Airframe Structural Components: 3P61566-101, 3P61576-101, 3P61577-111
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3P61566-101 3P61566101 | 1560-00-753-1697 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141 Material: Steel comp 4340 Material Document and Classification: MIL-S-5000 mil spec single material response | Lockheed Martin Corporation (98897) | |
| 3P61566-102 3P61566102 | 1560-00-753-1698 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141 Material: Steel comp 4340 Material Document and Classification: MIL-S-5000 mil spec single material response | Lockheed Martin Corporation (98897) | |
| 3P61566-103 3P61566103 | 1560-00-753-1699 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141 Material: Steel comp 4340 Material Document and Classification: MIL-S-5000 mil spec single material response | Lockheed Martin Corporation (98897) | |
| 3P61566-104 3P61566104 | 1560-00-753-1700 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141 Material: Steel comp 4340 Material Document and Classification: MIL-S-5000 mil spec single material response | Lockheed Martin Corporation (98897) | |
| 3P61569-101 3P61569101 | 1560-01-144-8442 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 Special Features: Matl: st, ams 5520 annealed;u/a: retainer, fireseal Aircraft Location: Pylon, pp station 139.217 | Lockheed Martin Corporation (98897) | |
| 3P61570-105 3P61570105 | 1560-00-789-9814 | Pan Assembly, Fireseal, Pylon | General Characteristics Item Description: Steel, 321 cres, MIL-S-6721, 8.820 in. O/a l, 5.400 in. O/a W, 1.720 in. deep, 30 mtg holes around flanged rim, 0.218 in. min, 0.229 in. max dia, threaded drain fitting welded to bottom | Lockheed Martin Corporation (98897) | |
| 3P61572-111 3P61572111 | 1560-01-134-4575 | Support, Structural Component, Air | III End Item Identification: C-141 acft Special Features: Matl laminated steel; matl size 0.050 by 1.000 by 5.000 in. lg; used on beam splice, pylon at pylon station 220.298 | Lockheed Martin Corporation (98897) | |
| 3P61572-123 3P61572123 | 1560-01-135-3684 | Support, Structural Component, Air | III End Item Identification: C-141 acft Special Features: Matl laminated steel; matl size 0.050 by 2.000 by 6.000 in. lg; used on fitting installation, beam splice, pylon station 220.298 | Lockheed Martin Corporation (98897) | |
| 3P61572-125 3P61572125 | 1560-01-136-0543 | Support, Structural Component, Air | III End Item Identification: C-141 aircraft Special Features: Matl titanium, AMS4901; matl size 0.050 by 8.000 by 10.000 in. lg; used as web on fitting installation-beam splice, pylon station 220.298 | Lockheed Martin Corporation (98897) | |
| 3P61576-101 3P61576101 | 1560-01-073-9511 | Skin, Aircraft | III End Item Identification: C-141 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-287-T6 fed spec single material response | Lockheed Martin Corporation (98897) | |
| 3P61576-102 3P61576102 | 1560-01-073-9512 | Skin, Aircraft | III End Item Identification: C-141 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-287-T6 fed spec single material response | Lockheed Martin Corporation (98897) | |
| 3P61576-103 3P61576103 | 1560-01-073-9513 | Skin, Aircraft | III End Item Identification: C-141 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-287-T6 fed spec single material response | Lockheed Martin Corporation (98897) | |
| 3P61576-104 3P61576104 | 1560-01-074-8021 | Skin, Aircraft | III End Item Identification: C-141 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-287-T6 fed spec single material response | Lockheed Martin Corporation (98897) | |
| 3P61576-105 3P61576105 | 1560-01-073-9514 | Skin, Aircraft | III End Item Identification: C-141 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-287-T6 fed spec single material response | Lockheed Martin Corporation (98897) | |
| 3P61576-106 3P61576106 | 1560-01-073-9515 | Skin, Aircraft | III End Item Identification: C-141 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-287-T6 fed spec single material response | Lockheed Martin Corporation (98897) | |
| 3P61577-103 3P61577103 | 1560-01-073-2106 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 | Lockheed Martin Corporation (98897) | |
| 3P61577-105 3P61577105 | 1560-01-071-2239 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 | Lockheed Martin Corporation (98897) | |
| 3P61577-107 3P61577107 | 1560-01-073-2104 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141 Aircraft Location: Fitting instl-pylon to wing, fwd, inboard | Lockheed Martin Corporation (98897) | |
| 3P61577-109 3P61577109 | 1560-01-073-2105 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141 Aircraft Location: Fitting instl.-pylon to wing fwd inboard | Lockheed Martin Corporation (98897) | |
| 3P61577-111 3P61577111 | 1560-01-071-1610 | Bracket, Pylon | III End Item Identification: Acft C141 | Lockheed Martin Corporation (98897) |