FSC 1620 Aircraft Landing Gear Components: 1620-00-118-0707, 1620-00-118-7433, 1620-00-120-1117
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1620-00-118-0707 1620001180707 | 12L9569-11 | Pin, Trunnion | III End Item Identification: F-111 aircraft General Characteristics Item Description: Steel, heat treat 260-280 ksi, 2.430 in. dia, 4.544 in. lg | Lockheed Martin Corporation (81755) | |
| 1620-00-118-0720 1620001180720 | C5730-15 | Arm, Steering Linka | Kaiser Fluid Technologies Inc. (99215) | ||
| 1620-00-118-0724 1620001180724 | C5730-17 | Piston, Steering Co | Kaiser Fluid Technologies Inc. (99215) | ||
| 1620-00-118-1514 1620001181514 | 175107 | Axle Assembly, Main | III End Item Identification: Landing gear component | Lockheed Martin Corporation (98897) | |
| 1620-00-118-7433 1620001187433 | 3-62685 | Filler, Radius, Torsion link | General Characteristics Item Description: Laminated phenolic HH-P-256, 0.900 in. lg, 0.620 in. W, 0.54 in. H | The Boeing Company (81205) | |
| 1620-00-118-7434 1620001187434 | 3-62685-1 | Filler, Radius, link | The Boeing Company (81205) | ||
| 1620-00-118-7445 1620001187445 | 12L9545-801 12L9545-803 12L9545-3 | Pin, Trunnion | Lockheed Martin Corporation (81755) | ||
| 1620-00-118-7446 1620001187446 | 12L9578-9 | Pin, Trunnion | Lockheed Martin Corporation (81755) | ||
| 1620-00-118-7447 1620001187447 | 12L9592-9 | Pin, Retraction Cyli | Lockheed Martin Corporation (81755) | ||
| 1620-00-118-8253 1620001188253 | 32-451085-7 | Restrictor, Shock St | Boeing Company, The (76301) | ||
| 1620-00-119-2693 1620001192693 | 12L9077-9 | Block, Upper Universal Main Landi | III End Item Identification: F-111 acft General Characteristics Item Description: 4340 steel per MIL-S-8844;2.000 in. ID;3.244 in. od III Fsc Application Data: Landing gear, retractable | Lebco Inc. (6M564) Lockheed Martin Corporation (81755) | |
| 1620-00-119-7125 1620001197125 | 4G52413-107A | Pin, Drag Brace, Land | III End Item Identification: C-5 aircraft | Lockheed Martin Corporation (98897) Schneebecks Industries Inc. (15400) Goodrich Corp. (17576) | |
| 1620-00-119-7150 1620001197150 | 4G52413-108A | Pin, Drag Brace, Land | III End Item Identification: C-5 aircraft | All Tools Inc. (32168) Lockheed Martin Corporation (98897) Eagle Tool & Machine Co. Inc. (24398) | |
| 1620-00-119-7160 1620001197160 | 67A30024-30 67A30024-10 67A30024 | Parts kit, Damper | General Characteristics Item Description: Spring 4, lock 1, lock ring 2, nut 1, pin cotter 2, pin straight 1, washer 2, scraper piston rod 1, bolt 1 | Ogden Air Logistics Center (98747) | |
| 1620-00-120-0567 1620001200567 | 6425-50160-041 | Bracket Assy, Fuel N | Sikorsky Aircraft Corporation (78286) | ||
| 1620-00-120-0573 1620001200573 | S1958 | Cover, Actuator, Land | Simmonds Precision Products Inc. (12511, 89305) | ||
| 1620-00-120-0982 1620001200982 | 0543061-1 | Damper, Shimmy | Special Features: Cessna aircraft model T-41B | Cessna Aircraft Company (71379) | |
| 1620-00-120-1055 1620001201055 | 14-41600-501 | Landing Gear, Retractable | Special Features: Multi material; 56.344 in. O/a lg; 12.312 in. O/a w; 8.875 in. O/a w; 1 cylinder and piston assy NO.14-41600-5, 1 housing NO.14-41602-501, 1 torque-arm NO.14-41642-1, 1 torque-arm NO.14-41643-1, cage 76823 | Northrop Grumman Technical Services (0JRC1) Northrop Grumman Systems Corporation (76823) | |
| 1620-00-120-1116 1620001201116 | 14-41604-1 | Stop, Landing Gear | III End Item Identification: F-5 aircraft Special Features: Reference data and LITERATURE:T.O.4S2-75-4; general characteristics item DESCRIPTION:AMS6415 no. 4340; 3.005 in. min to 3.010 in. max bore dia; as noted machined surfaces 32.0 63.0; heat treat 200000 to 220000 psi; 4 holes equally spaced 0.750 in. dia; 3 key ways spaced, 95 deg 117 deg and 148 deg apart 0.126 in. W 0.228 in. deep and 0.740 in. lg Overall Length: 2.641 inches nominal | Peacock Aerospace Inc. (91379) Circor Aerospace Inc. (50601) Triumph Actuation Systems - (33068) | |
| 1620-00-120-1117 1620001201117 | 14-41606-1 | Stop, Landing Gear | III End Item Identification: F-5 aircraft Special Features: Reference data and LITERATURE:AMS6381 no. 4140; 2.260 in. min to 2.270 in. max bore dia; counter bore 2.460 in. min to 2.470 in. max dia 4.400 in. deep; 1 hole thru 1.062 in. dia; 4 holes equally spaced 1.062 in. dia; as noted machine surfaces 32.0; heattreat 180000 to 200000 psi Overall Length: 5.776 inches nominal | Northrop Grumman Technical Services (0JRC1) International Precision Inc. (3H683) Northrop Grumman Systems Corporation (76823) |