SAE AS5000C
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Fitting, Plug-in Union, Ring Locked, 24 Degree Cone, Fluid Connection, 5080 psi (35 000 kPa), Specification for
Hardcopy , PDF
27-01-2020
English
07-07-2010
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1. SCOPE
2. REFERENCES
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. NOTES
Specifies the requirements for 24 degree cone AS5827 or EN 6123 flareless Ring locked fitting assemblies per AS5550 and AS5865, for use in aircraft fluid systems at nominal operating pressure of 5080 psi (35 000 kPa) maximum and operating temperature range of -65 to +275 degrees F (-54 to +135 degrees C).
| DocumentType |
Standard
|
| Pages |
31
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
This SAE Aerospace Standard (AS) establishes the requirements for 24 degree cone AS5827 or EN 6123 flareless Ring locked fitting assemblies per AS5550 and AS5865, for use in aircraft fluid systems at nominal operating pressure of 5080 psi (35 000 kPa) maximum and operating temperature range of -65 to +275 °F (-54 to +135 °C).The general requirements shall be for, but not limited to, commercial aircraft hydraulic components per AS4941, using port configuration as specified in AS5551.
| 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 |
| SAE AS5551B | Fitting Assembly - 24° Cone Flareless per AS5827, 5080 psi, Port Connection, Port Preparation, Installation and Removal of AS5550 and AS5865 |
| PREN 4833 : DRAFT 2017 | AEROSPACE SERIES - PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING LOCKED FITTING - FLARELESS END - INCH SERIES - EXTRA FINE THREAD PITCH |
| PREN 4836 : DRAFT 2017 | AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING REDUCER - FLARELESS END - INCH SERIES - EXTRA FINE THREAD PITCH |
| 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 |
| SAE AS5620A | Titanium Hydraulic Tubing, Ti-3Al-2.5V Cold Worked and Stress Relieved, Up to 35,000 kPa (5080 psi), Requirements for Qualification Testing and Control |
| SAE AS603B | Impulse Testing of Hydraulic Hose, Tubing, and Fitting Assemblies |
| SAE AMS 2488 : 2000 | ANODIC TREATMENT - TITANIUM AND TITANIUM ALLOYS SOLUTION PH 13 OR HIGHER |
| SAE AS5551B | Fitting Assembly - 24° Cone Flareless per AS5827, 5080 psi, Port Connection, Port Preparation, Installation and Removal of AS5550 and AS5865 |
| SAE AS1055D | Fire Testing of Flexible Hose, Tube Assemblies, Coils, Fittings, and Similar System Components |
| SAE AMS4965L | Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al 4.0V Solution Heat Treated and Aged |
| SAE AS7003D | Nadcap Program Requirements |
| SAE AS7112 | NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM REQUIREMENTS FOR FLUID SYSTEM COMPONENTS |
| SAE AS5272E | Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting, Procurement Specification |
| SAE AS5975C | FITTING ASSEMBLY, STRAIGHT, MALE FLARELESS, AXIALLY SWAGED, HYDRAULIC, 5080 PSI |
| SAE AS5550C | FITTING ASSEMBLY, RING LOCKED, ADAPTER, FLARELESS TO PORT, EXTRA FINE THREADS, 5080 PSI |
| 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 |
| SAE AS 8879 : 2004 | SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER |
| 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 |
| SAE ARP 5416 : 2013 | AIRCRAFT LIGHTNING TEST METHODS |
| SAE AS1241D | Fire Resistant Phosphate Ester Hydraulic Fluid for Aircraft |
| SAE AMS2700E | Passivation of Corrosion Resistant Steels |
| SAE AS4941B | Aerospace - General Requirements for Commercial Aircraft Hydraulic Components |
| SAE AS5865A | FITTING REDUCER ASSEMBLY, RING LOCKED, ADAPTER, FLARELESS TO PORT, EXTRA FINE THREADS, 5080 PSI |
| SAE AS5827A | FITTING END, FLARELESS, EXTRA FINE THREAD, DESIGN STANDARD |
| SAE AS478N | Identification Marking Methods |
| SAE ARP5412B | AIRCRAFT LIGHTNING ENVIRONMENT AND RELATED TEST WAVEFORMS |
| SAE AMS4967L | Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al - 4.0V Annealed, Heat Treatable |
| SAE AS2094A | Test Methods for Tube-Fitting Assemblies |
| SAE AMS4928V | Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes 6Al - 4V Annealed |
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