FSC 1620 Aircraft Landing Gear Components: 1620-00-301-0803, 1620-00-302-1676, 1620-00-302-9900
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1620-00-301-0803 1620003010803 | 1285045-101 | Drag link, Landing Gear | Lockheed Martin Corporation (98897) | ||
| 1620-00-301-0826 1620003010826 | 1285045-102 | Drag link, Landing Gear | III End Item Identification: Acft model S-3A Special Features: 200 psi min. tensile strength Basic Material: Steel | Lockheed Martin Corporation (98897) | |
| 1620-00-301-3184 1620003013184 | 5-65780 | Arm Assy, Steering V | III End Item Identification: B-52 aircraft | The Boeing Company (81205) | |
| 1620-00-302-1676 1620003021676 | 68A450989-2001 | Bracket, Steering Rigging | General Characteristics Item Description: Aluminum alloy QQ-A-225/9 cond T7351, anodized finish, 2.405 in. O/a lg, 1.180 in. O/a W, 0.880 in. O/a H, machinedsurfaces 125.0 microinch finish | Boeing Company, The (76301) | |
| 1620-00-302-1678 1620003021678 | 68A450646-2003 | Tie Down Ring, Nlg | III End Item Identification: F-15 acft General Characteristics Item Description: Aluminum alloy MIL-A-22771 comp 7075 cond T73, anodizefinish PS13201 type 2 class 1, 3.160 in. O/a lg, 2.860 in.O/a W, 0.880 in. O/a H III Reference Data and Literature: T.O. 4S2-73-4 | Goodrich Corporation (13002) Boeing Company, The (76301) | |
| 1620-00-302-1679 1620003021679 | 68A4450654-1001 68A450654-1001 65A450654-1001 | Retainer, Landing Gear | General Characteristics Item Description: Aluminum alloy QQ-A-225/9 comp 7075 cond T73 or QQ-200/11COMP 7075 cond T73, anodized finish per PS13201 type 2 class 1, 3.880 in. O/a dia, bore thru 3.315 in.min to 3.317 in. max dia, 0.548 in. min to 0.553 in. max thk, 2 matched halves | Ellanef MFG Corp. (6A394) Goodrich Corporation (13002) Goodrich Corp. (17576) | |
| 1620-00-302-1681 1620003021681 | 68A450655-2001 | Pin, cam Anchoring, Landing Gear | General Characteristics Item Description: Steel MIL-S-5626 comp 4140, 0.325 in. min to 0.335 in. maxo/a lg, 0.619 in. min to 0.621 in. max O/a W, 0.370 in. min TO0.375 in. max O/a H, heat treat 180000 to 200000 psi per PS15027 | Goodrich Corporation (13002) Daco Enterprises Inc. (4T965) Daco Government Sales LC (33FX0) | |
| 1620-00-302-4243 1620003024243 | 9205-171R | Drag Brace, Landing Gear | Special Features: 23.590 in. lg, 5.625 in. dp, 7.750 in. H | Goodrich Corporation (13002) | |
| 1620-00-302-7568 1620003027568 | 5-62956 | Housing, Swivel Joint | General Characteristics Item Description: Aluminum alloy, 2.100 in. lg, 1.720 in. W, 1.220 in. H | Downey Manufacturing Inc. (98315) Tect Aerospace Inc. (34336) The Boeing Company (81205) | |
| 1620-00-302-7569 1620003027569 | 8629415-10 5-63974-20 | Conduit, Landing Gear | III End Item Identification: Acft B52 General Characteristics Item Description: 3/4 O.D. X 19.0 l, rigid conduit, .028 wall, 525-0 per and 10106. finish F-2.72 | Air Force United States Department (98748) The Boeing Company (81205) | |
| 1620-00-302-7572 1620003027572 | 5-63974-23 7325163-01 7325163 | Conduit, Landing Gear | III End Item Identification: Acft model B52 | Air Force United States Department (98748) American Metal Fabrication Inc. (55127) The Boeing Company (81205) | |
| 1620-00-302-7573 1620003027573 | 7325164-01 5-63974-24 | Conduit, Landing Gear | III End Item Identification: Acft model B52 | Globe Engineering Co. Inc. (24586) Air Force United States Department (98748) American Metal Fabrication Inc. (55127) | |
| 1620-00-302-7574 1620003027574 | 5-63974-25 | Conduit, Landing Gear | III End Item Identification: Acft model B52 | The Boeing Company (81205) | |
| 1620-00-302-7640 1620003027640 | 9087-34-B-2 9-55788-1 | Socket, Door Strut F | III End Item Identification: B-52 aircraft | Triumph Structures-LOS Angeles Inc. (6D161) Clinton Engines Corp. (10391) Goodrich Corporation (13002) | |
| 1620-00-302-7708 1620003027708 | 345152 | Nut Assembly, Right | General Characteristics Item Description: Steel, MIL-S-6050 cond C-1 | Lockheed Martin Corporation (98897) | |
| 1620-00-302-7709 1620003027709 | 345153 | Nut Assembly, Left H | General Characteristics Item Description: Assembly consisting of plate 3, nut 1, spider 1 | Lockheed Martin Corporation (98897) | |
| 1620-00-302-9077 1620003029077 | S1625-50135 | Cylinder, Alighting | Sikorsky Aircraft Corporation (78286) | ||
| 1620-00-302-9117 1620003029117 | 1285343-101 | Torque Tube Assembly, Mainlanding | III End Item Identification: Aircraft model S-3A | Lockheed Martin Corporation (98897) Northrop Grumman Systems Corporation (61174) | |
| 1620-00-302-9899 1620003029899 | 8858A35L | Bracket Assembly, De | Goodrich Corporation (13002) | ||
| 1620-00-302-9900 1620003029900 | 8858A35R | Bracket Assembly, De | Goodrich Corporation (13002) Mancro Aircraft Co. (31556) |