Airframe Structural Components: 343596-40, 344030-36, 346901-91
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
343596-40 34359640 | 1560-01-601-7044 | Skin, Aircraft | Aircraft Mission Design Series: C-130 aircraft Aircraft Location: Beam assembly Part Name Assigned BY Controlling Agency: CAP | Lockheed Martin Corporation (98897) | |
343599-5 3435995 | 1560-01-605-7089 | Rib, Stiffener, Aircraft | Lockheed Martin Corporation (98897) | ||
344030-27 34403027 | 1560-01-602-0954 | Leading Edge, Aircraft | END Item Identification: C130 acft | Lockheed Martin Corporation (98897) | |
344030-28 34403028 | 1560-01-602-0948 | Leading Edge, Aircraft | End Item Identification: C130 acft | Lockheed Martin Corporation (98897) | |
344030-35 34403035 | 1560-01-602-6339 | Skin, Aircraft | Lockheed Martin Corporation (98897) | ||
344030-36 34403036 | 1560-01-602-6340 | Skin, Aircraft | Lockheed Martin Corporation (98897) | ||
344771R | 1560-01-602-6582 | Stiffener, Aircraft | END Item Identification: C130 acft | Lockheed Martin Corporation (98897) | |
345196-3R 3451963R | 1560-01-608-7979 | Rib, Airfoil | Aircraft Mission Design Series: C-130 Material: Aluminum alloy 2024 Aircraft Location: Rib center section, flap link, aft | Lockheed Martin Corporation (98897) | |
345196-4L 3451964L | 1560-01-601-7013 | Rib, Airfoil | Aircraft Mission Design Series: C-130 Special Features: Heat treat T42;C/O 1 rib, 1 former, 1 stiffener Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
345196-6L 3451966L | 1560-01-601-7015 | Rib, Airfoil | Aircraft Mission Design Series: C-130 Special Features: Heat treat T42;0.032 inch thick Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
345208-21 34520821 | 1560-01-601-7045 | Skin, Aircraft | Aircraft Mission Design Series: C-130 aircraft Special Features: 0.025 inch thick Material: Steel comp 301 | Aerometals Inc. (32664) Lockheed Martin Corporation (98897) | |
345208-22 34520822 | 1560-01-601-7049 | Skin, Aircraft | Aircraft Mission Design Series: C-130 aircraft Special Features: 0.025 inch thick Material: Steel comp 301 | Lockheed Martin Corporation (98897) | |
345208-23 34520823 | 1560-01-601-7051 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-130 aircraft Special Features: 0.025 inch thick Material: Steel comp 301 | Aerometals Inc. (32664) Lockheed Martin Corporation (98897) | |
345278-6L 3452786L | 1560-01-601-7687 | Rib, Stiffener, Aircraft | Aircraft Mission Design Series: C-130 aircraft Material: Aluminum alloy 2024 Aircraft Location: Aft center section rib flap | Lockheed Martin Corporation (98897) | |
345278-6R 3452786R | 1560-01-601-7686 | Rib, Stiffener, Aircraft | Aircraft Mission Design Series: C-130 aicraft Special Features: Heat treat 0 Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
345278-7 3452787 | 1560-01-613-0966 | Rib, Stiffener, Aircraft | END Item Identification: C130 aircraft Aircraft Mission Design Series: C130 Part Name Assigned BY Controlling Agency: RIB | Lockheed Martin Corporation (98897) | |
345294L | 1560-01-597-4527 | Support, Structural Component, Air | Aircraft Mission Design Series: C-130B/E/H Special Features: Opposite right;make from L53654 Aircraft Location: Waterbottle shelf tee | Lockheed Martin Corporation (98897) | |
345665-3L 3456653L | 1560-01-599-8174 | Skin, Aircraft | END Item Identification: Velivolo C130J Special Features: Located on lower skin assy | Lockheed Martin Corporation (98897) | |
345665-3R 3456653R | 1560-01-599-8183 | Skin, Aircraft | END Item Identification: Velivolo C130-J acft Special Features: Located lower skin assy | Lockheed Martin Corporation (98897) | |
346901-91 34690191 | 1560-01-611-6953 | Panel, Structural, Aircraft | Lockheed Martin Corporation (98897) |