Appendix 1 to AMC 20-29– Applicable CSs and Relevant Guidance

ED Decision 2010/003/R

1.         Applicable CSs. A list of applicable CS paragraphs is provided for subjects covered in this AMC (see notes). In most cases, these CS paragraphs apply regardless of the type of materials used in aircraft structures.

Notes:

(1)        This list may not be all inclusive and there may be differences between certification agencies (e.g. FAA and the Agency).

(2)        Special conditions may be issued in accordance with Part-21 21.A.16B for novel and unusual design features (e.g., new composite materials systems).

2.         Guidance

FAA issues guidance providing supportive information of showing compliance with regulatory requirements. Guidance may include the advisory circulars (AC) and policy statements (PS). In general, an AC presents information concerning acceptable means, but not the only means, of complying with regulations. The guidance listed below is deemed supportive to the purposes of this AMC. These FAA documents can be located via website:http://www.faa.gov/regulations_policies/. In addition, EUROCAE have developed industry standards that are recognised by the Agency.

Note: Many of the FAA documents are harmonised with EASA. Applicants should confirm with the Agency if in doubt regarding the status and acceptance of any such documents by the Agency.

a.         FAA/EUROCAE guidance documents

—            AC 20-53B “Protection of Airplane Fuel Systems Against Fuel Vapor Ignition Due to Lightning” [6/06]

—            AC 20-135 "Powerplant Installation and Propulsion System Component Fire Protection Test Methods, Standards, and Criteria" [2/90]

—            AC 21-26 "Quality Control for the Manufacture of Composite Structures" [6/89]

—            AC 21-31 "Quality Control for the Manufacture of Non-Metallic Compartment Interior Components" [11/91] 

—            AC 23-15A “Small Airplane Certification Compliance Program” [12/03]

—            AC 23-20 "Acceptance Guidance on Material Procurement and Process Specifications for Polymer Matrix Composite Systems" [9/03]

—            AC 25.571-1C “Damage Tolerance and Fatigue Evaluation of Structure” [4/98]

—            AC 29 MG 8 “Substantiation of Composite Rotorcraft Structure” [4/06]

—            AC 35.37-1A "Guidance Material for Fatigue Limit Tests and Composite Blade Fatigue Substantiation" [9/01]

—            AC 145-6 "Repair Stations for Composite and Bonded Aircraft Structure" [11/96]

—            RTCA DO-160 / EUROCAE ED-14

—            EUROCAE ED-81 “Certification of Aircraft Electrical/Electronic Systems for the Indirect Effects of Lightning”

—            EUROCAE ED-84 “Aircraft Lightning Environment and Related Test Waveforms”

—            EUROCAE ED-91 “Aircraft Lightning Zoning”

—            EUROCAE ED-107 “Guide to Certification of Aircraft in a High Intensity Radiated Field (HIRF)”

—            EUROCAE ED-113 Aircraft Lightning Direct Effects Certification

—            EUROCAE ED-14E Environmental Conditions and Test Procedures for Airborne Equipment

—            FAA Technical Report “Aircraft Lightning Protection Handbook” (DOT/FAA/CT-89/22).

b.         FAA Policy Statements

—                         "Static Strength Substantiation of Composite Airplane Structure"[PS-ACE100-2001-006, December 2001]

—                         "Final Policy for Flammability Testing per 14 CFR Part 23, Sections 23.853, 23.855 and 23.1359" [PS-ACE100-2001-002, January 2002]

—                         “Material Qualification and Equivalency for Polymer Matrix Composite Material Systems" [PS-ACE100-2002-006, September 2003]

—                         “Bonded Joints and Structures - Technical Issues and Certification

—                         Considerations” [PS-ACE100-2005-10038, September 2005]

[Amdt 20/6]