FAA AC 20-107 : 2009
Current
The latest, up-to-date edition.
COMPOSITE AIRCRAFT STRUCTURE
Hardcopy , PDF
English
01-01-2009
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1. Purpose of this Advisory Circular (AC)
2. To Whom this AC Applies
3. Cancellation
4. Related Regulations and Guidance
5. General
6. Material and Fabrication Development
7. Proof of Structure - Static
8. Proof of Structure - Fatigue and Damage Tolerance
9. Proof of Structure - Flutter and Other Aeroelastic
Instabilities
10. Continued Airworthiness
11. Additional Considerations
Appendix 1 - Applicable Regulations and Relevant Guidance
Appendix 2 - Definitions
Appendix 3 - Change of Composite Material and/or Process
Specifies an acceptable means, but not the only means of showing compliance with the provisions of Title 14 of the Code of Federal Regulations (14 CFR) parts 23, 25, 27, and 29 regarding airworthiness type certification requirements for composite aircraft structures involving fiber reinforced materials, e.g., carbon and glass fiber reinforced plastics.
| DocumentType |
Standard
|
| Pages |
37
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 25.613-1 : 2003 | MATERIAL STRENGTH PROPERTIES AND MATERIAL DESIGN VALUES |
| FAA AC 35-1 : 2008 | CERTIFICATION OF PROPELLERS |
| DEFSTAN 00-970(PT1)SEC3/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
| DEFSTAN 00-970(PT1)SEC3/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
| DEFSTAN 00-970(PT1)SEC3/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
| DEFSTAN 00-970(PT1)SEC3/14(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
| DEFSTAN 00-970(PT1)SEC3/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3 - STRUCTURE |
| DEFSTAN 00-970(PT1)SEC3/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3 - STRUCTURE |
| DEFSTAN 00-970(PT1)SEC3/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
| FAA AC 20-66 : 2011 | PROPELLER VIBRATION AND FATIGUE |
| FAA AC 120-77 : 0 | MAINTENANCE AND ALTERATION DATA |
| FAA AC 23-19 : 2007 | AIRFRAME GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES |
| FAA AC 147-3 : 2015 | CERTIFICATION AND OPERATION OF AVIATION MAINTENANCE TECHNICIAN SCHOOLS |
| SAE AIR 4938 : 2017 | COMPOSITE AND BONDED STRUCTURE TECHNICIAN/SPECIALIST TRAINING DOCUMENT |
| FAA AC 23-16 : 0 | POWERPLANT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS |
| FAA AC 145-6 : 0 | REPAIR STATIONS FOR COMPOSITE AND BONDED AIRCRAFT STRUCTURE |
| SAE AIR 5552 : 2015 | DEVELOPMENT AND QUALIFICATION OF COMPOSITE LANDING GEARS |
| FAA AC 121-22 : 2012 | MAINTENANCE REVIEW BOARDS, MAINTENANCE TYPE BOARDS, AND OEM/TCH RECOMMENDED MAINTENANCE PROCEDURES |
| DEFSTAN 00-970(PT1)SEC3/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| FAA AC 21-26 : 2010 | QUALITY SYSTEM FOR THE MANUFACTURE OF COMPOSITE STRUCTURES |
| FAA AC 120-104 : 2011 | ESTABLISHING AND IMPLEMENTING LIMIT OF VALIDITY TO PREVENT WIDESPREAD FATIGUE DAMAGE |
| FAA AC 43-214 : 2016 | REPAIRS AND ALTERATIONS TO COMPOSITE AND BONDED AIRCRAFT STRUCTURE |
| FAA AC 65-33 : 2017 | DEVELOPMENT OF TRAINING/QUALIFICATION AND CERTIFICATION PROGRAMS FOR COMPOSITE MAINTENANCE TECHNICIANS |
| FAA AC 23-20 : 2003 | ACCEPTANCE GUIDANCE ON MATERIAL PROCUREMENT AND PROCESS SPECIFICATIONS FOR POLYMER MATRIX COMPOSITE SYSTEMS |
| FAA AC 20-138 : 2014 | AIRWORTHINESS APPROVAL OF POSITIONING AND NAVIGATION SYSTEMS |
| FAA AC 23-2 : 2013 | FLAMMABILITY TESTS |
| SAE ARP 6461 : 2013 | GUIDELINES FOR IMPLEMENTATION OF STRUCTURAL HEALTH MONITORING ON FIXED WING AIRCRAFT |
| FAA AC 25.571-1 : 2011 | DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE |
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