SAE AS5272E
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting, Procurement Specification
Available format(s)
Hardcopy , PDF
Superseded date
11-06-2021
Superseded by
Language(s)
English
Published date
10-04-2016
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. USE LIMITATIONS
7. ACKNOWLEDGMENT
8. REJECTIONS
9. NOTES
Specifies the requirements for heat cured solid film lubricants.
| DocumentType |
Standard
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| Pages |
14
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| PublisherName |
SAE International
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
This SAE Aerospace Standard (AS) establishes the requirements for heat cured solid film lubricants. For other general or high temperature applications, see AS1701.
| MS27057 Revision E:2013 | Adapter Assembly, Flared, 90 Degrees Elbow, Tube to Hose - with Swivel Nut |
| MS27385 Revision C:2013 | Adapter Assembly, Flareless, 90 Degrees Forged Elbow, Tube to Hose - with Swivel Nut |
| MS27382 Revision C:2013 | Adapter Assembly, Flareless, 45 Degree Elbow, Tube to Hose-with Swivel Nut |
| MS27381 Revision C:2013 | Adapter, Assembly, Flareless, Straight, Tube to Hose - with Swivel Nut |
| MS27086 Revision D:2013 | Elbow, Nipple End, Flared, Tube to Hose - 90 Degrees Swivel Nut |
| MS27060 Revision E:2013 | Adapter Assembly, Flared, 90 Degrees Forged Elbow, Tube to Hose-with Swivel Nut |
| MS27087 Revision D:2013 | Elbow, Nipple End, Flared, Tube to Hose - 45 Degrees Swivel Nut |
| SAE AS5960B | Hose Assembly, Polytetrafluoroethylene, Metallic Braid Reinforced, 5080 psi (35 000 kPa), 400 °F (204 °C), Aircraft Hydraulic Systems |
| MS27383 Revision C:2014 | ADAPTER ASSEMBLY, FLARELESS, 90 DEGREES ELBOW, TUBE TO HOSE - WITH SWIVEL NUT |
| MS27056 Revision E:2013 | Adapter Assembly, 45 Degrees Elbow, Swivel Flange to Hose |
| MS27076 Revision E:2013 | Nipple, Straight, Swivel Flange |
| MS27387 Revision D:2013 | Elbow Subassembly, Flareless, 45 Degrees, Swivel Nut |
| SAE AS18280F | Fittings, 24° Cone Flareless, Fluid Connection, 3000 psi |
| SAE AS12500 | Corrosion Prevention and Deterioration Control in Electronic Components and Assemblies |
| MIL-DTL-27272 Revision D:2015 | Fittings, Polytetrafluoroethylene Hose, High-Temperature, Medium-Pressure, General Specification for |
| MIL-DTL-32258 Base Document:2007 | NUT, SELF-LOCKING (RING TYPE NON-METALLIC INSERT), HEAVY HEX, CONTROLLED ROOT RADIUS, NICKEL-COPPER ALLOY |
| MIL-DTL-25027 Revision H:1997 | NUT, SELF-LOCKING, 250 DEG F, 450 DEG F, AND 850 DEG F |
| MS27082 Revision E:2014 | ELBOW, NIPPLE END, SWIVEL FLANGE TO HOSE - 90 DEGREES |
| I.S. EN 6129:2016 | AEROSPACE SERIES - BLIND BOLT, PROTRUDING HEAD, HIGH STRENGTH, PULLTYPE |
| MS27055 Revision E:2013 | Adapter Assembly, Flared, 45 Degrees Elbow, Tube to Hose - with Swivel Nut |
| MS27061 Revision D:2013 | Nipple Subassembly, Flared, Straight - with Swivel Nut |
| MS27072 Revision F:2013 | WIRE, RETAINER |
| ASTM D 7217 : 2016 : REDLINE | Standard Test Method for Determining Extreme Pressure Properties of Solid Bonded Films Using a High-Frequency, Linear-Oscillation (SRV) Test Machine |
| MS27389 Revision D:2014 | ELBOW SUB ASSEMBLY, FLARELESS, 45 DEGREES FORGED, SWIVEL NUT |
| SAE AS85720B | Fittings, Tube, Fluid Systems, Separable, High Pressure Beam Seal, 5000/8000 psi, General Specification For |
| SAE AS5951D | Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 5080 psi (35000 kPa), 275 °F (135 °C), Aircraft Hydraulic Systems |
| MS27067 Revision D:2013 | Elbow Subassembly, Flared, 45 Degrees Forged, Swivel Nut |
| MS27624 Revision B:2009 | UNION, NIPPLE |
| SAE AS6449C | Solid Film Lubricant |
| SAE AS5420G | Hose Assembly, Heated, 125 psig, Lined Silicone, Potable Water, Procurement Specification |
| MIL-DTL-45932 Revision A:2015 | INSERT, SCREW THREAD, THIN WALL, LOCKED IN: GENERAL SPECIFICATION FOR |
| SAE AS4468G | Hose Assembly, 125 psi, Lined Silicone, Potable Water, Procurement Specification |
| MS27064 Revision E:2014 | ELBOW SUBASSEMBLY, SWIVEL FLANGE, 45 DEGREES |
| 15/30329889 DC : 0 | BS A 266 TO 271 - BOLT, 100 DEGREES COUNTERSUNK HEAD, HI-TORQUE SPEED DRIVE RECESS, UNJF THREAD, SPLIT PIN HOLE OPTION, TITANIUM ALLOY, VARIOUS FINISHES, CLASSIFICATION: 80 TF/IN[2] (1100 MPA) AT TA/+315 DEGREES C |
| MS27075 Revision D:2013 | NIPPLE, FLARED, TUBE TO HOSE - SWIVEL NUT |
| MS27071 Revision D:2013 | UNION, NIPPLE |
| MS27625 Revision D:2018 | Wire, Retainer |
| MS27070 Revision E:2013 | SLEEVE, HOSE COUPLING |
| MS27068 Revision D:2013 | Elbow Subassembly, Flared, 90 Degrees Forged, Swivel Nut |
| MS27390 Revision C:2013 | Elbow Subassembly, Flareless, 90 Degrees, Forged, Swivel Nut |
| MS27058 Revision E:2013 | Adapter Assembly, 90 Degrees Elbow, Swivel Flange to Hose |
| MS27384 Revision C:2014 | ADAPTOR ASSEMBLY, FLARELESS, 45 DEGREES FORGED ELBOW, TUBE TO HOSE - WITH SWIVEL NUT |
| MIL L 0046010 : D | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING |
| MS27626 Revision B:2009 | NIPPLE, FLARED, TUBE TO HOSE-SWIVEL NUT |
| 14/30310862 DC : 0 | BS EN 4832 - 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 |
| MS27065 Revision F:2013 | Elbow Subassembly, Flared, 90 Degrees, Swivel Nut |
| MS27062 Revision D:2013 | Nipple Subassembly, Straight, Swivel Flange |
| MS27635 Revision C:2009 | NIPPLE, FLARELESS, TUBE TO HOSE, SWIVEL NUT |
| BS 2A 266 to 2A 271:2016+A1:2019 | Aerospace Series. Bolt, 100° Countersunk head, Hi-Torque speed drive recess, close tolerance shank, UNJF thread, split pin hole option, titanium alloy, various finishes. Classification: R<sub>m</sub> 1100–1250 MPa (160 000–180 000 lbf/in<sup>2</sup>) at Ambient Temperature | +315 °C |
| SAE AS4623E | Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3,000 psi, 275 °F, Heavy Duty, Aircraft Hydraulic Systems |
| SAE ARP 4058 : 2017 | GENERAL SPECIFICATION GUIDE FOR MECHANICAL GEARED ROTARY ACTUATORS |
| SAE AS1975G | Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems |
| EN 6128:2017 | Aerospace series - Blind bolt, 100° flush head, high strength |
| NASA PRC 8001 : 2013 | PROCESS SPECIFICATION FOR DRY-FILM LUBRICANT APPLICATION |
| MS27391 Revision F:2013 | Nipple, Flareless, Tube to Hose - Swivel Nut |
| SAE ARP5824 | Recommended Solid Film Lubricants for Fluid System Components |
| SAE AS5528C | Lubricant Application, Solid Film, Heat Cured, Corrosion Inhibiting |
| MS27063 Revision F:2013 | Elbow Subassembly, Flared, 45 Degrees, Swivel Nut |
| SAE J2270_201606 | Ship Systems and Equipment - Threaded Fasteners - Inspection, Test, and Installation Guidance |
| MS27053 Revision E:2013 | Adapter Assembly, Flared, Straight, Tube to Hose - with Swivel Nut |
| SAE AS5000C | Fitting, Plug-in Union, Ring Locked, 24 Degree Cone, Fluid Connection, 5080 psi (35 000 kPa), Specification for |
| MS27394 Revision C:2014 | ELBOW, FLARELESS, TUBE TO HOSE - 90 DEGREE SWIVEL NUT |
| BS EN 6129:2016 | Aerospace series. Blind bolt, protruding head, high strength, pulltype |
| MS27066 Revision F:2013 | Elbow Subassembly, Swivel Flange, 90 Degrees |
| MS27388 Revision D:2014 | ELBOW SUBASSEMBLY, FLARELESS, 90 DEGREES, SWIVEL NUT |
| MS27386 Revision C:2013 | Nipple Subassembly, Flareless, Straight - with Swivel Nut |
| MS27054 Revision E:2013 | Adapter Assembly, Straight, Swivel Flange to Hose |
| MS27069 Revision H:2017 | SOCKET, HOSE COUPLING |
| MS27059 Revision E:2013 | Adapter Assembly, Flared, 45 Degrees Forged Elbow, Tube to Hose - with Swivel Nut |
| PREN 6122 : 200P1 | AEROSPACE SERIES - BLIND BOLT, 130 DEGREES FLUSH HEAD, HIGH STRENGTH, PREFERABLE IN COMPOSITE APPLICATION |
| MS27395 Revision D:2014 | ELBOW, FLARELESS, TUBE TO HOSE - 45 DEGREES SWIVEL NUT |
| MS27084 Revision D:2014 | ELBOW, NIPPLE END, SWIVEL FLANGE TO HOSE - 45 DEGREES |
| MS27623 Revision D:2018 | SLEEVE, HOSE COUPLING |
| SAE AMS2487B | Anodic Treatment of Titanium and Titanium Alloys Solution pH 12.4 Maximum |
| I.S. EN 6128:2017 | AEROSPACE SERIES - BLIND BOLT, 100 DEGREE FLUSH HEAD, HIGH STRENGTH |
| BS EN 6128:2017 | Aerospace series. Blind bolt, 100° flush head, high strength |
| ASME B18.29.1 : 2010 : R2017 | Helical Coil Screw Thread Inserts--Free Running and Screw Locking (Inch Series) (B18.29.1 - 2010) |
| ASME B18.29.1 : 2010 | HELICAL COIL SCREW THREAD INSERTS - FREE RUNNING AND SCREW LOCKING (INCH SERIES) |
| PREN 6127 : 200P2 | AEROSPACE SERIES - BLIND BOLT, 100 DEGREES REDUCED FLUSH HEAD, HIGH STRENGTH |
| PREN 6131 : 200P3 | AEROSPACE SERIES - COMPOSITE CLIP NUT, SELF LOCKING |
| PREN 6128 : 200P2 | AEROSPACE SERIES - BLIND BOLT, 100 DEGREES FLUSH HEAD, HIGH STRENGTH |
| PREN 6129 : 200P1 | AEROSPACE SERIES - BLIND BOLT, PROTRUDING HEAD, HIGH STRENGTH |
| ASME B18.29.2M:2005 | HELICAL COIL SCREW THREAD INSERTS: FREE RUNNING AND SCREW LOCKING (METRIC SERIES) |
| ASME B18.29.2M : 2005 : R2017 | HELICAL COIL SCREW THREAD INSERTS: FREE RUNNING AND SCREW LOCKING (METRIC SERIES) |
| SAE AS 1701 : 2017 | LUBRICANT, SOLID FILM |
| ISO/IEC 17025:2005 | General requirements for the competence of testing and calibration laboratories |
| NAS850:2012 | GENERAL PACKAGING STANDARD |
| SAE AMS1424M | Deicing/Anti-Icing Fluid, Aircraft SAE Type 1 |
| SAE AS5528C | Lubricant Application, Solid Film, Heat Cured, Corrosion Inhibiting |
| MIL-PRF-372 Revision E:2013 | Cleaning Compound, Solvent (For Bore of Weapons) |
| ASTM D 1400 : 2000 | Standard Test Method for Nondestructive Measurement of Dry Film Thickness of Nonconductive Coatings Applied to a Nonferrous Metal Base (Withdrawn 2006) |
| MIL-PRF-63460 Revision F:2017 | Cleaner, Lubricant, and Preservative for Weapons and Weapons Systems |
| ASTM D 1141 : 1998 : EDT 1 | Standard Practice for the Preparation of Substitute Ocean Water |
| MIL-DTL-16232 Revision G:2000 | PHOSPHATE COATING, HEAVY, MANGANESE OR ZINC BASE |
| MIL-C-81302 Revision D:1985 | CLEANING COMPOUND, SOLVENT, TRICHLOROTRIFLUOROETHANE |
| MIL L 46000 : C | LUBRICANT, SEMI-FLUID (AUTOMATIC WEAPONS) |
| ASTM F 22 : 2013 : REDLINE | Standard Test Method for Hydrophobic Surface Films by the Water-Break Test |
| SAE AS9100D | Quality Management Systems - Requirements for Aviation, Space, and Defense Organizations |
| VV-D-1078 Revision B:1983 | DAMPING FLUID, SILICONE BASE (DIMETHYL POLYSILOXANE) |
| 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 AMSQQA250/5B | Aluminum Alloy Alclad 2024, Plate and Sheet |
| CFR 29(PT1910.1000 TO END) : 0 | LABOR - OCCUPATIONAL SAFETY AND HEALTH ADMINISTRATION, DEPARTMENT OF LABOR |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| ASTM D 1186 : 2001 | Standard Test Methods for Nondestructive Measurement of Dry Film Thickness of Nonmagnetic Coatings Applied to a Ferrous Base (Withdrawn 2006) |
| 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) |
| NAS854:2013 | HAZARDOUS MATERIAL PACKAGING STANDARD PACKAGING AND SAFETY DATA SHEET NAS854 PREPARATION |
| MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
| SAE AMS2825B | Material Safety Data Sheets |
| FED-STD-791 Revision D:2007 | TESTING METHOD OF LUBRICANTS, LIQUID FUELS, AND RELATED PRODUCTS |
| FED-STD-595 Revision C:2008 | COLORS USED IN GOVERNMENT PROCUREMENT |
| MIL-PRF-14107 Revision D:2000 | LUBRICATING OIL, WEAPONS, LOW TEMPERATURE |
| MIL-PRF-46010 Revision H:2013 | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING NATO CODE S-1738 |
| MIL-T-81533 Revision A:1967 | TRICHLOROETHANE, 1, 1, 1, (METHYL CHLOROFORM) INHIBITED, VAPOR DEGREASING |
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