Airframe Structural Components: 65-23062, 652316-17, 652-3230
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 65-23062 6523062 | 1560-00-670-8802 | Suppressor Assembly | III End Item Identification: Acft model KC-135 III Functional Description: Used on auxiliary power unit sound suppressor assembly | The Boeing Company (81205) | |
| 65-23073-8 65230738 | 1560-00-356-5297 | Support, Structural Component, Air | III End Item Identification: Duct instl, cart, 35-32375, model B-52 acft Special Features: Aluminum alloy | The Boeing Company (81205) | |
| 6-52307-501 652307501 | 1560-00-907-2110 | Spacer, Fuel line | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | ||
| 65-2312-1 6523121 | 1560-01-022-7813 | Weight | The Boeing Company (81205) | ||
| 65-2312-2 6523122 | 1560-01-135-3051 | Baffle, Fuel Tank, Aircraft | Aircraft Mission Design Series: KC-135 Overall Length: 8.060 inches nominal Overall Width: 1.460 inches nominal | The Boeing Company (81205) | |
| 65-2312-4 6523124 | 1560-01-135-3052 | Balance Weight, Aileron | Special Features: Fansteel 77, finish zinc chromate primer; 7.420 in. lg, 1.230 in. W, 0.480 in. H tapering to 0.380 in. h; located at outboard nose of aileron End Item Identification: Acft model C135 | The Boeing Company (81205) | |
| 65-2312-5 6523125 | 1560-01-543-4017 | Balance Weight, Aileron | The Boeing Company (82918) | ||
| 65-2312-6 6523126 | 1560-01-135-3053 | Balance Weight, Aileron | Special Features: Antimony lead, L-16 (6% antimony), finish cadmium plate per QQ-P-416 type ii or III class b and 1 coat zinc chromate primer per MIL-P-6889; 8.060 in. lg, 1.460 in. W, 0.460 in. H tapering to 0.340 in. h; located on outboard nose of aileron End Item Identification: Acft model C135 | The Boeing Company (81205) | |
| 65-2312-7 6523127 | 1560-01-138-6842 | Baffle, Fuel Tank, Aircraft | Aircraft Mission Design Series: KC-135 Overall Length: 7.500 inches nominal Overall Width: 1.210 inches nominal | The Boeing Company (81205) | |
| 65-2312-7 6523127 | 1560-01-547-1826 | Balance Weight, Aileron | The Boeing Company (82918) | ||
| 65-2312-8 6523128 | 1560-01-135-3054 | Balance Weight, Aileron | Special Features: Antimony lead, L-16 (6% antimony), finish cadmium plate per QQ-P-416 type ii or III class b and 1 coat zinc chromate; manufacturers nomenclature is balance weight End Item Identification: Acft model C135 | The Boeing Company (81205) | |
| 6-52313-1 6523131 | 1560-00-931-5442 | Cover, Access | Hole Diameter: 0.312 inches nominal Securing Device Type: Threaded fastener Peripheral Shape Style: Round, multi holes | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 65-2314 652314 | 1560-01-187-3070 | Crank Assembly | III End Item Identification: Acft model C/KC-135 | The Boeing Company (82918) | |
| 65-2314-3 6523143 | 1560-01-018-4452 | Crank Assembly, Parking Brake | General Characteristics Item Description: Consists of crank 1, bearing-ball 1 III FSC Application Data: Aircraft, mo del no E3A | The Boeing Company (81205) | |
| 652316-1 6523161 | 1560-00-532-6425 | Insulation Blanket, Thermal | Lockheed Martin Corporation (98897) | ||
| 652316-17 65231617 | 1560-00-473-8796 | Insulation Blanket, Thermal | Lockheed Martin Corporation (98897) | ||
| 652316-19 65231619 | 1560-00-473-8797 | Insulation Blanket, Thermal | Lockheed Martin Corporation (98897) | ||
| 652316-3 6523163 | 1560-00-563-7916 | Insulation, Thermal, Special Purpo | Special Features: F-104G | Lockheed Martin Corporation (98897) | |
| 65-23224-1 65232241 | 1560-01-159-3296 | Cover, Access | Material: Aluminum alloy END Item Identification: KC-135 aircraft Material Document AND Classification: QQ-A-362, 0 tempered fed spec single material response | The Boeing Company (82918) | |
| 65-23224-3 65232243 | 1560-01-158-7187 | Cover, Access | Material: Aluminum alloy END Item Identification: KC-135 aircraft Material Document AND Classification: QQ-A-362, 0 tempered fed spec single material response | The Boeing Company (81205) | |
| 652-3230 6523230 | 1560-01-434-8004 | Plate, Structural, Aircraft | Aircraft Mission Design Series: E-3B, C Special Features: Mounting base Material: Aluminum alloy 5052 | Rockwell Collins Inc. (13499) |