Helicopter Rotor Blades, Drive Mechanisms and Components: 204-040-397-1, 204-040-399-17, 204-040-502-009
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 204-040-397-1 2040403971 | 1615-00-874-0862 | Spider Assembly | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 204-040-397-3 2040403973 | 1615-00-874-0863 | Spider Assembly | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-399-17 20404039917 | 1615-00-841-0153 | Sleeve Assembly, Gen | III End Item Identification: AH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 204-040-402-009 204040402009 | 1615-00-787-4268 | Shaft, Tail Rotor | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 204-040-402-9 2040404029 | 1615-00-787-4268 | Shaft, Tail Rotor | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 204-040-418-013 204040418013 | 1615-00-739-4574 | Case Assembly, Gear | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 204-040-418-13 20404041813 | 1615-00-739-4574 | Case Assembly, Gear | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) U S Army Aviation and Missile (81996) | |
| 204-040-422 204040422 | 1615-00-401-6150 | Fitting, Spacer | General Characteristics Item Description: Aluminum alloy 2024-T4 per QQ-A-225/6 temp 351;0.760/0.765 in. overall LENGTH;0.300 in. shaft DIA;0.900 in. largest O.D. | Bell Helicopter Textron Inc. (97499) | |
| 204-040-422-005 204040422005 | 1615-00-401-6150 | Fitting, Spacer | General Characteristics Item Description: Aluminum alloy 2024-T4 per QQ-A-225/6 temp 351;0.760/0.765 in. overall LENGTH;0.300 in. shaft DIA;0.900 in. largest O.D. | Bell Helicopter Textron Inc. (97499) | |
| 204-040-422-5 2040404225 | 1615-00-401-6150 | Fitting, Spacer | General Characteristics Item Description: Aluminum alloy 2024-T4 per QQ-A-225/6 temp 351;0.760/0.765 in. overall LENGTH;0.300 in. shaft DIA;0.900 in. largest O.D. | Bell Helicopter Textron Inc. (97499) Rotair Industries Inc. (54878) | |
| 204-040-423-001 204040423001 | 1615-00-898-1687 | Sleeve Assembly, Gea | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-423-1 2040404231 | 1615-00-898-1687 | Sleeve Assembly, Gea | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-425-001 204040425001 | 1615-00-972-2736 | Sleeve Assembly, Tai | III End Item Identification: UH-1 airframe unit power train | Bell Helicopter Textron Inc. (97499) | |
| 204-040-425-1 2040404251 | 1615-00-972-2736 | Sleeve Assembly, Tai | III End Item Identification: UH-1 airframe unit power train | Bell Helicopter Textron Inc. (97499) U S Army Aviation and Missile (81996) | |
| 204-040-430-001 204040430001 | 1615-00-128-1663 | Housing Assy, Nozzle | General Characteristics Item Description: Magnesium alloy QQ-M-56 comp AZ91C-T6, dim., 2.250 im. nom O/a lg, 1.580 im. nom O/a W, two 0.283 in. dia mounting holes W/2.613 in. C to C distance on base, 0.330 in. nom base thk, 7.525 in. radius of curvature on base, 0.749 in. min, 0.756 in. max dia input and output ports, two in-line holes perpendicular to input port bossed per AND10050-4 and tapped to 0.800 in. depth, item used as housing for no. 2 jet on planetary transmission | Bell Helicopter Textron Inc. (97499) | |
| 204-040-430-1 2040404301 | 1615-00-128-1663 | Housing Assy, Nozzle | General Characteristics Item Description: Magnesium alloy QQ-M-56 comp AZ91C-T6, dim., 2.250 im. nom O/a lg, 1.580 im. nom O/a W, two 0.283 in. dia mounting holes W/2.613 in. C to C distance on base, 0.330 in. nom base thk, 7.525 in. radius of curvature on base, 0.749 in. min, 0.756 in. max dia input and output ports, two in-line holes perpendicular to input port bossed per AND10050-4 and tapped to 0.800 in. depth, item used as housing for no. 2 jet on planetary transmission | Bell Helicopter Textron Inc. (97499) | |
| 204-040-432-1 2040404321 | 1615-00-221-5027 | Bracket, Rotor Control | General Characteristics Item Description: Magnesium alloy, AMS4453 comp AZ92A-T6, dim., 2.556 in. nom lg, 1.120 in. nom O/a W, 0.620 in. nom ht, one thru hole 0.280 in. min, 0.287 in. max dia drilled thru each end, one center hole 0.1875 in. min, 0.1915 in. max dia, item used for mounting sas transducer | Bell Helicopter Textron Inc. (97499) | |
| 204-040-433-101 204040433101 | 1615-01-235-7920 | Short Shaft Assy | End Item Identification: AH-1 , rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 204-040-502-003 204040502003 | 1615-00-488-4903 | Spring Assy, Oil cap | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-502-009 204040502009 | 1615-00-690-7280 | Cap, Transmission-Gearbox, Aircraf | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) |