auf die PDF haben nur Online-Abonnenten Zugriff.

 

AMC and GM to Part 21

Acceptable Means of Compliance

and

Guidance Material

for the airworthiness and environmental certification of aircraft and related products, parts and appliances, as well as for the certification of design and production organisations

Issue 2

30 October 2012

Amended by

 ED Decision 2013/001/R

ED Decision 2014/007/R

ED Decision 2015/016/R

ED Decision 2015/026/R

ED Decision 2016/003/R

ED Decision 2016/007/R

ED Decision 2017/024/R

 

 

TABLE OF CONTENTS


TERMINOLOGY

 

SECTION A
Subpart A - General
AMC No 1 to 21A.3A(a) Collection, investigation and analysis of data related to Flammability Reduction Means (FRM) reliability
AMC No 2 to 21A.3A(a) Collection, investigation and analysis of data related to ETOPS significant occurrences
GM 21A.3(a) The system for collection, investigation and analysis of data
GM 21A.3(b) Occurrence reporting
AMC 21A.3(b)(2) Reporting to the Agency
GM 21A.3B(d)(4) Defect correction – Sufficiency of proposed corrective action
AMC 21A.3B(b) Unsafe condition
GM 21A.3B(b) Determination of an unsafe condition
AMC 21A.4 Transferring of information on eligibility and approval status from the design holder to production organisations

 

Subpart B – Type-certificates
GM 21A.14(b) Eligibility for alternative procedures
AMC 21A.14(b) Alternative Procedures
GM No 1 to 21.A.15(d) Clarification of the term ‘as applicable’

GM No 2 to 21.A.15(d)

Determination of type or variant
GM No 3 to 21.A.15(d) OSD content
GM No 4 to 21.A.15(d) Scope of operational suitability data
GM No 1 to 21.A.15(d)6 Other type-related operational suitability elements
GM 21A.16B Special Conditions
GM 21.A.17B (a)(1) Reference date for operational suitability certification basis
AMC 21.A.20(b) Certification programme
Appendix to AMC 21.A.20(b) Means of compliance codes
GM 21.A.20(b) Update to the Certification Programme
AMC 21.A.20(c) Compliance documentation
GM 21.A.20(d) Final statement
GM to 21.A.21(f), 21.A.23(b) and 21.A.103(a)4 Approval of OSD
GM 21A.33 Investigation and Tests
GM 21A.35 Flight Tests
GM 21A.35(b)(2) Objective and Content of Function and Reliability Testing
GM 21A.35(f)(1) Flying Time for Function and Reliability Testing
GM 21A.35(f)(2) Flying Time for Function and Reliability Testing
GM to 21.A.62, 21.A108 and 21.A.120B Availability of Operational Suitability Data
GM to 21.A.90A Scope
GM 21.A.90B Standard changes — Certification Specifications

 

(Subpart C – Not applicable)
Subpart D – Changes to type-certificates
GM 21A.91 Classification of changes to a type design
Appendix A to GM 21A.91 Examples of Major Changes per discipline
GM 21A.93(b) Major Changes: Application
GM No 1 to 21.A.93(c) Interaction of changes to the type design and changes to operational suitability data (OSD)
GM No 2 to 21.A.93(c) Interaction of changes to the type design and changes to MMEL
AMC 21.A.97 Compliance demonstration process for major changes
GM 21A.101 Establishing the certification basis of changed aeronautical products
Appendix A to GM 21A.101 CLASSIFICATION OF DESIGN CHANGES
Appendix B to GM 21A.101 APPLICATION CHARTS FOR CHANGED PRODUCT RULE
Appendix C to GM 21A.101 A METHOD TO DETERMINE THE CHANGED AND AFFECTED AREAS
Appendix D to GM 21A.101 OTHER GUIDANCE FOR AFFECTED AREAS
Appendix E to GM 21A.101 PROCEDURE FOR EVALUATING MATERIAL CONTRIBUTION TO SAFETY OR IMPRACTICALITY OF APPLYING LATEST CERTIFICATION SPECIFICATIONS TO A CHANGED PRODUCT
Appendix F to GM 21A.101  THE USE OF SERVICE EXPERIENCE IN THE EXCEPTION PROCESS
Appendix G to GM 21A.101  CHANGED PRODUCT RULE (CPR) DECISION RECORD
Appendix H to GM 21A.101  EXAMPLES OF DOCUMENTING THE PROPOSED CERTIFICATION BASIS LIST
Appendix I to GM 21A.101  RELATED DOCUMENTS
Appendix J to GM 21A.101  DEFINITIONS AND TERMINOLOGY

 

Subpart E – Supplemental type-certificates
GM 21A.112B Demonstration of capability for supplemental type-certificate cases
AMC 21.A.114 Compliance demonstration process for Supplemental Type-Certificate
   
Subpart F – Production without production organisation approval
GM No. 1 to 21A.121 Applicability - Individual product, part or appliance
GM No. 2 to 21A.121 Applicability – Applicable design data
AMC No. 1 to 21A.122 Eligibility – Link between design and production
AMC No. 2 to 21A.122 Eligibility – Link between design and production
GM 21A.124(a) Application – Application form
GM 21A.124(b)(1)(i) Applicability - Inappropriate approval under Subpart G
GM 21A.124(b)(1)(ii) Certification or approval needed in advance of the issue of a POA
GM 21A.124(b)(2) Application - Minimum information to include with the application
GM No. 1 to 21A.125 Letter of agreement - Meaning of individual
GM No. 1 to 21A.125(b) Letter of agreement - Contents of the Manual
GM No. 2 to 21A.125(b) Letter of agreement - Production Inspection System: Functional Tests
GM 21A.125(c) Letter of agreement - Assistance
GM No. 1 to 21A.125B(a) Uncontrolled non-compliance with applicable design data
GM No. 2 to 21A.125B(a) Examples for level one findings
GM 21A.126 Production Inspection System
GM 21A.126(a)(1) Production Inspection System – Conformity of supplied parts, appliances and material
GM 21A.126(a)(2) Production Inspection System - Identification of incoming materials and parts
GM No. 1 to 21A.126(a)(3) Production Inspection System - List of specifications
GM No. 2 to 21A.126(a)(3) Production Inspection System - Means of checking of the production processes
GM 21A.126(a)(4) Production Inspection System – Applicable design/production data procedures
GM 21A.126(b)(1) Production Inspection System - Inspection of parts in process
GM 21A.126(b)(2) Production Inspection System – Suitable storage and protection
GM 21A.126(b)(3) Production Inspection System – Use of derived data instead of original design data
GM 21A.126(b)(4) Production Inspection System – Segregation of rejected material
GM 21A.126(b)(5) Production Inspection System – Engineering and manufacturing review procedure
GM 21A.126(b)(6) Production Inspection System – Recording and record keeping
GM 21A.127 Approved production ground and flight tests
GM No. 1 to 21A.128 Acceptable functional test - Engines
GM No. 2 to 21A.128 Acceptable functional test –Variable pitch propellers
GM No. 3 to 21A.128 Acceptable functional test - Engines and Propellers
GM 21A.129(a) Availability for inspection by the Competent Authority
AMC No. 1 to 21A.129(c) Obligations of the manufacturer – Conformity of prototype models and test specimens
AMC No. 2 to 21A.129(c) Obligations of the manufacturer – Conformity with Applicable Design Data
AMC No. 3 to 21A.129(c) Obligations of the manufacturer – Condition for safe operation
AMC No. 1 to 21A.130(b) Statement of Conformity for Complete Aircraft
AMC No. 2 to 21A.130(b) Statement of Conformity for Products (other than complete aircraft), parts, appliances and materials - The Authorised Release Certificate (EASA Form 1)
AMC 21A.130 (b) (4) Applicable emissions requirements
GM 21A.130 (b) (4) Definitions of engine type certification date and production date
AMC 21A.130(c) Validation of the Statement of Conformity
AMC 21A.130(c)(1) Initial transfer of ownership

 

Subpart G – Production organisation approval for products, parts and appliances
GM 21A.131 Scope – Applicable design data
GM 21A.133(a) Eligibility – Approval appropriate for showing conformity
AMC No. 1 to 21A.133(b) and (c) Eligibility – Link between design and production organisations
AMC No. 2 to 21A.133(b) and (c) Eligibility – Link between design and production organisations
GM 21A.134 Application – Application form and manner
GM No. 1 to 21A.139(a) Quality System
GM No. 2 to 21A.139(a) Quality System – Conformity of supplied parts or appliances
GM 21A.139(b)(1) Quality System – Elements of the quality system
AMC No. 1 to 21A.139(b)(1)(ii) Vendor and sub-contractor assessment, audit and control – Production Organisation Approval (POA) holder using documented arrangements with other parties for assessment and surveillance of a supplier
AMC No. 2 to 21A.139(b)(1)(ii) Vendor and sub-contractor assessment, audit and control - Production Organisation Approval (POA) holder using other party supplier certification
GM No. 1 to 21A.139(b)(2) Quality System – Independent quality assurance function
GM No. 2 to 21A.139(b)(2) Quality System – Adequacy of procedures and monitoring function
GM 21A.143 Exposition – Production Organisation Exposition (POE)
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 21A.145(a) Approval Requirements
GM 21A.145(b)(2) Approval Requirements – Airworthiness, noise, fuel venting and exhaust emissions /production data procedures
GM 21A.145(c)(1) Approval Requirements – Accountable manager
GM 21A.145(c)(2) Approval Requirements – Responsible managers
AMC 21A.145(d)(1) Approval Requirements – Certifying staff
AMC 21A.145(d)(2) Approval Requirements – Record of certifying staff
AMC 21A.145(d)(3) Approval requirements – Evidence of authorisation
GM 21A.147(a) Changes to the approved production organisation – Significant changes
AMC 21A.148 Changes of location – Management during change of location
GM 21A.149 Transferability
GM 21A.151 Terms of approval – Scope and categories
AMC 21A.153 Changes to the terms of approval – Application for a change to the terms of approval
GM 21A.157 Investigations – Arrangements
GM No. 1 to 21A.158(a) Uncontrolled non-compliance with applicable design data
GM No. 2 to 21A.158(a) Examples of level one findings
GM 21A.159(a)(3) Evidence of a lack of satisfactory control
AMC No 1 to 21A.163(c) Computer generated signature
AMC No 2 to 21A.163(c) Completion of the EASA Form 1
AMC 21A.163(d) Privileges – Maintenance
AMC 21A.163(e) Procedure for the issue of a permit to fly including approval of the flight conditions
GM 21A.165(a) Obligations of the holder – Basic working document
GM No. 1 to 21A.165(c) Obligations of the holder – Conformity of prototype models and test specimens
GM No. 2 to 21A.165(c) Obligations of holder – Conformity with type design
GM No. 3 to 21A.165(c) Obligations of the holder – Condition for safe operation
GM No. 4 to 21.165(c) Airworthiness Release or Conformity Certificate
AMC 21A.165(c)(3) Applicable emissions requirements
GM 21A.165(c)(3) Definitions of engine type certification date and production date
GM 21A.165(d) and (h) Obligations of the holder – Recording and archiving system

 

Subpart J – Design organisation approval

GM No. 1 to 21A.239(a)

Design assurance system 

GM No. 2 to 21A.239(a)

Design assurance system for minor changes to type design or minor repairs to products

AMC 21A.239(a)(3)

Design assurance system - Independent system monitoring

AMC 21A.239(b)

Design assurance system - Independent checking function of the showing of compliance

GM 21A.239(c)

Design assurance system

AMC No. 1 to 21A.243(a)

Data requirements

AMC No. 2 to 21A.243(a)

Data requirements - Model content of handbook for organisations designing minor changes to type design or minor repairs to products

GM No. 1 to 21A.243(d)

Statement of qualifications and experience

GM No. 2 to 21A.243(d)

Data requirements - Statement of the qualification and experience- Organisations designing minor changes to type design or minor repairs to products

GM No. 1 to 21A.245

Requirements for approval

GM No. 2 to 21A.245

Requirements for approval - Organisations designing minor changes to type design or minor repairs to products

GM 21A.247

Significant changes in the design assurance system

GM 21A.249

Transferability

GM No. 1 to 21A.251

Terms of approval

GM No. 2 to 21A.251

Terms of approval - Organisations designing minor changes to type design or minor repairs to products

GM 21A.257(a)

Investigations

GM 21A.263(b)

DOA privilege related to compliance documents

AMC 21A.263(b)(1)

Compliance documents with conditions related to engine or propeller without a type-certificate or with unapproved changes and fitted on aircraft for which a permit to fly is requested

AMC No. 1 to 21A.263(c)(1)

Procedure for the classification of changes to type design and repairs as minor and major

AMC No. 2 to 21A.263(c)(1)

Privileges - Organisations designing minor changes to type design or minor repairs to products : classification procedure

AMC No. 1 to 21A.263(c)(2)

Procedure for the approval of minor changes to type design or minor repairs

AMC No. 2 to 21A.263(c)(2)

Privileges - Organisations designing minor changes to type design or minor repairs to products : procedure for the approval of minor changes to type design or minor repairs

GM 21A.263(c)(3)

Issue of information or instructions

GM 21A.263(c)(4)

Procedure for the approval of documentary changes to the Aircraft Flight Manual

AMC 21A.263(c)(6)

Procedure for the approval of the conditions for issue of a permit to fly

AMC 21A.263(c)(7)

Procedure for the issue of a permit to fly

AMC 21A. 265(a)

Administration of the Handbook

GM 21A.265(b)

Use of the Handbook

Subpart K – Parts and appliances

GM No. 1 to 21A.303(c)

Standard Parts

GM No. 2 to 21A.303(c)

Officially recognised Standards

 

Subpart M - Repairs

GM 21A.431(a)

Scope

GM 21.A.431B

Standard repairs — Certification Specifications

GM 21A.431(d)

Repairs to ETSO articles other than an APU

AMC 21A.433 (a) and 21A.447

Repair design and Record Keeping

GM 21A.435(a)

Classification of repairs

GM 21A.437

Issue of repair design approval

GM 21A.437(a)

Issue of repair design approval

AMC 21A.437(b)

Issue of repair design approval

GM 21A.439

Production of repair parts

GM 21A.441

Repair Embodiment

GM 21A.443

Limitations

GM 21A.445

Unrepaired damage

Subpart O – European Technical Standard Order Authorisations

AMC 21A.602B(b)(2)

Procedures for ETSO authorisations

AMC 21A.608

Declaration of Design and Performance

GM to 21A .611

Design changes

Subpart P - Permit to fly

 

GM to Subpart P

 

GM 21A.701(a)

Permit to fly when certificate of airworthiness or restricted certificate of airworthiness is not appropriate

GM 21A.703

Applicant for a permit to fly

GM 21A.705

Competent Authority

GM 21A.707(b)

GM 21A.707(b)

GM 21A.708(b)(6)

Continuing airworthiness

GM No. 1 to 21A.708(c)

Safe flight

GM No. 2 to 21A.708(c)

Substantiations

GM No. 3 to 21A.708(c)

Operation of Overweight Aircraft

GM 21A.708(d)

Control of aircraft configuration

AMC 21A.709(b)

Submission of documentation supporting the establishment of flight conditions

GM 21A.710

Approval of flight conditions

GM 21A.711(e)

Additional conditions and restrictions

GM 21A.713

Changes

GM 21A.719

Transfer of a permit to fly

Subpart Q – Identification of products, parts and appliances

GM 21A.804(a)(1)

Identification of parts and appliances

SECTION B

Subpart A – General

GM 21B.20

Responsibility for implementation

GM 21B.25(a)

Organisation

GM 21B.25(b)

Resources

GM 21B.25(c)

Qualification and training

AMC 21B.30(a)

Documented procedures

AMC 21B.35(a)

Changes

GM 21B.40

Principles for the resolution of disputes

GM No. 1 to 21B.45

Co-ordination with other related activities

GM No. 2 to 21B.45

Co-ordination

GM No. 3 to 21B.45

Reporting - Information relevant to registers established by the Agency

GM 21B.55

Record keeping for design approvals transferred to the Agency

 

Subpart F - Production without production organisation approval

AMC 21B.120(a)

Investigation team - Qualification criteria for the investigation team members

AMC 21B.120(c)(1)

Evaluation of applications

GM 21B.120(c)(3)

Investigation preparation and planning

GM 21B.120(c)(5) and (6)

Auditing and investigation findings

GM 21.B.125(a)

Objective evidence

AMC 21B.130

Issue of the letter of agreement

GM 21B.130(b)

Issue of the letter of agreement

AMC 21B.140

Amendment of a letter of agreement

GM 21B.150(d)

Record keeping - Traceability of release certificates

 

Subpart G- Production organisation approval

GM 21B.220(a)

Investigation team

AMC 21B. 220(c)

Procedures for investigation - Evaluation of applications

GM No. 1 to 21B.220(c)

Procedures for investigation - Investigation preparation and planning

GM No. 2 to 21B.220(c)

Procedures for investigation – General

GM No. 3 to 21B.220(c)

Procedures for investigation - POA applications received from organisations with facilities/partners/suppliers/subcontractors located in a third country

GM No. 4 to 21B.220(c)

Procedures for investigation – Competent Authority surveillance of suppliers of a POA holder located in other Member States

GM 21B.225(a)

Objective evidence

AMC 21B.225(a)

Notification of findings

AMC No. 1 to 21B.230

Issue of the certificate

GM 21B.235(a)(4)

Guide to the conduct of monitoring production standards

GM 21B.235(b)

Maintenance of the POA - Work allocation within the Competent Authority

GM 21B.235(b) and (c)

Continued surveillance

AMC 21B.235(c)

Continuation of POA

AMC No. 1 to 21B.240

Application for significant changes or variation of scope and terms of the POA

GM 21B.245

Continued validity

AMC 21B.245

Corrective action plan

Subpart H - Airworthiness Certificates

GM 21B.320(b)(6)

Investigation

GM 21B.325(a)

Airworthiness Certificates

GM 21B.325(b)

Completion of the Airworthiness Review Certificate by a Member State

Subpart I - Noise certificates

GM 21B.425(a)

Noise Certificates

Subpart P — Permit to fly

AMC 21B.520(b) Application for a permit to fly

GM No 1 to Appendix XII to Part-21

Lead Flight Test Engineer (LFTE)

GM No. 2 to Appendix XII to Part-21

Competence and experience of pilots for Category 3 and Category 4 flight tests and of Lead Flight Test Engineers (LFTEs)

GM No 3 to Appendix XII

Demonstration of compliance with competence level 1 or level 2 requirements

AMC No. 1 

Training courses for Lead Flight Test Engineers (LFTEs)

AMC No. 2

Conditions for appointment of Lead Flight Test Engineers (LFTEs) — Medical fitness

AMC No. 3

Demonstration of compliance with competence level 1 or level 2 requirements

 

AMC & GM for PART 21

 



auf die PDF haben nur Online-Abonnenten Zugriff.
Diese Webseite nutzt Cookies. Wenn Sie weiter auf dieser Seite bleiben ohne die Cookie-Einstellungen in Ihrem Browser zu ändern, stimmen Sie zu unsere Cookies zu verwenden. Weiterlesen …