SAEITC TS172-4
Current
The latest, up-to-date edition.
TS172 Performance Specification for Nut, Union, Metric, Threaded, Self- Locking A286 Dry Film Lubricated
Hardcopy , PDF
English
01-12-2004
1.0 Scope and field of application
2.0 References
2.1 Controlling organisations
3.0 Definitions
3.1 Production batch
3.2 Inspection lot
3.3 Discontinuities
3.4 Test temperature
3.5 Simple random sampling
3.6 Critical defect
3.7 Major defect
3.8 Minor defect
3.9 Sampling plan
3.10 Limiting quality
3.11 Acceptable quality level
3.12 Finished union nut
3.13 Definition document
3.14 Self locking torque
3.15 Seating torque
3.16 Unseating torque
3.17 Breakaway torque
3.18 Crimp
4.0 Certification and quality assurance
4.1 Qualification
4.2 Acceptance
4.3 Quality system certification
4.4 Responsibility for inspection and test methods
4.5 Inspection and test report
5.0 Table 1: Technical requirement and test methods
5.1 Materials
5.2 Dimensions; tolerances of form and position;
threads and quality
5.3 Manufacturing
5.4 Mechanical properties
5.5 Metallurgical properties
5.6 Product identification
5.7 Delivery
Table 2: Summary of tests - Qualification and production
acceptance
Table 3: Qualification testing requirements for union
nut samples
Table 4: Dimensions and materials of mandrels for
permanent set tests
Table 5: Values for breakaway torque; locking torque
and assembly torque
Table 6: Dimensions and materials of test pieces for
reusability tests
Table 7: Classification of defects
Table 8: Sampling plans for visual inspections and
dimensional characteristics
Table 9: Sampling plans for the inspection of mechanical
and metallurgical characteristics
Table 10: Maximum depth of permissible discontinuities
Covers the technical qualification and quality assurance requirements for self locking union nuts.
DocumentType |
Standard
|
Pages |
24
|
PublisherName |
SAE Industry Technologies Consortia
|
Status |
Current
|
ISO 3534:1977 | Statistics — Vocabulary and symbols |
ISO 5855-2:1999 | Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts |
SAE AMS 5737 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS AND TUBING, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED, 1650 DEGREES F (899 DEGREES C), SOLUTION AND PRECIPITATION HEAT TREATED |
ISO 5855-1:1999 | Aerospace MJ threads Part 1: General requirements |
EN 3311:2009 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar for machining - D < 110 mm |
MIL L 23699 : E | LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE |
ISO 2859:1974 | Sampling procedures and tables for inspection by attributes |
EN 2398:2008 | Aerospace series - Heat resisting steel FE-PA2601 (X6NiCrTiMoV26-15) - Rm ≥ 900 MPa - Bars for machined bolts - D ≤ 25 mm |
BS HR 650:1972 | Specification for high expansion heat-resisting steel bar and wire for the manufacture of bolts, studs, set screws and nuts (Ni 25.5, Cr 15, Ti 2, Mn 1.5, Mo 1.25, Si 0.7, V 0.3) (limiting ruling section 20 mm) |
ISO 3453:1984 | Non-destructive testing — Liquid penetrant inspection — Means of verification |
ISO 9002:1994 | Quality systems — Model for quality assurance in production, installation and servicing |
ISO 3452:1984 | Non-destructive testing — Penetrant inspection — General principles |
ISO 5855-3:1999 | Aerospace MJ threads Part 3: Limit dimensions for fittings for fluid systems |
ISO 7481:2000 | Aerospace — Nuts, self-locking, with maximum operating temperature less than or equal to 425 degrees C — Test methods |
EN 2399:2008 | Aerospace series - Heat resisting steel FE-PA2601 (X4NiCrTiMoV26-15) - Rm ≥ 900 MPa - Bars for forged bolts - D ≤ 25 mm |
DEFSTAN 91-101/2(1997) : 1997 | LUBRICATING OIL, GAS TURBINE ENGINE, SYNTHETIC GRADE 5 CST |
SAE AMS4928V | TITANIUM ALLOY BARS, WIRE, FORGINGS, RINGS, AND DRAWN SHAPES, 6AL - 4V, ANNEALED |
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