Type Certification and Entry into Service. Ing. Giuseppe Serpico
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1 Type Certification and Entry into Service Ing. Giuseppe Serpico
2 AUTORITA AERONAUTICHE ICAO(International Civil Aviation Organization) The International Civil Aviation Organization (ICAO) is a UN specialized agency, created in 1944 upon the signing of the Convention on International Civil Aviation (Chicago Convention). ICAO works with the Convention s 191 Member States and global aviation organizations to develop international Standards and Recommended Practices (SARPs) which States reference when developing their legally-enforceable national civil aviation regulations.
3 AUTORITA AERONAUTICHE EASA (European Aviation Safety Agency) The European Aviation Safety Agency is the centrepiece of the European Union s aviation safety system comprised of the Agency, the European Commission and the National Aviation Authorities (NAAs). The main tasks of the Agency currently include: Drafting aviation safety legislation and providing technical advice to the European Commission and to the Member States; Inspections and training to ensure uniform implementation of European aviation safety legislation in all Member States; Airworthiness and environmental type-certification of aeronautical products, parts and appliances; Approval of aircraft design organisations world-wide and of production and maintenance organisations outside the EU; Coordination of the European Community SAFA (Safety Assessment of Foreign Aircraft) programme; Coordination of safety programmes, data collection, analysis and research to improve aviation safety.
4 AUTORITA AERONAUTICHE ENAC (Ente Nazionale Aviazione Civile) L'Ente Nazionale per l'aviazione Civile, unica Autorità di regolazione tecnica, certificazione, vigilanza e controllo nel settore dell'aviazione civile in Italia, è stato istituito il 25 luglio 1997 con Decreto Legislativo n. 250/97.
5 EASA MEMBERSHIP
6 EASA EASA REGULATION
7 EASA REGULATION REFERENCE
8 Initial Airworthness
9 Continuing Airworthness
10 ANNEX I PART 21 Certification of aircraft and related products, parts and appliances, and of design and production organisations SUBPART A GENERAL PROVISIONS SUBPART B TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES SUBPART D CHANGES TO TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES SUBPART E SUPPLEMENTAL TYPE-CERTIFICATES SUBPART F PRODUCTION WITHOUT PRODUCTION ORGANISATION APPROVAL SUBPART G PRODUCTION ORGANISATION APPROVAL SUBPART H CERTIFICATES OF AIRWORTHINESS AND RESTRICTED CERTIFICATES OF AIRWORTHINESS SUBPART I NOISE CERTIFICATES SUBPART J DESIGN ORGANISATION APPROVAL SUBPART K PARTS AND APPLIANCES SUBPART M REPAIRS SUBPART O EUROPEAN TECHNICAL STANDARD ORDER AUTHORISATIONS SUBPART P PERMIT TO FLY SUBPART Q IDENTIFICATION OF PRODUCTS, PARTS AND APPLIANCES
11 SUBPART B TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES SUBPART J DESIGN ORGANISATION APPROVAL CERTIFICATION SPECIFICATIONS CERTIFICATION PROCESS SUBPART G PRODUCTION ORGANISATION APPROVAL SUBPART P PERMIT TO FLY
12 SUBPART J DOA DESIGN ORGANISATION APPROVAL HDO HEAD OF DESIGN ORGANIZATION A/W OFFICE SYSTEM MONITORING CVE Compliance Verification Engineers CM Configuration Management Compliance Engineers
13 SUBPART J DOA DESIGN ORGANISATION APPROVAL Technical Specialisation Panel PCM 0 Flight Test Pilot 1/P Flight 1 Handling quality and performance 2 Structures 3 Hydro-mechanical System 4 Electrical System/HIRF 5 Avionics 6 Power plant and Fuel system and Fire Protection system 7 Cabin Safety 8.1 Environmental control systems 8.2 Noise 9 Software 10
14 SYSTEM MONITOR DESIGN ORGANIZATION SYSTEM TYPE INVESTIGATION SUBPART J DOA DESIGN ORGANISATION APPROVAL AIRWORTHINESS AND ENVIRONMENTAL PROTECTION REQUIREMENTS PRODUCT SPECIFICATION DESIGN TYPE INVESTIGATION PROGRAMME ANALYSIS AND TEST SHOW COMPLIANCE VERIFICATION OF COMPLIANCE DECLARATION OF COMPLIANCE ACCEPTANCE BY DCA CERTIFICATION (TC, MOD/ REPAIR APPROVAL) DESIGN ASSURANCE SYSTEM COMPONENTS
15 CERTIFICATION SPECIFICATIONS
16 CERTIFICATION SPECIFICATIONS
17 CERTIFICATION SPECIFICATIONS
18 CERTIFICATION SPECIFICATIONS
19 CERTIFICATION SPECIFICATIONS Amendment 2 23 December 2010
20 CERTIFICATION SPECIFICATIONS
21 CERTIFICATION SPECIFICATIONS Amendment 3 23 December 2010
22 CERTIFICATION SPECIFICATIONS Amendment 1 29 January 2013
23 CERTIFICATION SPECIFICATIONS Amendment 3 29 January 2013
24 CERTIFICATION PROCESS Certification Process Certification Basis MOC Identification Certification Programme Type Certificate Product Specification Aircraft Integration System Specification System Integration Item Specification Item Integration
25 CERTIFICATION PROCESS TYPE OF COMPLIANCE MEANS OF COMPLIANCE ASSOCIATED COMPLIANCE DOCUMENTS Engineering Evaluation: MC 0 = Compliance Statement MC 1 = Design Review MC 2 = Calculation/Analysis MC 3 = Safety Assessment Reference to type design Description Notes, Drawings Substantiation Reports Safety Analysis MC 4 = Laboratory Tests Tests : MC 5 = Ground Tests MC 6 = Flight Tests Test: Programme/Report/Interpretation MC 8 = Simulation Inspection : MC 7 = Design Inspection Inspection Reports Equipment Qualification : MC 9 = Equipment Qualification See Note Note : Equipment Qualification is a process which may include all previous means of compliance.
26 TYPE CERTIFICATE
27 TYPE CERTIFICATE A/C Type Configuration Engine TC Propeller TC APU TC (if necessary) AFM A/W Limitations C.M.R. Equipment List Maintenance Planning Document (MSG-3)
28 ENTRY INTO SERVICE AFM (Aircraft Flight Manual) MMEL (Master Minimum Equipment List) FCD (Flight Crew Data) CCD (Cabin Crew Data) AMM (Aircraft Maintenance Manual)
29 ENTRY INTO SERVICE Initial Issue 31 January 2014
30 ENTRY INTO SERVICE Initial Issue 31 January 2014
31 ENTRY IN TO SERVICE Initial Issue 31 January 2014
32 Grazie A.De.Sy. Consulting srl Ing. Giuseppe Serpico
Certification Directorate. Continuing Airworthiness of Type Design Procedure (CAP) C.P006-01
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