Airframe Structural Components: 26070, 2607258, 2612094
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 26070 | 1560-01-496-1995 | Housing, Air Intake, Aircraft | III End Item Identification: SH-2G seasprite helicopter Special Features: Anodize finish III Part Name Assigned BY Controlling Agency: Housing | Hydro-Aire Inc. (81982) | |
| 2607258 | 1560-01-357-3118 | Bracket, Structural Component, Air | Specification/Standard Data: 27914-2607258 manufacturers standard | Honeywell International Inc. (27914) | |
| 2607917 | 1560-01-357-3119 | Bracket, Structural Component, Air | Specification/Standard Data: 27914-2607917 manufacturers standard | Honeywell International Inc. (27914) | |
| 2607942-101 2607942101 | 1560-01-018-3466 | Duct Assembly, Air Conditioning-H | END Item Identification: A-7 aircraft Aircraft Mission Design Series: A-7 Material: Chromium alloy and iron alloy and nickel alloy | Senior Operations LLC (98769) | |
| 260835 | 1560-01-415-3337 | Insulation, Thermal, Special Purpo | Special Features: Used on F/A-18 aircraft, aft windscreen Thickness: 0.250 inches nominal Layer Quantity: 1 | Lockheed Martin Corp. (09205) | |
| 260948 | 1560-01-478-4917 | Cover, Access, Aircraft | End Item Identification: Fighter aircraft F18 E/F Criticality Code Justification: AGAV | Cando Industries Inc. (67616) Lockheed Martin Corporation (02GJ5,04939) | |
| 2-6095-1 260951 | 1560-00-030-4420 | Cover, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5, T3 fed spec single material response Securing Device Type: Threaded fastener | The Boeing Company (81205) | |
| 260953 | 1560-01-478-4920 | Fitting, Structural Component, Air | III End Item Identification: Fighter aircraft F18 E/F Criticality Code Justification: AGAV | Lockheed Martin Corporation (02GJ5,04939) Millipart Inc. (31095) | |
| 260960 | 1560-01-478-4933 | Cover, Access, Aircraft | End Item Identification: Fighter aircraft F18 E/F Criticality Code Justification: AGAV | Bell Precision Inc. (56122) Lockheed Martin Corporation (02GJ5,04939) | |
| 260961 | 1560-01-478-4944 | Cover, Access, Aircraft | End Item Identification: Fighter aircraft F18 E/F Criticality Code Justification: AGAV | Bell Precision Inc. (56122) Lockheed Martin Corporation (02GJ5,04939) | |
| 260A789-1 260A7891 | 1560-01-549-1543 | Panel, Structural, Aircraft | III End Item Identification: Panel, access MH-60 aircraft Aircraft Mission Design Series: MH-60 Special Features: Parts common to P/N 260A789-1, name/cage/P/n:stud, oval slotted (94222) 82-11-320-20; washer, nylon (94222) 82-46-101-39; spring, ejector (94222) 43-13-1-24/5; retainer, fastener stud (94222) 82-32-201-20 or 82-32-301-12/5 | Lockheed Martin Corporation (03640) | |
| 260A793-1 260A7931 | 1560-01-549-1513 | Panel, Structural, Aircraft | III End Item Identification: MH-60S/R aircraft Aircraft Mission Design Series: MH-60R/S Special Features: Parts common to P/N 260A793-1, name/cage/P/n:stud, oval slotted (94222) 82-11-320-20; washer, nylon (94222) 82-46-101-39; spring, ejector (94222) 43-13-1-24/5; retainer, fastener stud (94222) 82-32-201-20 or 82-32-301-12/5. | Lockheed Martin Corporation (03640) | |
| 260A794-1 260A7941 | 1560-01-549-1498 | Panel, Structural, Aircraft | III End Item Identification: MH-60S/R Aircraft Mission Design Series: MH-60 s/R Special Features: Items common to P/N 260A794-1 are (name, cage, P/n)=stud, oval slotted (94222) 82-11-320-20;WASHER, nylon (94222) 82-46-101-39;SPRING, ejector (94222) 43-13-1-24/5; retainer, fastener stud (94222) 82-32-201-20 or 82-32-301-12/5 | Lockheed Martin Corporation (03640) | |
| 261024 | 1560-01-478-5790 | Fitting, Structural Component, Air | III End Item Identification: Fighter aircraft F18 E/F III Part Name Assigned BY Controlling Agency: Inavy - fitting, structual, C Criticality Code Justification: AGAV | Lockheed Martin Corporation (02GJ5,04939) | |
| 261025 | 1560-01-478-5791 | Fitting, Structural Component, Air | III End Item Identification: Fighter aircraft F18 E/F III Part Name Assigned BY Controlling Agency: Inavy-fitting, structual, C Criticality Code Justification: AGAV | Lockheed Martin Corporation (02GJ5,04939) | |
| 261061 | 1560-01-478-5805 | Fitting, Structural Component, Air | III End Item Identification: Fighter aircraft F18 E/F III Part Name Assigned BY Controlling Agency: Fitting, structual, C Criticality Code Justification: AGAV | Lockheed Martin Corporation (02GJ5,04939) | |
| 26-1071-2 2610712 | 1560-01-155-4735 | Support, Structural Component, Air | III End Item Identification: Acft model B-52 Special Features: Aluminum alloy clad per 2024-T3 QQ-A-362, 8.000 in. lg, 2.400 in. W, 0.050 in. thk III Supplementary Features: Functional description:located frame station 85.27, nose cowl | The Boeing Company (82918) | |
| 261084 | 1560-01-478-5803 | Fitting, Structural Component, Air | III End Item Identification: Fighter aircraft F18 E/F III Part Name Assigned BY Controlling Agency: Inavy-fitting, structual, C Criticality Code Justification: AGAV | Lockheed Martin Corporation (02GJ5,04939) | |
| 2611926 | 1560-01-477-6025 | Plate, Structural, Aircraft | III End Item Identification: Fighter aircraft-first F18 E/F Special Features: (Inavy) retainer, flange, left Criticality Code Justification: AGAV | Honeywell International Inc. (55284) | |
| 2612094 | 1560-01-477-5898 | Support, Structural Component, Air | III End Item Identification: Fighter aircraft-first F18 E/F Special Features: (Inavy) block, radius Criticality Code Justification: AGAV | Honeywell International Inc. (55284) |