FSC 4710 Pipe, Tube and Rigid Tubing: 4710-00-015-1674, 4710-00-015-2218, 4710-00-016-0828
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 4710-00-015-1674 4710000151674 | 484025 646904 | Tube Assembly, Metal | Wall Thickness: 0.020 inches nominal Design Form: Prebent Tubing Material: Cres, ams 5576 | Tube Bends Incorporated (33830) Kreisler Industrial Corporation (05813) United Technologies Corporation (77445) | |
| 4710-00-015-1785 4710000151785 | 9-240004 SB244 | Tube Assembly, Metal | Design Form: Prebent Tubing Material: Steel, stainless Mating End Quantity: 2 single end | Westport International Inc. (96429) Unison Industries LLC (59501) | |
| 4710-00-015-2147 4710000152147 | 65-33340-27 | Tube Assembly, Oil System | III End Item Identification: C-135 acft General Characteristics Item Description: Aisi 304 tubing anld per MIL-T-8504(ASG), outside dia 0.500 in., 0.028 in. wall thickness, used on plumbing installation engine no. 3 | The Boeing Company (81205) | |
| 4710-00-015-2148 4710000152148 | 8347102-10 65-33340-804 | Tube Assembly, Metal | Special Features: On lubrication vent system | The Boeing Company (81205) Air Force United States Department (98748) | |
| 4710-00-015-2149 4710000152149 | 65-33340-805 | Tube Assembly, Oil s | III End Item Identification: C-135 acft General Characteristics Item Description: Aisi 304 tubing anld per MIL-T-8504(ASG); 0.500 in. outside tube dia, wall thickness 0.028 in., used on plumbing installation engines no. 1, 2 and 3 | The Boeing Company (81205) | |
| 4710-00-015-2150 4710000152150 | 65-33340-31 | Tube Assembly, Anti- | III End Item Identification: C-135 acft General Characteristics Item Description: Minimum wall thickness 0.035 in., used on plumbing installation engines no. 1, 2 and 4 | The Boeing Company (81205) | |
| 4710-00-015-2210 4710000152210 | 6842139 | Tube Assembly, Metal | III Fsc Application Data: T-56 aircraft engine | Allison Transmission Inc. (73342) International Aerospace Tubes LLC (96593) Rolls-Royce Corporation (63005) | |
| 4710-00-015-2218 4710000152218 | 6843446 | Tube Assembly, Metal | Wall Thickness: 0.031 inches minimum and 0.039 inches maximum Design Form: Prebent Tubing Material: Steel, ams 5570 | Rolls-Royce Corporation (63005) Allison Transmission Inc. (73342) General Motors Corp. (24617) | |
| 4710-00-015-2978 4710000152978 | 134H10014-301LGU6 | Tube Assembly, Metal | Wall Thickness: 0.028 inches nominal Design Form: Prebent Tubing Material: Steel, corrosion resisting, MIL-T-6845 | Northrop Grumman Systems Corporation (26512) | |
| 4710-00-015-3070 4710000153070 | 5181802 | Tube, Bent, Metallic | Wall Thickness: 0.062 inches nominal Material: Steel Second End Relationship With First End: Identical | General Motors Corp. (24617) MTU Detroit Diesel Inc. (72582) | |
| 4710-00-015-3071 4710000153071 | 5186429 | Tube, Bent, Metallic | MTU Detroit Diesel Inc. (72582) General Motors Corp. (24617) | ||
| 4710-00-015-6036 4710000156036 | RM392-1 | Tube Assembly, Metal | Wall Thickness: 0.035 inches nominal Design Form: Straight Tubing Material: Copper | Wisconsin Motors LLC (66289) | |
| 4710-00-015-6648 4710000156648 | 6774478 11A1/135596/2 | Tube, Oil Transfer | General Characteristics Item Description: STEEL;1.660 in. O/a LG;0.765 in. ID;0.870 in. tube od;two raised O-ring grooves;first GROOVE;0.921 in. od, 0.090 in. W, 0.825 in. root dia;second GROOVE;0.982 in. OD;0.090 in. W, 0.890 in. root dia | General Motors Corp. (24617) Allison Transmission Inc. (73342) Thales UK Limited, Aerospace (U4338) | |
| 4710-00-015-7134 4710000157134 | 304087C1 218737 | Tube, Torque Converter | General Characteristics Item Description: Steel, copper brazed, consists of tube, restrictor, plate and 2 RETAINERS;0.052 in.orifice SIZE;4.375 in.O/a LG;0.562 in.O/a W;0.906 in.O/a H | Clark Equipment Co. (12603) Dana Corp. (77237) Navistar Intl Corp. (31007, 89346) | |
| 4710-00-015-8510 4710000158510 | 65-33338-800 | Tube Assembly, Metal | Wall Thickness: 0.035 inches nominal Design Form: Prebent Tubing Material: Steel, MIL-T-8808, comp 321 or steel, ams 5556 or steel, ams 5557 | Rohr Inc. (51563) The Boeing Company (81205) | |
| 4710-00-015-8518 4710000158518 | 65-37495-1 | Tube Assembly, Metal | Wall Thickness: 0.035 inches nominal Tubing Material: Steel, aisi 321 Tube Outside Diameter: 1.743 inches minimum and 1.753 inches maximum | The Boeing Company (81205) | |
| 4710-00-015-8879 4710000158879 | 60C76000-35 | Tube Assembly, Metal | Wall Thickness: 0.049 inches nominal Design Form: Prebent Tubing Material: Aluminum alloy, WW-T-700/4 | Sacramento Air Logistics Center (98749) Department of the Air Force (80049) | |
| 4710-00-016-0020 4710000160020 | 4710000160020 10934807 | Tube Assembly, Metal | Wall Thickness: 0.049 inches nominal Design Form: Prebent Tubing Material: Steel, MIL-T-3520, type 3, comp 1010 to 1025 | E.C.A Etablissement Central DES (SCY13) U S Army Tank Automotive Command (19207) | |
| 4710-00-016-0022 4710000160022 | 10934808 4710000160022 | Tube Assembly, Metal | Wall Thickness: 0.035 inches nominal Design Form: Prebent Tubing Material: Steel, MIL-T-3520, type 3, comp 1010 to 1025 | U S Army Tank Automotive Command (19207) E.C.A Etablissement Central DES (SCY13) | |
| 4710-00-016-0828 4710000160828 | 6844785 | Tube Assembly, Metal | Wall Thickness: 0.044 inches minimum and 0.054 inches maximum Design Form: Prebent Tubing Material: Steel, ams 5570 | Rolls-Royce Corporation (63005) Allison Transmission Inc. (73342) General Motors Corp. (24617) |