Airframe Structural Components: 3F20168-339, 3F20175-113, 3F20175-119
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
3F20168-339 3F20168339 | 1560-00-907-7933 | Floor, Aircraft | Material: Aluminum alloy | Bonded Technology Inc. (61161) Lockheed Martin Corporation (98897) | |
3F20168-365 3F20168365 | 1560-00-968-4739 | Floor, Aircraft | Material: Aluminum alloy | Lockheed Martin Corporation (98897) | |
3F20168-377 3F20168377 | 1560-00-962-7634 | Floor, Aircraft | Material: Aluminum alloy | Lockheed Martin Corporation (98897) | |
3F20168-379 3F20168379 | 1560-00-962-7643 | Floor, Aircraft | Material: Aluminum alloy | Bonded Technology Inc. (61161) Lockheed Martin Corporation (98897) | |
3F20169-161 3F20169161 | 1560-00-738-9940 | Panel Assembly, Wheel Well | General Characteristics Item Description: Aluminum alloy | Lockheed Martin Corporation (98897) | |
3F20169-163 3F20169163 | 1560-00-738-9952 | Panel Assembly, Wheel Well | General Characteristics Item Description: Aluminum alloy | Lockheed Martin Corporation (98897) | |
3F20170-253 3F20170253 | 1560-01-370-9270 | Web, Structural Component, Aircraf | Aircraft Mission Design Series: C-141 Material: Aluminum alloy Aircraft Location: Bulkhead | Lockheed Martin Corporation (98897) | |
3F20171-131 3F20171131 | 1560-00-867-0796 | Platform, Electrical Access | III End Item Identification: Aircraft model C141 General Characteristics Item Description: Aluminum alloy, 7075-T6, QQ-A-250/13 | Lockheed Martin Corporation (98897) | |
3F20172-181 3F20172181 | 1560-00-915-0895 | Panel Assembly, Floor | General Characteristics Item Description: Aluminum QQ-A-287 | Lockheed Martin Corporation (98897) | |
3F20172-197 3F20172197 | 1560-00-506-3242 | Floor, Aircraft | III End Item Identification: C-141 | Lockheed Martin Corporation (98897) | |
3F20175-104 3F20175104 | 1560-01-147-0513 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141B | Lockheed Martin Corporation (98897) | |
3F20175-105 3F20175105 | 1560-01-235-3387 | Longeron | Aircraft Mission Design Series: C-141A/B Special Features: Cond 0 Material: Aluminum alloy 7075 | Lockheed Martin Corporation (98897) | |
3F20175-106 3F20175106 | 1560-01-065-3409 | Tee, Longeron | III End Item Identification: C-141 acft General Characteristics Item Description: Used on fuselage station 395.50 to 451.50 | Lockheed Martin Corporation (98897) | |
3F20175-107 3F20175107 | 1560-01-147-2664 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141 Special Features: Dim. are stock material Material: Aluminum alloy 7075 | Lockheed Martin Corporation (98897) | |
3F20175-109 3F20175109 | 1560-01-277-4712 | Plate, Structural, Aircraft | III End Item Identification: C-141 Aircraft Location: Clip, longeron Aircraft Station Number: FS395.5 to FS451.5 and BL28.0 | Warner Robins Air Logistics Center (98752) | |
3F20175-112 3F20175112 | 1560-01-147-0521 | Support, Structural Component, Air | III End Item Identification: C-141 acft Special Features: Used as clip | Lockheed Martin Corporation (98897) | |
3F20175-113 3F20175113 | 1560-01-147-0517 | Support, Structural Component, Air | III End Item Identification: C-141 acft Special Features: Used as filler on longeron installation, structure assy aft lower forward section forward fuselage | Lockheed Martin Corporation (98897) | |
3F20175-115 3F20175115 | 1560-01-279-4731 | Plate, Structural, Aircraft | III End Item Identification: C-141 Aircraft Location: Splice, bilge area | Warner Robins Air Logistics Center (98752) | |
3F20175-117 3F20175117 | 1560-01-147-0516 | Support, Structural Component, Air | III End Item Identification: C-141 acft Special Features: Part of longeron istallation on structure assy aft lower forward section, forward fuselage | Lockheed Martin Corporation (98897) | |
3F20175-119 3F20175119 | 1560-01-235-3387 | Longeron | Aircraft Mission Design Series: C-141A/B Special Features: Cond 0 Material: Aluminum alloy 7075 | Lockheed Martin Corporation (98897) |