Airframe Structural Components: 4F75096-183A, 4F75188-132A, 4F75205-233A
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 4F75096-183A 4F75096183A | 1560-01-250-0254 | Fairing, Aircraft | Aircraft Mission Design Series: C-5A/B Aircraft Location: Used on panel assembly, lower, forward wheelwell, main landing gear Side FOR Which Designed: Right side | Lockheed Martin Corporation (98897) | |
| 4F75102-349B 4F75102349B | 1560-00-161-8187 | Retainer, Seal, Wheel Well | III End Item Identification: Aircraft model C-5 | Lockheed Martin Corporation (98897) | |
| 4F75105-332A 4F75105332A | 1560-00-008-9490 | Frame, Aircraft | Aircraft Mission Design Series: C-5A Material Document and Classification: QQ-A-250 fed spec single material response Material Thickness: 0.050 inches nominal | Lockheed Martin Corporation (98897) | |
| 4F75172-125A 4F75172125A | 1560-00-401-2331 | Door, Access, Aircraft | Securing Device Type: Hinge and turnlock fastener FSC Application Data: Fairing, airframe structure | Lockheed Martin Corporation (98897) | |
| 4F75172-143A 4F75172143A | 1560-00-401-2331 | Door, Access, Aircraft | Securing Device Type: Hinge and turnlock fastener FSC Application Data: Fairing, airframe structure | Lockheed Martin Corporation (98897) | |
| 4F75184-142A 4F75184142A | 1560-00-498-1132 | Panel, Structural, Aircraft | Special Features: Core is STM28-102, outer skin O/a dim. 0.012X24X96 in., inner skin O/a dim. 0.012X18X94 in. Material: Aluminum alloy Aircraft Location: Edging, doublers and skin | Lockheed Martin Corporation (98897) | |
| 4F75184-167A 4F75184167A | 1560-00-762-7642 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-5A Special Features: Core, STM28-102; outer skin O/a dim. 0.016X24X96 in.; inner skin O/a dim. 0.012X18X94 in. Material: Aluminum alloy | Lockheed Martin Corporation (98897) | |
| 4F75184-171A 4F75184171A | 1560-00-762-7642 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-5A Special Features: Core, STM28-102; outer skin O/a dim. 0.016X24X96 in.; inner skin O/a dim. 0.012X18X94 in. Material: Aluminum alloy | Lockheed Martin Corporation (98897) | |
| 4F75184-172A 4F75184172A | 1560-00-762-7641 | Panel, Structural, Aircraft | Special Features: Core, STM28-102; outer skin O/a dim. 0.012X24X96 in.; inner skin O/a dim. 0.012X18X94 in. Material: Aluminum alloy Aircraft Location: Edging, doublers and skin | Lockheed Martin Corporation (98897) | |
| 4F75186-159A 4F75186159A | 1560-00-762-7643 | Panel, Structural, Aircraft | Special Features: Core, STM28-102 type 1; outer skin O/a dim. 0.016X23X85 in.; inner skin O/a dim. 0.012X20X84 in. Material: Aluminum alloy Aircraft Location: Edging, doublers and skin | Lockheed Martin Corporation (98897) | |
| 4F75186-160A 4F75186160A | 1560-00-762-7644 | Panel, Structural, Aircraft | Special Features: Aluminum alloy edging, doublers and skin, core is STM28-102 type I.outer skin O/a dim. 0.016 by 23.00 by 85.00 in., inner skin is 0.012 BY20.00 by 84.00 in. | Lockheed Martin Corporation (98897) | |
| 4F75186-163A 4F75186163A | 1560-00-762-7643 | Panel, Structural, Aircraft | Special Features: Core, STM28-102 type 1; outer skin O/a dim. 0.016X23X85 in.; inner skin O/a dim. 0.012X20X84 in. Material: Aluminum alloy Aircraft Location: Edging, doublers and skin | Lockheed Martin Corporation (98897) | |
| 4F75186-164A 4F75186164A | 1560-00-762-7644 | Panel, Structural, Aircraft | Special Features: Aluminum alloy edging, doublers and skin, core is STM28-102 type I.outer skin O/a dim. 0.016 by 23.00 by 85.00 in., inner skin is 0.012 BY20.00 by 84.00 in. | Lockheed Martin Corporation (98897) | |
| 4F75187-102A 4F75187102A | 1560-00-009-0724 | Panel, Structural, Aircraft | III End Item Identification: C-5A galaxy aircraft Aircraft Mission Design Series: C-5A Material: Titanium | Lockheed Martin Corporation (98897) | |
| 4F75188-131A 4F75188131A | 1560-00-498-1136 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-5A Special Features: Matl:alm aly inner & outer skin, 7079-T6, MIL-A-8923, & alum honeycomb core per stm 28-102 Aircraft Location: WING | Lockheed Martin Corporation (98897) | |
| 4F75188-132A 4F75188132A | 1560-00-498-1137 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-5A Special Features: Matl: titanium skin, stm 07-306, honeycomb core | Lockheed Martin Corporation (98897) | |
| 4F75189-137A 4F75189137A | 1560-00-102-7760 | Panel, Structural, Aircraft | III End Item Identification: C-5A aircraft | Lockheed Martin Corporation (98897) | |
| 4F75189-138A 4F75189138A | 1560-00-498-7500 | Panel, Structural, Aircraft | Special Features: Honeycomb core, MIL-C-8073; inner skin O/a dim. 0.010X20X54 in.; outer skin 0.010X22X56 in. Material: Titanium Aircraft Location: Edging, doublers and skin | Lockheed Martin Corporation (98897) | |
| 4F75205-215B 4F75205215B | 1560-00-485-1888 | Cover, Access, Aircraft | FSC Application Data: Fairing, airframe | Lockheed Martin Corporation (98897) | |
| 4F75205-233A 4F75205233A | 1560-00-438-9288 | Fairing, Aircraft | Aircraft Mission Design Series: C-5A | Lockheed Martin Corporation (98897) |