Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
FITTING ASSEMBLY, ELBOW, 90 DEGREE, AXIALLY SWAGED, HYDRAULIC, 5080 PSI
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
FITTING ASSEMBLY, ELBOW, 90°, AXIALLY SWAGED, HYDRAULIC, 5080 PSI
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
THIS STANDARD WAS PREPARED TO PROVIDE AN ENVELOPE REQUIREMENTS FOR AN AXIALLY SWAGED, FIELD ATTACHABLE, 5000 PSI, TUBE FITTING. /1/MATERIALS: CODE LETTER "T" RINGS-AMS 4965 TITANIUM ALLOY, 6.0AL 4.0V SOLUTION HEAT TREATED AND AGED OR AMS 4928 TITANIUM ALLOY 6.0 AL 4.0V ANNEALED WITH HIGH STRENGTH CARBON FIBER/EPOXY RESIN COMPOSITE REINFORCEMENT. BODY-AMS 4928 TITANIUM ALLOY, 6.0AL 4.0V ANNEALED 2FINISH: TITANIUM-NONE REQUIRED /3/COATINGS/LUBRICANTS: RINGS-THE OUTER SURFACE SHALL HAVE A .125" MINIMUM WIDTH BLUE COLORED RING OR COMPLETELY COLORED BLUE TO INDICATE 5080 PSI MAXIMUM OPERATION PRESSURE. AN AS1241 FLUID RESISTANT PTFE COATING OR PAINT MUST BE USED. BODY-SOLID FILM LUBRICANT PER AS5272, TYPE I OR II, PTFE OR PETROLEUM-BASED LUBRICANT MAY BE APPLIED TO PORTIONS OF THE ID AND OD. THE PETROLEUM-BASED LUBRICANT SHALL NOT BE IN CONTACT WITH THE SYSTEM FLUID. /4/ALL PRODUCTS SUPPLIED TO THIS SPECIFICATION SHALL BE MANUFACTURED BY AN ACCREDITED MANUFACTURER AS LISTED IN THE PERFORMANCE REVIEW INSTITUTE (PRI) QUALIFIED PRODUCTS LIST FOR PRI-QPL-AS5958 FOR THIS STANDARD. SEE HTTP:WWW.PRI.SAE.ORG/QPL/AS5958.PDF FOR CURRENT QPL ONLINE. PRIOR TO ISSUANCE OF THE PRI-QPL, USERS ARE ADVISED TO CONTROL SOURCE APPROVALS BY STANDARD PAGE SUPPLEMENT SHEET OR SIMILAR MEANS. 5DIMENSIONS AND TOLERANCES NOT DEFINED ON THIS STANDARD SHALL BE SPECIFIED AND CONTROLLED BY THE MANUFACTURER. THE MANUFACTURER IS RESPONSIBLE TO ENSURE COMPLIANCE WITH THE PROCUREMENT SPECIFICATION. /6/IDENTIFICATION SHALL BE IN ACCORDANCE WITH AS5958 AND SHALL BE IDENTIFIED ON EITHER RING IN THE AREA SHOWN. 7FITTINGS SHALL BE INSTALLED IN ACCORDANCE WITH AS5959. 8SURFACE TEXTURE SHALL BE IN ACCORDANCE WITH AMERICAN SOCIETY OF MECHANICAL ENGINEERS. ASME Y14.1 AND THE SYMBOLS IN ACCORDANCE WITH ASME14.36M. UNLESS OTHERWISE SPECIFIED, THE MAXIMUM MACHINED SURFACES SHALL BE 125 uin Ra AND THE MAXIMUM FORGED SURFACES SHALL BE 250 uin Ra. 9DIMENSIONS AND TOLERANCES SHALL BE IN ACCORDANCE WITH AMERICAN SOCIETY OF MECHANICAL ENGINEERS, ASME Y14.5M-1994. aDIMENSIONS ARE IN INCHES UNLESS OTHERWISE SPECIFIED bDIMENSIONAL TOLERANCES SHALL BE +/-.005 INCHES UNLESS OTHERWISE SPECIFIED cANGULAR TOLERANCES SHALL BE +/-0.50 DEGREES UNLESS OTHERWISE SPECIFIED dBREAK ALL EDGES .003-.010 INCHES UNLESS OTHERWISE SPECIFIED 10INTREPRETATION OF DRAWING PER AS4296 /11/THIS DIMENSION IS THE ALLOWABLE TUBE END POSITIONING FOR SYSTEM LAYOUT DESIGN. /12/.030 MIN RADIUS UNLESS QUALIFICATION OF SPECIAL PROCESS WITH SMALLER RADIUS. /13/
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
THIS STANDARD WAS PREPARED TO PROVIDE AN ENVELOPE REQUIREMENTS FOR AN AXIALLY SWAGED, FIELD ATTACHABLE, 5000 PSI, TUBE FITTING. /1/MATERIALS: CODE LETTER "T" RINGS-AMS 4965 TITANIUM ALLOY, 6.0AL 4.0V SOLUTION HEAT TREATED AND AGED OR AMS 4928 TITANIUM ALLOY 6.0 AL 4.0V ANNEALED WITH HIGH STRENGTH CARBON FIBER/EPOXY RESIN COMPOSITE REINFORCEMENT. BODY-AMS 4928 TITANIUM ALLOY, 6.0AL 4.0V ANNEALED 2FINISH: TITANIUM-NONE REQUIRED /3/COATINGS/LUBRICANTS: RINGS-THE OUTER SURFACE SHALL HAVE A .125" MINIMUM WIDTH BLUE COLORED RING OR COMPLETELY COLORED BLUE TO INDICATE 5080 PSI MAXIMUM OPERATION PRESSURE. AN AS1241 FLUID RESISTANT PTFE COATING OR PAINT MUST BE USED. BODY-SOLID FILM LUBRICANT PER AS5272, TYPE I OR II, PTFE OR PETROLEUM-BASED LUBRICANT MAY BE APPLIED TO PORTIONS OF THE ID AND OD. THE PETROLEUM-BASED LUBRICANT SHALL NOT BE IN CONTACT WITH THE SYSTEM FLUID. /4/ALL PRODUCTS SUPPLIED TO THIS SPECIFICATION SHALL BE MANUFACTURED BY AN ACCREDITED MANUFACTURER AS LISTED IN THE PERFORMANCE REVIEW INSTITUTE (PRI) QUALIFIED PRODUCTS LIST FOR PRI-QPL-AS5958 FOR THIS STANDARD. SEE HTTP:WWW.PRI.SAE.ORG/QPL/AS5958.PDF FOR CURRENT QPL ONLINE. PRIOR TO ISSUANCE OF THE PRI-QPL, USERS ARE ADVISED TO CONTROL SOURCE APPROVALS BY STANDARD PAGE SUPPLEMENT SHEET OR SIMILAR MEANS. 5DIMENSIONS AND TOLERANCES NOT DEFINED ON THIS STANDARD SHALL BE SPECIFIED AND CONTROLLED BY THE MANUFACTURER. THE MANUFACTURER IS RESPONSIBLE TO ENSURE COMPLIANCE WITH THE PROCUREMENT SPECIFICATION. /6/IDENTIFICATION SHALL BE IN ACCORDANCE WITH AS5958 AND SHALL BE IDENTIFIED ON EITHER RING IN THE AREA SHOWN. 7FITTINGS SHALL BE INSTALLED IN ACCORDANCE WITH AS5959. 8SURFACE TEXTURE SHALL BE IN ACCORDANCE WITH AMERICAN SOCIETY OF MECHANICAL ENGINEERS. ASME Y14.1 AND THE SYMBOLS IN ACCORDANCE WITH ASME14.36M. UNLESS OTHERWISE SPECIFIED, THE MAXIMUM MACHINED SURFACES SHALL BE 125 uin Ra AND THE MAXIMUM FORGED SURFACES SHALL BE 250 uin Ra. 9DIMENSIONS AND TOLERANCES SHALL BE IN ACCORDANCE WITH AMERICAN SOCIETY OF MECHANICAL ENGINEERS, ASME Y14.5M-1994. aDIMENSIONS ARE IN INCHES UNLESS OTHERWISE SPECIFIED bDIMENSIONAL TOLERANCES SHALL BE +/-.005 INCHES UNLESS OTHERWISE SPECIFIED cANGULAR TOLERANCES SHALL BE +/-0.50 DEGREES UNLESS OTHERWISE SPECIFIED dBREAK ALL EDGES .003-.010 INCHES UNLESS OTHERWISE SPECIFIED 10INTREPRETATION OF DRAWING PER AS4296 /11/THIS DIMENSION IS THE ALLOWABLE TUBE END POSITIONING FOR SYSTEM LAYOUT DESIGN. /12/.030 MIN RADIUS UNLESS QUALIFICATION OF SPECIAL PROCESS WITH SMALLER RADIUS. /13/
FITTING ASSEMBLY, RING LOCKED, ADAPTER, FLARELESS TO PORT, EXTRA FINE THREADS, 5080 PSI
Author: G-3C, AS-EN Harmonization Task Group
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
ADD AMS5853 OPTION FOR A286 MATERIAL.
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
ADD AMS5853 OPTION FOR A286 MATERIAL.
IPC-A-600K Acceptability of Printed Boards
Author: Ipc
Publisher:
ISBN: 9781951577483
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN: 9781951577483
Category :
Languages : en
Pages :
Book Description
December 4, 1979
Author: United States. Congress. Senate. Committee on Finance. Subcommittee on Private Pension Plans and Employee Fringe Benefits
Publisher:
ISBN:
Category : Pension trusts
Languages : en
Pages : 512
Book Description
Publisher:
ISBN:
Category : Pension trusts
Languages : en
Pages : 512
Book Description
Titanium-alloy Forgings
Author: H. J. Henning
Publisher:
ISBN:
Category : Titanium
Languages : en
Pages : 96
Book Description
Publisher:
ISBN:
Category : Titanium
Languages : en
Pages : 96
Book Description
The Life and Words of Deaconess Clara Strehlow
Author: Cheryl D. Naumann
Publisher:
ISBN: 9781613270103
Category : Lutheran Church--Missouri Synod
Languages : en
Pages : 161
Book Description
Publisher:
ISBN: 9781613270103
Category : Lutheran Church--Missouri Synod
Languages : en
Pages : 161
Book Description
Aws D17. 2/ D17. 2m
Author: American Welding Society
Publisher:
ISBN: 9780871719522
Category :
Languages : en
Pages : 60
Book Description
Publisher:
ISBN: 9780871719522
Category :
Languages : en
Pages : 60
Book Description
Standard Specification for Cold Weather Concreting (ACI 306.1-90)
Author: ACI Committee 306
Publisher:
ISBN:
Category : Concrete
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category : Concrete
Languages : en
Pages : 20
Book Description
Aws D17. 1/d17. 1m
Author: American Weling Society
Publisher:
ISBN: 9780871719171
Category : Airplanes
Languages : en
Pages : 116
Book Description
This specification provides the general welding requirements for welding aircraft and space hardware. It includes but is not limited to the fusion welding of aluminum-based, nickel-based, iron-based, cobalt-based, magnesium-based, and titanium-based alloys using electric arc and high energy beam processes. There are requirements for welding design, personnel and procedure qualification, inspection, and acceptance criteria for aerospace, support, and non-flight hardware. Additional requirements cover repair welding of existing hardware. A commentary for the specification is included.
Publisher:
ISBN: 9780871719171
Category : Airplanes
Languages : en
Pages : 116
Book Description
This specification provides the general welding requirements for welding aircraft and space hardware. It includes but is not limited to the fusion welding of aluminum-based, nickel-based, iron-based, cobalt-based, magnesium-based, and titanium-based alloys using electric arc and high energy beam processes. There are requirements for welding design, personnel and procedure qualification, inspection, and acceptance criteria for aerospace, support, and non-flight hardware. Additional requirements cover repair welding of existing hardware. A commentary for the specification is included.