SAE AS 4751 : 2005
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
COUPLING ASSEMBLY, V-BAND SHEET METAL WIDE FLANGE, PNEUMATIC TUBE
Hardcopy , PDF
29-02-2024
English
01-01-2005
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1 SCOPE
2 APPLICABLE DOCUMENTS
3 TECHNICAL REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 NOTES
This SAE Aerospace Standard (AS) establishes the requirements for a grooved clamp coupling and flanges suitable for joining intermediate pressure and temperature ducting in aircraft pneumatic systems.
| Committee |
G-3
|
| DocumentType |
Standard
|
| Pages |
25
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
| SAE AIR 869 : 2014 | V-COUPLINGS, INCLUDING V-BAND AND V-RETAINER COUPLING ASSEMBLIES, FLANGE AND SEAL DESIGN, APPLICATION OF |
| 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 AMS 5525 : 2012 | STEEL, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, 1800 DEGREE F (982 DEGREE C) SOLUTION HEAT TREATED |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| SAE AIR 869 : 2014 | V-COUPLINGS, INCLUDING V-BAND AND V-RETAINER COUPLING ASSEMBLIES, FLANGE AND SEAL DESIGN, APPLICATION OF |
| MIL-HDBK-831 Revision A:2013 | PREPARATION OF TEST REPORTS |
| SAE AMS 5513 : 2015 | STEEL, CORROSION-RESISTANT, SHEET, STRIP, AND PLATE, 19CR - 9.2NI (SAE 30304), SOLUTION HEAT TREATED |
| SAE AMS 5516 : 2012 | STEEL, CORROSION-RESISTANT, SHEET, STRIP, AND PLATE, 18CR - 9.0NI (SAE 30302), SOLUTION HEAT TREATED |
| NASM25027:2012 | NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F |
| SAE AMS W 6858 : 2000 | WELDING, RESISTANCE: SPOT AND SEAM |
| SAE AMS 5510S : 2014 | STEEL, CORROSION AND HEAT-RESISTANT, SHEET, STRIP AND PLATE, 18CR - 10.5NI - 0.40TI (SAE 30321) SOLUTION HEAT TREATED |
| 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 |
| AWS D17.1 : 2001 | SPECIFICATION FOR FUSION WELDING FOR AEROSPACE APPLICATIONS |
| SAE AS 8879 : 2004 | SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER |
| SAE AMS 5901B:2008 | STEEL, CORROSION-RESISTANT, SHEET, STRIP, AND PLATE, 18CR - 8NI (SAE 30301), SOLUTION HEAT TREATED |
| SAE AMS 5518 : 2014 | STEEL, CORROSION RESISTANT, SHEET AND STRIP 18CR - 8NI COLD ROLLED, 150 KSI (1034 MPA) TENSILE STRENGTH |
| SAE AS 478 : 2015 | IDENTIFICATION MARKING METHODS |
| ASME Y14.100 : 2017 | ENGINEERING DRAWING PRACTICES - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES |
| NASM7873:2012 | NUT, SELF-LOCKING, 1,200 DEGREES F |
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