Airframe Structural Components: 29-2517-10, 29260, 29-2829
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 29-2517-10 29251710 | 1560-01-161-2081 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-362 fed spec single material response | The Boeing Company (81205) | |
| 29-2517-11 29251711 | 1560-01-161-2082 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-362 fed spec single material response | The Boeing Company (81205) | |
| 29-2517-12 29251712 | 1560-01-161-2083 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-362 fed spec single material response | The Boeing Company (81205) | |
| 29-2517-2 2925172 | 1560-01-149-3931 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Special Features: Opposite to P/N 29-2517-1;USED tosupport tube; incl. nut plate Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 29-2517-3 2925173 | 1560-01-149-3932 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Special Features: Opposite to P/N 29-2517-4; includes nut plate, self-locking; used to support tube Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 29-2517-4 2925174 | 1560-01-149-3933 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Special Features: Opposite to P/N 29-2517-3;INCLUDES nut plate, self-locking;used to suppoort tube Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 29-2517-5 2925175 | 1560-01-149-3934 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Special Features: Opposite to P/N 29-2517-6;USED tosupport tube; includes nut plate, self-locking Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 29-2517-6 2925176 | 1560-01-152-1607 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 | The Boeing Company (81205) | |
| 29-2517-7 2925177 | 1560-01-161-2084 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-362 fed spec single material response | The Boeing Company (81205) | |
| 29-2517-8 2925178 | 1560-01-161-2085 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-362 fed spec single material response | The Boeing Company (81205) | |
| 29-2517-9 2925179 | 1560-01-161-2086 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-362 fed spec single material response | The Boeing Company (81205) | |
| 29-2519-502 292519502 | 1560-00-670-5584 | Cone, Engine Hanger | General Characteristics Item Description: Steel, MIL-S-5000, 5.800 in. lg, 0.750-16 UNF-3A thd 1 end | The Boeing Company (81205,82918) | |
| 29260 | 1560-01-050-2695 | Fitting, Engine Drain | Tara Technologies Corporation (07582) | ||
| 29260B1 | 1560-01-050-2695 | Fitting, Engine Drain | Tara Technologies Corporation (07582) | ||
| 29270-1 292701 | 1560-01-070-0245 | Fitting, Engine Drain Flexible | III End Item Identification: Acft model F-16 | Tara Technologies Corporation (07582) | |
| 29270B1 | 1560-01-070-0245 | Fitting, Engine Drain Flexible | III End Item Identification: Acft model F-16 | Tara Technologies Corporation (07582) | |
| 29-2739 292739 | 1560-01-502-5788 | Support, Structural Component, Air | The Boeing Company (81205) | ||
| 29-2739-1 2927391 | 1560-00-588-2077 | Bracket, Inflight Refueling | General Characteristics Item Description: Aluminum alloy, 2024, T3, QQ-A-250-5 | The Boeing Company (82918) | |
| 29-2739-2 2927392 | 1560-00-588-2078 | Bracket, Inflight Refueling | General Characteristics Item Description: Aluminum alloy, 2024, T3, QQ-A-250-5 | The Boeing Company (81205) | |
| 29-2829 292829 | 1560-00-588-0701 | Plate Assembly, Inboard | General Characteristics Item Description: 6.103 in. lg, 4 holes | The Boeing Company (81205) |