Airframe Structural Components: 5-88792-3085, 5-88792-3101, 5-88792-3123
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 5-88792-3085 5887923085 | 1560-01-503-7400 | Panel, Structural, Aircraft | The Boeing Company (17765,81205) | ||
| 5-88792-3093 5887923093 | 1560-00-759-6738 | Panel Assembly, Strut | General Characteristics Item Description: Aluminum alloy | The Boeing Company (81205) | |
| 5-88792-3095 5887923095 | 1560-00-759-6740 | Panel, Structural, Aircraft | Special Features: Aluminum alloy | The Boeing Company (81205,82918) | |
| 5-88792-3096 5887923096 | 1560-01-504-0039 | Panel, Structural, Aircraft | The Boeing Company (82918) | ||
| 5-88792-3097S 5887923097S | 1560-01-027-1611 | Panel, Structural, Aircraft | Aircraft Mission Design Series: E-3A | The Boeing Company (81205) | |
| 5-88792-3098S 5887923098S | 1560-01-022-4094 | Panel, Structural, Aircraft | The Boeing Company (81205) | ||
| 5-88792-3099S 5887923099S | 1560-01-022-5450 | Panel, Structural, Aircraft | Aircraft Mission Design Series: E-3A Aircraft Location: Outbd nacelle strut to wing | The Boeing Company (81205) | |
| 5-88792-31 58879231 | 1560-00-340-9311 | Cover, Access, Aircraft | Securing Device Type: Threaded fastener Mounting Opening Shape Style: 1 unthreaded hole Hole Diameter: 0.218 inches minimum and 0.229 inches maximum | The Boeing Company (81205) | |
| 5-88792-3100S 5887923100S | 1560-01-022-5451 | Panel, Structural, Aircraft | Aircraft Mission Design Series: E-3A Aircraft Location: Outbd nacelle strut to wing | The Boeing Company (81205) | |
| 5-88792-3101 5887923101 | 1560-01-503-7401 | Panel, Structural, Aircraft | The Boeing Company (17765,81205) | ||
| 5-88792-3102 5887923102 | 1560-01-504-4202 | Panel, Structural, Aircraft | The Boeing Company (17765) | ||
| 5-88792-3103 5887923103 | 1560-01-504-4222 | Panel, Structural, Aircraft | The Boeing Company (17765) | ||
| 5-88792-3104 5887923104 | 1560-01-504-4223 | Panel, Structural, Aircraft | The Boeing Company (17765) | ||
| 5-88792-3113S 5887923113S | 1560-01-021-9972 | Panel, Structural, Aircraft | Aircraft Mission Design Series: E-3A Aircraft Location: No. 1 door on nacelle | The Boeing Company (81205) | |
| 5-88792-3114S 5887923114S | 1560-01-022-4095 | Panel, Structural, Aircraft | The Boeing Company (81205) | ||
| 5-88792-3117 5887923117 | 1560-01-159-9579 | Cover, Access | Material: Aluminum alloy 2024 END Item Identification: Acft model C/KC-135 Material Document AND Classification: QQ-A-250/5 fed spec single material response | The Boeing Company (82918) | |
| 5-88792-3117S 5887923117S | 1560-01-021-9974 | Door, Access, Aircraft | End Item Identification: Acft model E-3A | The Boeing Company (81205) | |
| 5-88792-3118 5887923118 | 1560-01-159-9580 | Cover, Access | Material: Aluminum alloy 2024 END Item Identification: Acft model C/KC-135 Material Document AND Classification: QQ-A-250/5 fed spec single material response | The Boeing Company (82918) | |
| 5-88792-3118S 5887923118S | 1560-01-022-4096 | Door, Access, Aircraft | End Item Identification: Acft model E-3A | The Boeing Company (81205) | |
| 5-88792-3123 5887923123 | 1560-01-159-6747 | Panel, Structural, Aircraft | III End Item Identification: C/KC-135 Aircraft Mission Design Series: C/KC-135 Special Features: Opposite P/N -3124 | The Boeing Company (82918) |