Airframe Structural Components: 3C13049-103, 3C20061-111, 3C20222-101
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3C13049-103 3C13049103 | 1560-00-076-4947 | End, Tube, Rudder Pedal | General Characteristics Item Description: Aluminum alloy, QQ-A-225/6, 1.920 in. lg, 0.666 in. min, 0.668 in. maxdia | Falcon Manufacturing Corp. (0HM72) Lockheed Martin Corporation (98897) Skyspares Parts Inc. (6M132) | |
| 3C13065-109 3C13065109 | 1560-00-011-1332 | Cover, Access, Aircraft | Material: Glass fiber Securing Device Type: Threaded fastener FSC Application Data: Cabin, airframe | Coating Specialties Inc. (53616) Composite Engineering Inc. (7J998) Lockheed Martin Corporation (98897) Skyspares Parts Inc. (6M132) | |
| 3C13075-105 3C13075105 | 1560-00-011-1334 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141 Material: Aluminum alloy 2024 Aircraft Location: Cover, rudder pedal | Lockheed Martin Corporation (98897) | |
| 3C13078-101 3C13078101 | 1560-00-015-4714 | Bracket, Support, Controls | General Characteristics Item Description: 3.140 in. lg, 1.820 in. W, 1.010 in. H, 4 mtg holes 0.190 in. min, 0.196 in. max dia, 2 connecting holes in line 0.250 in. min, 0.251 in. max dia | Lockheed Martin Corporation (98897) | |
| 3C13092-105 3C13092105 | 1560-00-918-2260 | Quadrant, Input, Control | General Characteristics Item Description: Aluminum alloy, 11.454 in. dia, 1.500 in. H, 1.3125 in. min, 1.3165 in. max dia bore, 2 grooves on outer rim | Lockheed Martin Corporation (98897) | |
| 3C13093-123 3C13093123 | 1560-00-910-8615 | Quadrant Assembly, Control, Rudder | III End Item Identification: Aircraft model C-141A | Lockheed Martin Corporation (98897) | |
| 3C13127-101 3C13127101 | 1560-00-076-4950 | Collar, Retention, Rudder Pedal | III End Item Identification: Aircraft model C141 General Characteristics Item Description: Cres, MIL-S-7720 comp 303S cond C, 1.681 in. O/a lg, 0.875 in. O/a od, 0.249 in. min, 0.255 in. max id | Lockheed Martin Corporation (98897) | |
| 3C13150-101 3C13150101 | 1560-00-015-4723 | Ring, Stabilizing, Ru | III End Item Identification: Aircraft model C141 General Characteristics Item Description: Aluminum alloy, comp 7075 cond T651, 5.070 in. od, 3.070 in. min, 3.080 in. max id, 2.340 in. O/a H | Lockheed Martin Corporation (98897) | |
| 3C13170-103 3C13170103 | 1560-00-910-1954 | Bracket, Pulley | General Characteristics Item Description: Aluminum alloy, QQ-A-601 | Lockheed Martin Corporation (98897) | |
| 3C13175-107 3C13175107 | 1560-00-911-2011 | Screw Assembly, Rudder Pedal | III End Item Identification: Acft model C141 | Lockheed Martin Corporation (98897) | |
| 3C13176-101 3C13176101 | 1560-00-866-8407 | Collar, Threaded, Pedal Adjustment | III End Item Identification: Aircraft model C141 General Characteristics Item Description: Cres, MIL-S-7720 comp 303S surface cond C, 1.814 in. O/a lg | Lockheed Martin Corporation (98897) | |
| 3C13178-104 3C13178104 | 1560-00-799-6932 | Bracket Assembly, Pedal, Rudder | III End Item Identification: Aircraft model C141 General Characteristics Item Description: Aluminum alloy, 15.800 in. effective lg | Lockheed Martin Corporation (98897) | |
| 3C20000-109 3C20000109 | 1560-00-015-4724 | Bracket, Pulley, Secondary Control | General Characteristics Item Description: Aluminum alloy, 5.67 in. W, 8.95 in. lg | Lockheed Martin Corporation (98897) | |
| 3C20000-111 3C20000111 | 1560-00-015-4725 | Bracket, Pulley, Secondary Control | General Characteristics Item Description: Aluminum alloy, 8.950 in. lg, 5.670 in. W | Lockheed Martin Corporation (98897) | |
| 3C20061-111 3C20061111 | 1560-00-015-4729 | Bracket, Pulley, Life Raft Release | General Characteristics Item Description: Aluminum alloy QQ-A-250/11, 5.60 in. lg, 3.00 in. W | Lockheed Martin Corporation (98897) | |
| 3C20103-147 3C20103147 | 1560-00-032-6570 | Cover Assembly, Center Console | III End Item Identification: Aircraft model C141 | Lockheed Martin Corporation (98897) | |
| 3C20137-115 3C20137115 | 1560-00-907-7926 | Interlock Assembly, Flap, Spoiler | III End Item Identification: Aircraft model no. C-141 | Lockheed Martin Corporation (98897) | |
| 3C20146-101 3C20146101 | 1560-00-682-6067 | Guide, Indicator, Spoiler | III End Item Identification: Aircraft model C141 General Characteristics Item Description: Aluminum alloy, QQ-A-250/4, 1.250 in. lg, 0.420 in. W, 1 hole 0.138 in. dia, 2 holes 0.100 in. dia | A and M Aerospace Inc. (6Z800) Lockheed Martin Corporation (98897) Precise Aero Products Inc. (00AE2) | |
| 3C20174-101 3C20174101 | 1560-01-112-8845 | Adapter, Solenoid | III End Item Identification: C-141 acft General Characteristics Item Description: Matl al alloy, QQ-A-268, T351; miscellaneous hardware; 2.620 in. od; 1.650 in. id; 0.650 in. thk; two holes 0.260 in. dia; used on spoiler flap interlock | Lockheed Martin Corporation (98897) | |
| 3C20222-101 3C20222101 | 1560-01-076-1585 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141 Special Features: U/a:plate, spoiler, center console cover | Lockheed Martin Corporation (98897) |