Airframe Structural Components: 128B10005-607, 128B10170-13, 128B10201-5
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
128B10005-607 128B10005607 | 1560-01-016-2101 | Radome | Material: Plastic Radome Flexibility: Rigid Pressurizing Device: Not included | Northrop Grumman Systems Corporation (26512) | |
128B10005-9 128B100059 | 1560-00-150-9016 | Radome | Radome Flexibility: Rigid | Northrop Grumman Systems Corporation (26512) | |
128B10010-31 128B1001031 | 1560-00-949-6080 | Door Assy, Engine, Le | Northrop Grumman Systems Corporation (26512) | ||
128B10010-39 128B1001039 | 1560-00-179-5887 | Door, Access, Aircraft | Northrop Grumman Systems Corporation (26512) | ||
128B10010-41 128B1001041 | 1560-00-119-1572 | Dooor Assy, Engine | Northrop Grumman Systems Corporation (26512) | ||
128B10010-603 128B10010603 | 1560-01-046-2109 | Door, Access, Aircraft | Material: Aluminum Surface Treatment: Anodize | Northrop Grumman Systems Corporation (26512) | |
128B10010-604 128B10010604 | 1560-01-046-2110 | Door, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-25014 alloy 2024 fed spec single material response Surface Treatment: Anodize | Northrop Grumman Systems Corporation (26512) | |
128B10010-607 128B10010607 | 1560-01-284-5090 | Door, Access, Aircraft | End Item Identification: A-6E acft | Northrop Grumman Systems Corporation (26512) | |
128B10010-608 128B10010608 | 1560-01-252-8157 | Door, Access, Aircraft | End Item Identification: A-6E acft | Northrop Grumman Systems Corporation (26512) | |
128B10043-13 128B1004313 | 1560-01-319-5531 | Web, Structural Component, Aircraf | III End Item Identification: A-6 aircraft | Northrop Grumman Systems Corporation (26512,61174) | |
128B10054-601 128B10054601 | 1560-00-451-8816 | Frame Assy, Fuselage | Northrop Grumman Systems Corporation (26512) | ||
128B10054-625 128B10054625 | 1560-00-451-8816 | Frame Assy, Fuselage | Northrop Grumman Systems Corporation (26512) | ||
128B10119-21 128B1011921 | 1560-01-292-5150 | Frame Support, Assembly | General Characteristics Item Description: Aluminum alloy, QQ-A-200/11 | Northrop Grumman Systems Corporation (26512) | |
128B10170-11 128B1017011 | 1560-01-257-6197 | Tee, Stringer | General Characteristics Item Description: Aluminum alloy, QQ-A-250/11 7075-T6511, opposite of dash 12, for stringer number 4 | Northrop Grumman Systems Corporation (26512) | |
128B10170-12 128B1017012 | 1560-01-257-6198 | Tee, Stringer | General Characteristics Item Description: Aluminum alloy, QQ-A-200/11 7075-T6511, opposite of dash 11, for stringer number 4 | Northrop Grumman Systems Corporation (26512) | |
128B10170-13 128B1017013 | 1560-01-257-6199 | Tee, Stringer | General Characteristics Item Description: Aluminum alloy, QQ-A-200/11 7075-T6511, opposite of dash 14, for stringer number 3 | Northrop Grumman Systems Corporation (26512) | |
128B10170-14 128B1017014 | 1560-01-257-6200 | Tee, Stringer | General Characteristics Item Description: Aluminum alloy, QQ-A-200/11 7075-T6511, opposite of dash 13, for stringer number 3 | Northrop Grumman Systems Corporation (26512) | |
128B10171-11 128B1017111 | 1560-01-267-9369 | Stringer, Aircraft | III End Item Identification: A-6 aircraft Material: Aluminum Material Document and Classification: QQ-A-200/13 fed spec single material response | Northrop Grumman Systems Corporation (26512) | |
128B10171-12 128B1017112 | 1560-01-263-8563 | Stringer, Aircraft | III End Item Identification: A-6 aircraft Material: Aluminum Material Document and Classification: QQ-A-200/13 fed spec single material response | Northrop Grumman Systems Corporation (26512) | |
128B10201-5 128B102015 | 1560-00-971-3233 | Cover Assembly | Northrop Grumman Systems Corporation (26512) |