SAE AS 5000 : 2010
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 (35000 KPA), SPECIFICATION FOR
Hardcopy , PDF
27-01-2020
English
01-01-2010
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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).
| Committee |
G-3C
|
| DocumentType |
Standard
|
| Pages |
31
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
| 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 AS 5551 : 2017 | FITTING ASSEMBLY - 24 DEGREES 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 2486 : 2010 | CONVERSION COATING OF TITANIUM ALLOYS FLUORIDE-PHOSPHATE TYPE |
| 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 AS 5620 : 2013 | TITANIUM HYDRAULIC TUBING, TI-3AL-2.5V COLD WORKED AND STRESS RELIEVED, UP TO 35000 KPA (5080 PSI), REQUIREMENTS FOR QUALIFICATION TESTING AND CONTROL |
| SAE AS 603 : 2015 | 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 AS 5551 : 2017 | FITTING ASSEMBLY - 24 DEGREES CONE FLARELESS PER AS5827, 5080 PSI, PORT CONNECTION, PORT PREPARATION, INSTALLATION AND REMOVAL OF AS5550 AND AS5865 |
| SAE AS 1055 : 2013 | FIRE TESTING OF FLEXIBLE HOSE, TUBE ASSEMBLIES, COILS, FITTINGS AND SIMILAR SYSTEM COMPONENTS |
| SAE AMS 4965 : 2014 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6.0AL 4.0V, SOLUTION HEAT TREATED AND AGED |
| SAE AS 7003 : 2008 | NADCAP PROGRAM REQUIREMENTS |
| SAE AS 7112 : 1997 | NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM REQUIREMENTS FOR FLUID SYSTEM COMPONENTS |
| SAE AMS 5734 : 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 HEAT TREATED |
| SAE AS 5272 : 2016 | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING, PROCUREMENT SPECIFICATION |
| SAE AS 5975 : 2015 | FITTING ASSEMBLY, STRAIGHT, MALE FLARELESS, AXIALLY SWAGED, HYDRAULIC, 5080 PSI |
| SAE AS 5550 : 2015 | 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 AS 1241 : 2016 | FIRE RESISTANT PHOSPHATE ESTER HYDRAULIC FLUID FOR AIRCRAFT |
| SAE AMS 2700E : 2011 | PASSIVATION OF CORROSION RESISTANT STEELS |
| SAE AS 4941 : 2015 | AEROSPACE - GENERAL REQUIREMENTS FOR COMMERCIAL AIRCRAFT HYDRAULIC COMPONENTS |
| SAE AS5865A: 2015 | FITTING REDUCER ASSEMBLY, RING LOCKED, ADAPTER, FLARELESS TO PORT, EXTRA FINE THREADS, 5080 PSI |
| SAE AS 5827 : 2015 | FITTING END, FLARELESS, EXTRA FINE THREAD, DESIGN STANDARD |
| SAE AS 478 : 2015 | IDENTIFICATION MARKING METHODS |
| SAE ARP 5412 : 2013 | AIRCRAFT LIGHTNING ENVIRONMENT AND RELATED TEST WAVEFORMS |
| SAE AMS 4967 : 2014 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS 6.0AL - 4.0V ANNEALED, HEAT TREATABLE |
| SAE AS 2094 : 2011(S2018) | Test Methods for Tube-Fitting Assemblies(STABILIZED Jul 2018) |
| SAE AMS 4928 : 2016 | TITANIUM ALLOY BARS, WIRE, FORGINGS, RINGS, AND DRAWN SHAPES, 6AL - 4V, ANNEALED |
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