SAE AS5958F
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Fittings, Axially Swaged Tube with Flareless Separable, Fluid System for Operating Pressures up to and Including 5080 psi (35000 kPa), Specification for
Hardcopy , PDF
10-06-2019
English
11-09-2017
1. SCOPE
2. REFERENCES
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. NOTES
Sets up the requirements for axially swaged titanium fittings on titanium, CRES, and aluminum tubing with flareless separable fitting ends for use in hydraulic supply and return aerospace fluid systems up to operating pressure of 5080 psig (35000 kPa) maximum.
DocumentType |
Standard
|
Pages |
44
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
This SAE Aerospace Standard (AS) establishes the requirements for axially swaged titanium fittings on titanium, CRES, and aluminum tubing with flareless separable fitting ends for use in hydraulic supply and return aerospace fluid systems up to operating pressure of 5080 psig (35000 kPa) maximum. The operating temperature range for titanium tubing and CRES tubing is −65 to +275 °F (−54 to +135 °C) and the operating temperature range for aluminum return system tubing is −65 to +225 °F (−54 to +107 °C).This specification covers a common 5080 psi pressure titanium fitting that may be used for a range of operating pressures up to 5080 psi with different tubing materials and tubing wall thicknesses, and is assembled with the same tooling in accordance with AS5959. The flareless fitting operating pressure is based on the fitting thread pitch. Extra fine pitch is used for 5080 psi operating pressure and fine pitch for operating pressures 3000 psi and less. Table 14 shows applicable aerospace fitting part number standard and tubing materials and operating pressures.
SAE AS5545 | NUT COUPLING, FLARELESS, EXTRA FINE THREAD, 5080 PSI, |
SAE AS6106A | FITTING ASSEMBLY, STRAIGHT, EXTENDED BULKHEAD SHANK, FLARELESS, AXIALLY SWAGED, HYDRAULIC, 5080 PSI |
SAE AS5971C | FITTING ASSEMBLY, ELBOW, 45°, AXIALLY SWAGED, HYDRAULIC, 5080 PSI |
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 AMS1428J | Fluid, Aircraft Deicing/Anti-Icing, Non-Newtonian (Pseudoplastic), SAE Types II, III, and IV |
SAE AS5868C | FITTING ASSEMBLY, STRAIGHT, BULKHEAD FLARELESS, AXIALLY SWAGED, HYDRAULIC, 5080 PSI |
MIL-DTL-5624 Revision W:2016 | TURBINE FUEL, AVIATION, GRADES JP-4 AND JP-5 |
SAE AS5863 | FITTING END, 24° CONE, FLARELESS, FLUID CONNECTION, DESIGN STANDARD |
SAE AS5977B | FITTING ASSEMBLY, 90°, MALE FLARELESS, AXIALLY SWAGED, HYDRAULIC, 5080 PSI |
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 AS5969E | FITTING ASSEMBLY, UNION, AXIALLY SWAGED, HYDRAULIC 5080 PSI |
SAE AS5972G | FITTING ASSEMBLY, TEE AXIALLY SWAGED, HYDRAULIC, 5080 PSI |
EN 6123:2016 | Aerospace series - Fitting end, 24° internal cone, external thread, flareless type - Extra fine thread pitch - Inch series - Design standard |
MIL-PRF-5606 Revision H:2002 | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE |
SAE AS5959B | Axially Swaged Fittings, Installation and Inspection Procedure |
SAE AS85449/2 | CLAMP ASSEMBLY, SADDLE TYPE, CUSHIONED, PHOSPHATE ESTER FLUID RESISTANT |
SAE AMS5561G | Steel, Corrosion and Heat-Resistant, Welded and Drawn or Seamless and Drawn Tubing 9.0Mn - 20Cr - 6.5Ni - 0.28N High-Pressure Hydraulic |
SAE AS5767A | FITTING ASSEMBLY, TEE, FEMALE FLARELESS ON RUN, AXIALLY SWAGED, HYDRAULIC, 5,080 PSI |
SAE AS1055D | Fire Testing of Flexible Hose, Tube Assemblies, Coils, Fittings, and Similar System Components |
MIL-HDBK-831 Revision A:2013 | PREPARATION OF TEST REPORTS |
SAE ARP1185B | Flexure Testing of Hydraulic Tubing Joints and Fittings |
SAE AS5791A | FITTING ASSEMBLY, STRAIGHT, BULKHEAD FLARELESS, AXIALLY SWAGED, HYDRAULIC, 3000 PSI |
MIL-PRF-23377 Revision K:2012 | PRIMER COATINGS: EPOXY, HIGH-SOLIDS |
ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
SAE AS5805A | FITTING ASSEMBLY, ELBOW, 90°, BULKHEAD FLARELESS, AXIALLY SWAGED, HYDRAULIC, 3000 PSI |
SAE AS5807B | FITTING ASSEMBLY, TEE, AXIALLY SWAGED ON THE RUN, MALE FLARELESS ON THE BRANCH HYDRAULIC, 3000 PSI |
SAE AS5793A | FITTING ASSEMBLY, STRAIGHT, MALE FLARELESS, AXIALLY SWAGED, HYDRAULIC, 3000 PSI |
SAE AMS4965L | Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al 4.0V Solution Heat Treated and Aged |
MIL-PRF-87257 Revision C:2017 | HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE |
MIL-DTL-5541 Revision F:2006 | Chemical Conversion Coatings on Aluminum and Aluminum Alloys |
SAE AS5869E | FITTING ASSEMBLY, UNION, 3 HOLE FLANGE AXIALLY SWAGED, HYDRAULIC 5080 PSI |
SAE AS5810B | FITTING ASSEMBLY, TEE, MALE FLARELESS ON THE RUN, AXIALLY SWAGED ON THE RUN AND THE BRANCH, HYDRAULIC, 3000 PSI |
SAE AMS5637H | Steel, Corrosion Resistant, Bars and Wire 18Cr - 9.0Ni (SAE 30302) Solution Heat Treated, Cold Drawn and Stress Relieved 125 ksi (862 MPa) Tensile Strength |
SAE AS5974E | FITTING ASSEMBLY, STRAIGHT, FEMALE FLARELESS, AXIALLY SWAGED, HYDRAULIC, 5080 PSI |
SAE AS5975C | FITTING ASSEMBLY, STRAIGHT, MALE FLARELESS, AXIALLY SWAGED, HYDRAULIC, 5080 PSI |
SAE AS5804B | FITTING ASSEMBLY, TEE, FEMALE FLARELESS AND AXIALLY SWAGED ON THE RUN, AXIALLY SWAGED ON THE BRANCH, HYDRAULIC, 3,000 PSI |
MIL-PRF-23699 Revision G:2014 | Lubricating Oil, Aircraft Turbine Engine, Synthetic Base, NATO Code Numbers: O-152, O-154, O-156, and O-167 |
SAE AS5792C | FITTING ASSEMBLY, STRAIGHT, FEMALE FLARELESS, AXIALLY SWAGED, HYDRAULIC, 3000 PSI |
SAE AMS4945F | Titanium Alloy Tubing, Seamless, Hydraulic 3Al - 2.5V, Controlled Contractile Strain Ratio Cold Worked, Stress Relieved |
SAE AS5973A | FITTING ASSEMBLY, CROSS, AXIALLY SWAGED, HYDRAULIC, 5080 PSI |
SAE AMSSTD595A | Colors Used in Government Procurement |
SAE AS1376D | ALTERNATE DIMENSIONS, CENTER BODY SECTION, SHAPE FLUID FITTING, DESIGN STANDARD |
MIL-DTL-83133 Revision J:2015 | TURBINE FUEL, AVIATION, KEROSENE TYPE, JP-8 (NATO F-34), NATO F-35, AND JP-8+100 (NATO F-37) |
EN 2808:1997 | Aerospace series - Anodizing of titanium and titanium alloys |
SAE AS 6322 : 2016 | FITTING ASSEMBLY, EXTENDED UNION, AXIALLY SWAGED, HYDRAULIC, 5080 PSI |
SAE AS5976B | FITTING ASSEMBLY, ELBOW, 90°, FEMALE FLARELESS, AXIALLY SWAGED, HYDRAULIC, 5080 PSI |
SAE AS6107A | FITTING ASSEMBLY, STRAIGHT, EXTENDED BULKHEAD SHANK, FLARELESS, AXIALLY SWAGED, HYDRAULIC, 3000 PSI |
SAE AMS4946E | Titanium Alloy Tubing, Seamless, Hydraulic 3Al - 2.5V, Texture Controlled Cold Worked, Stress Relieved |
SAE AS5808C | FITTING ASSEMBLY, TEE FEMALE FLARELESS AND AXIALLY SWAGE ON RUN, FEMALE FLARELESS ON THE BRANCH, HYDRAULIC, 3000 PSI |
SAE AS1241D | Fire Resistant Phosphate Ester Hydraulic Fluid for Aircraft |
SAE AMS2700E | Passivation of Corrosion Resistant Steels |
MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
ISO 7137:1995 | Aircraft — Environmental conditions and test procedures for airborne equipment |
SAE AS5978B | FITTING ASSEMBLY, ELBOW 45°, FEMALE FLARELESS, AXIALLY SWAGED, HYDRAULIC, 5080 PSI |
SAE AS5809A | FITTING ASSEMBLY, TEE, FEMALE FLARELESS AND AXIALLY SWAGED ON THE RUN, MALE FLARELESS ON BRANCH, HYDRAULIC, 3000 PSI |
TT-I-735 Revision A:1963 | ISOPROPYL ALCOHOL |
SAE AS5828A | FITTING END, BULKHEAD, FLARELESS, EXTRA FINE THREAD, DESIGN STANDARD |
SAE AMS4083L | Aluminum Alloy Tubing, Hydraulic, Seamless, Drawn, Round 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-T6) Solution and Precipitation Heat Treated |
SAE AS5802A | FITTING ASSEMBLY, ELBOW, 90°, MALE FLARELESS, AXIALLY SWAGED, HYDRAULIC, 3000 PSI |
SAE AS5827A | FITTING END, FLARELESS, EXTRA FINE THREAD, DESIGN STANDARD |
SAE AS5979B | FITTING ASSEMBLY, ELBOW, 45°, MALE FLARELESS, AXIALLY SWAGED, HYDRAULIC, 5080 PSI |
SAE AS5864A | FITTING END, BULKHEAD, 24° CONE, FLARELESS, FLUID CONNECTION, DESIGN STANDARD |
SAE AS5685A | Steel, Corrosion Resistant, Safety Wire, 18Cr - 11.5Ni (UNS S30500) Solution Heat Treated, Cold Finished |
SAE AS85449/3 | CLAMP ASSEMBLY, SADDLE TYPE, CUSHIONED, HIGH TEMPERATURE |
SAE ARP4784A | Definitions and Limits, Metal Material Defects and Surface and Edge Features, Fluid Couplings, Fittings and Hose Ends |
SAE AS478N | Identification Marking Methods |
SAE AS5801A | FITTING ASSEMBLY, 90°, FEMALE FLARELESS, AXIALLY SWAGED, HYDRAULIC, 3000 PSI |
SAE ARP5412B | Aircraft Lightning Environment and Related Test Waveforms |
SAE AS5806A | FITTING ASSEMBLY, TEE, AXIALLY SWAGED ON THE RUN, FEMALE FLARELESS ON THE BRANCH, HYDRAULIC, 3,000 PSI |
SAE AS5546 | NUT, FITTING, FLARELESS, RETAINED, LIGHTWEIGHT, EXTRA FINE THREAD, UP TO 5080 PSI |
SAE AS5803A | FITTING ASSEMBLY, ELBOW, 45°, FEMALE FLARELESS, AXIALLY SWAGED, HYDRAULIC, 3,000 PSI |
ASTM E 8/E8M : 2016-09 | TEST METHODS FOR TENSION TESTING OF METALLIC MATERIALS |
SAE AMS4928V | Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes 6Al - 4V Annealed |
SAE AS5970C | FITTING ASSEMBLY, ELBOW, 90°, AXIALLY SWAGED, HYDRAULIC, 5080 PSI |
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