Airframe Structural Components: 3-71136, 371169-1L, 371208-1
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
3-71136 371136 | 1560-00-210-9007 | Bolt Assembly, Inboard Flap Carri | General Characteristics Item Description: Steel, 5.340 in. lg, 1.250 in. dia, both end threaded 5/8-18NF-3A, grease fitting on 1 end | The Boeing Company (81205) | |
371156-1 3711561 | 1560-00-670-9243 | Cover, Access, Aircraft | Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/13 fed spec single material response Securing Device Type: Flush catch and turnlock fastener | Lockheed Martin Corporation (98897) | |
371156-3 3711563 | 1560-00-986-2579 | Cover, Access | Material: Aluminum alloy 7075 Material Document AND Classification: QQ-A-250/13 fed spec single material response Securing Device Type: Flush catch and turnlock fastener | Lockheed Martin Corporation (98897) | |
371157-1 3711571 | 1560-00-614-7154 | Door Assy, Centering | Lockheed Martin Corporation (98897) | ||
371157-15 37115715 | 1560-00-822-8645 | Door Assy, Tank | Lockheed Martin Corporation (98897) | ||
371157-19 37115719 | 1560-00-869-5868 | Cover, Access | Securing Device Type: Threaded fastener Peripheral Shape Style: Rectangle, rounded corners, multi holes | Lockheed Martin Corporation (98897) | |
371157-7 3711577 | 1560-00-822-8645 | Door Assy, Tank | Lockheed Martin Corporation (98897) | ||
371162-11 37116211 | 1560-01-553-7368 | Drive Assembly Flap | III End Item Identification: C-130J-30 aircraft Special Features: Next higher assembly flap; technical document AAP7211.031-4-27 | Lockheed Martin Corporation (98897) | |
371162-3 3711623 | 1560-01-253-6399 | Drive Assy, Wing Fla | Lockheed Martin Corporation (98897) | ||
371162-5 3711625 | 1560-01-438-8785 | Drive Assy, Flap | III End Item Identification: Lockheed, C130J hercules aircraft | Lockheed Martin Corporation (98897) | |
371162-7 3711627 | 1560-01-438-8789 | Drive Assy, Flap | III End Item Identification: Lockheed, C130J hercules aircraft | Lockheed Martin Corporation (98897) | |
371169-1L 3711691L | 1560-00-160-4589 | Tee, Wing Rib cap | General Characteristics Item Description: 2.910 in. lg, 1.810 in. W, 1.400 in. H | Lockheed Martin Corporation (98897) | |
371169-1R 3711691R | 1560-00-160-4590 | Tee, Wing Rib cap | General Characteristics Item Description: 2.910 in. lg, 1.810 in. W, 1.400 in. H | Lockheed Martin Corporation (98897) | |
371174-1 3711741 | 1560-01-312-5300 | Support, Structural Component, Air | Aircraft Mission Design Series: C-130 Material: Aluminum alloy 7075 Aircraft Location: Rib cap-center wing | Lockheed Martin Corporation (98897) | |
371177-17 37117717 | 1560-00-161-5663 | Stiffener, Front Beam | General Characteristics Item Description: Aluminum alloy, 16.75 in. lg, 1.000 in. H, 0.900 in. W | Lockheed Martin Corporation (98897) | |
371179-1L 3711791L | 1560-01-311-5044 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-130 Special Features: Nha 371232-1L Aircraft Location: Center rib cap | Aero Components Inc. (59213) Aero Engineering & Manufacturing (17772) Atlas Safe Co. (52913) Falcon Manufacturing Corp. (0HM72) Lockheed Martin Corporation (98897) Southern Machine Specialist Inc. (3C5R6) | |
371179-1R 3711791R | 1560-01-311-5043 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-130 Special Features: Nha 371232-1R Aircraft Location: Center wing station | Lockheed Martin Corporation (98897) | |
371180-1L 3711801L | 1560-01-339-7337 | Fitting, Structural Component, Air | III End Item Identification: C130E acft Aircraft Location: Upper rib cap, center wing | Frazier Aviation Inc. (23162) Lockheed Martin Corporation (98897) | |
371180-1R 3711801R | 1560-01-339-7336 | Fitting, Structural Component, Air | III End Item Identification: C130E acft Aircraft Location: Upper rib cap, center wing | Aerometals Inc. (32664) Frazier Aviation Inc. (23162) Lockheed Martin Corporation (98897) | |
371208-1 3712081 | 1560-00-612-8068 | Cover, Access, Aircraft | Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/12, T6 fed spec single material response Securing Device Type: Threaded fastener | Lockheed Martin Corporation (98897) |