COUPLING BODY, THREADLESS - FLEXIBLE, FIXED CAVITY, SELF-BONDING PDF Download
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Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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Languages : en
Pages : 0
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Book Description
AS1655C HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
AS1655C HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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ISBN:
Category :
Languages : en
Pages : 0
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Book Description
AS5835 HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY. CAUTION: THE AS5830 SERIES COUPLING BODY AND SLEEVE WILL FIT ON AS1650 SERIES FERRULES DUE TO THE USE OF O-RING SEAL SIZES IN COMMON. ALSO, ASSEMBLY OF WORN AS1650 SERIES SLEEVE WITH AS5830 SERIES FERRULES MAY BE POSSIBLE.WARNING: DO NOT MIX AS5830 SERIES PARTS WITH AS1650 SERIES PARTS. THIS COMBINATION IS NOT QUALIFIED AND MAY RESULT IN CATASTROPHIC LEAKAGE AND/OR PREMATURE FAILURE OF THE JOINT AND DOES NOT PRODUCE A HIGH CURRENT CAPABLE JOINT TO THE REQUIREMENTS OF AS5830 SPECIFICATION.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
AS1652A HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
REVISE DIAMETER "F" FOR NOMINAL SIZES .500," .625," .750" TO ALLOW ADDITIONAL DIAMETRICAL CLEARANCE BASED ON PHYSICAL PART MEASUREMENTS.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
AS5831 HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY. CAUTION: THE AS5830 SERIES COUPLING BODY AND SLEEVE WILL FIT ON AS1650 SERIES FERRULES DUE TO THE USE OF O-RING SEAL SIZES IN COMMON. ALSO, ASSEMBLY OF WORN AS1650 SERIES SLEEVE WITH AS5830 SERIES FERRULES MAY BE POSSIBLE.WARNING: DO NOT MIX AS5830 SERIES PARTS WITH AS1650 SERIES PARTS. THIS COMBINATION IS NOT QUALIFIED AND MAY RESULT IN CATASTROPHIC LEAKAGE AND/OR PREMATURE FAILURE OF THE JOINT AND DOES NOT PRODUCE A HIGH CURRENT CAPABLE JOINT TO THE REQUIREMENTS OF AS5830 SPECIFICATION.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
This document defines the requirements for a threadless, flexible, self-bonding coupling assembly, which, when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing and components in aircraft fuel, vent, or other systems. This assembled coupling, hereafter referred to as the assembly, is designed for use from -54 to 204 °C and at 862 kPa operating pressure. AS coupling components referenced herein have been qualified to AS1650. Ferrules referenced herein are inch ferrules adapted to metric tubing. MA2241 has been reaffirmed to comply with the SAE five-year review policy.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
AS5832 HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY. CAUTION: THE AS5830 SERIES COUPLING BODY AND SLEEVE WILL FIT ON AS1650 SERIES FERRULES DUE TO THE USE OF O-RING SEAL SIZES IN COMMON. ALSO, ASSEMBLY OF WORN AS1650 SERIES SLEEVE WITH AS5830 SERIES FERRULES MAY BE POSSIBLE.WARNING: DO NOT MIX AS5830 SERIES PARTS WITH AS1650 SERIES PARTS. THIS COMBINATION IS NOT QUALIFIED AND MAY RESULT IN CATASTROPHIC LEAKAGE AND/OR PREMATURE FAILURE OF THE JOINT AND DOES NOT PRODUCE A HIGH CURRENT CAPABLE JOINT TO THE REQUIREMENTS OF AS5830 SPECIFICATION.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
NEW PART STANDARD AS PART OF AS7510 TO SUPERSEDE AS5835.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
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Category :
Languages : en
Pages : 0
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Book Description
This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, high conductive self-bonding coupling assembly which, when installed on defined ferrules, provides a flexible connection for joining ducting and components in pressurized fluid systems. The assembled coupling is designed to provide interchangeability of parts and components between qualified manufacturers for use from -65 to +265 °F at 130 psi nominal operating pressures and for the service life of the aircraft system. FAR 23.954, FAR 25.901, FAR 25.954 and FAR 25.981 certification requirements have identified the need for high current capable flexible fluid assembled couplings. The coupling assembly does not require inspection and maintenance to remain current capable for the life of the aircraft.This specification provides two test philosophies necessary for low pressure couplings: 1EME/lightning testing of assembled couplings to demonstrate electrostatic capabilities are retained through simulated service life test sequences to meet commercial airplane FAR 25.981 certification requirements. 2Grouping and goal posting of coupling test specimens based on size and material similarities.The assembled coupling's intended application and usage is for, but not limited to, commercial and military aircraft. Components defined herein and qualified to the performance capabilities and regulatory compliance requirements will support their use in fuel and other fluid conveyance systems.This specification requires manufactures to be qualified and accredited to Performance Review Institute (PRI)/National Aerospace and Defense Contractors Accreditation Program (Nadcap) requirements. New part specification to supersede AS5830.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
This aerospace specification defines the requirements for a threadless, flexible, self-bonding coupling assembly which, when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing and components in aircraft fuel, vent or other systems. This assembled coupling, hereafter referred to as the assembly, is designed for use from -65 to +400 °F and at 125 psig nominal operating pressure.
