DIN EN 3916:2008-12
Aerospace series - Insert, thin wall - Salvage procedure for components; German and English version EN 3916:2008
| Fecha edición: |
2008-12-01
En Vigor
|
|---|---|
| Idiomas disponibles: | Alemán, Inglés |
| Resumen: | This specification covers the accepted methods for the reclamation of installation holes for standard thin wall inserts, within assemblies. To enable rectification when defects or damage occur to the standard insert tapped installation hole, or to rectify any out of position of the hole within the specified parameters of use. To control there machining of the existing insert hole and the installation requirements of the replacement oversize thinwall insert. |
| Keywords: | Aerospace transport|Air transport|Aircraft|Alloys|Delivery conditions|Design|Designations|Dimensions|Fasteners|Heat-resistant materials|High temperature|Inconel|Materials|Methods|MJ-threads|Multilingual|Nickel|Nickel alloys|Nickel base alloys|Operating specification|Properties|Repairs|Rework|Sockets (threaded)|Space transport|Specification (approval)|Surface treatment|Thin-walled|Thread inserts|Threads |
| ICS: | 49.030.30 - Tuercas |
| CTN: | |
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Equivalencia Internacional |
Idéntica EN 3916:2008 |
|
Reemplazo Normas |
Reemplaza a DIN EN 3916:2000-02 |
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