ISO 413:1974
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Aircraft — Heads of lubricating nipples
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English, French
01-11-1974
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Specifies the envelope dimensions of axial type nipples and determines the clearance space which shall be provided in the region of the nipple to allow the lubricating gun to be connected, and the operating angle dimensions for the lubricating process. The tip design of the nipples is optional provided the profile remains within the envelope shown in figure 1.
| Committee |
ISO/TC 20
|
| DocumentType |
Standard
|
| Pages |
1
|
| PublisherName |
International Organization for Standardization
|
| Status |
Current
|
| Standards | Relationship |
| LN 71412:1970-09 | Identical |
| PN 92/L-01273 : 1992 | Identical |
| BS SP115-117(1956) : 1956 | Similar to |
| UNE 28559:1988 | Identical |
| DIN ISO 413:1987-12 | Identical |
| LN 71412:1970-09 | Corresponds |
| UNI 6246 : 1968 | Identical |
| PREN 2646 : 200P3 | AEROSPACE SERIES - NIPPLES, LUBRICATING, AXIAL TYPE, IN STEEL, CADMIUM PLATED |
| PREN 3908 : 200P2 | AEROSPACE SERIES - NIPPLES, LUBRICATING, AXIAL TYPE, IN CORROSION RESISTING STEEL, PASSIVATED |
| DEFSTAN 02-327/4(2016) : 2016 | STANDARDS FOR DEFENCE REQUIREMENTS AND GUIDANCE FOR THE PROCUREMENT OF PUMPS FOR AUXILIARY SYSTEMS |
| BS EN 3908:2017 | Aerospace series. Nipples, lubricating, axial type, in corrosion resisting steel, passivated |
| STANAG 3766 : 2017 | GREASE NIPPLES |
| EN 3908:2017 | Aerospace series - Nipples, lubricating, axial type, in corrosion resisting steel, passivated |
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