Sae-as5202_port_dimensions.pdf 6z15v

REVISED 2005-05

FIGURE 1 - FITTING END

THIRD ANGLE PROJECTION

CUSTODIAN: SAE G-3/G-3B

ISSUED 2001-08

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AS5202

REV. A

FEDERAL SUPPLY CLASS 4730

PROCUREMENT SPECIFICATION: NONE /1/

AEROSPACE STANDARD PORT OR FITTING END, INTERNAL STRAIGHT THREAD, DESIGN STANDARD --`,`,,,,,,,,,``````,,``,``,`,,-`-`,,`,,`,`,,`---

AS5202 SHEET 1 OF 3

REV. A

Copyright 2005 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. Copyright SAE International PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: 724-776-4970 (outside USA) Provided by IHS under license withTO SAE Licensee=NASA Technical Standards 4/9972545004, =Rosczypala, Craig Fax: 724-776-0790 [email protected] SAE WEB ADDRESS: http://www.sae.org No reproduction or networking permitted without license from IHS Not for Resale,Email: 08/25/2008 08:28:26 MDT

REV. A AS5202

TABLE 1A - DIMENSIONS BASIC NO. AS5202 /9/ SIZE CODE 01 02 03

(NOMINAL TUBE SIZE) -.125 .188

T THREAD PER AS8879 CLASS 3B .2500-28-UNJF .3125-24-UNJF .3750-24-UNJF

A -.000/+.015 .359 .438 .500

B .330 .482 .538

C .062 .062 .125

D -.000/+.005 .264 .328 .390

04 05 06

.250 .312 .375

.4375-20-UNJF .5000-20-UNJF .5625-18-UNJF

.562 .625 .688

.568 .568 .598

.172 .234 .297

.454 .517 .580

07 08 09

.438 .500 .562

.6250-18-UNJF .7500-16-UNJF .8125-16-UNJ

.750 .875 .938

.614 .714 .730

.360 .391 .438

.643 .769 .832

10 11 12

.625 .688 .750

.8750-14-UNJF 1.0000-12-UNJF 1.0625-12-UNJ

1.000 1.156 1.234

.802 .877 .877

.484 .547 .609

.896 1.023 1.086

14 16 18

.875 1.000 1.125

1.1875-12-UNJ 1.3125-12-UNJ 1.5000-12-UNJF

1.362 1.487 1.675

.877 .877 .877

.734 .844 .953

1.211 1.336 1.524

20 24 28

1.250 1.500 1.750

1.6250-12-UNJ 1.8750-12-UNJ 2.2500-12-UNJ

1.800 2.050 2.425

.877 .877 .877

1.078 1.312 1.547

1.648 1.898 2.273

32

2.000

2.5000-12-UNJ

2.675

.907

1.781

2.524

TABLE 1B - DIMENSIONS BASIC NO. AS5202 /9/ SIZE CODE 01 02 03

E -.000/+.015 .063 .063 .063

G .478 .602 .665

J .402 .577 .583

N .002 .003 .003

04 05 06

.075 .075 .083

.728 .790 .852

.656 .656 .709

.003 .003 .004

07 08 09

.094 .094 .107

.915 1.040 1.102

.725 .834 .850

.004 .004 .004

10 11 12

.107 .125 .125

1.165 1.352 1.415

.930 1.064 1.064

.004 .004 .004

14 16 18

.125 .125 .125

1.540 1.665 1.790

1.064 1.064 1.116

.004 .004 .004

20 24 28

.125 .125 .125

1.978 2.228 2.602

1.116 1.127 1.243

.004 .006 .006

32

.125

2.852

1.368

.006

AEROSPACE STANDARD PORT OR FITTING END, INTERNAL STRAIGHT THREAD, DESIGN STANDARD

AS5202 SHEET 2 OF 3

--`,`,,,,,,,,,``````,,``,``,`,,-`-`,,`,,`,`,,`---

Copyright SAE International Provided by IHS under license with SAE No reproduction or networking permitted without license from IHS

Licensee=NASA Technical Standards 4/9972545004, =Rosczypala, Craig Not for Resale, 08/25/2008 08:28:26 MDT

REV. A

REV. A AS5202

NOTES:

--`,`,,,,,,,,,``````,,``,``,`,,-`-`,,`,,`,`,,`---

/1/

THIS FITTING END IS DESIGNED FOR USE WITH FITTINGS PER AS4875. THIS STANDARD IS THE FUNCTIONAL EQUIVALENT OF MS33649 AND IS INTENDED TO BE A SUITABLE REPLACEMENT STANDARD.

/2/

MINIMUM DIAMETER FLAT SURFACE CLEARANCE PROVISIONS FOR FITTING, WRENCH, FITTING INSTALLATIONS AND TOOL FILLET RADII MUST BE ADDED AS REQUIRED. THE PERPENDICULARITY N TO THE THREADS APPLIES ONLY TO THE ∅G MINIMUM. G DIAMETER MAY BE REDUCED BY .040 WHEN IT DEFINES THE LIMITS OF A RAISED SURFACE AND WHEN STRENGTH REQUIREMENTS PERMIT.

3.

B DIMENSION IS THE FULL THREAD DEPTH REQUIREMENT FOR BLIND TAP DESIGN.

4.

INTERPRETATION OF DRAWING PER ARP4296.

5.

SURFACE TEXTURE: SYMBOLS PER ASME Y14.36M; REQUIREMENTS PER ASME B46.1. UNLESS OTHERWISE SPECIFIED, MACHINED SURFACES TO BE 125 µin Ra.

6.

BREAK EDGES .003 TO .015 UNLESS OTHERWISE SPECIFIED.

7.

DIMENSIONING AND TOLERANCING: ASME Y14.5M-1994.

8.

DIMENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED, TOLERANCES: LINEAR DIMENSIONS ±.005, ANGULAR DIMENSIONS ±0°30'.

/9/

EXAMPLE OF DRAWING CALLOUT: a.

TABULATED PART DRAWING: FITTING END PER AS5202

b.

INDIVIDUAL PART DRAWING:

10. NOTE: "THIS STANDARD IS USED TO IMPLEMENT INTERNATIONAL STANDARDIZATION AGREEMENTS: NATO STANAG 3510 AND ASCC AIR STD 25/6. PLEASE NOTIFY THE FOLLOWING OFFICES WHEN CHANGES ARE MADE OR THESE OFFICES FOR INQUIRIES PERTAINING TO THESE AGREEMENTS. NORTH ATLANTIC TREATY ORGANIZATION (NATO) STANDARDIZATION AGENCY, “[email protected]”, TEL - 1 703 696 8452, 1815 N. FORT MYER DRIVE, SUITE 400, ARLINGTON VA 22209-1809, USA. 11. THE CHANGE BAR ( l ) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE OF THE 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.

AEROSPACE STANDARD PORT OR FITTING END, INTERNAL STRAIGHT THREAD, DESIGN STANDARD

Copyright SAE International Provided by IHS under license with SAE No reproduction or networking permitted without license from IHS

AS5202 SHEET 3 OF 3

Licensee=NASA Technical Standards 4/9972545004, =Rosczypala, Craig Not for Resale, 08/25/2008 08:28:26 MDT

REV. A