Helicopter Rotor Blades, Drive Mechanisms and Components: 205-040-138-001, 205-040-200-1, 205-040-256-005
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 205-040-138-001 205040138001 | 1615-00-992-6474 | Plate, Oil cap, Trans | Bell Helicopter Textron Inc. (97499) | ||
| 205-040-138-1 2050401381 | 1615-00-992-6474 | Plate, Oil cap, Trans | Bell Helicopter Textron Inc. (97499) | ||
| 205-040-175-001 205040175001 | 1615-00-068-6634 | Retainer, Grease, Drive Shaft | General Characteristics Item Description: Aluminum alloy, QQ-A-225/6, anodized MIL-A-8625, dim., 5.1785 in. min, 5.1805 in. max od, 0.305 in. min, 0.308 in. max od width, 0.646 in. nom O/a wright side center raised surface 1.281 in. od by 0.500 in. high, counterboredto 1.000 in. dia by 0.375 in. deep, right side counterbored to 4.730 in. diaby 0.155 in. deep around raised surface, left side center counterbored TO1.000 in. dia by 0.104 in. deep, od center-grooved 0.125 in. W by 5.024 in.dia, max surface finish, all surfaces 63 microinches aa, fluorescent penetrantinspected per bps 4069 bell helicopter co | Bell Helicopter Textron Inc. (97499) | |
| 205-040-175-1 2050401751 | 1615-00-068-6634 | Retainer, Grease, Drive Shaft | General Characteristics Item Description: Aluminum alloy, QQ-A-225/6, anodized MIL-A-8625, dim., 5.1785 in. min, 5.1805 in. max od, 0.305 in. min, 0.308 in. max od width, 0.646 in. nom O/a wright side center raised surface 1.281 in. od by 0.500 in. high, counterboredto 1.000 in. dia by 0.375 in. deep, right side counterbored to 4.730 in. diaby 0.155 in. deep around raised surface, left side center counterbored TO1.000 in. dia by 0.104 in. deep, od center-grooved 0.125 in. W by 5.024 in.dia, max surface finish, all surfaces 63 microinches aa, fluorescent penetrantinspected per bps 4069 bell helicopter co | Bell Helicopter Textron Inc. (97499) | |
| 205-040-176-101 205040176101 | 1615-01-107-1788 | Boot Assembly | Bell Helicopter Textron Inc. (97499) | ||
| 205-040-178-001 205040178001 | 1615-00-076-1486 | Coupling, Main Driveshaft | General Characteristics Item Description: Steel, AMS6490 comp M-50 per bell spec 299-947-087, cadmium-plated QQ-P-416 class 2 type 2, gear teeth and splines casehardened, rockwell hardness rating C scale 42 to 46 body core hardness, dim., 2.223 in. min, 2.225 in. O/a lg, 6.500 in. nom left flange od, 0.080 in. flange top W, 6.125 in. nom right flange od, 0.162 in. nom right flange W, 5.730 in. nom od W/seven grooves 5.560 in. dia and groove sides at 45.0 deg angle, right face gear data, 60 teeth, 12 diametral pitch, 20.0 deg pressure angle, 5.000 in. pitch dia, 4.883 in. min, 4.886 in. minor dia, 5.1715 in. min, 5.1750 in. max major dia, id involute spline data, 4.883 in. min, 4.886 in. max line dia, 1.224 in. nom spline lg, 16.21 deg minor dia, 26.40 deg major dia, eight equally spaced threaded holes 0.250-28 unf class 1B on 6.000 in. bolt circle dia on left flange | Bell Helicopter Textron Inc. (97499) | |
| 205-040-178-1 2050401781 | 1615-00-076-1486 | Coupling, Main Driveshaft | General Characteristics Item Description: Steel, AMS6490 comp M-50 per bell spec 299-947-087, cadmium-plated QQ-P-416 class 2 type 2, gear teeth and splines casehardened, rockwell hardness rating C scale 42 to 46 body core hardness, dim., 2.223 in. min, 2.225 in. O/a lg, 6.500 in. nom left flange od, 0.080 in. flange top W, 6.125 in. nom right flange od, 0.162 in. nom right flange W, 5.730 in. nom od W/seven grooves 5.560 in. dia and groove sides at 45.0 deg angle, right face gear data, 60 teeth, 12 diametral pitch, 20.0 deg pressure angle, 5.000 in. pitch dia, 4.883 in. min, 4.886 in. minor dia, 5.1715 in. min, 5.1750 in. max major dia, id involute spline data, 4.883 in. min, 4.886 in. max line dia, 1.224 in. nom spline lg, 16.21 deg minor dia, 26.40 deg major dia, eight equally spaced threaded holes 0.250-28 unf class 1B on 6.000 in. bolt circle dia on left flange | Bell Helicopter Textron Inc. (97499) | |
| 205-040-179-1 2050401791 | 1615-00-438-6633 | Tube Assy, Filler Ne | Bell Helicopter Textron Inc. (97499) | ||
| 205-040-200-001 205040200001 | 1615-00-987-5152 | Quill Assembly, Tran | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 205-040-200-1 2050402001 | 1615-00-987-5152 | Quill Assembly, Tran | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 205-040-229-3 2050402293 | 1615-01-335-7548 | Sun Gear, Lower | Bell Helicopter Textron Inc. (97499) | ||
| 205-040-231-005 205040231005 | 1615-00-235-5472 | Ring Gear Assy | III End Item Identification: AH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 205-040-231-009S 205040231009S | 1615-01-149-2017 | Ring Gear Assembly | III End Item Identification: Aircraft model AH-1J, UH-1N | Bell Helicopter Textron Inc. (97499) | |
| 205-040-231-5 2050402315 | 1615-00-235-5472 | Ring Gear Assy | III End Item Identification: AH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 205-040-231-9 2050402319 | 1615-01-149-2017 | Ring Gear Assembly | III End Item Identification: Aircraft model AH-1J, UH-1N | Bell Helicopter Textron Inc. (97499) | |
| 205-040-236-001 205040236001 | 1615-00-071-8760 | Lockwasher, Transmission | General Characteristics Item Description: Steel, MIL-S-5626 comp 4140 or AMS6413 or AMS6415, black oxide COATEDMIL-C-13924, dim., 1.297 in. nom O/a lg, 4.260 in. min, 4.264 in. max id, 0.830IN. min, 0.835 in. max id lg, 4.380 in. nom od, 0.875 in. min, 0.880 in. max odlg, 6.000 in. nom flange od, 0.420 in. nom flange W, id internal spline DATA40 teeth, 0.125 in. face W, 10/20 diametral pitch, 30 deg pressure angle, 0.3142CIRCULAR pitch, 4.000 in. pitch dia, flange id internal spline data, 44 TEETH0.215 face W, 8/16 diametral pitch, 30 deg pressure angle, 0.3927 in. circularpitch, 5.500 in. pitch dia, six equally spaced slots on flange face 0.187 in.W by 30 deg lg on 4.800 in. bolt circle, one internal groove on flange idcorner 0.125 in. W by 5.775 in. dia, magnetic particle inspected, MAGNAFLUXEDBPS4075, bell helicopter co | Bell Helicopter Textron Inc. (97499) | |
| 205-040-236-1 2050402361 | 1615-00-071-8760 | Lockwasher, Transmission | General Characteristics Item Description: Steel, MIL-S-5626 comp 4140 or AMS6413 or AMS6415, black oxide COATEDMIL-C-13924, dim., 1.297 in. nom O/a lg, 4.260 in. min, 4.264 in. max id, 0.830IN. min, 0.835 in. max id lg, 4.380 in. nom od, 0.875 in. min, 0.880 in. max odlg, 6.000 in. nom flange od, 0.420 in. nom flange W, id internal spline DATA40 teeth, 0.125 in. face W, 10/20 diametral pitch, 30 deg pressure angle, 0.3142CIRCULAR pitch, 4.000 in. pitch dia, flange id internal spline data, 44 TEETH0.215 face W, 8/16 diametral pitch, 30 deg pressure angle, 0.3927 in. circularpitch, 5.500 in. pitch dia, six equally spaced slots on flange face 0.187 in.W by 30 deg lg on 4.800 in. bolt circle, one internal groove on flange idcorner 0.125 in. W by 5.775 in. dia, magnetic particle inspected, MAGNAFLUXEDBPS4075, bell helicopter co | Bell Helicopter Textron Inc. (97499) | |
| 205-040-237-001 205040237001 | 1615-00-128-1660 | Deflector, Dirt and Liquid | Special Features: Item used on main input trans Style Designator: 10 round, stepped Material: Steel, MIL-S-18729, comp 4130 | Bell Helicopter Textron Inc. (97499) | |
| 205-040-237-1 2050402371 | 1615-00-128-1660 | Deflector, Dirt and Liquid | Special Features: Item used on main input trans Style Designator: 10 round, stepped Material: Steel, MIL-S-18729, comp 4130 | Bell Helicopter Textron Inc. (97499) | |
| 205-040-256-005 205040256005 | 1615-00-488-5025 | Plate, Shim | Bell Helicopter Textron Inc. (97499) |