DIN 65349:2001-06
Current
The latest, up-to-date edition.
AEROSPACE - TESTING OF LOCKING TORQUES FOR NUTS AND RELATED THREADED PARTS, WITH METRIC SCREW THREAD - TEST METHODS
Hardcopy , PDF
German
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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