Helicopter Rotor Blades, Drive Mechanisms and Components: 204-040-616-001, 204-040-620-005, 204-040-620-9
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 204-040-616-001 204040616001 | 1615-00-765-2407 | Plate, Coupling Retainer | General Characteristics Item Description: Aluminum alloy QQ-A-225/6 comp 2024-T4, anodized bps FW4001, dim., 0.590 in. nom lg, 1.360 in. nom left flange od by 0.140 in. thk, 1.080 in. nom bodyod, 0.266 in. nom id, 0.680 in. right idcounterbore by 0.355 in. deep, right end od reduced to 0.805 in. min, 0.810 in. max od by 0.150 in. lg, left end counterbored to 0.940 in. dia by 0.095 in.deep, item used on tail rotor drive | Bell Helicopter Textron Inc. (97499) | |
| 204-040-616-005 204040616005 | 1615-00-448-9189 | Plate, Retaining, Tail Rotor Drive | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-616-1 2040406161 | 1615-00-765-2407 | Plate, Coupling Retainer | General Characteristics Item Description: Aluminum alloy QQ-A-225/6 comp 2024-T4, anodized bps FW4001, dim., 0.590 in. nom lg, 1.360 in. nom left flange od by 0.140 in. thk, 1.080 in. nom bodyod, 0.266 in. nom id, 0.680 in. right idcounterbore by 0.355 in. deep, right end od reduced to 0.805 in. min, 0.810 in. max od by 0.150 in. lg, left end counterbored to 0.940 in. dia by 0.095 in.deep, item used on tail rotor drive | Bell Helicopter Textron Inc. (97499) | |
| 204-040-616-5 2040406165 | 1615-00-448-9189 | Plate, Retaining, Tail Rotor Drive | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-616-5K 2040406165K | 1615-00-448-9189 | Plate, Retaining, Tail Rotor Drive | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-617-005 204040617005 | 1615-00-765-2416 | Hanger, Driveshaft | General Characteristics Item Description: Magnesium alloy QQ-M-56 comp AZ91COND hta or steel, corrosion resisting ams 5355, dichromate treated per MIL-M-3171 type 3, dim., 3.000 in. nom od, 2.650 in. nom liner od, 2.4401 in. min, 2.4406 in. max liner id, 0.754 in. min, 0.759 O/a W, 4.810 in. min, 4.820 in. max width across mounting brackets, 4.250 in.min, 4.260 in. max C to C distance between mounting holes, 0.250 in. bracket thk, one hole per side 0.268 in. dia drilled thru bracket on horizontal centerline 0.355 in. from side, hanger splitin half thru mounting brackets on horizontal centerline, item used on tail rotor drive | Bell Helicopter Textron Inc. (97499) | |
| 204-040-617-005 204040617005 | 1615-01-021-6150 | Hanger, Tail Rotor D | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-617-017 204040617017 | 1615-01-021-6150 | Hanger, Tail Rotor D | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-617-101 204040617101 | 1615-01-252-4326 | Hanger | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-617-15 20404061715 | 1615-01-449-4695 | Hanger, Driveshaft | III End Item Identification: UH-1N aircraft III Part Name Assigned By Controlling Agency: Hanger - driveshaft, tail rotor drive Material: Steel corrosion resisting | Bell Helicopter Textron Inc. (97499) | |
| 204-040-617-17 20404061717 | 1615-01-021-6150 | Hanger, Tail Rotor D | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-617-5 2040406175 | 1615-00-765-2416 | Hanger, Driveshaft | General Characteristics Item Description: Magnesium alloy QQ-M-56 comp AZ91COND hta or steel, corrosion resisting ams 5355, dichromate treated per MIL-M-3171 type 3, dim., 3.000 in. nom od, 2.650 in. nom liner od, 2.4401 in. min, 2.4406 in. max liner id, 0.754 in. min, 0.759 O/a W, 4.810 in. min, 4.820 in. max width across mounting brackets, 4.250 in.min, 4.260 in. max C to C distance between mounting holes, 0.250 in. bracket thk, one hole per side 0.268 in. dia drilled thru bracket on horizontal centerline 0.355 in. from side, hanger splitin half thru mounting brackets on horizontal centerline, item used on tail rotor drive | Bell Helicopter Textron Inc. (97499) | |
| 204-040-617-5 2040406175 | 1615-01-021-6150 | Hanger, Tail Rotor D | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-620-003 204040620003 | 1615-00-678-5414 | Shaft Assy, Tail Rot | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-620-005 204040620005 | 1615-00-019-0217 | Shaft Assembly, Tail | III End Item Identification: UH-1 airframe unit power train III Part Name Assigned By Controlling Agency: Shaft tailrotor drive transmission assembly of | Bell Helicopter Textron Inc. (97499) | |
| 204-040-620-007 204040620007 | 1615-01-008-2798 | Shaft Assembly, Tail | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 204-040-620-009 204040620009 | 1615-01-008-2797 | Shaft Assembly, Tail | III End Item Identification: Rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 204-040-620-011 204040620011 | 1615-01-249-5159 | Shaft Assy, Tailroto | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-620-3 2040406203 | 1615-00-678-5414 | Shaft Assy, Tail Rot | Agusta SPA UNA Societa' DI Agusta (A0126) Alto Vuoto DI Sarzi Sartori (A0216) Bell Helicopter Textron Inc. (97499) Ruag Aerospase Services GMBH (D0216) | ||
| 204-040-620-5 2040406205 | 1615-00-019-0217 | Shaft Assembly, Tail | III End Item Identification: UH-1 airframe unit power train III Part Name Assigned By Controlling Agency: Shaft tailrotor drive transmission assembly of | Agusta SPA UNA Societa' DI Agusta (A0126) Alto Vuoto DI Sarzi Sartori (A0216) Bell Helicopter Textron Inc. (97499) Lockheed Martin Corporation (80070) Ruag Aerospase Services GMBH (D0216) Textron Systems Corporation (04614) | |
| 204-040-620-7 2040406207 | 1615-01-008-2798 | Shaft Assembly, Tail | III End Item Identification: UH-1, rotary wing aircraft | Agusta SPA UNA Societa' DI Agusta (A0126) Alto Vuoto DI Sarzi Sartori (A0216) Bell Helicopter Textron Inc. (97499) | |
| 204-040-620-9 2040406209 | 1615-01-008-2797 | Shaft Assembly, Tail | III End Item Identification: Rotary wing aircraft | Agusta SPA UNA Societa' DI Agusta (A0126) Alto Vuoto DI Sarzi Sartori (A0216) Bell Helicopter Textron Inc. (97499) |