Airframe Structural Components: 4T22017-101A, 4T31018-104A, 4T31230-106A
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 4T22017-101A 4T22017101A | 1560-00-866-0429 | Flap Hinge, Rudder | III End Item Identification: Aircraft model C5A General Characteristics Item Description: Aluminum alloy, QQ-A-250/12 comp 7075 cond T351, 3.500 in. O/a lg, 3.150 in. O/a W, 2 holes in line 3 places 0.250 in. min, 0.256 in. max dia | Lockheed Martin Corporation (98897) | |
| 4T22018-101A 4T22018101A | 1560-00-865-4275 | Flap Hinge, Rudder | III End Item Identification: Aircraft model C5A General Characteristics Item Description: Aluminum alloy, QQ-A-250/12 comp 7075 cond T651, 5.000 in. O/a lg, 3.600 in. O/a W, 0.860 in. O/a H, 2 holes in line 2 places 0.374 in. min, 0.381 in. max dia | Lockheed Martin Corporation (98897) | |
| 4T22019-101B 4T22019101B | 1560-00-369-5492 | Flap Hinge, Rudder | III End Item Identification: Aircraft model C5A General Characteristics Item Description: Aluminum alloy, QQ-A-250/17 comp 7079 cond T651, 15.624 in. O/a lg, 4.290 in. O/a W, 4.010 in. O/a H | Lockheed Martin Corporation (98897) | |
| 4T2243-7 4T22437 | 1560-00-522-8206 | Skin, Aircraft | Lockheed Martin Corporation (81755) | ||
| 4T30000-101B 4T30000101B | 1560-01-080-5339 | Stabilizer, Horizontal | Aircraft Mission Design Series: C-5A Special Features: Contains 117 lbs on depleted uranium as elevator counterweights | Lockheed Martin Corporation (98897) | |
| 4T30002-101A 4T30002101A | 1560-00-477-7007 | Tip, Aircraft | Aircraft Mission Design Series: Aircraft C-5 Special Features: Removable | Aero Components Inc. (59213) CPI Aerostructures Inc. (9U679) Lockheed Martin Corporation (98897) MRA Systems Inc. (1B6R3) | |
| 4T30002-102A 4T30002102A | 1560-00-477-7008 | Tip, Aircraft | Aircraft Mission Design Series: Aircraft C-5 Special Features: Removable | Aero Components Inc. (59213) CPI Aerostructures Inc. (9U679) Lockheed Martin Corporation (98897) MRA Systems Inc. (1B6R3) | |
| 4T30007-101A 4T30007101A | 1560-00-449-8872 | Tip, Aircraft | Aircraft Mission Design Series: Aircraft model C5A | Lockheed Martin Corporation (98897) | |
| 4T30007-102A 4T30007102A | 1560-01-330-0053 | Tip, Aircraft | Aircraft Mission Design Series: C-5 Material: Aluminum alloy Aircraft Location: Horizontal stabilizer | Lockheed Martin Corporation (98897) | |
| 4T31018-103A 4T31018103A | 1560-00-689-8296 | Cover, Access, Aircraft | End Item Identification: Acft model C-5A | Lockheed Martin Corporation (98897) | |
| 4T31018-103B 4T31018103B | 1560-01-330-7672 | Cover, Access | END Item Identification: C-5B aircraft Special Features: Door assembly, rib, horizontal stabilizer box beam, pivot fitting | Lockheed Martin Corporation (98897) | |
| 4T31018-104A 4T31018104A | 1560-00-689-8298 | Cover, Access, Aircraft | End Item Identification: Acft model C-5A | Lockheed Martin Corporation (98897) | |
| 4T31018-104B 4T31018104B | 1560-01-330-7673 | Cover, Access | Material: Aluminum alloy END Item Identification: C-5B aircraft Special Features: Door assembly, rib, horizontal stabilizer box beam, pivot fitting | Lockheed Martin Corporation (98897) | |
| 4T31018-131A 4T31018131A | 1560-00-689-8299 | Cover, Access, Aircraft | Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/12, T6 fed spec single material response Securing Device Type: Threaded fastener | Lockheed Martin Corporation (98897) | |
| 4T31201-101A 4T31201101A | 1560-00-754-4065 | Cover, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 fed spec single material response End Item Identification: C-5A aircraft | Lockheed Martin Corporation (98897) | |
| 4T31201-102A 4T31201102A | 1560-00-754-4066 | Cover, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 fed spec single material response Securing Device Type: Threaded fastener | Lockheed Martin Corporation (98897) | |
| 4T31201-103A 4T31201103A | 1560-00-754-4067 | Cover, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 fed spec single material response Securing Device Type: Threaded fastener | Lockheed Martin Corporation (98897) | |
| 4T31201-104A 4T31201104A | 1560-00-754-4068 | Cover, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 fed spec single material response Securing Device Type: Threaded fastener | Lockheed Martin Corporation (98897) | |
| 4T31230-105A 4T31230105A | 1560-00-102-7743 | Skin, Aircraft | Special Features: Glass fabric impregnated W/resin | Aero Components Inc. (59213) CPI Aerostructures Inc. (9U679) Essner Precision Manufacturing LLC (92037) Lockheed Martin Corporation (98897) MRA Systems Inc. (1B6R3) Tect Aerospace Inc. (34336) | |
| 4T31230-106A 4T31230106A | 1560-00-102-7744 | Skin, Aircraft | Special Features: Glass fabric impregnated W/resin | Aero Components Inc. (59213) CPI Aerostructures Inc. (9U679) Essner Precision Manufacturing LLC (92037) Lockheed Martin Corporation (98897) MRA Systems Inc. (1B6R3) Swiss Pattern Corp. (8X065) |