SAE AMS5596L
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
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
Hardcopy , PDF
19-11-2017
English
01-01-2016
Important note : Users cannot be edited or removed once added to your Multi user PDF.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Superseded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 ARP699E | 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 |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.