Airframe Structural Components: CL281-1, CLM213-15FM, CM2430
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| CL281-1 CL2811 | 1560-00-915-7169 | Lock Assembly, cable | General Characteristics Item Description: 9.031 in. min, 9.062 in. max lg | Marathonnorco Aerospace Inc. (08844) | |
| CLF-4-A012BKCRNY6-12 CLF4A012BKCRNY612 | 1560-01-172-8054 | Brush Assy, Cover | Richards Brush Company (96383) | ||
| CLM213-15FM CLM21315FM | 1560-00-942-5074 | Locking Head, Strut | Marathonnorco Aerospace Inc. (08844) | ||
| CLM213-16 CLM21316 | 1560-01-011-8115 | Slide | Marathonnorco Aerospace Inc. (08844) | ||
| CLM213-6 CLM2136 | 1560-01-011-8113 | Lever | Marathonnorco Aerospace Inc. (08844) | ||
| CLT-0045-08 CLT004508 | 1560-01-441-3756 | Window Panel, Aircraft | Aircraft Mission Design Series: Uscg HH65A Material: Plastic acrylic and plastic polyimide Aircraft Location: Lower panel passenger door | Control Logistics Inc. (0YRW3) | |
| CLT-0045-53 CLT004553 | 1560-01-441-3768 | Window Panel, Aircraft | Aircraft Mission Design Series: Uscg HH65A Material: Plastic acrylic and plastic polyamide Aircraft Location: Lateral front right-hand panel | Control Logistics Inc. (0YRW3) | |
| CM00042-11-1-3 CM000421113 | 1560-00-436-0363 | Shaft Assembly, Torque-Flap | III End Item Identification: Acft model F-111 General Characteristics Item Description: 17.500 in. oa lg, internal splineone end with 11 teeth, external splineopposite end with 11 teeth, 0.625 in. shaft dia | Lockheed Martin Corporation (81755) | |
| CM00042-11-16-2 CM0004211162 | 1560-00-850-3039 | Shaft Assy, Torque | Lockheed Martin Corporation (81755) | ||
| CM00042-11-17-2 CM0004211172 | 1560-00-927-6184 | Shaft Assy, Torque F | Lockheed Martin Corporation (81755) | ||
| CM00042-11-18-2 CM0004211182 | 1560-00-927-6187 | Shaft Assy, Torque, F | Lockheed Martin Corporation (81755) | ||
| CM00042-11-2-3 CM000421123 | 1560-00-436-0365 | Shaft Assy, Torque, F | Lockheed Martin Corporation (81755) | ||
| CM00042-11-3-3 CM000421133 | 1560-00-520-3846 | Shaft Assy, Torque | Lockheed Martin Corporation (81755) | ||
| CM00042-11-4-3 CM000421143 | 1560-00-520-3847 | Shaft Assy, Torque | Lockheed Martin Corporation (81755) | ||
| CM00042-11-5-4 CM000421154 | 1560-00-436-0367 | Shaft Assy, Torque, F | Lockheed Martin Corporation (81755) | ||
| CM00042-11-7-3 CM000421173 | 1560-00-436-0364 | Shaft Assy, Torque, F | Lockheed Martin Corporation (81755) | ||
| CM00042-11-9-3 CM000421193 | 1560-00-850-3038 | Shaft Assembly | III End Item Identification: F-111 aircraft General Characteristics Item Description: Function-torque, flap drive MECHANISM;LENGTH-17.99 in.;both ends splined, one internal, one external; spring on end with external spline; steel surfaces plated W/cadmium, primed W/epoxy, and painted red-not on splines or bearing surfaces | Lockheed Martin Corporation (81755) | |
| CM100009 | 1560-00-099-5324 | Tube, Flexible, Heat and Vent Syst | III End Item Identification: Aircraft model F-86 | Senior Flexonics Inc. (96142) Senior Operations LLC (98769) | |
| CM2022 | 1560-00-714-4605 | Seal, Corner Angle | General Characteristics Item Description: Synthetic rubber, MIL-S-6855, 1.190 in. first leg lg, 1.190 in. second leg lg | Cessna Aircraft Company (71379) | |
| CM2430 | 1560-00-569-2281 | Cap, Filler Opening | System for Which Designed: Nonpressurized Cam Quantity: 1 Retaining Device Type: Chain | Dassault Aviation (F6117) Eaton Corp. Stamping Div. (81155) Eaton Corporation (81118) |