.A.105(c) Declaration of design compliance for minor changes
• SUBPART J -- DESIGN ORGANISATION APPROVAL
• GM 21.A.95(b) Requirements for the approval of a minor change
• 21.A.44 Obligations of the holder
• AMC1 21L.A.9(b) Instructions for continued airworthiness
• SUBPART F -- CHANGES TO AIRCRAFT FOR WHICH DESIGN COMPLIANCE HAS BEEN DECLARED
• 21L.A.81 Scope
• AMC1 21L.A.227(f) Compliance activities for declaring compliance of a major repair design
• GM1 21L.A.9(a) Instructions for continued airworthiness
• 21.A.113 Application for a supplemental type-certificate
• 21L.A.163 Application
• AMC1 21.A.433(b) Requirements for approval of a repair design
• AMC1 21.A.125B(c), 21.A.158(c), 21.A.258(c) Findings and observations
• AMC2 21.B.220 Initial certification procedure
• GM1 21.A.124A and 21.A.134A Means of compliance
• AMC1 21.A.165(c)(3)(ii) Obligations of the holder
• AMC 21.A.93(a) Form and manner
• GM1 21L.A.227(f) Compliance activities for declaring compliance of a major repair design
• 21L.B.251 Oversight
• 21.A.602B Demonstration of capability
• GM4 21.A.7(b) Integration of ICA between products (aircraft, engines, propellers)
• AMC1 21L.A.127(b) Obligations of the declared production organisation and AMC1 21L.A.177(b) Obligations of the declared design organisation
• 21.B.75 Special conditions
• GM1 21.A.307(b)(6) Part or appliance that is part of a higher-level assembly
• AMC1 21L.A.108(a) Compliance activities for declaring compliance of a major change
• GM 21.A.21(b), 21.A.95(c), 21.A.97(c), 21.A.115(c), 21.B.103(b), 21.B.107(b) and 21.B.111(b) Approval of operational suitability data (OSD)
• Appendix I -- EASA Form 24B -- Restricted certificate of airworthiness
• GM 21.A.431A Scope
• GM1 21L.B.19 Resolution of disputes
• 21.A.445 Unrepaired damage
• 21.A.117 Changes to that part of a product covered by a supplemental type-certificate
• 21L.B.145 Oversight activities
• AMC1 21.A.165(c)(3)(i) Obligations of the holder
• AMC1 21.A.247 Changes to the design management system
• 21.A.601 Scope
• 21.A.805 Identification of critical parts
• GM 21.A.3B(d)(4) Defect correction - Sufficiency of proposed corrective action
• AMC No 2 to 21.B.100(b) Level of involvement (LoI) in European technical standard order authorisation (ETSOA) projects
• GM1 21L.A.25(d) Demonstration of compliance
• GM1 21L.B.17 Allocation of tasks to qualified entities
• 21.A.239A Information security management system
• 21L.A.124 Management system for production
• EASA FORMS
• AMC1 21L.A.85(c) Demonstration of compliance
• 21L.B.13 Information to the Agency
• 21L.A.43 Declaration of design compliance
• 21.A.101 Type-certification basis, operational suitability data certification basis and environmental protection requirements for a major change to a type-certificate
• GM1 21.A.139(f) Production management system
• 21.A.308 Eligibility of a component for installation in a control and monitoring unit (CMU)
• 21.A.253 Changes to the terms of approval
• AMC1 21.A.139(c)(3) and (4) Production management system
• Appendix A to GM 21.A.91 Examples of major changes per discipline
• AMC1 21L.B.16(a)(3) Management system
• GM2 21L.2 Competent authority
• GM1 21.A.247 Significant changes to the design management system
• 21L.A.9 Instructions for continued airworthiness
• GM1 21L.A.174(b)(2) Management system for design
• GM1 21L.B.16(a)(5) Management system
• 21L.A.41 Scope
• GM1 21.A.7(a) Scope of ICA, their publication format and typical ICA data
• 21L.B.11 Oversight documentation
• 21L.B.103 Issuance of a supplemental type certificate
• AMC3 21L.B.16(a)(3) Management system
• GM1 21L.A.122(c) Eligibility
• SUBPART E -- SUPPLEMENTAL TYPE CERTIFICATES
• GM No 2 to 21.A.251 Terms of approval - Organisations that design minor changes to type design or minor repairs to products
• AMC to 21.A.143, 21.A.243, 21.A.14(b), 21.A.112B(b) and 21.A.432B(b) Flight Test Operations Manual (FTOM)
• Appendix X -- EASA Form 55 -- Production organisation approval certificate
• 21.B.80 Type-certification basis for a type-certificate or restricted type-certificate
• GM 21.A.20 Compliance demonstration process
• 21.A.65 Continuing structural integrity for aeroplanes structures
• 21.B.435 Changes in the design management system
• 21.B.430 Initial certification procedure
• AMC1 21.A.124A(b) and 21.A.134A(b) Means of compliance
• GM1 21L.A.211 Unrepaired damage
• GM3 21L.A.273(a)
• Appendix A to GM 21.A.101 Classification of design changes
• GM2 21.B.220 Initial certification procedure
• 21L.B.172 Issuance or amendment of noise certificates
• SUBPART Q -- IDENTIFICATION OF PRODUCTS, PARTS, APPLIANCES, CONTROL AND MONITORING UNITS (CMUs) AND CMU COMPONENTS
• SUBPART R -- STATEMENT OF CONFORMITY FOR AIRCRAFT AND AUTHORISED RELEASE CERTIFICATE (EASA FORM 1) FOR ENGINES AND PROPELLERS, OR PARTS THEREOF, WHICH CONFORM TO A DECLARATION OF DESIGN COMPLIANCE
• GM1 21L.A.43(c) Information to be provided to the Agency
• 21L.A.127 Obligations of the declared production organisation
• SUBPART H -- CERTIFICATES OF AIRWORTHINESS AND RESTRICTED CERTIFICATES OF AIRWORTHINESS
• AMC No 3 to 21.A.129(c) Obligations of the manufacturer - Condition for safe operation
• 21L.B.23 Airworthiness directives
• 21L.B.222 Registration of a declaration of a major repair design to an aircraft for which design compliance has been declared
• 21L.A.226 Declaration of design compliance of major repair designs
• 21L.A.3 Reporting system
• 21L.B.43 Type-certification basis for a type certificate
• AMC1 21L.A.84(a) Application for a supplemental type certificate
• AMC1 21L.B.144(a) and 21L.B.184(a) Oversight programme
• 21L.A.102 Standard changes
• 21.A.121 Scope
• AMC1 21L.B.203(d) Investigation of an application for the approval of a major repair design
• GM1 21.A.9 Access and investigations
• 21L.A.225 Declaration of design compliance for minor repair designs
• 21L.B.173 Oversight
• GM1 Appendix VII
• GM1 21.B.115 and 21.B.215 Means of compliance
• GM1 21.A.3A Reporting system
• GM1 21.B.25(a)(5) Management system
• GM1 21.A.149 and 21.A.249 Transferability
• GM1 21L.A.108(f) Compliance activities for declaring compliance of a major change
• GM No 1 to 21.A.93(b)(1)(iii) Interaction of changes to the type design and changes to operational suitability data (OSD)
• 21L.B.146 Changes to declarations
• AMC1 21L.A.11(b) Findings and observations
• 21L.B.104 Continuing airworthiness oversight of products for which a supplemental type certificate has been issued
• AMC1 21.A.101(h) Type-certification basis for changes to large aeroplanes subject to point 26.300 of Part-26
• GM to 21.A.611 Design changes
• 21L.A.28 Obligations of a type-certificate holder
• SUBPART A -- GENERAL PROVISIONS
• 21.A.124A Means of compliance
• 21.A.125C Duration and continued validity
• GM3 21.B.220 Initial certification procedure
• GM1 21L.A.3 Reporting system
• 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)
• AMC2 21.A.263(c)(2) Privileges
• AMC1 21L.A.125(c)(1) Resources of the declared production organisation
• 21.A.159 Duration and continued validity
• GM1 21.A.139, 21.A.239, 21.B.120, 21.B.140, 21.B.220, and 21.B.240 The use of information and communication technologies (ICT) for performing remote audits
• GM2 21.A.124A and 21.A.134A Means of compliance
• 21L.B.48 Continuing airworthiness oversight of products for which a type certificate has been issued
• GM No 1 to 21.A.126(a)(3) Production inspection system - List of specifications
• 21.A.441 Repair embodiment
• AMC3 21.B.430 Initial certification procedure
• Appendix B to GM 21L.A.63 Classification of changes to a type certificate
• 21.A.234 Application
• AMC1 21L.A.206 Demonstration of compliance
• 21L.A.63 Classification of changes to a type certificate
• 21L.A.271 Scope
• 21L.B.49 Transfer of a type certificate
• GM1 21.A.145(b)(2) Resources
• 21L.B.144 Oversight programme
• GM1 21L.A.221 Scope
• 21.B.525 Issuance of a permit to fly
• SUBPART K -- PARTS, APPLIANCES, AND CONTROL AND MONITORING UNIT (CMU) COMPONENTS
• 21.A.19 Changes requiring a new type-certificate
• GM2 Annex I Abbreviations
• AMC1 21.A.122 Eligibility
• GM No 3 to 21.A.708(c) Operation of Overweight Aircraft
• GM1 21L.B.23(b) Airworthiness directives
• 21.A.62 Availability of operational suitability data
• AMC1 21L.A.226(b) Declaration of design compliance of major repair designs
• GM1 21L.A.12 Means of compliance
• 21L.A.146 Continued validity of a certificate of airworthiness and of a restricted certificate of airworthiness
• 21.B.107 Issuance of an approval of a change to a type-certificate
• AMC1 21.B.431 Oversight principles
• 21.A.605 Data requirements
• 21L.A.7 Record-keeping
• AMC1 21L.B.102(d) Investigation
• 21.A.263 Privileges
• AMC1 21.B.222(c) Oversight programme
• 21.B.135 Maintenance of the letter of agreement
• GM 21.A.707(b) Application
• 21.A.125A Issuance of a letter of agreement
• GM1 21L.B.63(b) Registration of a declaration of design compliance
• AMC1 21L.B.24(a)
• AMC1 21L.A.205(a) Application for the approval of a repair design to a type-certificated product
• AMC1 21L.A.225(c) Declaration of design compliance for minor repair designs
• GM1 21.A.139(c)(1) Production management system
• 21L.A.251 Scope
• GM 21.A.703 Applicant for a permit to fly
• AMC1 21L.B.182 Registration of a declaration of production capability
• GM 21.A.263(c)(5), (8) and (9) Numbering system for supplemental type certificates (STCs), major changes and major repairs issued by design organisation approval (DOA) holders, and information to EASA
• GM No 1 to 21.A.165(c) Obligations of the holder - Conformity of prototype models and test specimens
• GM1 21.A.239(c)(1) Design management system
• AMC1 21L.A.66(c) Demonstration of compliance
• GM1 21L.B.16 Management system
• 21L.B.143 Oversight
• 21.A.603 Application
• AMC1 21L.A.86(a)(5) Requirements for approval of a supplemental type certificate
• SUBPART I -- NOISE CERTIFICATES
• GM1 21L.A.273(g) Production control system
• GM 21.A.15(c) Updates to the certification programme
• AMC1 21.A.145(d)(1) Resources
• GM1 21.A.130, 21.A.163 and 21.A.165 Performance of tasks in real time for the issuance of an 'EASA Form 1' for prototype and new parts, appliances and products other than complete aircraft, using information and communication technologies (ICT)
• 21.B.326 Certificate of airworthiness
• AMC2 21.A.130(b) Statement of Conformity for Products (other than complete aircraft), parts, appliances and materials -- The Authorised Release Certificate (EASA Form 1)
• SECTION A -- TECHNICAL REQUIREMENTS
• AMC 21.A.263(c)(7) Procedure for the issue of a permit to fly
• 21L.A.86 Requirements for approval of a supplemental type certificate
• 21.A.707 Application for permit to fly
• AMC2 21.A.263(c)(1) Privileges
• AMC1 21L.B.172(a) Issuance or amendment of noise certificates
• 21.A.249 Transferability
• GM1 21.A.130(b)(4)(i) Statement of conformity
• 21.A.90A Scope
• 21.B.85 Applicable environmental protection requirements for a type certificate or restricted type certificate
• GM1 21.B.125(b) and 21.B.225(b) Findings and corrective actions
• AMC 21.A.163(e) Procedure for the issue of a permit to fly including approval of the flight conditions
• GM1 21L.A.127(a) Obligations of the declared production organisation
• 21.A.134 Application
• AMC 21.B.140 Amendment of a letter of agreement
• GM 21.A.90B Standard changes -- Certification Specifications
• GM1 21.A.139(c)(4)(ii) Production management system
• SECTION A - TECHNICAL REQUIREMENTS
• AMC1 21.B.25(a)(3) Management system
• Appendix A to AMC1 21L.A.227(a) Compliance activities for declaring compliance of a major repair design
• GM1 21.B.125(e) and 21.B.225(e) Findings and corrective actions
• (SUBPART N -- NOT APPLICABLE)
• 21L.A.88 Obligations of a holder of a supplemental type certificate
• SUBPART O -- EUROPEAN TECHNICAL STANDARD ORDER AUTHORISATIONS (Reserved)
• 21.A.149 Transferability
• GM1 21.A.3A(a), 21.A.3A(e), and 21.A.3A(f) Reporting system
• 21L.A.241 Permit to fly and flight conditions
• AMC1 21L.A.175(b)
• 21L.A.202 Standard repairs
• Appendix G to GM 21.A.101 Changed product rule (CPR) decision record
• GM No 1 to 21.A.251 Terms of approval
• GM1 21.A.239(c)(2) Design management system
• AMC1 21.A.147 Changes to the production management system
• List of revisions
• AMC1 21.B.432(b)(1) Oversight programme
• 21.A.139 Production management system
• SUBPART I -- NOISE CERTIFICATES
• GM2 21L.A.163(c)(1)(ii) Application
• AMC 21.A.130(c) Validation of the Statement of Conformity
• GM1 21L.A.81 Scope
• GM1 21.A.239(c)(5) Design management system
• AMC2 21.A.7(a) Identification of ICA
• AMC1 21.A.65 Continuing structural integrity programme for aeroplane structures
• AMC1 21L.A.7(a) Record-keeping
• AMC1 21.B.115(b),(c) and 21.B.215(b),(c) Means of compliance
• SUBPART G -- DECLARED PRODUCTION ORGANISATIONS
• AMC1 21L.A.85 Demonstration of compliance
• GM 21.A.265(h) Designation of data and information issued under the authority of a design organisation approval (DOA) holder
• 21L.B.42 Initial investigation
• 21.B.480 Issuance of an ETSO authorisation
• 21L.B.203 Investigation of an application for the approval of a major repair design
• GM 21.A.93(c) Period of validity for the application
• GM1 21L.A.273(e) Production control system
• 21.2 Scope
• AMC2 21L.B.46(c) Investigation
• GM1 21L.A.124(e) Management system for production and 21L.A.126(e) Scope of work
• GM 21.A.101 Establishing the certification basis of changed aeronautical products
• 21L.B.21 Findings and observations
• 21.A.301 Scope
• 21L.A.6 Marking
• GM 21.A.124(b)(2) Application - Minimum information to include with the application
• GM1 21L.A.103 Classification of changes to the design of an aircraft for which design compliance has been declared
• AMC1 21.A.239(e) Design management system
• AMC3 21.B.120(a) Initial certification procedure
• GM1 21L.A.273(a)
• AMC1 21L.A.105(b) Declaration of design compliance for minor changes
• GM 21.A.124(b)(1)(i) Applicability - Inappropriate approval under Subpart G
• Appendix III --EASA Form 52B -- Aircraft statement of conformity
• AMC1 21.A.124A(b) and 21.A.134A(b) Means of compliance
• GM1 21L.A.23(b) Demonstration of design capability
• GM to 21.A.62, 21.A.108 and 21.A.120B Availability of Operational Suitability Data
• AMC2 21.B.435 Changes in the design management system
• Appendix IV -- EASA Form 20b -- Permit to Fly (issued by approval organisations)
• GM 21.A.710 Approval of flight conditions
• 21.A.179 Transferability and re-issuance within Member States
• SUBPART E -- SUPPLEMENTAL TYPE-CERTIFICATES
• AMC2 21.B.432(b) Oversight programme
• GM1 21L.A.193(b)(6) Part that is part of a higher-level assembly
• 21.A.233 Eligibility
• AMC 21.A.602B(b)(2) Procedures for ETSO authorisations
• AMC1 21L.B.102(c) Investigation
• GM1 21L.A.107(c) Declaration of design compliance for a major change
• GM4 21.A.15(d) Application
• AMC1 21L.A.123(c) Declaration of production capability
• 21.A.439 Production of repair parts
• GM1 21L.B.61(c)(1) Detailed technical specifications and applicable environmental protection requirements for declarations of design compliance
• AMC1 21.A.3B(b) Failures, malfunctions and defects
• 21.A.143 Production organisation exposition
• SUBPART M -- DESIGN OF REPAIRS TO TYPE-CERTIFIED PRODUCTS
• 21L.A.208 Requirements for the approval of a major repair design
• 21.A.235 Issue of design organisation approval
• Appendix H to GM 21.A.101 Examples of documenting the proposed certification basis list
• GM1 21L.B.144(a) Oversight programme
• GM 21.A.21(b), 21.A.95(c), 21.A.97(c), 21.A.115(c), 21.B.103(b), 21.B.107(b) and 21.B.111(b) Approval of operational suitability data (OSD)
• 21.A.120B Availability of operational suitability data
• 21.A.115 Requirements for approval of major changes in the form of a supplemental type-certificate
• AMC1 21.A.7(c) Completeness and timely availability of the ICA
• 21.A.211 Duration and continued validity
• 21.A.118A Obligations and EPA marking
• SUBPART B -- TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES
• GM2 21L.A.124(b) Management system for production
• GM1 21L.A.108 Compliance activities for declaring compliance of a major change
• 21L.B.252 Oversight programme
• 21L.B.82 Investigation and issuance of an approval of a minor change to a type certificate
• 21L.A.107 Declaration of design compliance for a major change
• AMC1 21L.B.221 Initial oversight investigation of a declaration of design compliance of a major repair design to an aircraft for which design compliance has been declared
• AMC1 21.B.432 Oversight programme
• AMC1 21.B.55(a)(1) and (a)(2) Record-keeping
• GM1 21.A.143 Production organisation exposition
• 21.B.240 Changes in production management system
• AMC3 21.A.7(a) DAH responsibility to check the supplier data which is part of the ICA or referenced with the ICA
• GM No 3 to Appendix XII. Demonstration of compliance with competence level 1 or level 2 requirements
• GM1 21.A.139(c) Production management system
• AMC1 21.B.432(d) and (e) Oversight programme
• AMC1 21.B.25(d) Management system
• GM 21.A.33(d) Inspections and tests
• 21.A.621 Transferability
• GM1 21.A.7(b) Other persons required to comply
• GM 21.A.605(b) Reporting from the compliance demonstration process and updates to the certification programme
• AMC1 21.A.125B(c), 21.A.158(c), 21.A.258(c) Findings and observations
• GM 21.B.320(b)(6) Investigation
• GM No 1 to Appendix XII - Lead Flight Test Engineer (LFTE)
• GM 21.A.131 Scope - Applicable design data
• AMC 21.A.15(b)(5) Breakdown of the certification programme into compliance demonstration items (CDIs)
• Annex Ib
• 21.A.307 The eligibility of parts and appliances for installation
• GM1 21.A.145(c)(1) Resources
• 21.B.111 Issuance of a supplemental type-certificate
• 21.A.709 Application for approval of flight conditions
• AMC1 21.B.222(b) Oversight programme
• SUBPART O -- EUROPEAN TECHNICAL STANDARD ORDER AUTHORISATIONS
• 21.A.431B Standard repairs
• GM1 21.B.115(b) and (c) and 21.B.215(b) and (c) Means of Compliance
• GM1 21L.A.24(c) Application for a type certificate
• 21.A.239 Design management system
• 21.A.4 Coordination between design and production
• GM1 21L.A.45 Detailed technical specifications and environmental protection requirements that are applicable to aircraft subject to declarations of design compliance
• 21L.B.162 Issuance or amendment of a certificate of airworthiness or a restricted certificate of airworthiness
• AMC 21.A.33 Inspections and tests
• Appendix A to AMC1 21L.A.44(a) Compliance activities for a declaration of design compliance
• 21L.A.4 Airworthiness directives
• 21L.A.87 Approval of a supplemental type certificate under a privilege
• AMC1 21L.A.12(b) Means of compliance
• (SUBPART L -- NOT APPLICABLE)
• AMC1 21L.A.85(e)(1) Demonstration of compliance
• 21.A.715 Language
• AMC1 21.B.25 Management system
• 21.A.801 Identification of products and control and monitoring units (CMUs)
• 21L.A.191 Scope
• 21L.A.209 Approval of a repair design under a privilege
• 21L.A.44 Compliance activities for a declaration of design compliance
• AMC No 3 to 21.A.263(c)(2) Procedure for the approval of minor changes to a type certificate (TC) which affect the aircraft flight manual (AFM)
• Appendix VIII -- EASA Form 52-- Aircraft/Unmanned Aircraft System statement of conformity
• GM1 21.A.307(b)(3) and (b)(4) Meaning of 'negligible safety effect'
• AMC1 21.B.435 Changes in the design management system
• AMC1 21L.B.16 Management system
• AMC No 1 to 21.A.130(b) Statement of conformity for complete aircraft
• Article 8 Design organisations
• AMC1 21L.A.206(e)(1) Demonstration of compliance
• AMC1 21L.A.205(b) Application for the approval of a repair design to a type-certificated product
• AMC1 21L.A.175(a) Resources of the declared design organisation
• AMC4 21.B.120(a) Initial certification procedure
• GM1 21.A.139(c)(2) Production management system
• AMC1 21L.A.206(e)(3) Demonstration of compliance
• GM No 1 to 21.A.708(c) Safe flight
• GM1 21.A.125B(a), 21.A.158(a) and 21.A.258(a) Findings and observations
• AMC1 21L.A.29 Transferability of a type certificate
• AMC1 21L.A.125(c)(2) Resources of the declared production organisation
• AMC1 21.A.145(c)(1) Resources
• 21L.A.176 Scope of work
• GM 21.A.435(a) Classification of repair designs
• GM1 21L.A.143(d)(1)(iii) Application for a certificate of airworthiness or a restricted certificate of airworthiness
• Appendix A to GM1 21L.A.103 Classification of changes to the design of an aircraft for which design compliance has been declared
• 21.A.130 Statement of conformity
• 21L.A.45 Detailed technical specifications and environmental protection requirements that are applicable to aircraft subject to declarations of design compliance
• GM1 21L.A.177(e) Obligations of the declared design organisation
• GM1 21L.A.3(a)
• SUBPART P -- PERMIT TO FLY
• AMC1 21.A.14(b) Demonstration of capability
• GM1 21.A.174(b)(3)(ii) Application
• 21L.A.143 Application for a certificate of airworthiness or a restricted certificate of airworthiness
• AMC2 21.A.145(c)(2) Resources
• AMC1 21.A.139(c)(2) Production management system
• 21L.A.10 Access and investigation
• AMC1 21L.A.11(a) Findings and observations
• AMC No 1 to 21.A.133(b) and (c) Eligibility - Link between design and production organisations
• 21.B.30 Allocation of tasks to qualified entities [applicable until 21 February 2026] / 21.B.30 Allocation of tasks [applicable from 22 February 2026 - Regulation (EU) 2023/203]
• 21L.B.142 Registration of a declaration of production capability
• 21.A.607 ETSO authorisation privileges
• GM1 21L.A.193(b)(3)
• Appendix II -- EASA Form 45B -- Restricted noise certificate
• GM1 21.A.239(c)(5)(i) Design management system
• GM1 21L.A.174(c) Management system for design
• (SUBPART N -- NOT APPLICABLE)
• 21.A.305 Approval of parts, appliances, and control and monitoring unit (CMU) components
• GM1 21.A.243(d) Handbook
• AMC1 21.A.125B(a)(3), 21.A.158(a)(3) and 21.A.258(a)(3) Findings and observations
• AMC1 21.B.220 Initial certification procedure
• 21.A.711 Issuance of a permit to fly
• 21L.B.121 Initial oversight investigation of a declaration of design compliance of a major change to the design of an aircraft for which design compliance has been declared
• 21L.A.21 Scope
• AMC1 21.B.430(a) Initial certification procedure
• AMC2 21.B.432(c) Oversight programme
• 21L.A.164 Transferability and re-issuance of noise certificates and restricted noise certificates within Member States
• 21L.B.45 Designation of the applicable environmental protection requirements for a type certificate
• GM1 21L.A.206(f) Demonstration of compliance
• AMC 21.B.520(b) Application for a permit to fly
• GM1 21.A.112B Demonstration of capability
• GM1 21.A.307(b)(5) Equipment exempted from an airworthiness approval in accordance with Commission Regulation (EU) No 965/2012
• AMC1 21.A.3A(a) Reporting system
• AMC1 21L.B.144 and 21L.B.184 Oversight programme