PREN 4192 : 200P1
Withdrawn
View Superseded by
AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - TEES, REDUCED, BULKHEAD BRANCH
Hardcopy , PDF
English
12-18-2023
1 Scope
2 Normative references
3 Required characteristics
4 Designation
5 Marking
6 Technical specification
Covers the characteristics of tee union, reduced bulkhead branch in titanium alloy intended for use in aircraft fluid system pipelines. Nominal pressure: up to 28000 kPa; Temperature range: -55 degree C to 135 degree C.
| Committee |
C4
|
| DocumentType |
Draft
|
| Pages |
7
|
| ProductNote |
Superseded by EN 4192:2001
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
|
| SupersededBy |
| Standards | Relationship |
| DIN EN 4192:2002-08 | Identical |
| EN 3275:2002 | Aerospace series - Pipe coupling 8°30' up to 28 000 kPa - Dynamic beam seal - Metric series - Technical specification |
| EN 2491:2011 | Aerospace series - Molybdenum disulphide dry lubricants - Coating methods |
| PREN 3314 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 - SOLUTION TREATED AND AGED - BAR FOR MACHINING - D <= 75 MM |
| PREN 3315 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 - SOLUTION TREATED AND AGED - FORGINGS - D[E] <= 75 MM |
| ISO 5855-3:1999 | Aerospace — MJ threads — Part 3: Limit dimensions for fittings for fluid systems |
| EN 2424:2008 | Aerospace series - Marking of aerospace products |
| EN 3274:2010 | Aerospace series - Pipe coupling 8°30' - Thread end - Geometric configuration |
| MIL L 46010 : D | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING |
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