Airframe Structural Components: 4-3929-135, 4-3929-139, 43983
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 4-3929-135 43929135 | 1560-01-526-1865 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Special Features: Material 6061-T4 EXTRUSION;QQ-A-270 temper T-4;DIM are stock matl Material: Aluminum alloy 6061 | The Boeing Company (82918) | |
| 4-3929-137 43929137 | 1560-01-526-2911 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 acft Special Features: Heat treat T4; dim are stock matl Material: Aluminum alloy 6061 | The Boeing Company (82918) | |
| 4-3929-139 43929139 | 1560-01-526-2927 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 acft Special Features: Heat treat T4; dim are stock matl Material: Aluminum alloy 6061 | The Boeing Company (82918) | |
| 4-3929-189 43929189 | 1560-01-445-6159 | Skin, Aircraft | Aircraft Mission Design Series: B-52H Special Features: Requested name hatch skin, pilot;heat treat T-4, finish F2.130 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 4-3929-190 43929190 | 1560-01-445-6160 | Skin, Aircraft | Aircraft Mission Design Series: B-52H Special Features: Hatch skin, co-pilot;heat treat T4, finish F2.130 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 4-3929-514 43929514 | 1560-00-671-8661 | Door, Access, Aircraft | Special Features: Pilots hatch assy End Item Identification: Aircraft model B52 | The Boeing Company (81205,82918) | |
| 4-3929-515 43929515 | 1560-00-671-8662 | Door, Access, Aircraft | Special Features: Copilot hatch assy End Item Identification: Aircraft model B52 | The Boeing Company (81205,82918) | |
| 439338 | 1560-00-047-5675 | Cover Assembly | III End Item Identification: P-2 aircraft General Characteristics Item Description: Consists of one cover P/N 439337; two studs P/N 4002-4; six studs P/N 4002-8; eight snap rings P/N R4G; eight grommets P/N 4002-N; one nameplate P/N 513053 | Lockheed Martin Corporation (98897) | |
| 4394166-503 4394166503 | 1560-00-210-7585 | Gland, Landing Gear | III End Item Identification: Aircraft model C54 | Boeing Company, The (18355,88277) | |
| 4394333 | 1560-00-213-2673 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-47 Aircraft Location: Combustible fluid shut off valves control idler pulley Overall Length: 2.281 inches nominal | Boeing Company, The (18355,88277) | |
| 4394890-1 43948901 | 1560-00-568-6302 | Windshield Panel, Aircraft | Aircraft Mission Design Series: C-118 | Boeing Company, The (18355,88277) | |
| 4394890-2 43948902 | 1560-00-568-6303 | Windshield Panel, Aircraft | Aircraft Mission Design Series: C-118 | Boeing Company, The (18355,88277) | |
| 4395388 | 1560-00-628-7361 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-118 Material Document and Classification: QQ-S-685 fed spec single material response | Boeing Company, The (18355) | |
| 4395926 | 1560-00-213-2900 | Joint Assembly, Cabi | III End Item Identification: Acft model C118 General Characteristics Item Description: 4.156 in. O/a lg | Boeing Company, The (18355,88277) | |
| 439712 | 1560-00-047-5687 | Panel | III End Item Identification: P-2 aircraft | Lockheed Martin Corporation (98897) | |
| 4397550-5 43975505 | 1560-00-444-9318 | Support, Structural Component, Air | Aircraft Mission Design Series: C-118 | Boeing Company, The (18355,88277) | |
| 43980 | 1560-01-172-4393 | Window Panel, Aircraft | Special Features: U/a: window assy, cam; C/o: forward oblique glass, to meet MIL-G-174; borosilicate crown type BK-7.517642, fine annealed, wedge angle max 15 aroseconds; modified pear shape; symmetrical about centerline, bottom with center to edge 3.990IN. min, 4.010 in. max; top center to edge wdth 2.460 in. min, 2.480 in max; hgt 14.950 in. nom, 14.980 in. max; thk 0.375 in. nom; coating, single layer of magnesium fluoride per MIL-C-675C; wedge angle per mil -W-1366 | Recon/Optical Inc. (93706) | |
| 439809 | 1560-00-047-5692 | Rod End Assembly | III End Item Identification: P-2 aircraft General Characteristics Item Description: Consists of one rod end P/N 439805; one bearing P/N AN200KP5 | Lockheed Martin Corporation (98897) | |
| 43982 | 1560-01-172-4394 | Window Panel, Aircraft | Special Features: U/a: window assy, cam; C/o: commercial plate glass; clear; surfa quality shall be 80-50 per MIL-O-13830; coating, anti-reflection, single layer of magnesium fluoride per MIL-C-675C, min ref 575 nm to 600NM wave length; O/a lg 16.790 in. min and 16.830 in. max; O/a wdth 6.380 in. min. and 6.420 in. max; thk 0.125 in. nom | Recon/Optical Inc. (93706) | |
| 43983 | 1560-01-172-4395 | Window Panel, Aircraft | Special Features: U/a: window assy, cam; matl: glass per MIL-G-174; borosilicate crown type BK-7.517642 or equivalent; grade NH-2A, fine annealed; min 87 percent transmission between 400 and 7050 nanometers; O/a lg 14.375 in.; O/a wdth, V 11.750 in.; O/a thk 0.745 in min, 0.755 in. max; surface coating, single layer of magnesium fluoride per MIL-C-675C | Recon/Optical Inc. (93706) |