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Standard Practice for Design, Alteration, and Certification of Airplane Electrical Wiring Systems (Includes all amendments And changes 10/6/2015).
Automatische name übersetzung:
Standard Praxis für Gestaltung, Umbau und Zertifizierung von Flugzeug Electrical Wiring Systems
NORM herausgegeben am 1.9.2007
Bezeichnung normen: ASTM F2639-07e1
Anmerkung: UNGÜLTIG
Ausgabedatum normen: 1.9.2007
SKU: NS-54287
Zahl der Seiten: 101
Gewicht ca.: 334 g (0.74 Pfund)
Land: Amerikanische technische Norm
Kategorie: Technische Normen ASTM
Keywords:
aircraft, airplane electrical wiring systems, alteration, aviation, certification, design, ICS Number Code 49.060 (Aerospace electric equipment and systems)
Significance and Use | ||||||||
Design—The design procedures defined in this practice are intended to provide acceptable guidance in the original design of electrical systems. Alteration—The alteration procedures defined in this practice are intended to provide acceptable guidance for modification of general aviation aircraft. Design of any modification shall follow the practices and processes defined in the design sections of this practice. Certification—Certification guidance provided in this practice is intended to provide generally accepted procedures and processes for certification of original and modified electrical systems and equipment. Requirements for certification shall be coordinated with the applicable National Aeronautics Association/Civil Aeronautics Administration (NAA/CAA) regulatory agency. |
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1. Scope | ||||||||
1.1 Definition - This practice defines acceptable practices and processes for the design, alteration, and certification of electric systems and installations in general aviation aircraft. This practice does not change or create any additional regulatory requirements nor does it authorize changes in or permit deviations from existing regulatory requirements. 1.2 Applicability - The guidance provided in this practice is directed to air carriers, air operators, design approval holders, Supplemental Type Certificate (STC) holders, maintenance providers, repair stations, and anyone performing field approval modifications or repairs. 1.3 Protections and CautionsThis practice provides guidance for developing actions and cautionary statements to be added to maintenance instructions for the protection of wire and wire configurations. Maintenance personnel will use these enhanced procedures to minimize contamination and accidental damage to electrical wiring interconnection system (EWIS) while working on aircraft. 1.4 "Protect and Clean As You Go" Philosophy - This philosophy is applied to aircraft wiring through inclusion in operators maintenance and training programs. This philosophy stresses the importance of protective measures when working on or around wire bundles and connectors. It stresses how important it is to protect EWIS during structural repairs, STC installations, or other alterations by making sure that metal shavings, debris, and contamination resulting from such work are removed. 1.5 Values - The values given in inch-pound units are to be regarded as the standard. The values in parentheses are for information only. See Appendix X2 for SI-based prefixes and powers of 10. Note 1Where SI units are required, refer to Annex 5 of ICAO. This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use. |
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2. Referenced Documents | ||||||||
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