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SAE AMS4945F

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC 3AL - 2.5V, CONTROLLED CONTRACTILE STRAIN RATIO COLD WORKED, STRESS RELIEVED

Available format(s)

Hardcopy , PDF

Superseded date

02-06-2018

Superseded by

SAE AMS4945G

Language(s)

English

Published date

01-01-2014

€93.68
Excluding VAT

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
10
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

SAE MA 4098 : 2015 HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, HEAVY DUTY, METALLIC REINFORCED, 204 DEGREE C, 35000 KPA, HYDRAULIC AND PNEUMATIC, METRIC
BS ISO 8913:2006 Aerospace. Lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 400°F/3000 psi (204°C/20684 kPa) and 204°C/21000 kPa (400°F/3046 psi). Procurement specification
MIL-DTL-85052 Revision B:2005 CLAMP, LOOP, CUSHION, GENERAL SPECIFICATION FOR
SAE MA 2151 : 2015 CLAMP ASSEMBLIES, SADDLE OR OMEGA STYLE, TWO POINT MOUNT, MULTIPLE SHAPES, METRIC
SAE MA614A HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE (PTFE), METALLIC REINFORCED, 28,000 KPA, 204 DEGREES C, HYDRAULIC, METRIC
SAE J1779_201305 SHIP SYSTEMS AND EQUIPMENT - HYDRAULIC SYSTEM DESIGN CRITERIA FOR MARINE VEHICLES
BS ISO 23933:2006 Aerospace series. Aramid reinforced lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 135°C/20 684 kPa (275°F/3 000 psi) and 135°C/21 000 kPa (275°F/3 046 psi). Procurement specification
MIL-H-5440 Revision H:1993 HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR
BS ISO 7169:2014 Aerospace. Separable tube fittings for fluid systems, for 24° cones, for pressures up to 3 000 psi or 21 000 kPa. Procurement specification, inch/metric
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
ISO 23933:2006 Aerospace Aramid reinforced lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 135 degrees C/20 684 kPa (275 degrees F /3 000 psi) and 135 degrees C/21 000 kPa (275 degrees F/3 046 psi) Procurement specification
SAE AS4623E HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA-ARAMID REINFORCED, 3,000 PSI, 275 DEGREES F, HEAVY DUTY, AIRCRAFT HYDRAULIC SYSTEMS
SAE AS 5958 : 2017 FITTINGS, AXIALLY SWAGED TUBE WITH FLARELESS SEPARABLE, FLUID SYSTEM FOR OPERATING PRESSURES UP TO AND INCLUDING 5080 PSI (35 000 KPA), SPECIFICATION FOR
SAE MA 4510 : 2015 FITTINGS, WELD, FLUID CONNECTION, 35,000 KPA, METRIC
SAE AS 4467 : 2013 STANDARDIZATION, HYDRAULIC TUBE WALLS
SAE AS614D HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 4000 PSI, 400 DEGREES F, HEAVY DUTY, HYDRAULIC AND PNEUMATIC
05/30128217 DC : DRAFT JAN 2005 ISO/DIS 23933 - AEROSPACE - ARAMID REINFORCED LIGHTWEIGHT POLYTETRAFLUOROETHYLENE (PTFE) HOSE ASSEMBLIES, CLASSIFICATION 135 DEGREE C/20 684 KPA (275 DEGREE F/3 000 PSI) AND 135 DEGREE C/21 000 KPA (275 DEGREE F/3 046 PSI) - PROCUREMENT SPECIFICATION
MIL-DTL-18866 Revision J:2015 Fittings, Hydraulic Tube, Flared, 37 Degree and Flareless, General Specification for
SAE AS4459B FITTINGS, TUBE, FLUID SYSTEM 3000 PSIG (21000 KPA) RATED PRESSURE, EXTERNALLY SWAGED, SPECIFICATION FOR
SAE AS 85052 : 2015 CLAMP ASSEMBLY, LOOP TYPE, CUSHIONED, GENERAL SPECIFICATION FOR
SAE AS 4510 : 2013 FITTINGS, WELD, FLUID CONNECTION, 5000 PSI
SAE AIR5005A AEROSPACE - COMMERCIAL AIRCRAFT HYDRAULIC SYSTEMS
SAE AS1975G Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems
SAE MA 1975 : 2015 HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID REINFORCED, 135 DEGREE C, STANDARD DUTY, 28000/21000 KPA, HYDRAULIC, AIRCRAFT SYSTEMS
SAE MA2126B HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE (PTFE), UP TO 232 DEGREES C AND 10 500 KPA PROCUREMENT SPECIFICATION, METRIC
NASA HDBK 6025 : 2014 GUIDELINES FOR THE SPECIFICATION AND CERTIFICATION OF TITANIUM ALLOYS FOR NASA FLIGHT APPLICATIONS
SAE MA2005B TUBE FITTINGS, AEROSPACE FLUID SYSTEMS, SEPARABLE, FOR 24 DEGREE CONE, GENERAL SPECIFICATION, METRIC
SAE ARP4146C COILED TUBING - TITANIUM ALLOY, HYDRAULIC APPLICATIONS, AEROSPACE
SAE AS4098A HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, HEAVY DUTY, METALLIC REINFORCED, 400 DEGREE F, 5000 PSI HYDRAULIC AND PNEUMATIC
ISO 8913:2006 Aerospace Lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 400 degrees F/3 000 psi (204 degrees C/20 684 kPa) and 204 degrees C/21 000 kPa (400 degrees F/3 046 psi) Procurement specification
SAE AS 4897 : 1994 HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE (PTFE), LOW PRESSURE, 450 DEGREES F AND FIREPROOF, PROCUREMENT SPECIFICATION FOR
ISO 7169:2014 Aerospace Separable tube fittings for fluid systems, for 24 degree cones, for pressures up to 3 000 psi or 21 000 kPa Procurement specification, inch/metric
SAE AS1576E FITTINGS, WELDED, HYDRAULIC, TITANIUM, CORROSION RESISTANT STEEL AND NICKEL, 3000 PSI HYDRAULIC
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 MA 2150 : 2015 CLAMPS, LOOP OR P STYLE, SINGLE POINT MOUNT, MULTIPLE SHAPES, METRIC
SAE ARP994B DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS
SAE AS4604B HOSE ASSEMBLY, 3000 PSI, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 400 DEGREES F, HEAVY DUTY, AIRCRAFT HYDRAULIC SYSTEMS
SAE ARP4752B AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS
SAE MA 4623 : 2015 Hose Assembly, Polytetrafluoroethylene, Para Aramid Reinforced Heavy-Duty, 21 000 kPa, 135 °C, Aircraft Hydraulic Systems, Metric
SAE AS1946E HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, UP TO 1500 PSI AND 450 DEGREES F, HYDRAULIC AND PNEUMATIC

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
ASTM E 2994 : 2016 Standard Test Method for Analysis of Titanium and Titanium Alloys by Spark Atomic Emission Spectrometry and Glow Discharge Atomic Emission Spectrometry (Performance-Based Method)
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 ARP 1917 : 2002 CLARIFICATION OF TERMS USED IN AEROSPACE METALS SPECIFICATIONS
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 4076 : 2013 CONTRACTILE STRAIN RATIO TESTING OF TITANIUM HYDRAULIC TUBING
SAE AS 33611 : 2015 TUBE BEND RADII

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