PREN 6129 : 200P1
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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AEROSPACE SERIES - BLIND BOLT, PROTRUDING HEAD, HIGH STRENGTH
Available format(s)
Hardcopy , PDF
Language(s)
English
Superseded date
14-04-2026
Superseded by
€96.61
Excluding VAT
1 Scope
2 Normative references
3 Requirements
3.1 Configuration, dimensions and tolerances
3.2 Grip range and mass
3.3 Material, finish and lubrication
4 Designation
5 Marking
6 Technical specification
Describes the configuration, dimension, tolerances and mass of a stainless steel and titanium blind bolt with protruding head for aerospace application.
| DocumentType |
Draft
|
| Pages |
10
|
| ProductNote |
Superseded by EN 6129:2016/AC:2017
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Superseded
|
| SupersededBy |
| Standards | Relationship |
| DIN EN 6129:2016-11 | Identical |
| NF EN 6129 : 2016 PR | Identical |
| ASTM B 348 : 2013 : REDLINE | Standard Specification for Titanium and Titanium Alloy Bars and Billets |
| SAE AMS5690M | Steel, Corrosion and Heat Resistant, Wire 17Cr - 12Ni - 2.5Mo (316) Solution Heat Treated |
| ISO 8080:1985 | Aerospace — Anodic treatment of titanium and titanium alloys — Sulfuric acid process |
| SAE AMSQQP35 | Passivation Treatments for Corrosion-Resistant Steel |
| SAE AS5272E | Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting, Procurement Specification |
| EN 2424:2008 | Aerospace series - Marking of aerospace products |
| SAE AMS5687M | Nickel Alloy, Corrosion and Heat-Resistant, Wire 74Ni - 15.5Cr - 8.0Fe Annealed |
| DOD-L-85645 Revision A:1988 | LUBRICANT, DRY THIN FILM, MOLECULAR BONDED (METRIC) |
| MIL-PRF-46010 Revision H:2013 | Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting NATO Code - S-1738 |
Summarise
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