Helicopter Rotor Blades, Drive Mechanisms and Components: 209-040-807-1, 209-060-743-1, 209-070-473-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 209-040-807-1 2090408071 | 1615-01-044-9769 | Fitting, Oil Cooler | General Characteristics Item Description: Aluminum alloy QQ-A-225/6, type 2024, temper T4, 2.940 in. lg, 2.175 in. W | Bell Helicopter Textron Inc. (97499) | |
| 209-040-826-101 209040826101 | 1615-01-464-3721 | Sleeve, Wear | III End Item Identification: AH-1W aircraft | Bell Helicopter Textron Inc. (97499) | |
| 209-040-915 209040915 | 1615-01-255-6218 | Jet Assembly, Oil, Transmitter | Bell Helicopter Textron Inc. (97499) | ||
| 209-040-915-101 209040915101 | 1615-01-255-6218 | Jet Assembly, Oil, Transmitter | Bell Helicopter Textron Inc. (97499) | ||
| 209-040-917-101 209040917101 | 1615-01-256-7466 | Retainer, Input Shaft | III End Item Identification: Aircraft model H-1 General Characteristics Item Description: Aluminum alloy 2024-T351, QQ-A-225/6 | Bell Helicopter Textron Inc. (97499) | |
| 209-040-917-103 209040917103 | 1615-01-256-7466 | Retainer, Input Shaft | III End Item Identification: Aircraft model H-1 General Characteristics Item Description: Aluminum alloy 2024-T351, QQ-A-225/6 | Bell Helicopter Textron Inc. (97499) | |
| 209-040-919-101 209040919101 | 1615-01-256-7472 | Housing Assembly, Gearbox | III End Item Identification: Helicopter model H-1 | Bell Helicopter Textron Inc. (97499) | |
| 209-060-400-5 2090604005 | 1615-00-837-1778 | Spinner Assembly, Ma | Bell Helicopter Textron Inc. (97499) | ||
| 209-060-720-1 2090607201 | 1615-00-089-9756 | Lever Assembly, Droo | Bell Helicopter Textron Inc. (97499) | ||
| 209-060-739-5 2090607395 | 1615-00-835-1457 | Rod Assembly, Droop | Bell Helicopter Textron Inc. (97499) | ||
| 209-060-743-1 2090607431 | 1615-00-834-6486 | Support, Droop Compensator | General Characteristics Item Description: Aluminum alloy MIL-A-21180 comp A356-T61, surface treatment chemical film bps FW4182, dim., 2.250 in. nom W, 2.800 in. nom lg, 2.810 in. nom O/a ht, twotriangular upright sections 0.880 in. apart 0.210 in. thk, two in-line holes 0.2500 in. dia drilled thru uprights 2.500 in. from base, three mounting holes 0.211 in. dia located on base corners 0.380 in. from edge W/1.500 in. C to C distance along W and 2.000 in. C to C along W, lower right corner REMOVED1.940 in. lg by 1.000 in. W | Bell Helicopter Textron Inc. (97499) | |
| 209-060-746-1 2090607461 | 1615-00-852-6712 | Shaft, Droop Compensator | General Characteristics Item Description: Steel MIL-S-6758 comp 4130 cond D4, cadmium-plated QQ-P-416 class 2 TYPE2, dim., 3.700 in. nom lg, 0.250-28 unf class 2A threaded left end od by 0.820IN. lg, 0.3740 in. min, 0.3745 in. max flange od by 0.1970 in. lg located 0.820 in. from left end, one rectangular flange 0.905 in. lg by 0.620 in. high BY0.190 in. W located 1.077 in. from left end, flange left end rounded by 0.570IN. radius, one hole 0.1207 in. dia drilled thru flange 0.670 in. from right end, 0.499 in. od by 1.750 in. lg following rectangular flange, one hole 0.193IN. dia drilled thru od 1.180 in. fromface, 0.2487 in. min, 0.2492 in. max right end od by 0.683 in. lg, item used oncontrol installation | Bell Helicopter Textron Inc. (97499) | |
| 209-060-747-1 2090607471 | 1615-00-834-6476 | Bracket Assembly, Droop Compensat | General Characteristics Item Description: Aluminum alloy QQ-A-200/3 comp 2024-T3, surface treatment chemical film bps FW4182, l-shaped bracket, dim., 1.680IN. nom upright lg, 1.240 in. nom upright W, 0.250 in. nom upright thk, top rounded by 0.620 in. radius, one center hole 0.7706 in. dia drilled thru UPRIGHT1.060 in. from base, NO.-209-060-731-1 sleeve and no. REST-4 bearing installed in hole, bracket base 1.820 in. W by 1.380 in. lg by 0.120 in. thk, two mounting holes 0.211 in. dia 0.420 in. from back 0.180 in. left of upright vertical centerline, 1.000 in. C to C distance between holes | Bell Helicopter Textron Inc. (97499) | |
| 209-060-748-1 2090607481 | 1615-00-852-6714 | Bracket Assembly, Droop Compensat | General Characteristics Item Description: Aluminum alloy MIL-A-21180 comp A356-T61, surface treatment chemical film bps FW4182, U-shaped bracket, dim., 1.530 in. O/a W, 2.580 in. back leg ht, 1.160 in. back leg W, 0.180 in. back leg thk, 1.750 in. front leg ht, 1.240 in. front leg W, 0.250 in. front leg thk, top rounded by 0.620 in. radius, front leg located at left end, back leg locatedat right end W/connecting web 1.750 in. high between legs, front leg drilled 1.130 in. from base W/0.7706 in. dia hole for no. 209-060-738-1 sleeve and no. RSST-4 bearing, back leg drilled W/two holes 0.211 in. dia 0.560 in. from base W/1.680 in. C to C distance between holes, back leg holes located 1.500 in. C to C distance from front leg hole | Bell Helicopter Textron Inc. (97499) | |
| 209-060-749-1 2090607491 | 1615-00-852-6716 | Support, Droop Control | General Characteristics Item Description: Aluminum alloy MIL-A-21180 comp A356-T61, surface treatment chemical film bps FW4182, dim., 4.500 in. O/a lg, 2.350 in. nom O/a ht, 3.020 in. nom O/abase W, front end of base rounded by 0.320 in. radius, two triangular upright sections 0.875 in. min, 0.880 in. max apart on right side of base 0.210 in. thk, two in-line holes 0.2500 in. dia drilled thru top center of upright section 0.960 in. from base right edge, three mounting holes in base on each corner 0.211 in. dia, two holes 2.250 in. C to C distance, front hole 4.180 in. C to C distance from back holes, one lightening hole 1.000 in. dia in base 2.340 in. from wide end on horizontal centerline | Bell Helicopter Textron Inc. (97499) | |
| 209-060-750-1 2090607501 | 1615-00-834-6480 | Arm Assembly, Droop Compensator | General Characteristics Item Description: Aluminum alloy ams 4218 comp A356-T6, surface treatment chemical film bps FW4182, dim., 5.120 in. nom O/a lg, 1.350 in. nom center W, 0.720 in. nom leftand right end W, 0.960 in. nom left andright end ht, 0.443 in. W between arm end tines, 0.980 in. tine depth, two in-line holes 0.1895 in. min, 0.1905 in. max dia thru arm end tines 0.360 in. from each end, 0.750 in. nom center ht, one thru center hole 0.8660 in. dia parallel to end holes, no. 120-015-4KA sleeve and one no. DW4 bearing installed in hole, 2.200 in. C to C distance between end and center holes | Bell Helicopter Textron Inc. (97499) | |
| 209-060-757-1 2090607571 | 1615-00-834-6480 | Arm Assembly, Droop Compensator | General Characteristics Item Description: Aluminum alloy ams 4218 comp A356-T6, surface treatment chemical film bps FW4182, dim., 5.120 in. nom O/a lg, 1.350 in. nom center W, 0.720 in. nom leftand right end W, 0.960 in. nom left andright end ht, 0.443 in. W between arm end tines, 0.980 in. tine depth, two in-line holes 0.1895 in. min, 0.1905 in. max dia thru arm end tines 0.360 in. from each end, 0.750 in. nom center ht, one thru center hole 0.8660 in. dia parallel to end holes, no. 120-015-4KA sleeve and one no. DW4 bearing installed in hole, 2.200 in. C to C distance between end and center holes | Bell Helicopter Textron Inc. (97499) | |
| 209-070-472-1 2090704721 | 1615-00-851-9108 | Fitting, Blower Wheel | General Characteristics Item Description: Aluminum alloy MIL-A-21180 comp A356 or comp A357, anodized bps FW4001 shape, flanged sleeve, dim., 1.811 in. nom O/a lg, 3.000 in. nom flange od by 0.125 in. nom thk, 1.503 in. min, 1.505 in. max flange 1ST step od by 0.125 in. thk, 1.160 in. body od, spline id data, sliding a side fit, 27 teeth by 1.811 in. lg, 32/64 diametral pitch, 0.8438 in.pitch dia, 0.8125 in. min, 0.8160 in. max minor dia, 0.8081 in. min, 0.8742 in. max major dia, four mounting holes on flange 0.269 in. dia located on 2.200 in. dia bolt circle, flange id counterbored to 0.922 in. dia by 0.786 in. nomdeep | Bell Helicopter Textron Inc. (97499) | |
| 209-070-472-3 2090704723 | 1615-00-459-4469 | Fitting, Blower Wheel | General Characteristics Item Description: Aluminum alloy MIL-A-21180 alloy A356 class 10 or QQ-A-225/6 alloy 2024-T351, anodized bps FW4001, shape, flanged sleeve, dim., 1.306 in. nom O/a lg, 3.000 in. nom flange od, 0.125 in. nom flange W, 1.503 in. min, 1.505 in. max 1ST step flange od, 0.125 in. nom 1ST step flange W, 1.160 in. nom body od, four equally spaced holes 0.268 in. dia drilled thru flange on 2.200 in. dia bolt circle, id spline data, side fit sliding a fillet or flat root, 27 teeth 1.306 in. lg, 32/64 diametral pitch, 0.8125 in.min, 0.8160 in. max minor dia, 0.8742 in. min, 0.9081 in. max major dia, 0.8438 in. pitch dia, item used as fitting from blower wheel to transmission | Bell Helicopter Textron Inc. (97499) | |
| 209-070-473-1 2090704731 | 1615-00-851-8935 | Adapter, Blower Housing | General Characteristics Item Description: Aluminum alloy QQ-A-250/5 comp 2024-TO, surface treatment chemical film bps FW4182, dim., 0.650 in. O/a lg, 7.600IN. nom flange od, 0.040 in. nom flangethk, 6.120 in. nom body od, 0.610 in. nom od lg, 4.000 in. nom id, 6.040 in. flange side id by 0.570 in. lg, six holes 0.268 in. dia equally spaced drilled thru flange face on 6.880 in. dia boltcircle W/hole at 270.0 deg slotted to flange edge, six holes 0.268 in. dia equally spaced drilled thru right body face on 5.000 in. dia bolt circle | Bell Helicopter Textron Inc. (97499) |