14/30310866 DC : 0
NA
NA
Status of Standard is Unknown
BS EN 4836 - AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREE CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING REDUCER- FLARED END - WITH EXTRA FINE THREAD PITCH - INCH SERIES
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Language(s)
English
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Foreword
1 Scope
2 Normative references
3 Requirements
4 Quality Assurance
5 Designation
6 Marking
7 Packaging
8 Technical Specification
9 REACH
BS EN 4836.
| Committee |
ACE/12
|
| DocumentType |
Draft
|
| Pages |
13
|
| PublisherName |
British Standards Institution
|
| Status |
NA
|
| PREN 4832 : DRAFT 2017 | AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING AND RING-LOCKED FITTING-REDUCER - INCH SERIES - TECHNICAL SPECIFICATION |
| PREN 6123 : 200P2 | AEROSPACE SERIES - FITTING END, 24 DEGREES INTERNAL CONE, EXTERNAL THREAD, FLARELESS TYPE - EXTRA FINE THREAD PITCH - INCH SERIES - DESIGN STANDARD |
| SAE AMS 5737 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS AND TUBING, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED, 1650 DEGREES F (899 DEGREES C), SOLUTION AND PRECIPITATION HEAT TREATED |
| PREN 4835 : DRAFT 2017 | AEROSPACE SERIES - INSTALLATION AND REMOVAL REQUIREMENTS FOR RING LOCKED FITTING AND REDUCER, 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) - INCH SERIES |
| ISO 4287:1997 | Geometrical Product Specifications (GPS) — Surface texture: Profile method — Terms, definitions and surface texture parameters |
| EN 3311:2009 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar for machining - D < 110 mm |
| SAE AMS 2488 : 2000 | ANODIC TREATMENT - TITANIUM AND TITANIUM ALLOYS SOLUTION PH 13 OR HIGHER |
| EN 4315:2007 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section a or D ≤ 100 mm, Rm ≥ 900 MPa |
| EN 4317:2007 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Non heat treated, forging stock a or D ≤ 200 mm |
| PREN 3314 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 - SOLUTION TREATED AND AGED - BAR FOR MACHINING - D <= 75 MM |
| SAE AMS5853C | Steel, Corrosion and Heat-Resistant, Bars and Wire 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V Consumable Electrode Melted 1800 °F (982 °C) Solution Treated and Work-Strengthened 160 ksi (1103 MPa) Tensile Strength |
| SAE AMS 5732 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, TUBING AND RINGS, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED 1800 DEGREES F (982 DEGREES C), SOLUTION AND PRECIPITATION HEAT TREATED |
| ISO 1302:2002 | Geometrical Product Specifications (GPS) Indication of surface texture in technical product documentation |
| SAE AMS 5731 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, TUBING, AND RINGS, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED, 1800 DEGREES F (982 DEGREES C) SOLUTION HEAT TREATED |
| EN 2424:2008 | Aerospace series - Marking of aerospace products |
| SAE AMS2700E | Passivation of Corrosion Resistant Steels |
| ISO 3161:1999 | Aerospace — UNJ threads — General requirements and limit dimensions |
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