Weapon System - Hardware: 1697W78P001, 16A11480-31, 16B1892-7
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1697W78P001 | 5342-01-166-4712 | Bracket, Ejector | General Characteristics Item Description: Aluminum alloy, QQ-A-225/8, T4; 0.590 in. lg; 0.420 in. w; 0.220 in. H III End Item Identification: Acft model AV-8 | Ametek Inc. (97424) Evans Machine Co. Inc. (6Y843) | |
| 1697W79P001 | 5342-01-166-4713 | Bracket, Ejector | General Characteristics Item Description: Aluminum alloy, QQ-A-225/8, T4; 0.890 in. lg; 0.850 in. w; 0.510 in. H III End Item Identification: Acft model AV-8 | Ametek Inc. (97424) Evans Machine Co. Inc. (6Y843) | |
| 1697W80P001 | 5342-01-166-4714 | Bracket, Ejector | General Characteristics Item Description: Aluminum alloy, QQ-A-225/8, T4; 0.810 in. lg; 0.590 in. w; 0.356 in. H III End Item Identification: Acft model AV-8 | Ametek Inc. (97424) Evans Machine Co. Inc. (6Y843) | |
| 1697W87P001 | 5342-01-166-4717 | Bracket, Ejector | General Characteristics Item Description: Aluminum alloy, QQ-A-225/8, T4; 0.760 in. lg; 0.590 in. w; 0.370 in. H III End Item Identification: Acft model AV-8 | Ametek Inc. (97424) Evans Machine Co. Inc. (6Y843) | |
| 1697W96P001 | 5342-01-166-4718 | Bracket, Electronic Components as | General Characteristics Item Description: Aluminum alloy; 0.255 in. lg; 0.220 in. w; 0.160 in. H III End Item Identification: Aircraft model AV-8 | Ametek Inc. (97424) | |
| 16984 | 5342-01-285-1559 | Lock, tab | Terex Reedrill (03476) | ||
| 1698AS150 | 5342-01-277-4529 | Base, link | General Characteristics Item Description: Steel, astm A108, pivot block; steel, astm A569, radius plate; fork arm 0.375 in. thk; fork span 1.500 in. thk; pivot pin holes 0.375 in. dia; 2 mounting slots 0.940 in. lg by 0.250 in. wd; finish paint; color olive | Naval Air Systems Command (30003) | |
| 1698W16P002 | 5342-01-309-8399 | Bracket, Engine Accessory | General Characteristics Item Description: Aluminum per QQ-A-250/11, T4, 0.041 in. material thickness, bracket contains 5 legs, all legs are bent at 90.0 degree angles, 1 leg contains 3 mounting holes with 0.172 in. min to 0.175 in. max diameter, 1 leg contains 2 countersunk holes, 0.070 in. dia with 0.140 in. dia by 100.0 degree countersink, 1 leg contains 2 holes with 0.121 in. diameter, 1 leg contains 2 holes with 0.160 in. diameter, 1 leg contains 2 countersunk holes with same dimensions as other leg with countersunk holes III End Item Identification: B-1B acft | Ametek Inc. (97424) | |
| 169992 | 5342-00-723-0333 | Latch, Special | Goodrich Corp. (17576) Goodrich Corporation (13002) Honeywell International Inc. (06848,55284) Smith and Smith Aircraft Co. (28298) | ||
| 1699M33G01 | 5342-01-387-2146 | Bracket, Engine Accessory | General Characteristics Item Description: Nickel alloy 625, ams 5599; C/o: brkt, 90 deg, P/N 1699M33P001A, 1/16" thk, welded to spacer P/N 1699M33P01, 1/8" thk X 1/2" dia; clip P/N 1541M25P05, riveted by two AN123164 solid rivets; hole 0.213-.224" dia thru spacer & brkt Special Features: Spacer one side rd end; clip opp side sq end Test Data Document: 07482-P3TF2-CL-A specification (includes engineering type bulletins, brochures, etc., that reflect specification type data in specification format; excludes commercial catalogs, industry directories, and similar trade publications, reflecting general type data on certain environmental and performance requirements and test conditions that are shown as "typical", "average", "nominal", etc.). | General Electric Company (07482) | |
| 16A087 | 5342-00-355-9727 | Mount, Resilient, Weapon System | Material: Steel overall (Non-Core Data) Resilient Member Material: Rubber Style Designator: 2 round W/flange threaded stud | Northrop Grumman Systems Corporation (26916) | |
| 16A091A | 5342-00-597-6434 | Mount, Resilient, Weapon System | Material: Copper alloy overall (Non-Core Data) Resilient Member Material: Rubber Style Designator: 4 round W/flange threaded stud | Northrop Grumman Systems Corporation (26916) | |
| 16A11480-31 16A1148031 | 5342-01-126-1464 | Clamp | General Characteristics Item Description: Cadmium plate all surfaces including holes; 2.500 in. lg; 1.000 in. w; 0.690 in. h; 0.781 in. dia groove; 2 holes 0.281 in. dia min, 0.289 in. dia max, 1.500 in. C to c; chamfer 4 places 45.0 deg X 0.310 in. | Lockheed Martin Corporation (81755) | |
| 16A13039-271 16A13039271 | 5342-01-129-4228 | Plate | Lockheed Martin Corporation (81755) | ||
| 16A2302-31 16A230231 | 5342-01-058-2590 | Slide | General Characteristics Item Description: 13.500 in. lg; 1.000 in. W | Lockheed Martin Corporation (81755) | |
| 16A2330-17 16A233017 | 5342-01-058-2591 | PAD | General Characteristics Item Description: 2.000 in. lg; 1.240 in. w; 1 hole 0.397 in. dia min, 0.402 in. dia max, 0.530 in. center to end, 0.560 in. center to side | Lockheed Martin Corporation (81755) | |
| 16A7645 | 5342-00-734-7198 | Spring Retaining | Napco International LLC (95201) | ||
| 16B1706-65 16B170665 | 5342-01-587-6596 | Fairlead, Tubular | END Item Identification: F-16 aircraft Special Features: Item is A half circle, outside radius is 0.610 inside radius is 0.334 has A 0.875 radius head .11 thick, end opposit of the head has A 0.056 wide grove 0.019 up from the end, item is made from P6102-3 or P5085-1S-32 Part Name Assigned BY Controlling Agency: Fairlead, support, wiring and coax | Lockheed Martin Corporation (81755) | |
| 16B1802-17 16B180217 | 5342-01-071-9274 | Hinge, half Nose Radome | General Characteristics Item Description: 5.990 in. lg III End Item Identification: Aircraft F-16 | Lockheed Martin Corporation (81755) | |
| 16B1892-7 16B18927 | 5342-01-132-1231 | Guide, Roller | General Characteristics Item Description: 1.000 in. lg, 1.000 in. od, 0.259 in. id with a 0.300 in. wide guide | C. E. Machine Co. Inc. (3L665) Essner Manufacturing L.P. (2B834) Lockheed Martin Corporation (81755) |