Airframe Structural Components: 128B11342-1, 128B11376-2, 128B11401-1
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
128B11342-1 128B113421 | 1560-00-567-5796 | Clip Assembly, Sprin | Essner Manufacturing L.P. (2B834) Kaman Aerospace Corporation (84955) MIL-Craft Mfg. Inc. (50036) Northrop Grumman Systems Corporation (26512) | ||
128B11344-5 128B113445 | 1560-01-313-1900 | Channel, Aircraft | III End Item Identification: A-6 aircraft | Kaman Aerospace Corporation (84955) Northrop Grumman Systems Corporation (26512) | |
128B11346-10 128B1134610 | 1560-01-300-4761 | Latch Installation, Access Door | III End Item Identification: KA-6D aircraft | Capy Machine Shop Inc. (0BVP9) Kaman Aerospace Corporation (84955) Northrop Grumman Systems Corporation (26512) | |
128B11346-7 128B113467 | 1560-00-970-9683 | Hook Assembly | Kaman Aerospace Corporation (84955) Maven Engineering Corporation (65273) Northrop Grumman Systems Corporation (26512,61174) | ||
128B11356-7 128B113567 | 1560-01-117-0285 | Fairing, Fuselage, Aircraft | III End Item Identification: Aircraft model A-6E Special Features: Cognizant service:navy; | Northrop Grumman Systems Corporation (26512) | |
128B11356-9 128B113569 | 1560-01-117-0285 | Fairing, Fuselage, Aircraft | III End Item Identification: Aircraft model A-6E Special Features: Cognizant service:navy; | Northrop Grumman Systems Corporation (26512) | |
128B11359-3 128B113593 | 1560-01-373-7007 | Cover, Access | END Item Identification: Aircraft model A-6D/E Special Features: Components include control brackets 3, pulley brackets 2, frames (sta 341.375/STA 325, 625/STA 306.625) 3, cover assy 1; mfg. nomenclature describes item as cover installation fus sta 285.5-368.5 aft fuel tank | Northrop Grumman Systems Corporation (26512) | |
128B11365-3 128B113653 | 1560-00-971-3232 | Cover Assembly | Northrop Grumman Systems Corporation (26512,61174) | ||
128B11375-3 128B113753 | 1560-00-971-2554 | Ladder Assembly | Northrop Grumman Systems Corporation (26512) | ||
128B11375-601 128B11375601 | 1560-00-078-5856 | Ladder, Aircraft Boarding | Design Type: Straight Safety Shoes: Included Crosspiece Tread: Included | Northrop Grumman Systems Corporation (26512) | |
128B11376-14 128B1137614 | 1560-00-166-8094 | Channel, Aircraft | Special Features: Fsc application data:air structural components | Northrop Grumman Systems Corporation (26512) | |
128B11376-2 128B113762 | 1560-01-259-9367 | Support, Structural Component, Air | Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/13 fed spec single material response Material Thickness: 0.050 inches nominal | Northrop Grumman Systems Corporation (26512,61174) | |
128B11377-12 128B1137712 | 1560-01-306-0656 | Step Assembly, Retractable, Aircra | III End Item Identification: A-6E aircraft | Northrop Grumman Systems Corporation (26512) | |
128B11377-23 128B1137723 | 1560-01-317-0736 | Step Assembly, Retractable, Aircra | III End Item Identification: A-6E intruder aircraft | Northrop Grumman Systems Corporation (26512) | |
128B11377-26 128B1137726 | 1560-00-159-1267 | Step, Fuselage | Northrop Grumman Systems Corporation (26512) | ||
128B11379-19 128B1137919 | 1560-01-309-1815 | Tee, Special | III End Item Identification: EA-6B aircraft | Maven Engineering Corporation (65273) Northrop Grumman Systems Corporation (26512) | |
128B11381-33 128B1138133 | 1560-01-246-7226 | Support, Structural Component, Air | Northrop Grumman Systems Corporation (26512) | ||
128B11389-3 128B113893 | 1560-01-313-3239 | Skin, Aircraft | III End Item Identification: A-6 aircraft Side FOR Which Designed: Right side Thickness: 0.040 inches nominal | Northrop Grumman Systems Corporation (26512,61174) | |
128B11389-5 128B113895 | 1560-00-971-0099 | Cover Assembly | Special Features: Cover assembly | Northrop Grumman Systems Corporation (26512) | |
128B11401-1 128B114011 | 1560-01-246-9248 | Latch Assembly Fuse | General Characteristics Item Description: Aluminum alloy, QQ-A-362 2024-T3, 0.025 in. matl thk, shim; aluminum alloy, QQ-A-362 2024-T42, 0.063 in. matl thk, bracket; steel, MIL-S-18729 4130, 0.035 in. matl thk, channel | Northrop Grumman Systems Corporation (26512) |