BS 4084:1996
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
UNJ threads, with controlled root radius, for aerospace. Inch series
Available format(s)
Hardcopy , PDF
Language(s)
English
Published date
15-08-1996
Publisher
Superseded date
15-01-2000
Superseded by
$531.66
Including GST where applicable
| Committee |
ACE/12
|
| DevelopmentNote |
SUPERSEDES BS 4084 1978
|
| DocumentType |
Standard
|
| Pages |
42
|
| PublisherName |
British Standards Institution
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| Standards | Relationship |
| ISO 3161:1999 | Identical |
| ISO 3161:1996 | Identical |
| BS 3A 100:1991 | Specification for general requirements for bolts and free running nuts of tensile strength not exceeding 1249 MPa |
| SAEITC TS41-6 | TS41 Manufacturing Specification for Inserts, Screw Thread, Unified, Screw Locking Helical Coil, BS HR503 (Nimonic 90) Silver Coated |
| SAEITC TS121-4 | TS121 Manufacturing Specification for Studs, Bolts and Screws in DTD5639, EN2959 and EN3220 Material 1210 MPa (175,000 lbf/in²) Tensile at Room Temperature (for which Forging is Optional and Qualification is not a Requirement |
| BS 4A 228:1997 | Specification for steel double hexagon bolts. 1250 MPa (180,000 lbf/in<sup>2</sup>) for aircraft |
| SAEITC TS108-5 | TS108 Manufacturing Specification for Studs, Bolts and Screws in BS S159 Material 1100 MPa (159,000 lbf/in² ) Tensile at Room Temperature (for which Forging Is Optional and Qualification not a Requirement) |
| SAEITC TS21-11 | TS21 Manufacturing Specification for Bolts 900 MPa (130,000 lbf/in²) Tensile at Room Temperature |
| SAEITC TS109-5 | TS109 Manufacturing Specification for Studs, Bolts and Screws in BS HR650, EN2398, EN2399 and EN3639 Material 900 MPa (130,000 lbf/in² ) Tensile at Room Temperature (for which Forging is Optional and Qualification not a Requirement) |
| SAEITC TS153-2 | TS153 Performance Specification of Insert Salvage, Imperial, Thinwall Screw Locking, Inconel 718 Silver Coated |
| SAEITC TS27-4 | TS27 Manufacturing Specification for Studs, Bolts and Screws in BS HR601 Material 1000 MPa (145,000 lbf/in²) Tensile at Room Temperature (for which Forging is optional and Qualification not a requirement) |
| BS 3G 101:1987 | Specification for general requirements for mechanical and electromechanical aircraft indicators |
| SAE AS1338A | Aerospace Metric 60° Screw Thread Profile and Tolerance Classes |
| BS 3G 197:1982 | Specification for stud-type terminal blocks for terminations on aircraft electric cables |
| SAEITC TS148-4 | TS148 Manufacturing Specification for Studs, Bolts and Screws in DTD5638, EN2952, EN2961 and EN3219 Material, 1275 MPa (185,000 lbf/in²) Tensile at Room Temperature (for which Forging is Optional and Qualification not a Requirement) |
| SAEITC TS138-6 | TS138 Manufacturing Specification for Inserts, Imperial, Thinwall, Screw Locking, (Inconel 718), Silver Coated |
| BS 4A 100:2003 | Specification for general requirements for bolts and free running nuts of tensile strength not exceeding 1249 MPa |
| SAEITC TS149-2 | TS149 Technical Specification for All Metal Self-Locking Nuts (UNJ Threads) 1550 MPa (225,000 lbf/in²) Minimum Tensile Strength at Ambient Temperature |
| BS 3G 100-2.1:1973 | Specification for general requirements for equipment for use in aircraft. All equipment Construction |
Summarise
$531.66
Including GST where applicable
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