BS 2A 122; 2A 123; 2A 124:1981 - Specification for clinch nuts (Unified threads) for aircraft

BS 2A 122; 2A 123; 2A 124:1981

Specification for clinch nuts (Unified threads) for aircraft

Status : Confirmed, Current   Published : December 1981


Standard NumberBS 2A 122; 2A 123; 2A 124:1981
TitleSpecification for clinch nuts (Unified threads) for aircraft
StatusConfirmed, Current
Publication Date31 December 1981
Confirm Date02 November 2018
Normative References(Required to achieve compliance to this standard)No other standards are normatively referenced
Informative References(Provided for Information)No other standards are informatively referenced
DescriptorsDesignations, Test equipment, Aircraft components, Brass, Protective coatings, Steels, Air transport engineering, Performance testing, Torque, Inspection, Endurance testing, Qualification approval, Internal-thread fasteners, Aluminium alloys, Nuts, Vibration-resistant fasteners, Dimensions, Hexagonal-head fasteners, Marking, Threaded fasteners, Low-temperature testing, Fitting, Unified screw threads, Statistical quality control, Fasteners, High-temperature testing, Dimensional tolerances, Locknuts, Anodizing, Threaded components, Bronzes, Torsion testing
Title in FrenchSpécification pour les écrous à téton rivé (filetages unifiés) pour l'aéronautique
Title in GermanSpezifikation fuer verniete Muttern (vereinheitlichtes Gewinde) fuer Flugzeuge
ISBN0 580 12355 3
File Size1.359 MB
NotesThis standard was withdrawn in error and has now been reinstated

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