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FITTING ASSEMBLY, UNION, AXIALLY SWAGED, HYDRAULIC 5080 PSI
- Aerospace Standard
- AS5969E
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Rationale
UPDATING PART STANDARD WITH THE NEW CLASS “D” FOR USE ON ALUMINUM TUBING. THIS IS IN CONCURRENCE WITH AS5958 REV F PROJECT G3B16-09.
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/1/
MATERIALS:CODE LETTER “T”RINGS - AMS4965 TITANIUM ALLOY, 6.0Al-4.0V SOLUTION HEAT TREATED AND AGED OR AMS4928 TITANIUM ALLOY 6.0AL 4.0V ANNEALED WITH HIGH STRENGTH CARBON FIBER/EPOXY RESIN COMPOSITE REINFORCEMENT.BODY - AMS4928 TITANIUM ALLOY, 6.0Al-4.0V ANNEALED
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2
FINISH:TITANIUM - NONE
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/3/
COATINGS/LUBRICANTS /16/:
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a
NO SUFFIX CODE LETTER
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(1)
RINGS - THE OUTER SURFACE SHALL HAVE A .125 INCH MINIMUM WIDTH BLUE COLORED RING OR COMPLETELY COLORED BLUE TO INDICATE 5080 PSI MAXIMUM OPERATION PRESSURE. PTFE COATING OR PAINT SHALL BE RESISTANT TO AS1241 FLUID WHEN USED. MARKING METHODS SHALL BE IN ACCORDANCE WITH AS5958.
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(2)
BODY - LEAD FREE SOLID FILM LUBRICANT PER AS5272 TYPE I OR II, OR PER AS6449 TYPE III OR IV, PTFE OR PETROLEUM-BASED LUBRICANT MAY BE APPLIED TO PORTIONS OF THE ID AND OD. THE PETROLEUM-BASED LUBRICANT SHALL NOT BE IN CONTACT WITH THE SYSTEM FLUID.
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(1)
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b
SUFFIX CODE LETTER A
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(1)
RINGS - NO BLUE PTFE COATING OR PAINT. THE WORD “BLUE” SHALL BE MARKED ON THE RING TO INDICATE 5080 PSI MAXIMUM OPERATING PRESSURE. MARKING METHODS SHALL BE IN ACCORDANCE WITH AS5958.
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(2)
BODY - LEAD FREE SOLID FILM LUBRICANT PER AS5272 TYPE I OR II, OR PER AS6449 TYPE III OR IV, PTFE OR PETROLEUM-BASED LUBRICANT MAY BE APPLIED TO PORTIONS OF THE ID AND OD. THE PETROLEUM-BASED LUBRICANT SHALL NOT BE IN CONTACT WITH THE SYSTEM FLUID.
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(1)
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c
SUFFIX CODE LETTER B
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(1)
RINGS - PARTIALLY (.125 INCH MINIMUM WIDTH) OR COMPLETELY ANODIZED BLUE TO INDICATE 5080 PSI MAXIMUM OPERATING PRESSURE. MARKING METHODS SHALL BE IN ACCORDANCE WITH AS5958.
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(2)
BODY - LEAD FREE SOLID FILM LUBRICANT PER AS5272 TYPE I OR II, OR PER AS6449 TYPE III OR IV, PTFE OR PETROLEUM-BASED LUBRICANT, MAY BE APPLIED TO PORTIONS OF THE ID AND OD. THE PETROLEUM-BASED LUBRICANT SHALL NOT BE IN CONTACT WITH THE SYSTEM FLUID.
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(1)
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a
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/4/
PROCUREMENT SPECIFICATION: AS5958 EXCEPT AS SPECIFIED ON THIS STANDARD. PRODUCT SUPPLIED TO THIS SPECIFICATION SHALL BE MANUFACTURED BY AN ACCREDITED MANUFACTURER AS LISTED IN THE PERFORMANCE REVIEW INSTITUTE (PRI) QUALIFIED PRODUCTS LISTING FOR PRI-QPL-AS5958 FOR THIS STANDARD. SEE www.eAuditNet.com FOR CURRENT QPL ON-LINE.
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5
DIMENSIONS AND TOLERANCES NOT DEFINED ON THIS STANDARD SHALL BE SPECIFIED AND CONTROLLED BY THE MANUFACTURER. THE MANUFACTURER IS RESPONSIBLE TO ENSURE COMPLIANCE WITH THE PROCUREMENT SPECIFICATION.
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/6/
IDENTIFICATION SHALL BE IN ACCORDANCE WITH AS5958 AND SHALL BE IDENTIFIED ON EITHER RING IN THE AREA SHOWN.
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/7/
FITTINGS SHALL BE INSTALLED IN ACCORDANCE WITH AS5959. THE AFTER SWAGE ACCEPTABILITY LIMIT DIMENSION “Z” FOR EACH PORT SIZE IS DEFINED IN AS5959.
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8
SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M. REQUIREMENTS PER ASME B46.1. UNLESS OTHERWISE SPECIFIED, THE MAXIMUM MACHINED SURFACES SHALL BE 125 MICROINCHES Ra.
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9
DIMENSIONING AND TOLERANCING: ASME Y14.5M-1994.
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a
DIMENSIONS ARE IN INCHES UNLESS OTHERWISE SPECIFIED
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b
DIMENSIONAL TOLERANCES SHALL BE ±.005 INCHES UNLESS OTHERWISE SPECIFIED
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c
ANGULAR TOLERANCES SHALL BE ±.50° UNLESS OTHERWISE SPECIFIED
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d
BREAK ALL EDGES .003 TO .010 INCHES, UNLESS OTHERWISE SPECIFIED
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a
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10
INTERPRETATION OF DRAWING PER ARP4296.
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/11/
THIS DIMENSION IS THE ALLOWABLE TUBE END POSITIONING FOR SYSTEM LAYOUT DESIGN.
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/12/
FOR JUMP SIZE FITTINGS, A TRANSITION DIAMETER WILL OCCUR IN THIS AREA.
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/13/
DIMENSION A IS THE FITTING ASSEMBLY LENGTH PRIOR TO SWAGE AND A1 IS THE FITTING BODY LENGTH BEFORE SWAGE.
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14
REVISION INDICATOR: A CHANGE BAR (|) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE OF THE USER IN LOCATING AREAS WHERE TECHNICAL REVISIONS, NOT EDITORIAL CHANGES, HAVE BEEN MADE TO THE PREVIOUS ISSUE OF THIS DOCUMENT. AN (R) SYMBOL TO THE LEFT OF THE DOCUMENT TITLE INDICATES A COMPLETE REVISION OF THE DOCUMENT, INCLUDING TECHNICAL REVISIONS. CHANGE BARS AND (R) ARE NOT USED IN ORIGINAL PUBLICATIONS, NOR IN DOCUMENTS THAT CONTAIN EDITORIAL CHANGES ONLY.
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/15/
EXAMPLE OF PART NUMBER:
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/16/
UNPAINTED RINGS “CODE A” WERE NEEDED TO PREVENT COATING/PAINT DEBRIS OF RINGS “NO CODE” IN CONTAMINATION SENSITIVE SYSTEMS. NO CODE LETTER AND CODE LETTER “A” PARTS ARE NOT RECOMMENDED FOR PROCUREMENT AFTER 03/31/2014 AND SHOULD BE REPLACED BY ANODIZED PARTS WITH CODE LETTER “B”.
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/17/
CLASS 1 - NO CODE IN PART NUMBER. PARTS ARE QUALIFIED FOR INSTALLATION ON TITANIUM AND CRES TUBINGCLASS 2 - CODE “D” IN PART NUMBER. PARTS ARE QUALIFIED FOR INSTALLATION ON TITANIUM, CRES, AND ALUMINUM TUBING.
Recommended Content
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| TABLE 1A | DIMENSIONS A THROUGH J | |
| TABLE 1B | DIMENSIONS W THROUGH W3 AND WEIGHTS |
Issuing Committee
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This Committee is responsible for developing and maintaining standards for design, test, and procurement of fluid systems part standards to improve reliability and economy. Their primary focus is on AS standards development and support of military standards. The Committee also develops ISO standards in a Subcommittee Advisory Group (SCAG) to ISO/TC 20/SC 10, and SAE-MA derivatives thereof.
Structure: SAE G-3 -- Parent committee SAE G-3A -- Aerospace Couplings Subcommittee SAE G-3B -- Aerospace Fittings Subcommittee SAE G-3D -- Aerospace Hose Subcommittee SAE G-3E - Aerospace Tubing Assemblies Subcommittee U.S. SCAG to ISO/TC 20/SC 10 -- ISO standards Major projects: Support of Military Standards Reform Support of military standard conversions to MIL-PERF and MIL-DTL. Development of AS replacements for military standards designated for conversion. Establish document to list G-3 accepted replacements for replaced part standards and military back-up specifications. Development of PRI QML/QPL Development of Performance Review Institute (PRI) process for approval and surveillance of manufacturers (Qualified Manufacturer List, QML) and for approval of standard parts as qualified for use (Qualified Parts List, QPL). Development of ISO Standards, Imperial Units ISO/TC 20/SC 10 standards have typically been developed in SI units. The ISO has approved development of inch-based ISO standards to support commercial aviation. Basic design, test, and procurement specifications will be selected from military standards that are to be converted to Non-Government standard (NGS) and developed as ISO standards.Reference
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