Source: http://www.faa.gov/regulations_policies/advisory_circulars/index.cfm/go/document.list/parentTopicID/101/display/current/changeNumber/0/sortResults/1/currentPage/3/sortColumn/dateIssued/sortOrder/ASC
Timestamp: 2015-02-28 05:48:10
Document Index: 49515630

Matched Legal Cases: ['art 23', 'arts 23', '§ 23', 'arts 23', 'arts 23', 'art 33', 'art 23', 'arts 23']

ANM-100 Recommended Method for FAA approval of Aircraft Fire Extinguishing System Components
Provides guidance on the various aspects that should be considered in the FAA approval process of fire extinguishing system components manufactured under a Production Certificate (PC), components to be FAA approved under the Part Manufacturer Approval (PMA) process, or design changes to components originally approved by either method. This AC does not constitute a regulation, however, it provides a method, for obtaining approval of aircraft fire extinguishing system components. This is intended to enhance the standardization of all FAA Aircraft Certification Offices (ACO) and Manufacturing Inspection District Offices (MIDO) in the approval process of the critical components of an aircraft fire extinguishing system. 09-22-2000
ANM-100 Methodology for Dynamic Seat Certification by Analysis for Use in Part 23, 25, 27, and 29 Airplanes and Rotorcraft
This advisory circular (AC) sets forth an acceptable means, but not the only means, for demonstrating compliance to the following by computer modeling analysis techniques validated by dynamic tests: • Title 14 Code of Federal Regulations (14 CFR) parts 23, 25, 27, and 29, §§ 23.562, 25.562, 27.562, and 29.562. • The Technical Standard Order (TSO) associated with the above regulations, TSO-C127/C127a. 05-19-2003
AIR-100 Turbojet, Turboprop, and Turbofan Engine Induction System Icing and Ice Ingestion
This advisory circular (AC) provides guidance and acceptable methods, but not the only methods, for demonstrating compliance with the applicable engine induction system icing and engine ice ingestion requirements. These requirements are applicable to the Federal Aviation Regulations, parts 23, 25, and 33 of Title 14 of the Code of Federal Regulations (14 CFR parts 23, 25, and 33). The primary purpose of this AC is to reduce inconsistencies and eventual surprises to both engine manufacturers and engine installers, when installing a part 33 certified engine in a part 23 or 25 aircraft. 02-02-2004
20-65A
Provides general information and guidance concerning issuance of airworthiness certificates for U.S. registered aircraft, and issuance of special flight authorizations for operation in the United States of foreign aircraft not having standard airworthiness certificates issued by the country of registry. 07-08-2004
AIR-100 Reusable Software Components
Supplies one means for developers, integrators and applications to gain FAA acceptance of software. 12-07-2004
20-37E
AFS-350 Aircraft Propeller Maintenance
Provides information and suggested procedures to increase service life and to minimize blade failures of metal propellers. 09-09-2005
AFS-300 Guide for Developing a Receiving Inspection System for Aircraft Parts and Material
Provides guidance and information for incorporation into operators' existing receiving/inspection systems to help prevent the introduction of unairworthy parts into inventories. 12-12-2005
20-53B
AIR-100 Protection of Aircraft Fuel Systems Against Fuel Vapor Ignition Caused by Lightning
Provides information and guidance concerning an acceptable means, but not the only means, of compliance with Parts 23 or 25 of the Federal Aviation Regulations (FAR) applicable to preventing ignition of fuel vapors due to lightning. 06-05-2006
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