SAE AMS4944L
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC 3.0AL - 2.5V COLD WORKED, STRESS RELIEVED
Hardcopy , PDF
03-02-2020
English
01-01-2015
1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES
Specifies a titanium alloy in the form of seamless tubing.
Committee |
AMS-G
|
DocumentType |
Standard
|
Pages |
9
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
MIL-DTL-85052 Revision B:2005 | CLAMP, LOOP, CUSHION, GENERAL SPECIFICATION FOR |
ASTM F 2146 : 2013 : REDLINE | Standard Specification for Wrought Titanium-3Aluminum-2.5Vanadium Alloy Seamless Tubing for Surgical Implant Applications (UNS R56320) |
SAE MA 2060 : 2015 | FITTINGS, WELDED, HYDRAULIC, TITANIUM AND CORROSION RESISTANT STEEL, 21 000 KPA, METRIC |
SAE AS 4076 : 2013 | CONTRACTILE STRAIN RATIO TESTING OF TITANIUM HYDRAULIC TUBING |
SAE AS1946E | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, UP TO 1500 PSI AND 450 DEGREES F, HYDRAULIC AND PNEUMATIC |
SAE J1779_201305 | SHIP SYSTEMS AND EQUIPMENT - HYDRAULIC SYSTEM DESIGN CRITERIA FOR MARINE VEHICLES |
SAE ARP 4698 : 2013 | GUIDE FOR CHOOSING A MINIMUM WALL THICKNESS OF TUBING FOR USE WITH WELD FITTINGS CODED FOR A RANGE OF WALL SIZES |
SAE AIR1388B | SERVICE DAMAGE LIMITS FOR AIRCRAFT HYDRAULIC TUBING |
SAE ARP1185B | FLEXURE TESTING OF HYDRAULIC TUBING JOINTS AND FITTINGS |
SAE AIR5005A | AEROSPACE - COMMERCIAL AIRCRAFT HYDRAULIC SYSTEMS |
SAE MA 2150 : 2015 | CLAMPS, LOOP OR P STYLE, SINGLE POINT MOUNT, MULTIPLE SHAPES, METRIC |
SAE AS 85052 : 2015 | CLAMP ASSEMBLY, LOOP TYPE, CUSHIONED, GENERAL SPECIFICATION FOR |
SAE ARP4752B | AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS |
NASA HDBK 6025 : 2014 | GUIDELINES FOR THE SPECIFICATION AND CERTIFICATION OF TITANIUM ALLOYS FOR NASA FLIGHT APPLICATIONS |
SAE AIR 1529 : 1989 | FLEXURE TESTING OF HYDRAULIC TUBING JOINTS AND FITTINGS BY PLANAR RESONANT VIBRATION (FREE-FREE BEAM) |
SAE AS 4510 : 2013 | FITTINGS, WELD, FLUID CONNECTION, 5000 PSI |
MIL H 85800 : 0 | HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID FIBER REINFORCED, 5000 & 8000 PSI, GENERAL SPECIFICATION FOR |
MIL-F-85720 Base Document:1985 | FITTING, TUBE, FLUID SYSTEMS, SEPARABLE, HIGH PRESSURE, DYNAMIC BEAM, SEAL, GENERAL SPECIFICATION FOR |
SAE AS1241D | FIRE RESISTANT PHOSPHATE ESTER HYDRAULIC FLUID FOR AIRCRAFT |
SAE MA 2151 : 2015 | CLAMP ASSEMBLIES, SADDLE OR OMEGA STYLE, TWO POINT MOUNT, MULTIPLE SHAPES, METRIC |
SAE AS 4388 : 2013 | HOSE ASSEMBLY PTFE HEAVY DUTY, -65 TO 400 DEGREES F (-55 TO 204 DEGREES C) 8000 PSI (56000 KPA) HYDRAULIC AND PNEUMATIC |
SAE ARP4925B | AEROSPACE DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT HELICOPTER HYDRAULIC SYSTEMS |
ASTM E 2371 : 2013 | Standard Test Method for Analysis of Titanium and Titanium Alloys by Direct Current Plasma and Inductively Coupled Plasma Atomic Emission Spectrometry (Performance-Based Test Methodology) |
SAE AMS 2809 : 2007(R2011) | IDENTIFICATION, TITANIUM AND TITANIUM ALLOY WROUGHT PRODUCTS |
ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
SAE AMS2750E | PYROMETRY |
ASTM E 1409 : 2013 : REDLINE | Standard Test Method for Determination of Oxygen and Nitrogen in Titanium and Titanium Alloys by Inert Gas Fusion |
SAE AMS2249G | CHEMICAL CHECK ANALYSIS LIMITS, TITANIUM AND TITANIUM ALLOYS |
SAE AMS 2634 : 2013 | ULTRASONIC INSPECTION, THIN WALL METAL TUBING |
ASTM E 8/E8M : 2016-09 | TEST METHODS FOR TENSION TESTING OF METALLIC MATERIALS |
SAE AS 33611 : 2015 | TUBE BEND RADII |
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