FSC 4710 Pipe, Tube and Rigid Tubing: 4710-00-001-5199, 4710-00-001-9552, 4710-00-003-0095
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 4710-00-001-5199 4710000015199 | 364474 | Tube Assembly, Metal | Design Form: Prebent | Eaton Aerospace LLC (62983) | |
| 4710-00-001-5201 4710000015201 | 370744-4 | Tube Assembly, Metal | Wall Thickness: 0.028 inches nominal Design Form: Prebent Tubing Material: Steel, MIL-T-6845, type 304, cond 1/8H | Lockheed Martin Corporation (98897) | |
| 4710-00-001-5202 4710000015202 | 9084M63G01 3039M81G01 | Tube, Bent, Metallic | Wall Thickness: 0.035 inches nominal III End Item Identification: C-5A/B aircraft Special Features: Similar to: 4710-01-098-2806 // end fitting a: none // fitting b: 4730-00-460-8486 connector // end fitting c: none // use on: TF39-GE-1/ -1A/ -1C turbofan engines // T.O.2J-TF39-4 F.179 I.33 | General Electric Company (07482) | |
| 4710-00-001-6142 4710000016142 | 1068A11G01 | Tube Assembly, Metal | Wall Thickness: 0.032 inches nominal Design Form: Prebent Tubing Material: Copper | Thermo King Corporation (61510) | |
| 4710-00-001-6169 4710000016169 | 639-216 639-512 | Tube Assembly, Metal | Wall Thickness: 0.028 inches nominal Design Form: Prebent Tubing Material: Steel, copper brazed, astm A254-64, class 1 | American Coleman Company, The (96606) | |
| 4710-00-001-6331 4710000016331 | 5145230 | Pipe, Water Pump | MTU Detroit Diesel Inc. (72582) | ||
| 4710-00-001-6555 4710000016555 | 123EC10261-1 | Tube Assembly, Metal | Wall Thickness: 0.028 inches nominal Design Form: Prebent Tubing Material: Steel, corrosion resisting | Northrop Grumman Systems Corporation (26512) | |
| 4710-00-001-6790 4710000016790 | 370730-162 | Tube Assembly, Metal | Wall Thickness: 0.028 inches nominal Design Form: Prebent Tubing Material: Steel, corrosion resisting, MIL-T-8504A, comp 304 | Lockheed Martin Corporation (98897) | |
| 4710-00-001-8114 4710000018114 | 123ECP50020-1 | Tube, Air Duct | General Characteristics Item Description: Plastic | Northrop Grumman Systems Corporation (26512) | |
| 4710-00-001-9509 4710000019509 | 2667826 | Tube Assembly, Metal | Wall Thickness: 0.026 inches minimum and 0.033 inches maximum Design Form: Prebent Tubing Material: Copper | Navair and Navsea Managed (10001) | |
| 4710-00-001-9550 4710000019550 | A51E16125 A51E16125-9 | Tube Assembly, Metal | Wall Thickness: 0.028 inches nominal Design Form: Prebent Tubing Material: Aluminum alloy, WW-T-700/4, O | Northrop Grumman Systems Corporation (61174, 26512) | |
| 4710-00-001-9552 4710000019552 | 975611-1 | Tube, Bent, Metallic | Wall Thickness: 0.022 inches nominal Material: Aluminum alloy Second End Relationship With First End: Identical | Honeywell International Inc. (59364, 99193) | |
| 4710-00-001-9563 4710000019563 | 123EC51178 123EC51178-5 | Tube, Metallic, Branched | Design Form: Prebent Material: Aluminum alloy Material Document and Classification: WW-T-700/4, 5052 fed spec single material response | Northrop Grumman Systems Corporation (26512) | |
| 4710-00-001-9567 4710000019567 | 123CSM51780-1 | Tube, Torque, Fin | General Characteristics Item Description: Aluminum alloy, 12.829 in. lg, 3.275 in. id, 3.900 in. od | Northrop Grumman Systems Corporation (26512) | |
| 4710-00-001-9962 4710000019962 | 8148650 10C-0019-0089 10C0019-0089 | Tube Assembly, Metal | Wall Thickness: 0.035 inches nominal Design Form: Prebent Tubing Material: Aluminum alloy, WW-T-700/4, O, type 1 | Essex Cryogenics of Missouri Inc. (19062) Essex Industries Inc. (83533) Air Force United States Department (98748) | |
| 4710-00-001-9963 4710000019963 | 61-10975-2 | Tube Assembly, Metal | Wall Thickness: 0.058 inches nominal Design Form: Prebent Tubing Material: Steel, MIL-T-8808, type 1 or 2, comp 321 or 347 | The Boeing Company (82918) | |
| 4710-00-001-9965 4710000019965 | C6616-1 11406-1 | Tube Assembly, Comb | III End Item Identification: Aircraft model F-111F General Characteristics Item Description: Steel, corrosion resistant, type 304L, type 321 and/or type 347, 500 psi operating pressure, minus 65 to plus 450 deg F temperature range, prebent, 1 end connection per AN818-8J, 2 end connection per AN818-6J | F M H Corporation (99755) Lockheed Martin Corporation (81755) | |
| 4710-00-001-9966 4710000019966 | C6616-2 11406-2 | Tube Assembly, Comb | III End Item Identification: Aircraft model F-111F General Characteristics Item Description: Steel, corrosion resistant, type 304L, type 321 and/or type 347, 500 psi operating pressure, minus 65 to plus 450 deg F temperature range, prebent, 1 end connection per AN818-8J, 2 end connections per AN818-6J | Lockheed Martin Corporation (81755) F M H Corporation (99755) | |
| 4710-00-001-9967 4710000019967 | 1972L016-2 | Tube Assembly, Metal | Wall Thickness: 0.035 inches nominal Design Form: Prebent Tubing Material: Steel, MIL-T-6845, type 304, cond 1/8H | Goodrich Corp. (17576) | |
| 4710-00-003-0095 4710000030095 | AMS5557 4.00OD.042WT | Tube, Metallic | Wall Thickness: 0.028 inches nominal III End Item Identification: Grumman aerospace corp A10 aircraft Material: Steel | Future Metals Inc. (9G696) Society of Automotive Engineers Inc. (81343) |