AEROSPACE
MATERIAL
SPECIFICATION
Aluminum Alloy, Rolled or Cold Finished Bars and Rods
(7075-T651)
Solution and Precipitation Heat Treated
(Composition similar to UNS A97075)
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Copyright © 2006 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.
TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada)
Tel: 724-776-4970 (outside USA)
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AMS 4123H®
Issued NOV 1946
Revised JAN 2006
Superseding AMS 4123G
Rationale: AMS 4123B is a Five Year Review and update of this specification.
1. SCOPE:
1.1 Form:
This specification covers an aluminum alloy in the form of bars and rods.
1.2 Application:
These products have been used typically for machined parts subject to excessive warpage
during machining due to residual stresses and for parts requiring high strength and whose
fabrication does not involve welding or forming, but usage is not limited to such applications.
1.2.1 Certain design and processing procedures may cause these products to become susceptible
to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.
2. APPLICABLE DOCUMENTS:
The issue of the following documents in effect on the date of the purchase order forms a part of
this specification to the extent specified herein. The supplier may work to a subsequent revision of
a document unless a specific document issue is specified. When the referenced document has
been cancelled and no superseding document has been specified, the last published issue of that
document shall apply.
Copyright SAE International
Provided by IHS under license with SAE
Not for ResaleNo reproduction or networking permitted without license from IHS
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SAE
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AMS 4123H AMS 4123H
2.1 SAE Publications:
Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001 or www.sae.org.
AMS 2355 Quality Assurance Sampling and Testing, Aluminum Alloys and Magnesium
Alloys, Wrought Products, Except Forging Stock, and Rolled, Forged, or
Flash Welded Rings
AMS 2772 Heat Treatment of Aluminum Alloy Raw Materials
ARP823 Minimizing Stress-Corrosion Cracking in Wrought Heat-Treatable Aluminum
Alloy Products
AS 1990 Aluminum Alloy Tempers
2.2 ASTM Publications:
Available from ASTM, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-
2959 or www.astm.org.
ASTM B 660 Packing/Packaging of Aluminum and Magnesium Products
ASTM B 666/B666M Identification Marking of Aluminum and Magnesium Products
2.3 ANSI Publications:
Available from ANSI, 25 West 43rd Street, New York, NY 10036 or www.ansi.org.
ANSI H35.2/H35.2M Dimensional Tolerances for Aluminum Mill Products
3. TECHNICAL REQUIREMENTS:
3.1 Composition:
Shall conform to the percentages by weight shown in Table 1, determined in accordance with
AMS 2355.
TABLE 1 - Composition
Element min max
Silicon -- 0.40
Iron -- 0.50
Copper 1.2 2.0
Manganese -- 0.30
Magnesium 2.1 2.9
Chromium 0.18 0.28
Zinc 5.1 6.1
Titanium -- 0.20
Other Elements, each -- 0.05
Other Elements, total -- 0.15
Aluminum remainder
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SAE
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AMS 4123H AMS 4123H
3.2 Condition:
Rolled or cold finished, solution heat treated, stress-relieved by stretching to produce a nominal
permanent set of 1-1/2% but not less than 1% nor more than 3% and precipitation heat treated.
Heat treatments shall be performed in accordance with AMS 2772 (See AS 1990).
3.2.1 Product shall receive no further straightening operations after stretching unless specifically
authorized by purchaser.
3.3 Properties:
The product shall conform to the following requirements, determined in accordance with AMS
2355 on the mill produced size and as specified herein.
3.3.1 Tensile Properties: Shall be as shown in Table 2 for rods 0.50 to 4.00 inches (12.7 to 101.6
mm) in diameter, for square, hexagonal, and octagonal bar 0.50 to 3.50 inches (12.7 to 88.9
mm) in nominal distance between parallel faces, and for rectangular bar 3.00 inches (76.2
mm) in nominal thickness with width up to 6.00 inches (152.4 mm) or for rectangular bar 0.50
to 3.00 inches (12.7 to 76.2 mm) in nominal thickness with width up to 10 inches (254 mm).
TABLE 2 - Minimum Tensile Properties
Property Value
Tensile Strength 77.0 ksi (531 MPa)
Yield Strength at 0.2% Offset 66.0 ksi (455 MPa)
Elongation in 4D 7%
3.4 Quality:
The product, as received by purchaser, shall be uniform in quality and condition, sound, and
free from foreign materials and from imperfections detrimental to usage of the product.
3.5 Tolerances:
Shall conform to all applicable requirements of ANSI H35.2 or ANSI H35.2M.
4. QUALITY ASSURANCE PROVISIONS:
4.1 Responsibility for Inspection:
The vendor of the product shall supply all samples for vendor’s tests and shall be responsible
for the performance of all required tests. Purchaser reserves the right to sample and to perform
any confirmatory testing deemed necessary to ensure that the product conforms to specified
requirements.
4.2 Classification of Tests:
Acceptance Tests: Composition (3.1), tensile properties (3.3) and tolerances (3.5) are
acceptance tests and except for composition, shall be performed on each lot.
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SAE
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AMS 4123H AMS 4123H
4.3 Sampling and Testing:
Shall be in accordance with AMS 2355.
4.4 Reports:
The vendor of the product shall furnish with each shipment a report stating that the product
conforms to the composition and tolerances, and showing the numerical results of tests on each
inspection lot to determine conformance to the tensile property requirements. This report shall
include the purchase order number, inspection lot number, AMS 4123H, size, and quantity. The
report shall also identify the producer, the product form, and the size of the mill product.
4.5 Resampling and Retesting:
Shall be in accordance with AMS 2355.
5. PREPARATION FOR DELIVERY:
5.1 Identification:
Shall be in accordance with ASTM B 666/B666M.
5.2 Packaging:
The product shall be prepared for shipment in accordance with ASTM B 660 and in compliance
with applicable rules and regulations pertaining to the handling, packaging, and transportation
of the product to ensure carrier acceptance and safe delivery.
6. ACKNOWLEDGMENT:
A vendor shall mention this specification number and its revision letter in all quotations and when
acknowledging purchase orders.
7. REJECTIONS:
Product not conforming to this specification, or to modifications authorized by purchaser, will be
subject to rejection.
8. NOTES:
8.1 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
specification. An (R) symbol to the left of the document title indicates a complete revision of the
specification, including technical revisions. Change bars and (R) are not used in original
publications, nor in specifications that contain editorial changes only.
Copyright SAE International
Provided by IHS under license with SAE
Not for ResaleNo reproduction or networking permitted without license from IHS
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SAE
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AMS 4123H AMS 4123H
8.2 Hardness should not be lower than 135 HB/10/500 or 140 HB/10/1000, or equivalent,
determined in accordance with ASTM E 10. Hardness has been used to verify that product is
properly processed, but an “out-of-range hardness number” is not always indicative of product
with “out-of-specified tensile strength”. Further analysis, including material composition
verification, heat treat process parameter review, and/or tensile property measurement may be
necessary.
8.3 Hardness conversion tables for metals are presented in ASTM E 140.
8.4 Terms used in AMS are clarified in ARP1917.
8.5 Dimensions and properties in inch/pound units and Fahrenheit temperatures are primary;
dimensions and properties in SI units and Celsius temperatures are shown as the approximate
equivalents of the primary units and are presented only for information.
8.6 Purchase documents should specify not less than the following:
AMS 4123H
Form and size of product desired
Quantity of product desired.
8.7 Keywords:
Bars and rods, aluminum alloy, rolled or cold finished, 7075-T651, UNS A97075
PREPARED UNDER THE JURISDICTION OF AMS COMMITTEE “D”
Copyright SAE International
Provided by IHS under license with SAE
Not for ResaleNo reproduction or networking permitted without license from IHS
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