FSC 1620 Aircraft Landing Gear Components: 1620-00-125-7388, 1620-00-125-9149, 1620-00-132-1036
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1620-00-125-7388 1620001257388 | 3G61221-101 | Spacer, Upper Torque arm Stop, sho | General Characteristics Item Description: Steel, MIL-S-5000, comp 4340;1.561 in. OD;1.250 in. ID;3.508 in. lg;w/two 0.255 in. dia holes in line, 1.755 in. from end | Lockheed Martin Corporation (98897) | |
| 1620-00-125-7860 1620001257860 | 90324 3G61226-101 1156B9A | Positioner, Landing Gear | RBC Transport Dynamics Corp. (09455) Goodrich Corporation (13002) Lockheed Martin Corporation (98897) | ||
| 1620-00-125-9140 1620001259140 | 3G61243-101 | Bolt, Landing Gear, b | III End Item Identification: C-141 aircraft | Goodrich Corp. (17576) Aviation Manufacturing Group LLC (84596) Hardill Associates LTD (23292) | |
| 1620-00-125-9149 1620001259149 | 3G61244-101 | Bolt, Brace, Drag link Assembly | General Characteristics Item Description: Steel alloy, ams 64O7;5.850 in. LG;2.000 in. OD;0.800 in. id;chromium plated, spec 0496 cl 2, fscm 98897;W/1.250-12UNF-3A thd;countersunk on head end 60 deg by 0.860 in. dia | S F M Company Inc. (4N455) Lockheed Martin Corporation (98897) | |
| 1620-00-126-2617 1620001262617 | A51G9002-11 HP1118300-7 | Damper, Steernose | Northrop Grumman Systems Corporation (26512, 61174) Tactair Fluid Controls Inc. (70236) Teledyne Hydra-Power (84685) | ||
| 1620-00-127-4348 1620001274348 | 4926844-1 | Washer, Nose Landing | Boeing Company, The (88277) | ||
| 1620-00-127-4393 1620001274393 | 2923594-1 | Spring, Main | III End Item Identification: Douglas DC9 | Boeing Company, The (88277) | |
| 1620-00-127-4400 1620001274400 | 3926843-1 | Nut Assembly Nose | Boeing Company, The (88277) | ||
| 1620-00-127-5785 1620001275785 | 14-41607-3 14-41607-33 | Cylinder and Piston Assembly, Lan | III End Item Identification: F-5 aircraft Special Features: U/a:cylinder, piston assembly, nose landing gear; matl: steel NAI-1274 hy-tuf, 21.562IN O/a lg, 3.625IN. min O/a dia, 1.875IN. dia bore thru, 1 end counter bored 2.243IN. min to 2.245IN. max dia 2.090IN. deep, 1 end counter bored 2.648IN. min to 2.650IN. max dia 19.250IN. deep, 1 end 2.625-16 UN-3A thd 0.500IN. lg. 1 end 2.845-16 UN-3B thd 0.562IN. lg, as noted machined surfaces 16.0 32.0 63.0 and 125.0 microinch finish, heat treat 220000 to 245000 psi, shot peen all external surfaces excep threads | Triumph Actuation Systems - (33068) Eagle Tool & Machine Co. Inc. (24398) Northrop Grumman Technical Services (0JRC1) | |
| 1620-00-127-5787 1620001275787 | 14-41620-1 | Cylinder, Follower, Landing Gear | General Characteristics Item Description: Steel, ams 6431 D6AC, 4.125 in. dia, 1.090 in. O/a H, 2.500IN. radius 80.0 deg arc lg cam, 3.165 in. min 2.3175 in. maxcenterbore thru, 4 holes thru 0.1874 in. min to 0.1876 in. maxdia on 1.785 in. bolt circle radius, 2 holes spaced 60.0 deg apartthe other two opposite side, heat treat 220, 000 to 245, 000 psi | Northrop Grumman Technical Services (0JRC1) Northrop Grumman Systems Corporation (76823) | |
| 1620-00-129-9158 1620001299158 | 12L598M1-1 | Cylinder and Piston Assembly, Lan | Special Features: Multi material, 5.870 in. O/a lg | Lockheed Martin Corporation (81755) | |
| 1620-00-129-9160 1620001299160 | 14-41600-5 | Cylinder and Piston Assembly, Lan | III End Item Identification: F-5E aircraft Special Features: Multi material, 56.344 in. O/a lg, 12.312 in. O/a W, 8.625 in. O/a H, major components, 1 cam no. 14-41620-1, 1 cyl no. 14-41607-3, 1 guide no. 14-41614-1, 1 orifice no. 14-41633-1, 1 pin-metering no. 14-41612-1, 1 piston no. 14-41608-1, 1 stop no. 14-41604-1, 1 stop 14-41606-1, 1 valve no. 3-43933-3, 1 valve no. 14-41617-1, fscm 76823 | Northrop Grumman Technical Services (0JRC1) Northrop Grumman Systems Corporation (76823) | |
| 1620-00-129-9168 1620001299168 | 4G12409-101B | Tube, Piston Stop, Landing Gear | General Characteristics Item Description: Steel, 23.000 in. O/a lg, 8.780 in. O/a dia, 4.438 in. boredia, counter bore 6.920 in. dia 2.000 in. deep from one end, counterbore 7.670 in. dia fore 15.640 in. length, 1 end 4 7/16-8UNJS-3B thd 1.410 in. lg, 1 end outside corner chamfered 0.250 in.deep 45.0 deg angle, other end chamfered 0.310 in. deep 45.0 degangle, machined surfaces 125.0 microinch finish, shot peen | Lockheed Martin Corporation (98897) | |
| 1620-00-130-5940 1620001305940 | 204-030-319-1 | Landing Gear, Fixed | Special Features: INCLUDES:2 PLATES;1 strut End Item Identification: Helicopter, bell helicopter textron inc, model UH-1 | Bell Helicopter Textron Inc. (97499) | |
| 1620-00-130-5941 1620001305941 | 204-030-319-2 | Landing Gear, Fixed | Special Features: Consists of 3 parts, plante 2 strut 1 End Item Identification: Helicopter, bell helicopter textron inc, model UH-1 | Bell Helicopter Textron Inc. (97499) | |
| 1620-00-130-9197 1620001309197 | 4G13556-101A | Key, Gudgeon | General Characteristics Item Description: Main landing gear, matl steel SAE4140, 0.460 in. lg, 0.405 in. H, 0.249IN. W | Aero Components Inc. (59213) Remarque Manufacturing Corp. (1DW95) Williams Aerospace & Manufacturing (3P104) | |
| 1620-00-130-9235 1620001309235 | 4G13696-101A | Key, Strut Assembly | III End Item Identification: C-5 acft General Characteristics Item Description: Main landing gear, matl steel, 0.780 in. lg, 0.315 in. H, 0.249 in. W | MIL-Craft MFG. Inc. (50036) Aero Engineering & Manufacturing (17772) Essner Precision Manufacturing LLC (92037) | |
| 1620-00-132-1034 1620001321034 | 206-050-121-3 | Plate, Landing Gear | Bell Helicopter Textron Inc. (97499) | ||
| 1620-00-132-1035 1620001321035 | 206-050-121-5 | Plate, Landing Gear | Triumph Fabrications-HOT Springs (3H339) Bell Helicopter Textron Inc. (97499) | ||
| 1620-00-132-1036 1620001321036 | 206-050-121-1 206-050-121-001 | Plate, Landing Gear | Bell Helicopter Textron Inc. (97499) |