Miscellaneous Aircraft Accessories and Components: 1560K0171243ABF, 1560-OH58-202, 1560UH1-350-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1560K0171243ABF | 1680-01-419-9059 | Modification kit, Aircraft Compon | Boeing Company, The (76301) | ||
| 1560K0172783ABF | 1680-01-419-9060 | Modification kit, Aircraft Compon | Boeing Company, The (76301) | ||
| 1560K0174199ABF | 1680-01-419-9056 | Modification kit, Aircraft Compon | Boeing Company, The (76301) | ||
| 1560K0174693ABF | 1680-01-419-9058 | Modification kit, Aircraft Compon | Boeing Company, The (76301) | ||
| 1560K0175262BBF | 1680-01-419-9057 | Modification kit, Aircraft Compon | Boeing Company, The (76301) | ||
| 1560-K017-5933-ABF 1560K0175933ABF | 1680-01-419-9045 | Modification kit, Aircraft Compon | Lockheed Martin Corporation (81755) | ||
| 1560K0176499ABF | 1680-01-419-9061 | Modification kit, Aircraft Compon | Boeing Company, The (76301) | ||
| 1560K0197715DWF | 1680-01-559-5592 | Modification kit, Aircraft Compon | III Part Name Assigned By Controlling Agency: Modification kit, na End Item Identification: F-16/B aircraft | Lockheed Martin Corporation (81755) | |
| 1560K0197715FWF | 1680-01-559-5593 | Modification kit, Aircraft Compon | III Part Name Assigned By Controlling Agency: Modification kit, na End Item Identification: F-16/B aircraft | Lockheed Martin Corporation (81755) | |
| 1560K0502492BBF | 1680-01-419-9064 | Modification kit, Aircraft Compon | Boeing Company, The (76301) | ||
| 1560L19-035 1560L19035 | 1680-00-197-1180 | Pedal, Control | Width: 5.344 inches minimum and 5.406 inches maximum Length: 5.940 inches minimum and 6.126 inches maximum Mounting Position: In line W/mounting center | U S Army Aviation and Missile (81996) | |
| 1560L19-153-1 1560L191531 | 1680-00-189-1181 | Panel Assembly, Firewall | General Characteristics Item Description: Fiberglass pad, MIL-B-5924, ty 2, artificial leather cover, nylon thd, 34.500 in. lg, 18.250 in. W | U S Army Aviation and Missile (81996) | |
| 1560L20-026-1 1560L200261 | 1680-00-040-6152 | Spring Assembly, Adjustable Seat | General Characteristics Item Description: 13.000 in. effective lg | U S Army Aviation and Missile (81996) | |
| 1560L23-127 1560L23127 | 1680-00-029-1161 | Pedal, Control | Width: 5.250 inches nominal Length: 6.031 inches nominal Mounting Method: Hinge W/mounting leaf | U S Army Aviation and Missile (81996) | |
| 1560-OH58-111-23 1560OH5811123 | 1680-01-061-6952 | Cover, Switch box, Collective Pitc | General Characteristics Item Description: Aluminum alloy, QQ-A-250/5, comp 2024 temper o; 0.040 in. nom thk matl; decals, vinyl film, MIL-F-8799 type 2, 0.100 in. H white letters on black background, inscribed ext, retr, incr, decr, gov rpm, loglt R, stow, on, off, loglt, starter | U S Army Aviation and Missile (81996) | |
| 1560-OH58-202 1560OH58202 | 1680-01-325-8201 | Modification kit, Aircraft Compon | End Item Identification: OH-58C observation helicopter Component Quantity: 63 | U S Army Aviation and Missile (81996) | |
| 1560-UH1-1049 1560UH11049 | 1680-01-140-2749 | Strap, Bonding | U S Army Aviation and Missile (81996) | ||
| 1560UH1-347-3 1560UH13473 | 1680-00-879-1441 | Weight, Ballast | III End Item Identification: 1520007139912, 1520008092631 General Characteristics Item Description: C/O2 wt, 8 washers, 4 bolts, 4 washers | U S Army Aviation and Missile (81996) | |
| 1560UH1-347-5 1560UH13475 | 1680-00-879-1442 | Weight, Ballast | General Characteristics Item Description: Lead-antimony AMS7720, surface finish, red enamel fed std 595 no. 11136, white letters no. 17875, dim., 10.800 in. nom lg, 4.300 in. min, 4.350 in. max od, 1.400 in. min, 1.450 in. maxid, 1.600 in. min, 1.650 in. max id counterbored right end 1.200 in. deep, four holes 0.505 in. min, 0.525 in. maxdia drilled thru od, two holes located 1.500 in. from right end and 1.400 in.each side of horizontal centerline, twoholes 5.500 in. from right end and 1.400 in. from each side of horizontalcenterline, holes counterbored to 1.250IN. min, 1.255 in. max dia by 0.900 in.deep, cylinder cut perpendicular to holes W/0.062 to 0.250 in. max gap, weight 50.000 lbs used on all UH1 tailskids to move center of gravity to compensate for forward loading, assembly consists of 18 components, twoweight halves, 8 washers AN960-816L, four bolts AN8-27A and four nuts MS21044N, | U S Army Aviation and Missile (81996) | |
| 1560UH1-350-1 1560UH13501 | 1680-00-067-8208 | Cushion, Seat, Aircraft | Special Features: Cloth, army duck, CCC-C-419, cloth bag, strap, webbing, MIL-W-550 type 3 class 3, buckle MS51929-2, strap, webbing MIL-W-530 type 2 class 3 handle, plastric, ensolite m and ah padding, dim. 16.700 in. nom sq. cloth bag filled 16 in. sq. ensolite m PADDING0.380 in. thl ensolite ah padding 1.00 in. thk separated by base assy P/N 156OUH1-351-1, two straps 49.50 in. lg X 1.00 in. wd W/buckle, two handles 3.70 in. lg attached to back of cushion | U S Army Aviation and Missile (81996) |