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4710-01-532-2367
Metallic Tube
4710015322367 015322367 SAE-AMS-T-7081 AMST7081-T6-0.250X0.035 AMS-T-7081 AMS-T-7081-T6-0.250X0.035 AMS-T-7081-CDT6-0,250X0,035
A straight, hollow product, welded or seamless, of round, square, or any other cross section and continuous periphery, which does not conform in cross sectional dimensions to recognized pipe standards, or those in Tables 1 through 10, Appendix C, FIIG A004A. It is designed to convey fluids, gasses, and/or semisolids. It may be rolled into coils for ease in handling. For items designed to join a tube or tube fitting to another tube, pipe, or hose or fitting, see ADAPTER (as modified); COUPLING (as modified); or NIPPLE (as modified). Excludes TUBE, BENT (as modified); PIPE, METALLIC; SPACER, SLEEVE; METAL BAR (hollow); and items with fittings, except end protectors. View more Metallic Tube
January 2023
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Related Documents 4710-01-532-2367 5+ Documents (More...)
015502320 SAE-AMS4083MIL-T-7081 CONDT6X1.000X.049 AMS4083-1.000X0.049 SAE-AMS-4083MIL-T-7081 SAE-AMS-T-7081
7081SAE-AMS4083 SAE-AMS4083MIL-T-7081 CONDT6X1.000X.049 AMS4083-1.000X0.049 SAE-AMS-4083MIL-T-7081 SAE-AMS-T-7081
SAE-AMS4083 MIL-T-7081 CONDT6X1.000X.049 AMS4083-1.000X0.049 SAE-AMS-4083MIL-T-7081 SAE-AMS-T-7081
SAE-AMS4083 MIL-T-7081 CONDT6X1.000X.049 AMS4083-1.000X0.049 SAE-AMS-4083MIL-T-7081 SAE-AMS-T-7081
Metallic Tube 4710015322367 015322367 SAE-AMS-T-7081 SAE-AMS4083 MIL-T-7081 CONDT6X1.000X.049 AMS4083
SAE-AMS4083 MIL-T-7081 CONDT6X1.000X.049 AMS4083-1.000X0.049 SAE-AMS-4083MIL-T-7081 SAE-AMS-T-7081
SAE-AMS4083 MIL-T-7081 CONDT6X1.000X.049 AMS4083-1.000X0.049 SAE-AMS-4083MIL-T-7081 SAE-AMS-T-7081
Metallic Tube 4710015322367 015322367 SAE-AMS-T-7081 SAE-AMS4083 MIL-T-7081 CONDT6X1.000X.049 AMS4083
SAE-AMS4083 MIL-T-7081 CONDT6X1.000X.049 AMS4083-1.000X0.049 SAE-AMS-4083MIL-T-7081 SAE-AMS-T-7081
Metallic Tube 4710015322367 015322367 SAE-AMS-T-7081 SAE-AMS4083 MIL-T-7081 CONDT6X1.000X.049 AMS4083
Restrictions 4710-01-532-2367
4710-01-532-2367 is a Metallic Tube that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 4710-01-532-2367
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 4710-01-532-2367
- Germany (ZG01)
- Effective Date:
- 1 Aug 2005
Approved Sources 4710-01-532-2367
- Part Number
- Manufacturer
- Status
- SAE-AMS-T-7081
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- AMST7081-T6-0.250X0.035
- 0U583 - Sae International (Active)
- Primary Buy
- Primary Buy
- AMS-T-7081
- 0U583 - Sae International (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-T-7081
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-T-7081-T6-0.250X0.035
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-T-7081-CDT6-0,250X0,035
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 4710-01-532-2367
- Characteristic
- Specifications
- FIIG
- Specifications
- A004A0
- End Item Identification [AGAV]
- Fuselage F4f Jet Aircraft
- Construction [CQCF]
- Seamless
- Cross-Sectional Shape Style [AAGR]
- Plain Round
- Diameter [ABMZ]
- 0.250 Inches Nominal
- First End Style [AAGZ]
- Plain
- Heat Treatment [HEAT]
- T-6 Solution Heat Treated And Artificially Aged
- Material [MATT]
- Aluminum Alloy 6061
- Material Document And Classification [MDCL]
- Ams-T-7081 Assn Std Single Material Response
- Second End Relationship With First End [CQBB]
- Identical
- Special Features [FEAT]
- Psupplied In Mill Lengths; Ultimate Tensile Strength 42000.0 Pounds Per Square Inch (Psi) Minimum; Yield Strength 35000.0 Psi Minimum; Used In Hydraulic And Pneumatic Systems Of Aircraft, Including 3000.0 Psi Systems
- Wall Thickness [AAGT]
- 0.035 Inches Nominal
NATO Stock Numbers Related to 4710-01-532-2367
Freight Information 4710-01-532-2367
4710-01-532-2367 has freight characteristics.. 4710-01-532-2367 has a variance between NMFC and UFC when transported by rail and the description should be consulted.