Aircraft Landing Gear Components: 1958-C-533-C02, 1958C-73, 1J-3L147
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1958-C-533-C02 1958C533C02 | 1620-01-107-6850 | Cap Assembly, Housing | General Characteristics Item Description: Aluminum alloy per QQ-A-367, 7075-T73; 5.630 in. O/a dia; 0.650 in. thk | Goodrich Corporation (13002) | |
| 1958-C-540 1958C540 | 1620-01-107-6855 | Adapter, Mount, Power unit | End Item Identification: Mcdonnell aircraft company insert-power unit mounting, model no. nlg; CF18A; CF18B, F/A18A; TF/A18A, and F/A18A aircraft General Characteristics Item Description: Aluminum per QQ-A-225/9, 7075-T73; anodized; 2.410 in. lg; largest dia 1.212 in; smallest dia 1.000 in. | Goodrich Corporation (13002) | |
| 1958C541 | 1620-01-107-6853 | Stop, cap Assembly | General Characteristics Item Description: Aluminum alloy per QQ-A-225/9, 7075-T73; 2.380 in. O/a lg; 1 in. O/a w; 1/2 in. O/a thk | Goodrich Corporation (13002) | |
| 1958-C-57 1958C57 | 1620-01-113-6074 | Lock Ring Assembly | Special Features: Spline outer periphery 91 teeth, pressure angle 45 deg; 4 holes 0.066 in. dia thru; O/a dim. 5.750 in. od by 0.800 in. thk Material: Steel | Goodrich Corporation (13002) | |
| 1958-C-60 1958C60 | 1620-01-116-1522 | Cap, Actuator Attach Pin | General Characteristics Item Description: Steel per MIL-S-8848, class 3, cond E-2; 1.250 in. O/a dia; 0.327 in. dia dentrally located hole; 0.400 in. O/a thk | Goodrich Corporation (13002) | |
| 1958-C-61 1958C61 | 1620-01-107-6812 | Ring Assembly | General Characteristics Item Description: Aluminum alloy per QQ-A-225/9; circular shape; 3.000-12 UNJ-3A external thd; 1.190 in. O/a thk | Goodrich Corporation (13002) | |
| 1958-C-66-A 1958C66A | 1620-01-107-6800 | Manifold Assembly | General Characteristics Item Description: Aluminum alloy comp 7175-T736 | Goodrich Corporation (13002) | |
| 1958C6A | 1620-01-107-6804 | Piston, Floating, Cylinder | General Characteristics Item Description: Aluminum per QQ-A-225/9, 7075-T73; 4.739 in. O/a dia; 7.220 in. O/a lg | Goodrich Corporation (13002) | |
| 1958C-73 1958C73 | 1620-01-107-6828 | Cylinder, Drag Brace | Overall Length: 35.560 inches nominal Special Features: Chamfer 0.150X45 deg Material: Aluminum alloy | Goodrich Corporation (13002) | |
| 1958-C-78 1958C78 | 1620-01-107-6828 | Cylinder, Drag Brace | Overall Length: 35.560 inches nominal Special Features: Chamfer 0.150X45 deg Material: Aluminum alloy | Goodrich Corporation (13002) | |
| 1958-D-100 1958D100 | 1620-01-210-2450 | Cylinder and Piston | Goodrich Corporation (13002) | ||
| 1958-D-50 1958D50 | 1620-01-210-2451 | Collar Assy | Goodrich Corporation (13002) | ||
| 1967B-211 1967B211 | 1620-01-140-3257 | Lock, Head Cylinder Mlg | General Characteristics Item Description: Cres per MIL-S-5059, ty 302 annealed; fabricated from 0.063 in. stock; 0.500 O/a w; 0.812 in. lg to 45 deg tab; tab is 0.281 in lg W/ 0.060 in. centrally located hole 0.090 in. from end | Goodrich Corporation (13002) | |
| 1967B-607 1967B607 | 1620-01-115-5594 | Retainer, Helical Compression Spr | Style Designator: Irregular Overall Height: 1.190 inches nominal Material: Steel, QQ-S-763, class 440C | Goodrich Corporation (13002) | |
| 1967B-674 1967B674 | 1620-01-267-0442 | Piston Assembly, Main Landing Gea | General Characteristics Item Description: Bolt shaped; circular head one end; 0.750-16 UNJF-3A threads other end; 0.500 in. id bore approx 7.000 in. deep; 0.748 in. od | Goodrich Corporation (13002) | |
| 1967B93 | 1620-01-116-1445 | Plate, Lock | General Characteristics Item Description: Aluminum per QQ-A-225/9; 2.000 in. O/a lg; 0.615 in. min., 0.625 in. max O/a h; 0.220 in. O/a thk | Goodrich Corporation (13002) | |
| 1967C306C02 | 1620-01-144-4161 | Crank Assembly, Lever | End Item Identification: Aircraft model F-18 | Goodrich Corporation (13002) | |
| 1967C675A | 1620-01-121-4424 | Link Assembly, Planing | III End Item Identification: Aircraft model F-18 | Goodrich Corporation (13002) | |
| 1967C-701C-02 1967C701C02 | 1620-01-213-5130 | Support, Swing Joint | End Item Identification: Aircraft model F-18 | Goodrich Corporation (13002) | |
| 1J-3L147 1J3L147 | 1620-01-171-3371 | Cylinder and Piston Assembly, Lan | Special Features: Steel cylinder body, ams 5082; steel heads, caps, tie rods; and piston rod; piston rod case hardened to rockwell C54, and chrome plated per QQ-C-320, cl 2, ty 1; 1.000 in. cylinder bore; 10.880 in. body lg; 12.000 in. approx lg O/a; 5/16-24 unf 2A thd connection end on piston rod; rectangular mtg flange; four 0.250 in. dia mtg holes; holes spaced 2.000 in. C to C along lg, and 1.080 in. across w; 2.500 in. lg by 1.500 in. W by 0.370 in. mtg flange thickness | Parker-Hannifin Corporation (84561) |