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

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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
Cross ReferencesBS 919:Part 1, BS 1580:Parts 1 & 2, BS 1580:Part 3, BS 2874, BS 3488, BS A 102, BS A 125 to A 168, BS A 169, BS A 180, BS A 181, BS A 186, BS A 187, BS A 192, BS A 193, BS A 200, BS A 201, BS A 213 to A 216, BS B 11, BS L 102, BS L 168, BS S 95, BS S 112, BS S 113, BS S 154, DEF 151, DEF 2331, DEF STAN 03-8, DTD 417, DTD 904
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NotesThis standard was withdrawn in error and has now been reinstated

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