Airframe Structural Components: 3P21679-185, 3P21680-101, 3P21701-169
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3P21679-185 3P21679185 | 1560-01-276-6375 | Plate, Structural, Aircraft | III End Item Identification: C-141 Special Features: Cond 0 clad Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3P21679-186 3P21679186 | 1560-01-018-3387 | Vane, Cowl | III End Item Identification: Aircraft, type C141 | Lockheed Martin Corporation (98897) | |
| 3P21680-101 3P21680101 | 1560-00-240-1230 | Bellmouth, Pressure Relief | III End Item Identification: C141 acft General Characteristics Item Description: Matl QQ-A-362 T6 TEMPER-0; 14.000IN. O/a lg, 9.970 in. O/a W | Lockheed Martin Corporation (98897) | |
| 3P21681-118 3P21681118 | 1560-01-292-8999 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141 Special Features: T6 clad; wed Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3P21681-125 3P21681125 | 1560-01-269-3571 | Vane Assembly, Cowl | III End Item Identification: C-141 aircraft General Characteristics Item Description: Matl 2024-0 clad per QQ-A-362;SIZE .071X8X18;VANE assembly, splitter-no.four, aft cowl | Lockheed Martin Corporation (98897) | |
| 3P21681-133 3P21681133 | 1560-01-263-2445 | Former, Aircraft | III End Item Identification: C-141 | Lockheed Martin Corporation (98897) | |
| 3P21681-134 3P21681134 | 1560-01-345-5072 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-141 Material: Aluminum alloy 2024 Aircraft Location: Vane, splitter, NO.4, aft cowl | Lockheed Martin Corporation (98897) | |
| 3P21681-135 3P21681135 | 1560-01-263-0456 | Support, Structural Component, Air | III End Item Identification: C-141 acft Special Features: U/O l-H aft cowl support | Lockheed Martin Corporation (98897) | |
| 3P21681-136 3P21681136 | 1560-01-034-1168 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-141 | Lockheed Martin Corporation (98897) | |
| 3P21681-138 3P21681138 | 1560-01-021-1184 | Stiffener, Aircraft | Aircraft Mission Design Series: C-141A/C | Lockheed Martin Corporation (98897) | |
| 3P21681-139 3P21681139 | 1560-01-345-5073 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-141 Material: Aluminum alloy 2024 Aircraft Location: Vane, splitter, NO.4, aft cowl | Lockheed Martin Corporation (98897) | |
| 3P21681-140 3P21681140 | 1560-01-021-1618 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141A/C Aircraft Location: Cowling | Lockheed Martin Corporation (98897) | |
| 3P21681-144 3P21681144 | 1560-01-345-5034 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141 Material: Aluminum alloy 2024 Aircraft Location: Vane-splitter, NO.4, aft, cowl | Lockheed Martin Corporation (98897) | |
| 3P21682-135 3P21682135 | 1560-00-918-7421 | Door, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 fed spec single material response Securing Device Type: Hinge | Lockheed Martin Corporation (98897) | |
| 3P21683-133 3P21683133 | 1560-00-759-7119 | Door, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 fed spec single material response Securing Device Type: Hinge | Lockheed Martin Corporation (98897) | |
| 3P21690-101 3P21690101 | 1560-00-072-7808 | Cover, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 fed spec single material response Securing Device Type: Spring clip | Lockheed Martin Corporation (98897) | |
| 3P21695-103 3P21695103 | 1560-00-945-6953 | Louver, Blow out Door | III End Item Identification: Aircraft model C-141 General Characteristics Item Description: 356-T6, 8.800 in. lg center to center of mounting holes | Lockheed Martin Corporation (98897) | |
| 3P21701-103 3P21701103 | 1560-01-297-0585 | Skin, Aircraft | III End Item Identification: C-141 Special Features: Cond T6 clad Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3P21701-125 3P21701125 | 1560-01-345-3897 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141 Material: Steel comp 301 Aircraft Location: Seal-cowl door, forward, l-H | Lockheed Martin Corporation (98897) | |
| 3P21701-169 3P21701169 | 1560-01-152-6390 | Panel, Structural, Aircraft | III End Item Identification: C-141 Special Features: C/O cowl door assy, P/N 3P21701-169; fire detector instl, P/N 6680-1 Aircraft Location: Fwd, pylon | Lockheed Martin Corporation (98897) |