Airframe Structural Components: 204-001-825-3, 204-001-850-001, 204-001-947-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 204-001-825-3 2040018253 | 1560-00-931-8331 | Bracket, Pulley, Tail Rotor | III End Item Identification: Aircraft model UH1 General Characteristics Item Description: Magnesium alloy AZ91C QQ-M-56 | Bell Helicopter Textron Inc. (97499) | |
| 204-001-828-001 204001828001 | 1560-00-908-6463 | Bell Crank | Center to Center Distance Between Fulcrum and Arm End Hole/Slot/Ball: 2.585 inches minimum 1ST end and 2.615 inches maximum 1ST end Center to Center Distance Between Fulcrum and Arm End Hole/Slot/Ball: 2.995 inches minimum 2ND end and 3.305 inches maximum 2ND end End Hole/Ball Diameter: 1.480 inches minimum 1ST end and 1.520 inches maximum 1ST end | Bell Helicopter Textron Inc. (97499) | |
| 204-001-828-1 2040018281 | 1560-00-908-6463 | Bell Crank | Center to Center Distance Between Fulcrum and Arm End Hole/Slot/Ball: 2.585 inches minimum 1ST end and 2.615 inches maximum 1ST end Center to Center Distance Between Fulcrum and Arm End Hole/Slot/Ball: 2.995 inches minimum 2ND end and 3.305 inches maximum 2ND end End Hole/Ball Diameter: 1.480 inches minimum 1ST end and 1.520 inches maximum 1ST end | Bell Helicopter Textron Inc. (97499) Lockheed Martin Corporation (80070) | |
| 204-001-835-001 204001835001 | 1560-00-085-7368 | Arm, Collective Transducer | General Characteristics Item Description: Aluminum alloy, QQ-A-225/6, 2.010 in. lg, 0.500 in. W, 0.500 in. H, mtg hole 0.190 in. min, 0.196 in. max dia, connecting hole 0.190 in. min, 0.196 in. max dia | Bell Helicopter Textron Inc. (97499) | |
| 204-001-835-1 2040018351 | 1560-00-085-7368 | Arm, Collective Transducer | General Characteristics Item Description: Aluminum alloy, QQ-A-225/6, 2.010 in. lg, 0.500 in. W, 0.500 in. H, mtg hole 0.190 in. min, 0.196 in. max dia, connecting hole 0.190 in. min, 0.196 in. max dia | Bell Helicopter Textron Inc. (97499) | |
| 204-001-844-001 204001844001 | 1560-00-871-9570 | Bell Crank | III Material: Aluminum alloy | Bell Helicopter Textron Inc. (97499) | |
| 204-001-844-1 2040018441 | 1560-00-871-9570 | Bell Crank | III Material: Aluminum alloy | Bell Helicopter Textron Inc. (97499) Lockheed Martin Corporation (80070) | |
| 204-001-850-001 204001850001 | 1560-00-993-1864 | Collar Assembly, Pedal Adjusting | General Characteristics Item Description: Plastic, molded phenolic, L-P-509, 0.190 in. min, 0.196 max dia hole 2 places, 2.000 in. hole to hole center | Bell Helicopter Textron Inc. (97499) | |
| 204-001-850-1 2040018501 | 1560-00-993-1864 | Collar Assembly, Pedal Adjusting | General Characteristics Item Description: Plastic, molded phenolic, L-P-509, 0.190 in. min, 0.196 max dia hole 2 places, 2.000 in. hole to hole center | Bell Helicopter Textron Inc. (97499) | |
| 204-001-854-2 2040018542 | 1560-00-867-6034 | Support Assembly, Bell Crank | III End Item Identification: Aircraft model UH-1F General Characteristics Item Description: 3.880 in. O/a lg, 3.130 in. O/a W, 2.515 in. O/a H | Bell Helicopter Textron Inc. (97499) Lockheed Martin Corporation (80070) | |
| 204-001-856-001 204001856001 | 1560-00-996-2134 | Fairlead, cable, Control | General Characteristics Item Description: Plastic, 1.53 in. lg, 0.980 in. W | Bell Helicopter Textron Inc. (97499) | |
| 204-001-856-1 2040018561 | 1560-00-996-2134 | Fairlead, cable, Control | General Characteristics Item Description: Plastic, 1.53 in. lg, 0.980 in. W | Bell Helicopter Textron Inc. (97499) | |
| 204-001-858-001 204001858001 | 1560-00-074-9014 | Cover, Access, Aircraft | Special Features: Two slots on horizontal centerline 0.021 in. from front and 1.750 in. from back, 3.400 in. nom backwidth, 2.020 in. front radius measured from point 4.980 in. from back Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5, T4 fed spec single material response | Bell Helicopter Textron Inc. (97499) | |
| 204-001-858-1 2040018581 | 1560-00-074-9014 | Cover, Access, Aircraft | Special Features: Two slots on horizontal centerline 0.021 in. from front and 1.750 in. from back, 3.400 in. nom backwidth, 2.020 in. front radius measured from point 4.980 in. from back Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5, T4 fed spec single material response | Bell Helicopter Textron Inc. (97499) | |
| 204-001-937-005 204001937005 | 1560-00-718-6478 | Horn Assembly, Elevator | General Characteristics Item Description: Aluminum alloy, QQ-A-601 | Bell Helicopter Textron Inc. (97499) | |
| 204-001-937-5 2040019375 | 1560-00-718-6478 | Horn Assembly, Elevator | General Characteristics Item Description: Aluminum alloy, QQ-A-601 | Bell Helicopter Textron Inc. (97499) | |
| 204-001-944-001 204001944001 | 1560-00-789-0913 | Idler Assembly, Elevator | III End Item Identification: Aircraft model UH1F | Bell Helicopter Textron Inc. (97499) | |
| 204-001-944-1 2040019441 | 1560-00-789-0913 | Idler Assembly, Elevator | III End Item Identification: Aircraft model UH1F | Bell Helicopter Textron Inc. (97499) | |
| 204-001-947-001 204001947001 | 1560-00-862-2783 | Bell Crank | Bore Diameter: 1.000 inches nominal Bore Length: 0.812 inches nominal Center to Center Distance Between Fulcrum and Arm End Hole/Slot/Ball: 3.870 inches nominal 1ST end | Bell Helicopter Textron Inc. (97499) | |
| 204-001-947-1 2040019471 | 1560-00-862-2783 | Bell Crank | Bore Diameter: 1.000 inches nominal Bore Length: 0.812 inches nominal Center to Center Distance Between Fulcrum and Arm End Hole/Slot/Ball: 3.870 inches nominal 1ST end | Bell Helicopter Textron Inc. (97499) |