Helicopter Rotor Blades, Drive Mechanisms and Components: 204-040-600-11, 204-040-603-9, 204-040-614-3
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 204-040-600-11 20404060011 | 1615-01-056-5365 | Hanger Assembly, Dri | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 204-040-600-7 2040406007 | 1615-00-766-8578 | Hanger Assembly, Dri | Bell Helicopter Textron Inc. (97499) Ruag Aerospase Services GMBH (D0216) | ||
| 204-040-600-9 2040406009 | 1615-00-832-8951 | Hanger Assembly, Dri | Bell Helicopter Textron Inc. (97499) Ruag Aerospase Services GMBH (D0216) | ||
| 204-040-603-007 204040603007 | 1615-00-791-6073 | Coupling, Male Spherical | General Characteristics Item Description: Steel AMS6260, cadmium-plated QQ-P-416 class 2 type 2, casehardened spherical spline teeth, dim., 1.870 in. min, 1.880 in. max O/a lg, 1.591 in. min, 1.597 in. max od, 1.375 in. min, 1.377 in. max flange end id by 1.170 in. lg, leftend spherical spline teeth located 0.130 in. from left end, 32 teeth 0.200 in. lg, 16 diametral pitch, 20.0 deg pressure angle, 2.000 in. pitch dia, 1.842 in. min, 1.852 in. max minor dia, 2.0990 in. min, 2.1010 in. max major dia, 0.1963IN. circular pitch, 0.107 in. circular tooth thk, right end id involute splinedata, 24 teeth 0.605 in. lg, 20/30 diametral pitch, 30.0 deg pressure angle, 0.1571 in. circular pitch, 1.200 in. pitchdia, 1.295 in. min, 1.315 in. max minor dia, 1.133 in. min, 1.138 in. max dia, item used on drive shaft tail rotor drive | Bell Helicopter Textron Inc. (97499) | |
| 204-040-603-009 204040603009 | 1615-00-523-9770 | Spherical Drive Shaft, Tail Rotor | III End Item Identification: Bell helicopter uhin Special Features: 32 gear teeth, 2.000 in. pitch dia; 0.105 in. circular tooth thk, pressure angle 20 deg; internal involute splines; 2.075 in. lg O/a; one end 1.575 in. dia; other end 1.954 in. dia Material: Steel | Bell Helicopter Textron Inc. (97499) | |
| 204-040-603-5 2040406035 | 1615-00-239-3809 | Coupling, Spherical | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-603-7 2040406037 | 1615-00-791-6073 | Coupling, Male Spherical | General Characteristics Item Description: Steel AMS6260, cadmium-plated QQ-P-416 class 2 type 2, casehardened spherical spline teeth, dim., 1.870 in. min, 1.880 in. max O/a lg, 1.591 in. min, 1.597 in. max od, 1.375 in. min, 1.377 in. max flange end id by 1.170 in. lg, leftend spherical spline teeth located 0.130 in. from left end, 32 teeth 0.200 in. lg, 16 diametral pitch, 20.0 deg pressure angle, 2.000 in. pitch dia, 1.842 in. min, 1.852 in. max minor dia, 2.0990 in. min, 2.1010 in. max major dia, 0.1963IN. circular pitch, 0.107 in. circular tooth thk, right end id involute splinedata, 24 teeth 0.605 in. lg, 20/30 diametral pitch, 30.0 deg pressure angle, 0.1571 in. circular pitch, 1.200 in. pitchdia, 1.295 in. min, 1.315 in. max minor dia, 1.133 in. min, 1.138 in. max dia, item used on drive shaft tail rotor drive | Bell Helicopter Textron Inc. (97499) Equitable Engineering Company Inc. (11867) Precision Gear Incorporated (21540) SPX Corporation (82001) U S Army Aviation and Missile (81996) | |
| 204-040-603-9 2040406039 | 1615-00-523-9770 | Spherical Drive Shaft, Tail Rotor | III End Item Identification: Bell helicopter uhin Special Features: 32 gear teeth, 2.000 in. pitch dia; 0.105 in. circular tooth thk, pressure angle 20 deg; internal involute splines; 2.075 in. lg O/a; one end 1.575 in. dia; other end 1.954 in. dia Material: Steel | Bell Helicopter Textron Inc. (97499) Equitable Engineering Company Inc. (11867) Precision Gear Incorporated (21540) SPX Corporation (82001) | |
| 204-040-604-005 204040604005 | 1615-00-701-4142 | Coupling Driveshaft | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 204-040-604-005S 204040604005S | 1615-00-701-4142 | Coupling Driveshaft | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 204-040-604-5 2040406045 | 1615-00-701-4142 | Coupling Driveshaft | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 204-040-607-003 204040607003 | 1615-00-765-2406 | Retainer, Helical Compression Spr | Overall Height: 1.800 inches nominal Material: Aluminum alloy, QQ-A-225/6, alloy 2024 Mounting Hole Diameter: 0.073 inches nominal | Bell Helicopter Textron Inc. (97499) | |
| 204-040-607-007 204040607007 | 1615-00-401-6196 | Retainer, Driveshaft | Special Features: Bore dia 0.880 in. depth of bore, W/hex protrusion 0.500 in. across flats 0.500 in. lg, one groove 0.188 in. W 0.114 in. dp Material: Aluminum alloy Overall Length: 1.600 inches nominal | Bell Helicopter Textron Inc. (97499) | |
| 204-040-607-3 2040406073 | 1615-00-765-2406 | Retainer, Helical Compression Spr | Overall Height: 1.800 inches nominal Material: Aluminum alloy, QQ-A-225/6, alloy 2024 Mounting Hole Diameter: 0.073 inches nominal | Bell Helicopter Textron Inc. (97499) | |
| 204-040-607-5 2040406075 | 1615-01-034-7858 | Retainer, Spring | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-607-7 2040406077 | 1615-00-401-6196 | Retainer, Driveshaft | Special Features: Bore dia 0.880 in. depth of bore, W/hex protrusion 0.500 in. across flats 0.500 in. lg, one groove 0.188 in. W 0.114 in. dp Material: Aluminum alloy Overall Length: 1.600 inches nominal | Bell Helicopter Textron Inc. (97499) | |
| 204-040-610-001 204040610001 | 1615-00-701-4144 | Plate Assembly, Tail Rotor Drive | General Characteristics Item Description: Aluminum alloy QQ-A-225/6 comp 2024-T4 or QQ-A-355 comp 2024-T4, anodized, rubber MIL-R-6855 comp buna N seal, dim., 2.372 in. min, 2.374 in. max od, 0.125 in. od W, right face surface flat, left face raised surface 0.189 in. W by 2.120 in. od, 2.000 in. id, center raised surface on left face 0.380 in. W by 0.300 in. dia W/one thru center HOLE0.040 in. dia, rubber seal 2.373 in. od, 2.120 in. id by 0.092 in. W bonded toleft face, item used on drive shaft coupling | Bell Helicopter Textron Inc. (97499) | |
| 204-040-610-1 2040406101 | 1615-00-701-4144 | Plate Assembly, Tail Rotor Drive | General Characteristics Item Description: Aluminum alloy QQ-A-225/6 comp 2024-T4 or QQ-A-355 comp 2024-T4, anodized, rubber MIL-R-6855 comp buna N seal, dim., 2.372 in. min, 2.374 in. max od, 0.125 in. od W, right face surface flat, left face raised surface 0.189 in. W by 2.120 in. od, 2.000 in. id, center raised surface on left face 0.380 in. W by 0.300 in. dia W/one thru center HOLE0.040 in. dia, rubber seal 2.373 in. od, 2.120 in. id by 0.092 in. W bonded toleft face, item used on drive shaft coupling | Bell Helicopter Textron Inc. (97499) | |
| 204-040-614-003 204040614003 | 1615-00-765-2417 | Coupling, Hanger | General Characteristics Item Description: Steel MIL-S-5626 comp 4140 cond C1, cadmium-plated bps FW4006 class C type 1, dim., 2.221 in. min, 2.223 in. max O/a lg, 3.625 in. nom left end od by 0.155 in. thk, 3.000 in. nom left end id, 1.614 in. nom right end od by 0.605 in. lg, sides tapered at 27.0 deg angle, left end flange face fixed curvic coupling teeth, 30 teeth 0.312 in. lg by 0.062 in. high, 30.0 deg pressure angle to mate W/concave teeth on 204-040-605, right end id spline data, 24 teeth 0.610 in. lg, 20/30 diametral pitch, 0.1571IN. circular pitch, 30.0 deg pressure angle, 1.200 in. pitch dia, 1.133 in. min, 1.138 in. max minor dia, 1.295 in. min, 1.315 in. max major dia, item used ontail rotor drive | Bell Helicopter Textron Inc. (97499) | |
| 204-040-614-3 2040406143 | 1615-00-765-2417 | Coupling, Hanger | General Characteristics Item Description: Steel MIL-S-5626 comp 4140 cond C1, cadmium-plated bps FW4006 class C type 1, dim., 2.221 in. min, 2.223 in. max O/a lg, 3.625 in. nom left end od by 0.155 in. thk, 3.000 in. nom left end id, 1.614 in. nom right end od by 0.605 in. lg, sides tapered at 27.0 deg angle, left end flange face fixed curvic coupling teeth, 30 teeth 0.312 in. lg by 0.062 in. high, 30.0 deg pressure angle to mate W/concave teeth on 204-040-605, right end id spline data, 24 teeth 0.610 in. lg, 20/30 diametral pitch, 0.1571IN. circular pitch, 30.0 deg pressure angle, 1.200 in. pitch dia, 1.133 in. min, 1.138 in. max minor dia, 1.295 in. min, 1.315 in. max major dia, item used ontail rotor drive | Bell Helicopter Textron Inc. (97499) |