SAE AS1710D-2014

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AEROSPACE

STANDARD

AS1710 REV. D

Issued 1982-05

Revised 2009-02

Reaffirmed 2014-11

Superseding AS1710C

Coupling, Fuel, Flexible, Variable Cavity,

Threaded Type With Ferrules

RATIONALE

AS1710D has been reaffirmed to comply with the SAE five-year review policy.

__________________________________________________________________________________________________________________________________________

SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely

voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.”

SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and

suggestions.

recording, or otherwise, without the prior written permission of SAE.

TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada)

Tel: +1 724-776-4970 (outside USA)

Fax: 724-776-0790

Email: CustomerService@sae.org

SAE WEB ADDRESS: http://www.sae.org

SAE values your input. To provide feedback

on this Technical Report, please visit

http://www.sae.org/technical/standards/AS1710D

1. SCOPE

This SAE Aerospace Standard (AS) defines the requirements for a threaded flexible coupling assembly, which utilizes

ferrules or machined tube end fittings to join tubing and components in aircraft fuel and fuel vent or other systems. This

coupling assembly is designed for use from -65 to +200 °F and at 125 psig peak working pressure, and the coupling

assembly may be used in other fluid systems when requirements are within the limits.

2. APPLICABLE DOCUMENTS

The following documents form a part of this specification to the extent specified herein.

2.1 SAE Publications

Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside

USA and Canada) or 724-776-4970 (outside USA), www.sae.org

AMS-R-25988 Rubber, Fluorosilicone Elastomer, Oil-and-Fuel-Resistant, Sheet, Strips, Molded Parts, and Extruded

Shapes

AMS-WW-T-700/6 Tube, Aluminum Alloy, Drawn, Seamless, 6061

ARP9013 Statistical Product Acceptance Requirements

AS567 Safety Cable, Safety Wire, Key Washers, and Cotter Pins for Propulsion Systems, General Practices

for Use of

AS568 Aerospace Size Standard for O-rings

AS1055 Fire Testing of Flexible Hose, Tube Assemblies, Coils, Fittings, and Similar System Components

AS1711 Coupling, Flexible, Variable Cavity, Threaded Ferrule Type Tube Ends, Envelope Dimensions Design

Standard

AS1712 Coupling Subassembly, Flexible, Variable Cavity, Threaded, Ferrule Type Tube Ends

AS1713 Half Coupling Subassembly, Flexible, Variable Cavity, Threaded, Ferrule Type Tube Ends

AS1714 Nut Assembly, Coupling, Flexible, Variable Cavity, Threaded, Ferrule Type Tube Ends

AS1715 Washer, Coupling, Flexible, Variable Cavity, Threaded, Ferrule Type Tube Ends

AS1716 Ferrule, Coupling, Flexible, Variable Cavity, Threaded, Ferrule Tube End

AS1717 Retainer, Coupling, Flexible, Variable Cavity, Threaded Ferrule Type Tube Ends

AS1718 Coupling Body, Flexible, Variable Cavity, Threaded Ferrule Type Tube Ends

AS1719 Fitting End, Half-Coupling, Flexible Variable Cavity Threaded, Ferrule Type Design Standard

AS1720 Ferrule End, Coupling, Flexible Variable Cavity, Threaded, Ferrule Type, Design Standard

AS4060 Tube Fitting Swaged Joint, Roller Expander, Manual Process, Requirements for

AS7003 NADCAP Program Requirements

AS7112 National Aerospace and Defense Contractors Accreditation Program Requirements for Fluid System

Components

2.2 U.S. Government Publications

Available from Document Automation and Production Service (DAPS), Building 4/D, 700 Robbins Avenue, Philadelphia,

PA 19111-5094, Tel: 215-697-6257, http://assist.daps.dla.mil/quicksearch/.

FED-STD-H28/2 Screw-Thread Standards for Federal Services Section 2: Unified Inch Screw Threads - UN and UNR

Thread Forms

MIL-HDBK-831 Military Handbook, Preparation of Test Reports

MIL-L-10547 Liners, Case and Sheet, Overwrap; Water-Vaporproof or Waterproof, Flexible

MIL-PRF-680 Performance Specification, Degreasing Solvent (Stoddard Solvent)

MIL-PRF-7024 Performance Specification, Calibrating Fluids, Aircraft Fuel System Components

MIL-STD-129 Military Marking for Shipment and Storage

MIL-STD-130 Identification Marking of U.S. Military Property

MIL-STD-810 Environmental Engineering Considerations and Laboratory Tests

MIL-STD-889 Dissimilar Metals

MIL-STD-2073-1 Department of Defense, Standard Practice for Military Packaging

PPP-B-566 Boxes, Folding, Paperboard

PPP-B-585 Boxes, Wood, Wirebound

PPP-B-676 Boxes, Set-up

VV-P-236 Petrolatum, Technical

SAE INTERNATIONAL

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2.3 ASTM Publications

Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel:

610-832-9585, www.astm.org.

ASTM D 473 Standard Test Method for Sediment in Crude Oils and Fuel Oils by the Extraction Method

ASTM D 5118/D5118M Standard Practice for Fabrication of Fiberboard Shipping Boxes

ASTM D 5486/D5486M Standard Specification for Pressure Sensitive Tape for Packaging, Box Closure, and Sealing

ASTM D 6251/D6251M Standard Specification for Wood Cleated Panelboard Shipping Boxes

2.4 PRI Publications

Available from Performance Review Institue, 161 Thornhill Road, Warrendale, PA 15086-7527, Tel: 724-772-1616,

www.pri-network.org.

PD2001 Qualified Product Management Council Procedures for Qualified Products Group

PD2101 Aerospace Quality Assurance, Product Standard, Qualification Procedures, Fluid Systems

2.5 ASME Publications

Available from American Society of Mechanical Engineers, 22 Law Drive, P.O. Box 2900, Fairfield, NJ 07007-2900, Tel:

973-882-1170, www.asme.org.

ASME B1.1 Unified Inch Screw Threads (UN and UNR Thread Form)

2.6 ANSI Publications

Available on-line at www.asq.org or from American National Standards Institute, 25 West 43rd Street, New York, NY

10036-8002, Tel: 212-642-4900, www.ansi.org.

ANSI/ASQC Z.1.4 Sampling Procedures and Tables for Inspection by Attributes.

3. TECHNICAL REQUIREMENTS

3.1 Qualification

Full coupling assemblies furnished under this document shall be products that are qualified by meeting all of the

requirements covered by this document. Manufacturers choosing to produce only a part or parts of the coupling assembly

shall qualify the part or parts by complying with the requirements and performing all tests of this document. The test

specimens for qualification of a part or parts shall be completed with a qualified part or parts made by other

manufacturers. Half coupling parts shall be qualified parts of the full coupling.

3.1.1 Manufacturer Qualification

A manufacturer producing a product in conformance to this procurement specification shall be accredited in accordance

with the requirements of PD2101, AS7003 and AS7112, and shall be listed in a Performance Review Institute (PRI)

Qualified Manufacturers List (QML).

3.1.2 Product Qualification

All products shall conform to the requirements of this procurement specification and shall be approved in accordance with

the requirements of PD2001 and PD2101 for listing in a Performance Review Institute (PRI) Qualified Parts List (QPL).

SAE INTERNATIONAL

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摘要：

SAE AS1710D-2014是一项由国际自动机工程师学会（SAE）发布的航空航天领域关键标准，主要针对密封件与密封系统的设计、选材、测试及性能要求进行了全面更新与规范。该标准取代了之前的AS1710C版本，适用于航空航天发动机、液压系统、燃料系统等高压、高温或极端环境下使用的密封元件，旨在确保密封结构的可靠性、耐久性与安全性。通过明确密封件材料兼容性、泄漏率限制、安装间隙及寿命验证方法，SAE AS1710D-2014为航空航天制造商、维修商及质检机构提供了统一的技术基准，有助于降低飞行器系

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SAE AS1710D-2014

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