Airframe Structural Components: 128CE10044-402, 128CE10052-+27, 128CE10151-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 128CE10044-402 128CE10044402 | 1560-01-280-8171 | Windshield Panel, Aircraft | Aircraft Mission Design Series: A-6 Special Features: Bullet resistant; color to be green or clear | Northrop Grumman Systems Corporation (26512,61174) | |
| 128CE10050-3 128CE100503 | 1560-00-923-5268 | Bow Assy, Windshield | Northrop Grumman Systems Corporation (26512) | ||
| 128CE10052-21 128CE1005221 | 1560-01-338-9581 | Skin, Aircraft | Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/13 fed spec single material response Overall Length: 36.000 inches nominal | Northrop Grumman Systems Corporation (26512,61174) | |
| 128CE10052-23 128CE1005223 | 1560-01-314-5745 | Skin, Aircraft | III End Item Identification: A-6 aircraft Side FOR Which Designed: Right side | Northrop Grumman Systems Corporation (26512,61174) | |
| 128CE10052-25 128CE1005225 | 1560-01-265-9100 | Skin, Aircraft | Special Features: Zinc cromate primer MIL-P-6808 on inside surface and chem-mill area Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/13 fed spec single material response | Northrop Grumman Systems Corporation (26512,61174) | |
| 128CE10052-+27 128CE1005227 | 1560-01-265-9101 | Skin, Aircraft | Special Features: Aluminum alloy, QQ-A-250/13, alloy 7075; zinc chromate primer, MIL-P-6808, on inside surface and chem-mill area; 0.063 in. thk | Northrop Grumman Systems Corporation (61174) | |
| 128CE10052-27 128CE1005227 | 1560-01-265-9101 | Skin, Aircraft | Special Features: Aluminum alloy, QQ-A-250/13, alloy 7075; zinc chromate primer, MIL-P-6808, on inside surface and chem-mill area; 0.063 in. thk | Northrop Grumman Systems Corporation (26512) | |
| 128CE10052-29 128CE1005229 | 1560-01-265-6428 | Skin, Aircraft | Special Features: Heat treat per T6, chromate per MIL-C-5541 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/13 fed spec 1ST material response and MIL-C-5541 mil spec 2ND material response | Northrop Grumman Systems Corporation (26512) | |
| 128CE10052-31 128CE1005231 | 1560-01-265-9102 | Skin, Aircraft | III End Item Identification: Acft model A-6E or A-6A Special Features: Aluminum alloy, QQ-A-250/13, alloy 7075 and alloy 7072, T6, anodize, MIL-A-8625, cl 1, ty 2; 0.063 in. thk | Northrop Grumman Systems Corporation (26512,61174) | |
| 128CE10053-21 128CE1005321 | 1560-01-292-6961 | Skin, Aircraft | III End Item Identification: A-6E aircraft Special Features: Aluminum alloy, QQ-A-250/13; 0.063 in. thk; 59.000 in. w; 64.000 in. lg | Northrop Grumman Systems Corporation (26512,61174) | |
| 128CE10053-22 128CE1005322 | 1560-01-292-6962 | Skin, Aircraft | III End Item Identification: A-6E aircraft Special Features: Aluminum alloy; QQ-A-250/13; 0.063 in. thk; 59.000 in. w; 64.000 in. lg | Northrop Grumman Systems Corporation (26512) | |
| 128CE10075-1 128CE100751 | 1560-01-243-9622 | Support, Structural Component, Air | III End Item Identification: Air craft model A-6A Material: Aluminum alloy 6061 Material Document and Classification: QQ-A-200/8 fed spec single material response | Northrop Grumman Systems Corporation (26512) | |
| 128CE10103-23 128CE1010323 | 1560-01-158-5827 | Skin, Special | III End Item Identification: Aircraft model A-6E | Northrop Grumman Systems Corporation (26512) | |
| 128CE10103-24 128CE1010324 | 1560-01-154-2524 | Skin, Installation | III End Item Identification: Aircraft model A-6E General Characteristics Item Description: Aluminum alloy QQ-A-250/13, aluminum clad 7075, 0.071 in. thk | Northrop Grumman Systems Corporation (26512) | |
| 128CE10103-33 128CE1010333 | 1560-01-154-2529 | Skin, Installation | III End Item Identification: Aircraft model A-6E General Characteristics Item Description: Aluminum alloy QQ-A-250/13, aluminum clad 7075, 0.036 in. thk | Northrop Grumman Systems Corporation (26512) | |
| 128CE10118-5 128CE101185 | 1560-00-971-2796 | Door Assembly | Northrop Grumman Systems Corporation (26512,61174) | ||
| 128CE10129-17 128CE1012917 | 1560-01-156-1002 | Bracket | III End Item Identification: Aircraft A-6B General Characteristics Item Description: Material al alloy sh | Northrop Grumman Systems Corporation (26512,61174) | |
| 128CE10141-1 128CE101411 | 1560-01-156-1003 | ARM Assembly, Canopy AFT Release | Northrop Grumman Systems Corporation (26512) | ||
| 128CE10150-11 128CE1015011 | 1560-00-971-2795 | Bow, Canopy | Northrop Grumman Systems Corporation (26512,61174) | ||
| 128CE10151-1 128CE101511 | 1560-00-971-2792 | Glass Assembly | III Part Name Assigned BY Controlling Agency: Glass assembly | Northrop Grumman Systems Corporation (26512) |