Airframe Structural Components: 128AB66046-11, 128AB66214-109, 128AB66446-21
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 128AB66046-11 128AB6604611 | 1560-01-293-0708 | Molding, Metal | Material: Aluminum alloy Mounting Method: HOLE | Northrop Grumman Systems Corporation (26512,61174) | |
| 128AB66203-3 128AB662033 | 1560-01-259-8059 | Support, Structural Component, Air | Special Features: C/O chafing strips, brackets, supports, clamps, retainers, hinge and securing hardware | Northrop Grumman Systems Corporation (26512) | |
| 128AB66205-17 128AB6620517 | 1560-01-325-2477 | Canopy, Fixed | III End Item Identification: A-6E acft Aircraft Mission Design Series: A-6E | Northrop Grumman Systems Corporation (26512) | |
| 128AB66205-19 128AB6620519 | 1560-01-325-2477 | Canopy, Fixed | III End Item Identification: A-6E acft Aircraft Mission Design Series: A-6E | Northrop Grumman Systems Corporation (26512) | |
| 128AB66205-9 128AB662059 | 1560-01-325-2477 | Canopy, Fixed | III End Item Identification: A-6E acft Aircraft Mission Design Series: A-6E | Northrop Grumman Systems Corporation (26512) | |
| 128AB66214-109 128AB66214109 | 1560-01-038-7641 | Truss Assembly | III End Item Identification: E-6A aircraft | Northrop Grumman Systems Corporation (26512) | |
| 128AB66214-113 128AB66214113 | 1560-01-038-7642 | Truss Assembly | III End Item Identification: E-6A aircraft | Northrop Grumman Systems Corporation (26512) | |
| 128AB66226-25 128AB6622625 | 1560-01-316-7727 | Plate, Structural, Aircraft | III End Item Identification: KA-60 aircraft Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/15 fed spec single material response | Northrop Grumman Systems Corporation (26512) | |
| 128AB66226-27 128AB6622627 | 1560-01-302-6115 | Plate, Structural, Aircraft | III End Item Identification: A-6 intruder airplane. Aircraft Mission Design Series: A-6E | Northrop Grumman Systems Corporation (26512,61174) | |
| 128AB66226-31 128AB6622631 | 1560-01-316-7727 | Plate, Structural, Aircraft | III End Item Identification: KA-60 aircraft Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/15 fed spec single material response | Northrop Grumman Systems Corporation (26512,61174) | |
| 128AB66235-23 128AB6623523 | 1560-01-302-6113 | Plate, Structural, Aircraft | III End Item Identification: A-6 intruder airplane. Aircraft Mission Design Series: A-6E | Northrop Grumman Systems Corporation (26512) | |
| 128AB66235-25 128AB6623525 | 1560-01-316-7763 | Latch, Cockpit, Aircraft | General Characteristics Item Description: Left hand side; 2.440 in. length; 0.750 in. width; 0.040 in. thick | Northrop Grumman Systems Corporation (26512) | |
| 128AB66247-27 128AB6624727 | 1560-01-259-8061 | Support, Structural Component, Air | Special Features: 0.127 in. min and 0.133 in. max hole dia twelve places Material: Aluminum alloy Material Document and Classification: QQ-A-250/5 fed spec single material response | Northrop Grumman Systems Corporation (26512) | |
| 128AB66266-1 128AB662661 | 1560-01-060-5452 | Handle Assembly | III End Item Identification: Model A-6E aircraft | Northrop Grumman Systems Corporation (26512,61174) | |
| 128AB66267-24 128AB6626724 | 1560-01-260-0649 | Skin, Aircraft | Material: Aluminum alloy Thickness: 0.090 inches nominal | Northrop Grumman Systems Corporation (61174) | |
| 128AB66267-25 128AB6626725 | 1560-01-260-4953 | Clamp Assembly | General Characteristics Item Description: C/O one tube, steel, MIL-T-6736, comp 4130, 0.437 in. od, 128AB66267-27; and one tab, steel, MIL-S-18729, comp 4130, 0.036 in. thk, 128AB66267-29 | Northrop Grumman Systems Corporation (26512) | |
| 128AB66267-7 128AB662677 | 1560-01-267-3033 | Bracket Assembly | General Characteristics Item Description: C/O two tubes, steel, MIL-T-6736, comp 4130, 0.437 in. od, 128AB66267-27; one tab, steel, MIL-S-18729, comp 4130, 0.036 in. thk, 128AB66267-31; one tab, steel, MIL-S-18729, comp 4130, 0.036 in. thk, 128AB66267-29; two arms, steel, MIL-S-18729, comp 4130, 0.050 in. thk, 128AB66267-33; two rivets, MS20470AD6-24; and TW0 spacers, NAS43DD3-67 | Maven Engineering Corporation (65273) Northrop Grumman Systems Corporation (26512) | |
| 128AB66302-15 128AB6630215 | 1560-01-257-0863 | Support, Structural Component, Air | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 fed spec single material response Material Thickness: 0.063 inches nominal | Northrop Grumman Systems Corporation (26512,61174) | |
| 128AB66302-7 128AB663027 | 1560-01-257-0863 | Support, Structural Component, Air | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 fed spec single material response Material Thickness: 0.063 inches nominal | Northrop Grumman Systems Corporation (26512) | |
| 128AB66446-21 128AB6644621 | 1560-01-259-3855 | Plate, Structural, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4 fed spec single material response Overall Length: 13.000 inches nominal | Northrop Grumman Systems Corporation (26512) |