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SAE AMS 5596 : 2016

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, FOIL AND PLATE, 52.5NI - 19CR - 3.0MO - 5.1CB (NB) - 0.90TI - 0.50AL - 18FE, CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED, 1775 DEGREES F (968 DEGREES C) SOLUTION HEAT TREATED
Available format(s)

Hardcopy , PDF

Superseded date

11-19-2017

Language(s)

English

Published date

01-01-2016

This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, foil, and plate 1.00 inch (25.4 mm) and under in thickness (see8.5).

Committee
AMS F
DocumentType
Standard
Pages
9
PublisherName
SAE International
Status
Superseded
SupersededBy

SAE ARP 699 : 2015 HIGH TEMPERATURE PNEUMATIC DUCT SYSTEMS FOR AIRCRAFT
ASTM F 3055 : 2014 Standard Specification for Additive Manufacturing Nickel Alloy (UNS N07718) with Powder Bed Fusion
ASTM F 3055 : 2014 : EDT 1 Standard Specification for Additive Manufacturing Nickel Alloy (UNS N07718) with Powder Bed Fusion
SAE AMS 2774 : 2016 HEAT TREATMENT, WROUGHT NICKEL ALLOY AND COBALT ALLOY PARTS
SAE ARP 1755 : 2000 EFFECT OF CLEANING AGENTS ON AIRCRAFT ENGINE MATERIALS, STOCK LOSS TEST METHOD

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