Airframe Structural Components: 3F21033-105, 3F21047-102, 3F21122-101
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3F21033-105 3F21033105 | 1560-00-947-5318 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-141 Material: Aluminum alloy Aircraft Location: Bulkhead | Lockheed Martin Corporation (98897) | |
| 3F21041-101 3F21041101 | 1560-00-016-1542 | Box, Receptacle, External Power | III End Item Identification: C141 aircraft General Characteristics Item Description: Fiberglass, laminated, glass cloth per MIL-C-9084, resin per MIL-P-9300, lamination data, MIL-P-25421, 12 ply minimum, 45.0 deg application, 7.100 in. H, 7.120 in. W, tapered depth | Lockheed Martin Corporation (98897) | |
| 3F21044-101 3F21044101 | 1560-00-073-5086 | Torque Tube, Emergency Exit | General Characteristics Item Description: Steel, 0.500 in. od, 0.058 in. wall thk, 7.660 in. lg, appl to C-141 acft | Lockheed Martin Corporation (98897) | |
| 3F21047-101 3F21047101 | 1560-00-075-8974 | Latch, Emergency Exit Release | III End Item Identification: Aircraft model C141 General Characteristics Item Description: Aluminum alloy, QQ-A-250/12, 2.330 in. lg, 0.800 in. W, 0.420 in. thk, 1 hole 0.506 in. dia, 1 hole 0.193 in. dia | Aero Components Inc. (59213) Aero Engineering & Manufacturing (17772) Kent Associates Inc. (8R034) Lockheed Martin Corporation (98897) Skyspares Parts Inc. (6M132) | |
| 3F21047-102 3F21047102 | 1560-00-075-8975 | Latch, Emergency Exit Release | III End Item Identification: Aircraft model C141 General Characteristics Item Description: Aluminum alloy, QQ-A-250/12, 2.330 in. lg, 0.800 in. W, 0.420 in. thk, 1 hole 0.506 in. dia, 1 hole 0.193 in. dia | G. M. J. Machine Company Inc. (8T119) Lockheed Martin Corporation (98897) | |
| 3F21057-101 3F21057101 | 1560-00-075-8978 | Pull Ring, Hatch Release | General Characteristics Item Description: Aluminum alloy QQ-A-250/13, 3.595 in.lg, 3.140 in. W | Lockheed Martin Corporation (98897) | |
| 3F21062-101 3F21062101 | 1560-01-359-3724 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 Material: Aluminum alloy Aircraft Location: Angle-post NO.3, windshield | Lockheed Martin Corporation (98897) | |
| 3F21062-102 3F21062102 | 1560-01-359-7164 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 Material: Aluminum alloy Aircraft Location: Angle-post NO.3, windshield | Lockheed Martin Corporation (98897) | |
| 3F21070-103 3F21070103 | 1560-01-240-3499 | Support, Structural Component, Air | III End Item Identification: C-141 acft Special Features: Bracket; aluminum alloy 7075-T6; water line 146.0, fuselage station 395.5 | Lockheed Martin Corporation (98897) | |
| 3F21100-105 3F21100105 | 1560-00-075-8979 | Track Assembly, Seat | General Characteristics Item Description: Consists of 2 inserts and 1 track, LS30048-1 X 23, appl to C-141 acft | Lockheed Martin Corporation (98897) | |
| 3F21100-106 3F21100106 | 1560-00-075-8980 | Track Assembly, Seat | General Characteristics Item Description: Consists of 2 inserts and 1 track, LS30048-1 X 23, appl to C-141 acft | Lockheed Martin Corporation (98897) | |
| 3F21105-102 3F21105102 | 1560-01-146-9419 | Support, Structural Component, Air | III End Item Identification: C-141 acft Special Features: Matl al alloy, 7075-T651; used as fitting-kick, frame at fuselage station 379.55 | Lockheed Martin Corporation (98897) | |
| 3F21106-102 3F21106102 | 1560-01-146-9427 | Support, Structural Component, Air | III End Item Identification: C-141 acft Special Features: Matl al alloy, 7075-T651; matl size 2.000 by 2.000 by 5.000 in. lg; five holes along lg 3/16 in. dia; one hole 0.315 in. dia; opposite to P/N 3F21106-101; used as fitting-back up frame on fuselage station 386.75 | Lockheed Martin Corporation (98897) | |
| 3F21107-104 3F21107104 | 1560-01-149-3927 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141B Special Features: 10 holes along lg W/3/16 in. dia equally spaced;opposite to P/N 3F21107-103;USED as fitting-tee, frame Material: Aluminum alloy 7075 | Lockheed Martin Corporation (98897) | |
| 3F21108-102 3F21108102 | 1560-01-146-9426 | Support, Structural Component, Air | III End Item Identification: C-141 acft Special Features: Matl al alloy, 7075-T651; matl size 2.000 by 2.000 by 5.000 in. lg; five holes along lg with 3/16 in. dia; one hole 0.315 in. dia; used as fitting-back up frame on fuselage station 386.75 | Lockheed Martin Corporation (98897) | |
| 3F21116-101 3F21116101 | 1560-00-011-1200 | Block, Bumper | General Characteristics Item Description: Nylon, molded, L-P-410A, 1.800 in. lg, 1.260 in. W, 0.640 in. H, two 0.206 in. dia mtg holes, spaced 1.000 in. C to C | Lockheed Martin Corporation (98897) | |
| 3F21119-105 3F21119105 | 1560-01-160-1159 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141B Special Features: Pre-impregnated glass fabric resin per MIL-R-9299, type 11, class 2; includes 1 connector, 4 washers, 17 nuts, pan pn 3F21119-107 Material: Plastic phenolic | Lockheed Martin Corporation (98897) | |
| 3F21119-106 3F21119106 | 1560-00-073-5088 | Pan, Pressure Seal, Rain Removal | General Characteristics Item Description: Fiberglass | Lockheed Martin Corporation (98897) | |
| 3F21120-101 3F21120101 | 1560-00-074-3361 | Bracket, Actuator, Door | General Characteristics Item Description: Aluminum alloy, 7075-T6, QQ-A-367 | Lockheed Martin Corporation (98897) | |
| 3F21122-101 3F21122101 | 1560-00-074-3362 | Hinge, Door, Nose Landing Gear | III End Item Identification: Aircraft model C141 | Delta HI-Tech (1EC54) G. M. J. Machine Company Inc. (8T119) Lockheed Martin Corporation (98897) |