Airframe Structural Components: 239A703-1, 23D0177-1, 23H1458-2
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 239A703-1 239A7031 | 1560-01-506-3517 | Fairing, Aircraft | Aircraft Mission Design Series: C-130 Special Features: U/O MC-130E, H AC130H, u; nha 239A700; material prepreg LTM45 RESIN/7725 gbid Aircraft Location: Directional infra red countermeasures | Lockheed Martin Corporation (03640) | |
| 239A703-2 239A7032 | 1560-01-506-3506 | Fairing, Aircraft | Aircraft Mission Design Series: C-130 Special Features: U/O MC-130E, H AC-130H, u; nha 239A700; material prepreg LTM45 RESIN/7725 gbid Aircraft Location: Directional infra red countermeasures | Lockheed Martin Corporation (03640) | |
| 239A705-1 239A7051 | 1560-01-507-0212 | Plate, Structural, Aircraft | Lockheed Martin Corporation (03640) | ||
| 239A705-2 239A7052 | 1560-01-507-0359 | Plate, Structural, Aircraft | Lockheed Martin Corporation (03640) | ||
| 239A706-1 239A7061 | 1560-01-507-0590 | Plate, Structural, Aircraft | Lockheed Martin Corporation (03640) | ||
| 239A706-2 239A7062 | 1560-01-507-0619 | Plate, Structural, Aircraft | Lockheed Martin Corporation (03640) | ||
| 239A709-1 239A7091 | 1560-01-506-3598 | Cover, Access, Aircraft | Special Features: Nha 239A700; U/O MC-130H, MC-130E, AC-130H, AC-130U; materials are GLASS(LTM45SEL/7725 GF38 class pre preg), film adhesive(lta 45ELNC/PM25), ASTROSTIKE(AL016) Material: Glass End Item Identification: C-130 | Lockheed Martin Corporation (03640) | |
| 239A711-1 239A7111 | 1560-01-519-4449 | Support, Structural Component, Air | Lockheed Martin Corporation (03640) | ||
| 239A711-2 239A7112 | 1560-01-519-4446 | Support, Structural Component, Air | Lockheed Martin Corporation (03640) | ||
| 239A807-1 239A8071 | 1560-01-567-5467 | Plate, Structural, Aircraft | III End Item Identification: C-130 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 fed spec single material response | Lockheed Martin Corporation (03640) | |
| 239A807-2 239A8072 | 1560-01-567-4182 | Plate, Structural, Aircraft | III End Item Identification: C-130 Special Features: Heat treat T3 per QQ-A-250/5 Material: Aluminum alloy 2024 | Lockheed Martin Corporation (03640) | |
| 23C0187-2 23C01872 | 1560-01-528-0189 | Support, Structural Component, Air | III End Item Identification: UH1 aircraft Criticality Code Justification: AGAV | Bell Helicopter Textron Inc. (97499) | |
| 23CSM10014-601 23CSM10014601 | 1560-01-213-2027 | Fitting Assembly | Vangard Intl (61741) | ||
| 23D0177-1 23D01771 | 1560-01-479-1279 | Boom, Aircraft | III End Item Identification: Helicopter (H1) Part Name Assigned BY Controlling Agency: (Inavy) tailboom, aircraft, m Criticality Code Justification: AGAV | Commanding Officer (96916) | |
| 23D0177-2 23D01772 | 1560-01-479-1288 | Fuselage Section | III End Item Identification: Helicopter (H1) Part Name Assigned BY Controlling Agency: (Inavy) tailboom, aircraft, main Criticality Code Justification: AGAV | Commanding Officer (96916) | |
| 23D0187-1 23D01871 | 1560-01-528-0185 | Support, Structural Component, Air | III End Item Identification: UH1 aircraft Criticality Code Justification: AGAV | Bell Helicopter Textron Inc. (97499) | |
| 23D0187-2 23D01872 | 1560-01-528-0189 | Support, Structural Component, Air | III End Item Identification: UH1 aircraft Criticality Code Justification: AGAV | Bell Helicopter Textron Inc. (97499) | |
| 23D0187-3 23D01873 | 1560-01-528-0192 | Support, Structural Component, Air | III End Item Identification: UH1 aircraft Criticality Code Justification: AGAV | Bell Helicopter Textron Inc. (97499) | |
| 23D0187-4 23D01874 | 1560-01-528-0194 | Support, Structural Component, Air | III End Item Identification: UH1 aircraft Criticality Code Justification: AGAV | Bell Helicopter Textron Inc. (97499) | |
| 23H1458-2 23H14582 | 1560-00-124-0724 | Fitting Assy, Right | Naval Air Rework Facility (97057) |