Airframe Structural Components: 246-52218-11, 246-52231-509, 24720
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 246-52218-11 2465221811 | 1560-00-796-8069 | Support, Longren Con | Boeing Company, The (43999) | ||
| 246-52218-12 2465221812 | 1560-00-796-8048 | Support, Longeron Co | Boeing Company, The (43999) | ||
| 246-52231-509 24652231509 | 1560-00-446-6810 | Support, Structural Component, Air | Special Features: Magnesium alloy AZ91C, 7.375 in. lg, 2.750 in. high, 2.189 in. wide | Boeing Company, The (43999) | |
| 246-52231-7 246522317 | 1560-00-796-8974 | Support, Longeron Co | Boeing Company, The (43999) | ||
| 246-52231-9 246522319 | 1560-00-796-8980 | Support, Longeron Co | Boeing Company, The (43999) | ||
| 246-52256 24652256 | 1560-00-799-4213 | Rod End Assembly | III End Item Identification: T-39 aircraft General Characteristics Item Description: Control system elevator bias bungee; matl 4130 steel bar MIL-S-6758 cond F4 | Boeing Company, The (43999) | |
| 246-52303-1 246523031 | 1560-00-960-0642 | Support, Structural Component, Air | III End Item Identification: T-39 aircraft Material: Aluminum | Boeing Company, The (43999) Sabreliner Corp. (32184) Sabreliner Corporation (0ESK8) | |
| 246-52303-2 246523032 | 1560-01-117-8452 | Support, Structural Component, Air | III End Item Identification: Acft model T-39 Special Features: C/O support P/N 246-52303-4, bolt P/N 265-523016, 2 ea. nut P/N AN316-4R, nut plate P/N NAS1068A4, 2 ea. insert P/N NAS1222-4D, 4 ea. nut plate P/N NAS698A4, bolt P/N NAS428H4-6 | Boeing Company, The (43999) | |
| 246-52305-2 246523052 | 1560-00-793-8211 | Sector, Lateral Control | General Characteristics Item Description: Consists of 1 aluminum alloy spacer, 2.000 in. thk, 2, plugs, 2 bearings, 0.9009 | Boeing Company, The (43999) | |
| 246-52314 24652314 | 1560-00-793-8230 | Sector, Lateral Control | General Characteristics Item Description: Consists of 1 aluminum alloy cast spacer, irregular shaped 1.366 in. W at larger end, 0.438 in. W at opposite end, 2 holes, 0.531 in. dia, 2 bearings, 0.9014 in. dia, 0.438 in. thk | Boeing Company, The (43999) | |
| 246-52417-11 2465241711 | 1560-00-476-1561 | Lever, Control, Directional | III End Item Identification: Aircraft model T39 General Characteristics Item Description: Aluminum alloy, QQ-A-225/9 comp 7075 cond T6, 13.000 in. O/a lg, 1.250 in. O/a W, 0.823 in. O/a H, 2 holes in line both ends 0.2495 in. min, 0.2505 in. max dia, center bearing hole 0.8745 in. min, 0.8750 in. dia | Boeing Company, The (43999) | |
| 246-52418 24652418 | 1560-00-793-8205 | Support, Directional | Boeing Company, The (43999) | ||
| 246-53456 24653456 | 1560-00-440-2735 | Reservoir Assy, Heat | Boeing Company, The (43999) | ||
| 24664-5 246645 | 1560-01-287-2630 | Guard, Main Cockpit | Solnave S.A. (P1049) | ||
| 246A040-1 246A0401 | 1560-01-563-9193 | Conditioner, Aircraf | Lockheed Martin Corporation (03640) | ||
| 246A044-1 246A0441 | 1560-01-563-9195 | Cable Assy, Aircraft | Lockheed Martin Corporation (03640) | ||
| 24-70212-30 247021230 | 1560-01-060-8866 | Shield Assembly, Hea | III End Item Identification: E-3A acft | The Boeing Company (81205) | |
| 247-1025-010 2471025010 | 1560-01-467-0122 | Tray Assembly | III End Item Identification: KC-135 Special Features: Aluminum, steel; surface treatment is chromium; length is 14.060; width is 7.480; thickness is 5.750; mark with manufacturer's name or trademark and part number | Rockwell Collins Inc. (95105) | |
| 247-1025-050 2471025050 | 1560-01-467-0780 | Tie Downs | III End Item Identification: KC-135 Material: Steel corrosion resisting III Part Name Assigned BY Controlling Agency: Type a hold down | Rockwell Collins Inc. (95105) | |
| 24720 | 1560-00-311-1569 | Fitting, Engine Drain | III End Item Identification: Aircraft, model F15 General Characteristics Item Description: 6.000 in. lg, 3.140 in. od | Tara Technologies Corporation (07582) |