SAE AS1712D-2024

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AEROSPACE STANDARD

COUPLING SUBASSEMBLY, FLEXIBLE,

VARIABLE CAVITY, THREADED,

FERRULE TYPE TUBE ENDS

AS1712

™

or otherwise, or used for text and data mining, AI training, or similar technologies, 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

ISSUED 1982-05 REVISED 2006-08 REAFFIRMED 2013-01 STABILIZED 2024-06

THIRD ANGLE PROJECTION

CUSTODIAN: G-3/G-3A

REV.

FEDERAL SUPPLY CLASS

4730

AS1712

™ REV.

PROCUREMENT SPECIFICATION: AS1710 /2/

SAE Executive Standards Committee 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.

For more information on this standard, visit

https://www.sae.org/standards/content/AS1712D/

RATIONALE

THIS TECHNICAL REPORT IS BEING STABILIZED BECAUSE IT COVERS TECHNOLOGY, PRODUCTS, OR

PROCESSES WHICH ARE MATURE AND NOT LIKELY TO CHANGE IN THE FORESEEABLE FUTURE.

STABILIZED NOTICE

THIS DOCUMENT HAS BEEN DECLARED "STABILIZED" BY SAE G-3, AEROSPACE COUPLINGS, FITTINGS, HOSE,

TUBING ASSEMBLIES COMMITTEE AND WILL NO LONGER BE SUBJECTED TO PERIODIC REVIEWS FOR

CURRENCY. USERS ARE RESPONSIBLE FOR VERIFYING REFERENCES AND CONTINUED SUITABILITY OF

TECHNICAL REQUIREMENTS. NEWER TECHNOLOGY MAY EXIST.

AEROSPACE STANDARD

AS1712™

SHEET 1 OF 3

REV.

COUPLING SUBASSEMBLY, FLEXIBLE,

VARIABLE CAVITY, THREADED,

FERRULE TYPE TUBE ENDS

FIGURE 1 - COUPLING SUBASSEMBLY, FLEXIBLE

AEROSPACE STANDARD

AS1712™

SHEET 2 OF 3

REV.

COUPLING SUBASSEMBLY, FLEXIBLE,

VARIABLE CAVITY, THREADED,

FERRULE TYPE TUBE ENDS

TABLE 1 - COUPLING SUBASSEMBLY WEIGHTS

AS1712

DASH NO.

TUBE

SIZE

(REF)

O-RING

DASH NO.

(REF)

/1/

SUBASSEMBLY

WEIGHT

LB/EA

APPROX. REF.

-08

.500

114

.043

-10

.625

116

.050

-12

.750

212

.067

-16

1.000

216

.084

-20

1.250

220

.098

-24

1.500

326

.139

-28

1.750

328

.156

-32

2.000

330

.227

-36

2.250

332

.249

-40

2.500

334

.239

-44

2.750

336

.259

-48

3.000

338

.280

-56

3.500

342

.333

-64

4.000

346

.374

-72

4.500

426

.524

-80

5.000

430

.700

-88

5.500

434

.704

NOTES:

/1/ THE DASH NUMBERS LISTED IN THE TABULATION ARE STANDARD O-RING SIZES AS DEFINED BY AS568 AND

ARE NOT A PART OF THIS ASSEMBLY.

/2/ COUPLING SUBASSEMBLIES SUPPLIED TO THIS SPECIFICATION SHALL BE MANUFACTURED AND

ASSEMBLED BY AN ACCREDITED MANUFACTURER OR ASSEMBLED BY AN ACCREDITED DISTRIBUTOR

LISTED IN THE PERFORMANCE REVIEW INSTITUTE (PRI) QUALIFIED PRODUCTS LIST FOR PRI-QPL-AS1710

FOR THIS STANDARD. THE QPL IS AVAILABLE AT www.eauditnet.com.

3. RATED OPERATING CHARACTERISTICS: SEE AS1710.

4. MATERIALS AND FINISH: SEE INDIVIDUAL STANDARDS.

5. MARKING: EACH COUPLING SUBASSEMBLY SHALL BE MARKED PER AS478-30, .062 in OR LARGER

CHARACTERS, WITH MANUFACTURER’S NAME, TRADEMARK OR CAGE CODE, COMPLETE “AS” NUMBER, AND

DATE OF MANUFACTURE IN QUARTERS (1Q91 – FIRST QUARTER OF 1991). SIZES -08, -10, AND -12 MAY BE

MARKED PER AS478-35D WITH THIS INFORMATION.

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摘要：

SAE AS1712D-2024 是国际自动机工程师学会（SAE）发布的最新版航空航天标准，专用于规范高性能电连接器的设计、材料、测试与安装要求。该标准替代了先前版本，更新内容包括增强的环境耐受性、插拔耐久性以及屏蔽效能指标，适用于飞机、卫星及导弹等严苛应用场景。遵循SAE AS1712D-2024可确保连接器在极端温度、振动和电磁干扰下维持可靠信号传输，提升航空航天系统的安全性与互操作性。本标准是航空电子工程师、质量检测人员及采购部门进行选型验收的重要技术依据，有助于降低故障风险并符合适航认证

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