Airframe Structural Components: 128BP30135-11, 128BP66100-1, 128C11241-5
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 128BP30135-11 128BP3013511 | 1560-00-918-1004 | Fairing, Antenna, fus | Northrop Grumman Systems Corporation (26512,61174) | ||
| 128BP66100-1 128BP661001 | 1560-00-451-1474 | Scoop Assy, Cooling | Northrop Grumman Systems Corporation (26512) | ||
| 128C10102-3 128C101023 | 1560-00-971-3362 | Base Assembly | Northrop Grumman Systems Corporation (26512) | ||
| 128C10105-1 128C101051 | 1560-00-971-3400 | Adjustment Assembly | Northrop Grumman Systems Corporation (26512,61174) | ||
| 128C10201-1 128C102011 | 1560-00-971-3554 | Pushrod Assembly | Northrop Grumman Systems Corporation (26512) | ||
| 128C10216-3 128C102163 | 1560-00-795-6944 | Pushrod Assembly | Design/OL Inc. (0R2T5) Northrop Grumman Systems Corporation (26512,61174) | ||
| 128C10822-25 128C1082225 | 1560-01-260-9014 | Support, Structural Component, Air | Material: Aluminum alloy 2014 Material Document and Classification: QQ-A-250/3 fed spec single material response Material Thickness: 0.050 inches nominal | Northrop Grumman Systems Corporation (26512) | |
| 128C10822-26 128C1082226 | 1560-01-260-9917 | Support, Structural Component, Air | Special Features: Aluminum alloy, QQ-A-250/3 alloy 2014 T6, primer, zinc chromate, MIL-P-6808; 0.050 in. material thickness | Northrop Grumman Systems Corporation (26512) | |
| 128C10822-27 128C1082227 | 1560-01-260-7858 | Support, Structural Component, Air | Material: Aluminum alloy 2014 Material Document and Classification: QQ-A-250/3 fed spec single material response Material Thickness: 0.050 inches nominal | Maven Engineering Corporation (65273) Northrop Grumman Systems Corporation (26512) | |
| 128C10822-28 128C1082228 | 1560-01-260-7859 | Support, Structural Component, Air | Material: Aluminum alloy 2014 Material Document and Classification: QQ-A-250/3 fed spec single material response Material Thickness: 0.050 inches nominal | Maven Engineering Corporation (65273) Northrop Grumman Systems Corporation (26512) | |
| 128C10822-41 128C1082241 | 1560-01-260-9918 | Support, Structural Component, Air | Special Features: Aluminum alloy, QQ-A-250/5 alloy 2024 T3, primer, zinc chromate, MIL-P-6808 | Northrop Grumman Systems Corporation (26512) | |
| 128C10822-47 128C1082247 | 1560-01-260-9015 | Support, Structural Component, Air | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 fed spec single material response Material Thickness: 0.020 inches nominal | Northrop Grumman Systems Corporation (26512) | |
| 128C10822-49 128C1082249 | 1560-01-265-6383 | Support, Structural Component, Air | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 fed spec single material response Material Thickness: 0.020 inches nominal | Northrop Grumman Systems Corporation (26512) | |
| 128C10822-51 128C1082251 | 1560-01-258-8916 | Support, Special | Northrop Grumman Systems Corporation (26512) | ||
| 128C10822-53 128C1082253 | 1560-01-260-7860 | Support, Structural Component, Air | Material: Aluminum alloy 2014 Material Document and Classification: QQ-A-250/3 fed spec single material response Material Thickness: 0.050 inches nominal | Northrop Grumman Systems Corporation (26512) | |
| 128C10824-3 128C108243 | 1560-00-971-3459 | Bungee Assembly | Northrop Grumman Systems Corporation (26512,61174) | ||
| 128C11216-1 128C112161 | 1560-00-971-3240 | Bell Crank | Northrop Grumman Systems Corporation (26512) | ||
| 128C11221-5 128C112215 | 1560-00-971-3371 | Bell Crank | Material: Aluminum alloy | Northrop Grumman Systems Corporation (26512) | |
| 128C11239-1 128C112391 | 1560-00-971-3369 | Torque Tube Assembly | General Characteristics Item Description: Consists of one tube, three cranks, one armone fitting, fourteen washers, four pins, six bolts, six nuts, and twobearings | Northrop Grumman Systems Corporation (26512) | |
| 128C11241-5 128C112415 | 1560-00-166-0686 | Sector, Flight Control | General Characteristics Item Description: P/O 128C11003 used on A-6A aircraft | Capy Machine Shop Inc. (0BVP9) D F P Manufacturing Corp. (9J659) Northrop Grumman Systems Corporation (26512) |