Airframe Structural Components: 4071357-1, 40721-00, 4074
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 4071357-1 40713571 | 1560-01-370-1320 | Fitting, Structural Component, Air | Aircraft Mission Design Series: MC-130E Special Features: Next ASSEMBLY:4071347;MATERIAL:356-T6 aluminum alloy, C-03-656 class ii-a Material: Aluminum alloy | Lockheed Martin Corporation (02GJ5,0L1E5,92685) | |
| 4071357-3 40713573 | 1560-01-374-8523 | Fitting, Structural Component, Air | Aircraft Mission Design Series: MC-130E Material: Aluminum alloy 2024 Aircraft Location: Mount | Lockheed Martin Corporation (0L1E5,92685) | |
| 4071362-1 40713621 | 1560-01-374-8522 | Fitting, Structural Component, Air | Aircraft Mission Design Series: MC-130E Material: Aluminum alloy 2024 Aircraft Location: Sway brace, pod | Lockheed Martin Corporation (0L1E5,92685) | |
| 4071362-3 40713623 | 1560-01-375-1434 | Fitting, Structural Component, Air | Aircraft Mission Design Series: MC-130E Material: Aluminum alloy 2024 Aircraft Location: Sway brace, pod | Lockheed Martin Corporation (0L1E5,92685) | |
| 4071363-1 40713631 | 1560-01-375-4333 | Jackscrew Assembly, Sway Brace | III End Item Identification: MC-130E General Characteristics Item Description: Consists of the 1 screw P/N 4071363-3;1 pad P/N 4017363-7 and 2 jam nutp/N NAS509-8;NEXT assembly P/N is 4071349, used on 20091 | Lockheed Martin Corporation (0L1E5,92685,98897) | |
| 4071364-1 40713641 | 1560-01-374-7832 | Fairing, Aircraft | Aircraft Mission Design Series: MC-130E Material: Aluminum alloy 6061 Aircraft Location: Pylon | Lockheed Martin Corporation (0L1E5,92685) | |
| 4071364-13 407136413 | 1560-01-374-7747 | Cover, Access, Aircraft | Special Features: Cover assembly used on P/N 4071364-1 fairing assembly, PYLON;MC-130E aircraft Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/3 fed spec single material response | Lockheed Martin Corporation (0L1E5,92685) | |
| 4071365-1 40713651 | 1560-01-375-0184 | Lug, Forward, Pod Mounting | III End Item Identification: MC-130E General Characteristics Item Description: MATERIAL:2.000 dia 4340 steel BAR;MIL-S-5000 condition E-1;NEXT assembly P/N 4071344, used on 20091 | Lockheed Martin Corporation (0L1E5,92685) | |
| 4071365-3 40713653 | 1560-01-375-0185 | Lug, Aft, Pod Mounting | III End Item Identification: MC-130E General Characteristics Item Description: MATERIAL:2.000 dia 4340 steel BAR;MIL-S-5000 condition E-1;NEXT assembly P/N 4071344, used on 20091 | Lockheed Martin Corporation (0L1E5,92685) | |
| 4071374-1 40713741 | 1560-01-370-2134 | Band Assembly, Conduit Mounting | III End Item Identification: MC-130E General Characteristics Item Description: MATERIAL:.080 2024-T3 alclad;material SPECIFICATION:QQ-A-250/3;NEXT ASSEMBLY:4071348-1 tank assembly lh and 4071348-2 tank assembly rh | Lockheed Martin Corporation (0L1E5,92685) | |
| 40721-00 4072100 | 1560-01-479-4789 | Block, Rubbing | Piper Aircraft Inc. (77294) | ||
| 4072880 | 1560-00-396-7561 | Lever, Cowling Flap | III End Item Identification: Aircraft model C54 | Boeing Company, The (18355,88277) | |
| 4073 | 1560-00-875-7985 | Cover, Access | Material: Aluminum alloy 7075 Material Document AND Classification: QQ-A-250/13 fed spec single material response Length: 6.750 inches nominal | Rubbercraft Corporation Of (77969,98159) | |
| 40730-1 407301 | 1560-01-220-4588 | Fitting Assembly, Left hand | Commanding Officer (96916) | ||
| 40730-2 407302 | 1560-01-312-0068 | Fitting, Main Landing Gear | III End Item Identification: A-4 acft | Commanding Officer (96916) | |
| 40730-301 40730301 | 1560-01-312-0063 | Fitting, Main Landing Gear | III End Item Identification: A-4 acft Criticality Code Justification: AGAV | Boeing Company, The (88277) Commanding Officer (96916) Derco Aerospace Inc. (8X044) Kitco Inc. (34087) | |
| 40730-302 40730302 | 1560-01-312-0068 | Fitting, Main Landing Gear | III End Item Identification: A-4 acft | Commanding Officer (96916) Derco Aerospace Inc. (8X044) Kitco Inc. (34087) Technical Support Center (89771) | |
| 407304-01 40730401 | 1560-01-266-9650 | Door, Access, Aircraft | End Item Identification: F-4 aircraft Securing Device Type: Hinge and threaded fastener Peripheral Shape Style: 1 rectangle, no holes | GE Aviation Systems LLC (35351) | |
| 4073-3 40733 | 1560-00-802-8074 | Cover, Access | Material: Aluminum alloy 7075 Material Document AND Classification: QQ-A-250/13, T6 fed spec single material response Length: 6.750 inches nominal | Rubbercraft Corporation Of (77969,98159) | |
| 4074 | 1560-00-875-1459 | Cover, Access | Material: Aluminum alloy 7075 Special Features: One hole, 0.190 in. min, 0.195 in. max dia, 2.310 in. from hole C to end of cover along lg, 2.310 in. from hole C to end of cover along W Material Document AND Classification: QQ-A-250/13, T6 fed spec single material response | Rubbercraft Corporation Of (77969,98159) |