BS EN 3916:2008 - Aerospace series. Insert, thin wall. Salvage procedure for components

BS EN 3916:2008

Aerospace series. Insert, thin wall. Salvage procedure for components

Status : Confirmed, Current   Published : September 2008



1.1 This specification covers the accepted methods for the reclamation of installation holes for standard thin wall inserts, within assemblies. 1.2 To enable rectification when defects or damage occur to the standard insert tapped installation hole, or to rectify any out of position of the hole within the specified parameters of use. 1.3 To control the machining of the existing insert hole and the installation requirements of the replacement oversize thin wall insert.

Standard NumberBS EN 3916:2008
TitleAerospace series. Insert, thin wall. Salvage procedure for components
StatusConfirmed, Current
Publication Date30 September 2008
Confirm Date30 June 2017
Normative References(Required to achieve compliance to this standard)EN 3913, EN 3914, EN 3915, ISO 965-1, EN 3676:1998, ISO 5855-2
Informative References(Provided for Information)No other standards are informatively referenced
International RelationshipsEN 3916:2008
DescriptorsThread inserts, Dimensions, Internal-thread fasteners, Holes, Hand tools, Cutting, Assembling, Repair, Re-usable, Aircraft components, Fasteners, Threaded fasteners
Title in FrenchSérie aérospatiale. Douilles filetées, à paroi mince. Procédure pour récupération
Title in GermanLuft- und Raumfahrt. Gewindeeinsätze, dünnwandig. Verfahren für Nacharbeit von Bauteilen
ISBN978 0 580 60983 1
File Size488 KB

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