Airframe Structural Components: LS60249-4, LS6095-5, LS6428
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| LS60249-4 LS602494 | 1560-01-340-1365 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-5 Material: Glass fiber Overall Length: 82.000 inches nominal | Advanced Composite Technology Inc. (0AEN5) | |
| LS60250-1 LS602501 | 1560-01-342-4705 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-5 Material: Glass fiber Overall Length: 52.000 inches nominal | Advanced Composite Technology Inc. (0AEN5) | |
| LS60250-2 LS602502 | 1560-01-340-1363 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-5 Material: Glass fiber Overall Length: 80.000 inches nominal | Lockheed Martin Corporation (98897) | |
| LS60250-3 LS602503 | 1560-01-342-4705 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-5 Material: Glass fiber Overall Length: 52.000 inches nominal | Advanced Composite Technology Inc. (0AEN5) | |
| LS60250-4 LS602504 | 1560-01-340-1363 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-5 Material: Glass fiber Overall Length: 80.000 inches nominal | Advanced Composite Technology Inc. (0AEN5) | |
| LS60251-1 LS602511 | 1560-01-272-3086 | Panel, Structural, Aircraft | III End Item Identification: C-5 aircraft Special Features: Trim panel;matl nomex phenolic honeycomb core | Advanced Composite Technology Inc. (0AEN5) Lockheed Martin Corporation (98897) | |
| LS60251-2 LS602512 | 1560-01-272-3088 | Panel, Structural, Aircraft | III End Item Identification: C-5 aircraft Special Features: Trim panel;matl nomex phenolic honeycomb core | Advanced Composite Technology Inc. (0AEN5) Lockheed Martin Corporation (98897) | |
| LS60251-3 LS602513 | 1560-01-272-3086 | Panel, Structural, Aircraft | III End Item Identification: C-5 aircraft Special Features: Trim panel;matl nomex phenolic honeycomb core | Advanced Composite Technology Inc. (0AEN5) Lockheed Martin Corporation (98897) | |
| LS60251-4 LS602514 | 1560-01-272-3088 | Panel, Structural, Aircraft | III End Item Identification: C-5 aircraft Special Features: Trim panel;matl nomex phenolic honeycomb core | Advanced Composite Technology Inc. (0AEN5) Lockheed Martin Corporation (98897) | |
| LS6095-1 LS60951 | 1560-00-677-7660 | Guard, Pulley | III End Item Identification: Acft model C141 General Characteristics Item Description: Wire, aluminum, MIL-W-7986, center hole dia 0.500 in. min, 0.560 in. max | Lockheed Martin Corporation (98897) | |
| LS6095-3 LS60953 | 1560-00-677-7659 | Guard, Pulley | III End Item Identification: Acft model C141 General Characteristics Item Description: Wire, aluminum, MIL-W-7986, center hole dia 0.500 in. min, 0.560 in. max | Lockheed Martin Corporation (98897) | |
| LS6095-5 LS60955 | 1560-00-255-8868 | Guard, Pulley | III End Item Identification: Aircraft model C141 General Characteristics Item Description: Aluminum, MIL-W-7986, 0.125 in. material dia, 1.306 in. min, 1.336 in. max H, 3.187 in. lg, 0.315 in. min, 0.322 in. max id eye, 3.000 in. lg base leg | Lockheed Martin Corporation (98897) | |
| LS6095A1 | 1560-00-886-9023 | Guard, Pulley | III End Item Identification: Acft model C141 General Characteristics Item Description: Wire, aluminum, MIL-W-7986, center hole dia, 0.500 in. min, 0.560 in. max | Lockheed Martin Corporation (98897) | |
| LS60-S17B6 LS60S17B6 | 1560-01-223-0013 | Strip, Lighting | Dayton-Granger International Inc. (55635) | ||
| LS60-S22B3 LS60S22B3 | 1560-01-223-3128 | Strip, Lighting | Dayton-Granger International Inc. (55635) | ||
| LS6227-8 LS62278 | 1560-01-426-5580 | Stiffener, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5, T3 clad fed spec single material response Overall Length: 0.970 inches minimum and 1.030 inches maximum | Lockheed Martin Corporation (98897) | |
| LS6228-8 LS62288 | 1560-01-492-5332 | Stiffener, Aircraft | III End Item Identification: P-3 aircraft Part Name Assigned BY Controlling Agency: Section | Lockheed Martin Corporation (98897) | |
| LS6315-280-40 LS631528040 | 1560-00-403-7632 | Fitting, Impact Extr | Lockheed Martin Corporation (98897) | ||
| LS634-42 LS63442 | 1560-00-473-8459 | Spacer, Flanged | Lockheed Martin Corporation (98897) | ||
| LS6428 | 1560-01-507-4811 | Plate, Hinged | Special Features: Length 1.620; metal; extruded end; material 2024-T4 | Lockheed Martin Corporation (98897) |