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DIN 65349:2001-06

Current
Current

The latest, up-to-date edition.

AEROSPACE - TESTING OF LOCKING TORQUES FOR NUTS AND RELATED THREADED PARTS, WITH METRIC SCREW THREAD - TEST METHODS
Available format(s)

Hardcopy , PDF

Language(s)

German

Published date

01-01-2001

Foreword
1 Scope
2 Normative references
3 Terms and definitions
4 Tightening/untightening cycle
5 Testing of self-locking torques
6 Designation
Annex A (informative) example of test rig for the
        determination of self-locking torques via
        thread friction in accordance with DIN 946

Applicable for testing the self-locking torques to ISO 5858 and LN 65016 when subjecting self-locking nuts and related threaded parts with M thread to LN 9163-1, -2 and -6 or MJ thread to ISO 5855-1 and -2 to acceptance and qualification testing.

DevelopmentNote
Supersedes DIN 65208:04-1983. (09/2014)
DocumentType
Standard
Pages
16
PublisherName
German Institute for Standardisation (Deutsches Institut für Normung)
Status
Current

DIN 29782:1988-07 Aerospace; wire thread inserts; free running or screw-locking; technical specification

DIN EN 10087:1999-01 FREE-CUTTING STEELS - TECHNICAL DELIVERY CONDITIONS FOR SEMI-FINISHED PRODUCTS, HOT ROLLED BARS AND RODS
WL 3.1354-2 : 1987 AEROSPACE; WROUGHT ALUMINIUM ALLOY WITH APPROX. 4,4CU-1,5MG-0,6MN; BARS
ISO 5855-2:1999 Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
ISO 5855-1:1999 Aerospace MJ threads Part 1: General requirements
WL 1.1174 : 1978 UNALLOYED HEAT-TREATABLE STEEL WITH ABOUT 0.35C - RODS AND FORGINGS
WL 1.4534 : 1984 ULTRA HIGH-STRENGTH PRECIPITATION-HARDENING STAINLESS CHROMIUM-NICKEL-MOLYBDENUM-ALUMINIUM STEEL WITH ABOUT 0.04C-13CR-8NI-2.2MO-1AL; RODS AND FORGINGS
ISO 5858:1999 Aerospace Nuts, self-locking, with maximum operating temperature less than or equal to 425 degrees C Procurement specification
WL 1.6604-1 : 1982 HEAT-TREATABLE CHROMIUM-NICKEL-MOLYBDENUM STEEL WITH ABOUT 0.3C-2CR-2NI-0.4MO; RODS AND FORGINGS
WL 1.7224-1 : 1992 AEROSPACE; HARDENED AND TEMPERED CHROMIUM-MOLYBDENUM STEEL WITH APPROX. 0,35C-1CR-2MO; BARS AND WIRE FOR BOLTS AND NUTS TO BE COLD OR HOT FORMED
WL 1.4944-2 : 1984 COR 1 2008 HIGH TEMPERATURE PRECIPITATION-HARDENING NICKEL-CHROMIUM-TITANIUM STEEL WITH ABOUT 0,06C-25NI-15CR-2,1TI-1,2MO; RODS AND FORGINGS
WL 2.4668-4 : 1993 AEROSPACE; HEAT-RESISTING NICKEL ALLOY WITH APPROX. 0,05C-19CR-18FE-5NB-3MO; VACUUM MELTED AND CONSUMABLE ELECTRODE REMELTED; BARS AND WIRE FOR SCREWS AND BOLTS
WL 1.7784-3 : 2012 AEROSPACE SERIES - ULTRAHIGH-STRENGTH CHROMIUM-MOLYBDENUM-VANADIUM STEEL WITH APPROX. 0,4 C - 5 CR - 1,3 MO - 0,5 V - PART 3: BAR AND WIRE FOR COLD-OR-HOT-FORMED BOLTS AND NUTS
LN 65016:2014-05 Self-locking nuts for temperatures up to 425 øC; Procurement Specification; Inactive for new design
DIN 50014:1985-07 CLIMATES AND THEIR TECHNICAL APPLICATION; STANDARD ATMOSPHERES
LN 29962:2001-02 Aerospace - Bolts and nuts - Additional ordering data for special designs and arrangement of code letters in individual items blocks
WL 1.4548-2 : 1989 AEROSPACE; PRECIPITATION-HARDENING STAINLESS CHROMIUM-NICKEL-COPPER STEEL WITH APPROXIMATE 0,05C-16CR-4CU-4NI; BARS AND FORGINGS
DIN 1654-4:1989-10 COLD HEADING AND COLD EXTRUDING STEELS - TECHNICAL DELIVERY CONDITIONS FOR STEELS FOR QUENCHING AND TEMPERING
DIN 17440:2001-03 STAINLESS STEELS - TECHNICAL DELIVERY CONDITIONS FOR DRAWN WIRE

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