Airframe Structural Components: 39-25831-1, 39-26107-501, 39-26113-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 39-25831-1 39258311 | 1560-00-141-8965 | Cylinder, Inner, Strut Assembly, Ra | III End Item Identification: Strut assembly part no. 35-30194 General Characteristics Item Description: Consisting of 1EA fitting part no. 23-1916, 1EA adapter part no. 39-25831-3 aluminum alloy, QQ-A-250/8, ALLOY6061, T4, thd data 1.2500-12UNF-3B per MIL-S-7742, 1EA tube part no. 39-25831-2 aluminum alloy, WW-T-700/6, ALLOY6061, T6 III FSC Application Data: Airframe structural components | Acro Tech Inc. (9G503) The Boeing Company (82918) | |
| 39-25831-501 3925831501 | 1560-01-183-7225 | Cylinder, Strut | III End Item Identification: Acft model B-52 General Characteristics Item Description: Finish F-2.70; heat treat to T6 per BAC5602; consist of 1 adapter, 1 tube; nha 35-30194 III Functional Description: Used as strut inner cylinder kit | The Boeing Company (82918) | |
| 392583-19 39258319 | 1560-01-289-4008 | Panel, Harpcloth | Lockheed Martin Corporation (98897) | ||
| 39-25899-1 39258991 | 1560-01-060-8319 | Link Assembly kit, Retractable An | III End Item Identification: B-52 acft | The Boeing Company (81205) | |
| 39-25907-1 39259071 | 1560-01-160-9309 | Support, Structural Component, Air | III End Item Identification: B-52 acft Special Features: C/O plenum; seal, cooling air; orifice plat latch; retainer; screws 8 places; used as plenum assy kit | The Boeing Company (82918) | |
| 39-25924-1 39259241 | 1560-00-199-3147 | Duct Assembly, Air Conditioning-H | END Item Identification: B-52 aircraft Special Features: 4.000 in. od; 3.930 in. id Aircraft Mission Design Series: B-52 | The Boeing Company (82918) | |
| 39-25927-1 39259271 | 1560-00-199-3158 | Duct Assembly, Air Conditioning-H | Special Features: G4.000 in. od; 3.937 in. id; aluminum alloy, alclad 6061, condition O, QQ-A-250/11 sheet for ducting attached to tube 7.900 in. lg, 4.600 in. W, 0.050 in. thk, heat treat duct to T42 per bac 5602 cage 82918 Material: Aluminum alloy 5052 Material Document AND Classification: WW-T-700/14 fed spec single material response | The Boeing Company (82918) | |
| 39-25928-1 39259281 | 1560-00-199-3160 | Duct Assembly, Air Conditioning-H | END Item Identification: B-52 aircraft Special Features: 4.000 in. od; 3.902 in. id Aircraft Mission Design Series: B-52 | The Boeing Company (82918) | |
| 39-25956-501 3925956501 | 1560-01-005-0659 | Lock, Indicator | General Characteristics Item Description: 0.760 in. D III FSC Application Data: Aircraft structural components | The Boeing Company (82918) | |
| 39-25969-501 3925969501 | 1560-00-196-9775 | Duct Assembly, Air Conditioning-H | END Item Identification: B-52 aircraft Special Features: 4.050 in. distance between center opening, orificespaced Aircraft Mission Design Series: B-52 | The Boeing Company (82918) | |
| 39-25974-1 39259741 | 1560-01-121-5767 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Side FOR Which Designed: Left side | The Boeing Company (81205) | |
| 39-25974-2 39259742 | 1560-01-121-5768 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Aircraft Location: Fairing kit treactable ANTENNA6 Side FOR Which Designed: Right side | The Boeing Company (81205) | |
| 39-26063-1 39260631 | 1560-00-377-7488 | Support, Structural Component, Air | III End Item Identification: 35-31818, model B52H Special Features: Steel, MIL-S-18729, comp SAE4130, 0.071 in. thk, 9.600 in. W, 10.000IN. lg, 2 holes 0.404 in. min 0.411 in. max dia, 1 hole 0.890 in. min 0.921IN. max dia, 1 hole 1.343 in. min 1.384 in. max dia, heat treat per BOEINGBAC5617, 1 hole 0.578 in. min 0.598 in. max dia (Non-Core Data) FSC Application Data: Airframe structural components | The Boeing Company (82918) | |
| 39-26063-3 39260633 | 1560-01-020-0443 | Support, Plate | General Characteristics Item Description: Steel, 0.071 in. thk, 3.900 in. W, 5.300 in. lg III FSC Application Data: Structural component, airframe | The Boeing Company (82918) | |
| 39-26063-501 3926063501 | 1560-01-020-0443 | Support, Plate | General Characteristics Item Description: Steel, 0.071 in. thk, 3.900 in. W, 5.300 in. lg III FSC Application Data: Structural component, airframe | The Boeing Company (82918) | |
| 39-26063-502 3926063502 | 1560-01-020-0442 | Bracket Assembly, Support | General Characteristics Item Description: Steel III FSC Application Data: Structural component, airframe | The Boeing Company (82918) | |
| 39-26086-1 39260861 | 1560-01-379-4905 | Channel, Aircraft | Aircraft Mission Design Series: B-52H Special Features: Cowl channel & clip kit;finish F-2.16 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 39-26086-2 39260862 | 1560-01-379-4842 | Bracket, Structural Component, Air | Aircraft Mission Design Series: B-52 Special Features: Finish F-2.16;HEAT treat T42 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 39-26107-501 3926107501 | 1560-00-542-6305 | Bracket Assembly, Support | General Characteristics Item Description: Cres, MIL-S-6721, 0.063 in. thk, 4 mtg holes, 0.188 in. dia, 6 mtg holes, 0.250 in. dia III FSC Application Data: Structural component, airframe | The Boeing Company (82918) | |
| 39-26113-1 39261131 | 1560-00-231-9245 | Former, Aircraft | Aircraft Mission Design Series: B-52 | The Boeing Company (82918) |