Airframe Structural Components: 3P21553-102, 3P21554-101, 3P21567-109
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3P21553-102 3P21553102 | 1560-00-929-1074 | Seal half, Firewall | III End Item Identification: Aircraft model C141 General Characteristics Item Description: Steel, MIL-S-6721 comp 321 annealed, 1.680 in. O/a lg, 0.780 in. O/a W, 0.530 in. O/a H, 2 mtg holes 0.220 in. min, 0.226 in. max dia | Aero Components Inc. (59213) Ballistic Missile Defense Systems (17773) Lockheed Martin Corporation (98897) Skyspares Parts Inc. (6M132) TRI-Star Fabricating Inc. (6U340) | |
| 3P21554-101 3P21554101 | 1560-01-345-5078 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-141 Material: Aluminum alloy 2024 Aircraft Location: Ejector, compartment cooling | Lockheed Martin Corporation (98897) | |
| 3P21554-102 3P21554102 | 1560-01-345-3301 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-141 Special Features: Nha 3P21615, 619, 620 and 624 Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3P21555-131 3P21555131 | 1560-00-404-6687 | Duct Assembly, Cowling | General Characteristics Item Description: Cres, MIL-S-6721 | Globe Engineering Co. Inc. (24586) Lockheed Martin Corporation (98897) Metal Forming Incorporated. (7U583) | |
| 3P21555-133 3P21555133 | 1560-00-110-3095 | Retainer, Duct, Cowl | Lockheed Martin Corporation (98897) | ||
| 3P21555-135 3P21555135 | 1560-00-410-5290 | Bracket, Duct, Surge Bleed | III End Item Identification: Aircraft model C141 General Characteristics Item Description: Steel, MIL-S-6721 | Lockheed Martin Corporation (98897) | |
| 3P21555-137 3P21555137 | 1560-00-404-6687 | Duct Assembly, Cowling | General Characteristics Item Description: Cres, MIL-S-6721 | Lockheed Martin Corporation (98897) | |
| 3P21560-101 3P21560101 | 1560-00-759-9222 | Fitting, Hinge, Cowl | III End Item Identification: Aircraft model C141 General Characteristics Item Description: Aluminum alloy, QQ-A-367 comp 7075 cond T6, 6.080 in. O/a lg, 2.400 in. O/a W, 2.400 in. O/a H, 4 mtg holes 0.250 in. min, 0.261 in. max dia, two holes in line 0.3750 in. min, 0.3758 in. max dia | Comptech Corporation (0BR38) G. M. J. Machine Company Inc. (8T119) Lockheed Martin Corporation (98897) | |
| 3P21561-101 3P21561101 | 1560-00-072-7806 | Strut Assembly, Radial, Cowl Suppo | General Characteristics Item Description: Steel, 304 1/8 hard, MIL-T-6845, 0.500 in. dia tube, 0.035 in. wallthkns, female thd connector one end, tongue connector opposite end, 5.540IN. center to end lg | A and M Aerospace Inc. (6Z800) G. M. J. Machine Company Inc. (8T119) Lockheed Martin Corporation (98897) Precise Aero Products Inc. (00AE2) | |
| 3P21561-103 3P21561103 | 1560-00-072-7807 | Strut Assembly, Radial, Cowl Suppo | General Characteristics Item Description: Steel, 304 1/8 hard, MIL-T-6845, 0.500 in. dia tube, 0.035 in. wallthkns, female thd connector one end, tongue connector opposite end, 8.750IN. center to end lg | Lockheed Martin Corporation (98897) | |
| 3P21566-105 3P21566105 | 1560-01-247-8116 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-141B Special Features: P/O firewall, horizontal-forward cowl support Material: Titanium alloy | Lockheed Martin Corporation (98897) | |
| 3P21566-107 3P21566107 | 1560-01-345-2614 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 Material: Aluminum alloy Aircraft Location: Splice tee-firewall, horizontal, forward cowl support | Lockheed Martin Corporation (98897) | |
| 3P21566-109 3P21566109 | 1560-01-240-3481 | Plate, Structural, Aircraft | III End Item Identification: C-141 Special Features: Frame; cond 0 Material: Aluminum alloy 7076 | Lockheed Martin Corporation (98897) | |
| 3P21566-115 3P21566115 | 1560-01-269-6942 | Plate, Structural, Aircraft | III End Item Identification: C-141 Special Features: T3 clad Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3P21566-117 3P21566117 | 1560-01-268-8481 | Plate, Structural, Aircraft | III End Item Identification: C-141 Aircraft Location: Doubler, forward cowl support | Lockheed Martin Corporation (98897) | |
| 3P21566-123 3P21566123 | 1560-01-289-4556 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141 Special Features: T3 clad; doubler Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3P21566-125 3P21566125 | 1560-00-188-3629 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-141 Special Features: U/a:firewall drain fitting assy | Lockheed Martin Corporation (98897) | |
| 3P21566-129 3P21566129 | 1560-01-473-6607 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-141 Material: Titanium alloy Aircraft Location: Firewall, horizontal forward cowl support | Lockheed Martin Corporation (98897) | |
| 3P21567-106 3P21567106 | 1560-01-345-7288 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141 Material: Steel comp 632 Aircraft Location: Stub-longeron, support, forward cowl | Lockheed Martin Corporation (98897) | |
| 3P21567-109 3P21567109 | 1560-01-345-2595 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141 Material: Steel comp 301 Aircraft Location: Fireseal-longeron, support, forwardcowl | Lockheed Martin Corporation (98897) |