Helicopter Rotor Blades, Drive Mechanisms and Components: 15539-1, 1560AC1-019-3, 1560H13-121
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
15539-1 155391 | 1615-00-115-2195 | Brush and Spring as | Electro-TEC Corp. (98089) | ||
15560-1 155601 | 1615-00-115-2193 | Busbar Assy, Slip ri | Electro-TEC Corp. (98089) | ||
15562-1 155621 | 1615-00-109-9784 | Terminal Assy, Slip | Electro-TEC Corp. (98089) | ||
15600H13-428-3 15600H134283 | 1615-00-650-7031 | Bracket | U S Army Aviation and Missile (81996) | ||
15600H13-429 15600H13429 | 1615-00-532-2268 | Cap, Stabilizer bar | U S Army Aviation and Missile (81996) | ||
15600H13-466-1 15600H134661 | 1615-00-545-7086 | Kit, Main Rotor hub | U S Army Aviation and Missile (81996) | ||
15600H13-476-3 15600H134763 | 1615-00-030-6515 | Weight, Tail Rotor Blade | General Characteristics Item Description: Steel, fed std 66 comp 1010 or MIL-S-7952 comp 1020, dim., 1.180 in. nomlg arc segment of 5.000 in. id, 5.250 in. od by 13.5 deg W, 0.250 in. nom W0.050 in. nom thick, two holes 0.096 in. dia drilled thru on 5.125 in. boltcircle 0.250 in. from each end, max surface finish, all surfaces 63MICROINCHES aa | U S Army Aviation and Missile (81996) | |
15600H13-476-5 15600H134765 | 1615-00-030-6516 | Weight, Tail Rotor Blade | General Characteristics Item Description: Steel, fed std 66 comp 1010, dim., 1.180 in. nom lg arc segment of 5.000IN. id, 5.250 in. od by 13.5 deg W, 0.250 in. nom W, 0.025 in. nom thick, twoholes 0.096 in. dia drilled thru on 5.125 in. bolt circle 0.250 from eachend, max surface finish, all surfaces 63 microinches aa | U S Army Aviation and Missile (81996) | |
1560AC1-019-3 1560AC10193 | 1615-00-740-6472 | Cap, Trailing, Hinge Pin | General Characteristics Item Description: Steel, MIL-S-5000 comp 4340 cond F, cadmium-plated QQ-P-416 class 2 type 1, dim., 5.890 in. nom flange od, 0.255 in. nom flange thk, flange left corner chamfered 45.0 by 0.120 in. lg, 1.000 in. nom O/a cap ht, 5.400-12 uns class 3A threads on od by 0.671 in. lg, four equally spaced drive points 0.380 in. W by 0.225 in. deep, flange end center drilled 0.806 in. deep W/corner rounded by 0.620 in. radius, right end raisedsurface 0.074 in high W/4.360 in. od and 2.750 in. id, item used on rotary wing head | U S Army Aviation and Missile (81996) | |
1560CH21-469-1 1560CH214691 | 1615-00-231-6396 | Cover Assembly, Roto | U S Army Aviation and Missile (81996) | ||
1560CH34-370-1 1560CH343701 | 1615-00-574-6392 | Shock Absorber Asse | U S Army Aviation and Missile (81996) | ||
1560CH47D-043 1560CH47D043 | 1615-01-274-9798 | Modification kit, Aircraft Compon | End Item Identification: 1520-01-088-3669 End Item Name: Helicopter, cargo-tr Component Quantity: 23 | U S Army Aviation and Missile (81996) | |
1560H13 | 1615-00-124-3049 | Fork Assembly, Swash | A and K Mfg Co. Inc. (16410) | ||
1560H13-065-1 1560H130651 | 1615-00-626-8405 | Weight, Rotary Wing Blade | General Characteristics Item Description: Cres, MIL-S-5059 comp 301 or 302 annealed, dim., 3.000 in. nom lg, 0.680IN. nom W, 0.050 in. nom thk, one hole 0.260 in. min, 0.267 in. max dia andone hole 0.376 in. min, 0.382 in. max dia on horizontal centerline 0.600 in.and 2.100 in. respectively from one end | U S Army Aviation and Missile (81996) | |
1560H13-065-3 1560H130653 | 1615-00-626-8406 | Weight, Rotary Wing Blade | General Characteristics Item Description: Cres, MIL-S-5059 comp 301 or 302 annealed, dim., 3.000 in. nom lg, 1.100IN. nom W, 0.050 in. nom thk, one hole 0.260 in. min, 0.267 in. max dia andone hole 0.376 in. min, 0.382 in. max dia on horizontal centerline 0.600 in.and 2.100 in. respectively from one end | U S Army Aviation and Missile (81996) | |
1560H13-068 1560H13068 | 1615-00-674-4664 | Drum, Tail Rotor Dri | U S Army Aviation and Missile (81996) | ||
1560H13-083 1560H13083 | 1615-00-767-7995 | Rod, Tie | U S Army Aviation and Missile (81996) | ||
1560H13-107-2 1560H131072 | 1615-00-124-3049 | Fork Assembly, Swash | U S Army Aviation and Missile (81996) | ||
1560H13-107-6 1560H131076 | 1615-00-228-3567 | Swivel Assembly, Pla | U S Army Aviation and Missile (81996) | ||
1560H13-121 1560H13121 | 1615-00-606-4835 | Tab, Trim, Aircraft | U S Army Aviation and Missile (81996) |