Airframe Structural Components: 399860-1, 39-9915-15, 39-9915-9
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 399860-1 3998601 | 1560-00-435-1672 | Door, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5, T3 fed spec single material response Securing Device Type: Flush catch and hinge | Lockheed Martin Corporation (98897) | |
| 399863-1 3998631 | 1560-01-372-5915 | Support, Structural Component, Air | III End Item Identification: C-130N, hercules aircraft Aircraft Mission Design Series: C-130N Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) Lockheed Martin Services Inc. (1WL60) | |
| 39-9901-1 3999011 | 1560-01-362-7063 | Bracket, Structural Component, Air | Aircraft Mission Design Series: B-52H Special Features: Used as a duct gate channel Material: Titanium | The Boeing Company (81205) | |
| 39-9901-2 3999012 | 1560-01-358-4188 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52G/H Special Features: Finish F-8.05;USED as doubler Material: Steel comp 301 | The Boeing Company (81205) | |
| 39-9905 399905 | 1560-00-773-3973 | Fitting, Fairing, Trailing Edge | III End Item Identification: Aircraft model B52 General Characteristics Item Description: Steel, MIL-S-6721, 3.120 in. lg, 0.760 in. W, 1.700 in. lg by 1.700 in. W base, 4 mounting holes 0.192 in. dia | The Boeing Company (81205,82918) | |
| 39-9907-505 399907505 | 1560-00-731-5427 | Shaft Assy, Torque, Engine Control | III End Item Identification: B-52 acft General Characteristics Item Description: Consists of shaft and crank arm, shaft lg 4.66, dia .811, no. teeth 34, pitch dia .850, major dia .875, pressure angle 45 degrees, pin dia .0480, circular tooth thk-max effective .0443, min effective .0430, max actual .0427, min actual .0414, max form dia .8333;CRANK arm bearing bore .755-.7505 dia | The Boeing Company (81205,82918) | |
| 39-9909-501 399909501 | 1560-01-157-0099 | Plate, Structural, Aircraft | The Boeing Company (81205) | ||
| 39-9912-501 399912501 | 1560-00-991-8035 | Clip, Tank | General Characteristics Item Description: Titanium alloy, MIL-T-9046, 0.342 in. min, 0.354 max dia hole 3 places | The Boeing Company (82918) | |
| 39-9913-801 399913801 | 1560-01-472-3339 | Plate, Structural, Aircraft | Air Force United States Department (98748) | ||
| 39-9913-802 399913802 | 1560-01-154-4952 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-355 T4 fed spec single material response | The Boeing Company (81205) | |
| 39-9914 399914 | 1560-00-802-0776 | Support, Structural Component, Air | III End Item Identification: Acft model B-52 Special Features: C/O bushing P/N 33-1859, hinge half P/N 39-9914-2 | The Boeing Company (82918) | |
| 39-9915-10 39991510 | 1560-01-162-6497 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Opposite to P/N 39-9915-9; used as web fwd Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 39-9915-15 39991515 | 1560-01-162-9889 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Aircraft Location: Channel on longeron NO.2 nose cowl | The Boeing Company (81205) | |
| 39-9915-16 39991516 | 1560-01-162-9890 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Aircraft Location: Channel on longeron NO.2 nose cowl | The Boeing Company (81205) | |
| 39-9915-5 3999155 | 1560-01-154-1555 | Plate, Structural, Aircraft | III End Item Identification: B-52 Aircraft Location: Forward assembly web | The Boeing Company (81205) | |
| 39-9915-507 399915507 | 1560-01-154-1560 | Web, Structural Component, Aircraf | Aircraft Mission Design Series: B-52 | The Boeing Company (81205) | |
| 39-9915-508 399915508 | 1560-01-154-1561 | Web, Structural Component, Aircraf | Aircraft Mission Design Series: B-52 | The Boeing Company (81205) | |
| 39-9915-7 3999157 | 1560-01-162-6494 | Panel, Structural, Aircraft | III End Item Identification: B-52 Special Features: Opposite P/N 39-99295-8 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 39-9915-8 3999158 | 1560-01-162-6495 | Panel, Structural, Aircraft | III End Item Identification: B-52 Special Features: Opposite P/N 39-9915-7 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 39-9915-9 3999159 | 1560-01-162-6496 | Panel, Structural, Aircraft | III End Item Identification: B-52 Special Features: Opposite P/N 39-9915-10 Material: Aluminum alloy 2024 | The Boeing Company (81205) |