Airframe Structural Components: 35-35442-21, 35-35504-14, 35-35504-4
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 35-35442-21 353544221 | 1560-01-163-1606 | Plug Assembly, Aircraft | III End Item Identification: Acft model KC-135 General Characteristics Item Description: Al alloy sheet 2024-T3 per QQ-A-250/5; finish F-18.05; C/O 1 plug, 1 flange, 1 rivnut; plug 1.620 in. dia., 0.080 in. thk; flange 1.950 in. dia., 0.063 in. thk; nha 35-35442-5 III Functional Description: Used as plug assy on torque bulkhead hydraulic pressure plug instl | The Boeing Company (82918) | |
| 35-35442-22 353544222 | 1560-01-163-1603 | Plug Assembly, Aircraft | III End Item Identification: Acft model KC-135 General Characteristics Item Description: Al alloy clad sheet 2024-T3 per QQ-A-250/5; finish F-18.05; C/O 1 plug, 1 flange, 1 rivnut; plug 0.900 in. dia., 0.080 in. thk; flange 1.150 in. dia., 0.063 in. thk; nha 35-35442-14 III Functional Description: Used as plug assy on midspar air cond. plug instl | The Boeing Company (82918) | |
| 35-35442-23 353544223 | 1560-01-163-6751 | Plug Assembly, Aircraft | III End Item Identification: Acft model KC-135 General Characteristics Item Description: Al alloy clad sheet 2024-T3 per QQ-A-250/5; finish F-18.05; C/O 1 plug, 1 flange, 1 rivnut; plug 0.900 in. dia, 0.080 in. thk; flange 1.150 in. dia, 0.063 in. thk; nha 35-35442-7 III Functional Description: Used as plug assy on torque bulkhead hydraulic pressure plug instl | The Boeing Company (82918) | |
| 35-35442-24 353544224 | 1560-01-163-6752 | Plug Assembly, Aircraft | III End Item Identification: Acft model KC-135 General Characteristics Item Description: Al alloy sheet 2024-T3 per QQ-A-250/5; finish F-18.05; C/O 1 plug, 1 flange, 1 rivnut; plug 0.570 in. dia, 0.140 in. thk; flange 0.900 in. dia, 0.063 in. thk; nha 35-35442-8 III Functional Description: Used as plug assy on midspar hydraulic flaps plug instl | The Boeing Company (82918) | |
| 35-35453-3 35354533 | 1560-01-177-5052 | Support, Structural Component, Air | III End Item Identification: Acft model KC-135 Special Features: Al alloy clad sheet 2024-T3 per QQ-A-362; finish F-2.59; BAC1490-2540 by 4.100 in. lg; nha 35-35453-2 terminal board assembly III Supplementary Features: Functional description:used as support on engine no. 4 wire bundle stowage terminal strip | The Boeing Company (82918) | |
| 35-35463-3 35354633 | 1560-01-159-5357 | Plate, Structural, Aircraft | III End Item Identification: Acft model C/KC-135 Special Features: 6/6 wear resistant nylon sheet per L-P-410; 4.400 in. lg, 4.400 in. W, 0.125 in. thk; contains 4 irregular holes; 6 holes for attachment (Non-Core Data) Supplementary Features: Used as fairlead on station 312 bulkhead | The Boeing Company (82918) | |
| 35-35463-4 35354634 | 1560-01-159-5358 | Plate, Structural, Aircraft | III End Item Identification: Acft model C/KC-135 Special Features: 6/6 wear resistant nylon sheet per L-P-410; 5.600 in. lg, 4.300 in. W, 0.125 in. thk; 5 irregular holes; 9 holes for attachment (Non-Core Data) Supplementary Features: Used as fairlead on station 312 bulkhead | The Boeing Company (82918) | |
| 35-35466-3 35354663 | 1560-01-159-5359 | Plate, Structural, Aircraft | Aircraft Mission Design Series: KC-135 Aircraft Location: Bulkhead grommet Overall Length: 1.600 inches nominal | The Boeing Company (82918) | |
| 35-35473-1 35354731 | 1560-01-158-7307 | Fairing, Aircraft | Aircraft Mission Design Series: KC-135 Aircraft Location: NO.2 inbd fairing nacelle | The Boeing Company (82918) | |
| 35-35473-2 35354732 | 1560-01-158-7308 | Fairing, Aircraft | Aircraft Mission Design Series: KC-135 Aircraft Location: Inboard NO.3 nacelle | The Boeing Company (82918) | |
| 35-35489-2 35354892 | 1560-01-174-8010 | Scoop Assembly | III End Item Identification: Acft model C-135 | The Boeing Company (82918) | |
| 35-35489-3 35354893 | 1560-01-173-5392 | Plate, Structural, Aircraft | III End Item Identification: Acft model C-135 Special Features: Stock SIZE-.050X1.9X2.4IN;MATERIAL 2024-T3 alclad sheet per QQ-A-250/5;FINISH F-2.59;USED on -2 scoop instl kit-cooling air, R.H. cowling | The Boeing Company (82918) | |
| 35-35503-1 35355031 | 1560-01-146-0782 | Cowling | Aircraft Mission Design Series: KC-135 Aircraft Location: Right hand engine cowl | The Boeing Company (82918) | |
| 35-35504-10 353550410 | 1560-01-158-7364 | Plate, Structural, Aircraft | III End Item Identification: C/KC-135 aircraft Special Features: Opposite -9;EFFECTIVE for acft with 64-1071-14 fairing splice DELETED;MATERIAL-2024-T3 clad al. sht. per QQ-A-250/5 | The Boeing Company (82918) | |
| 35-35504-11 353550411 | 1560-01-158-7365 | Plate, Structural, Aircraft | III End Item Identification: C/KC-135 aircraft Special Features: Opposite -12;EFFECTIVE for acft with 64-1071-14 fairing splice DELETED;MATERIAL-2024-T3 clad al sht per QQ-A-250/5 | The Boeing Company (82918) | |
| 35-35504-12 353550412 | 1560-01-158-7366 | Plate, Structural, Aircraft | III End Item Identification: C/KC-135 aircraft Special Features: Opposite -11;EFFECTIVE for acft with 64-1071-14 fairing splice DELETED;MATERIAL-2024-T3 clad al sht per QQ-A-250/5 | The Boeing Company (82918) | |
| 35-35504-13 353550413 | 1560-01-150-0044 | Plate, Structural, Aircraft | III End Item Identification: Acft model C/KC-135 Special Features: Al clad sheet 2024-T3 per QQ-A-250/5; finish F-2.59; 2.800 in. lg, 1.100 in. W, 0.040 in. thk; opposite P/N -14 (Non-Core Data) Supplementary Features: Used as attachment plate on engine nacelle number 1 attachment | The Boeing Company (82918) | |
| 35-35504-14 353550414 | 1560-01-150-0045 | Plate, Structural, Aircraft | III End Item Identification: Acft model C/KC-135 Special Features: Al clad sheet 2024-T3 per QQ-A-250/5; finish F-2.59; 2.800 in. lg, 1.100 in. W, 0.040 in. thk; opposite P/N -13 (Non-Core Data) Supplementary Features: Used as attachment plate on engine nacelle number 4 attachment | The Boeing Company (82918) | |
| 35-35504-3 35355043 | 1560-01-150-0046 | Plate, Structural, Aircraft | III End Item Identification: Acft model C/KC-135 Special Features: Al clad sheet 2024-T3 per QQ-A-250/5; finish F-2.59; 2.800 in. lg, 2.500 in. W, 0.050 in. thk; opposite P/N -4 (Non-Core Data) Supplementary Features: Used as attachment plate on engine nacelle number 1 attachment | The Boeing Company (82918) | |
| 35-35504-4 35355044 | 1560-01-150-0047 | Plate, Structural, Aircraft | III End Item Identification: Acft model C/KC-135 Special Features: Al clad sheet 2024-T3 per QQ-A-250/5; finish F-2.59; 2.800 in. lg, 2.500 in. W, 0.050 in. thk; opposite P/N -3 (Non-Core Data) Supplementary Features: Used as attachment plate on engine nacelle number 4 attachment | The Boeing Company (82918) |