FSC 1615 Helicopter Rotor Blades, Drive Mechanisms and Components: 1615-00-471-3324, 1615-00-472-7294, 1615-00-475-0805
NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
1615-00-471-3324 1615004713324 | 65351-11282-047 | Filler Neck and cap | III End Item Identification: OH-54B Special Features: Tube, filler assembly, main gear box | Sikorsky Aircraft Corporation (78286) | |
1615-00-471-3325 1615004713325 | 369A1600-21 | Hub and Blade Assem | McDonnell Douglas Helicopter Co. Inc. (02731) Boeing Company, The (8V613) | ||
1615-00-471-5918 1615004715918 | 212-010-403-5 212-010-403-005 | Lever, Main Rotor | General Characteristics Item Description: C/O lever;pin;steel fitting;steelbearing and NAMEPLATE;18.273 in. lg approx by 3.250 in. hgt approx O/a | Bell Helicopter Textron Inc. (97499) | |
1615-00-472-7292 1615004727292 | 114D3303-4 | Shaft Assembly, fan | The Boeing Company (77272, 81205) | ||
1615-00-472-7294 1615004727294 | 114R3131-8 | Seal Assembly, Slider Shaft | General Characteristics Item Description: Aluminum alloy QQ-A-362 alloy 2024-T3 plate, anodized MIL-C-5541, rubber, synthetic MIL-R-7362 type 2 seal, dim., 11.080 in. nom plate extensions by 42.0 deg W 180.0 deg apart, 10.530 in. nom plate od, 0.250 in. nom plate thk, 7.000 in. nom plate id, 8.500 in. nom seal od, 6.500 in. nom seal id, 0.125 in. nom seal thk, 9.610 in. nom plate bolt circle dia, 7.750 in. nom seal bolt circle dia, seal riveted to plate by 8 equally spaced rivets, 10 mounting holes irregularly spaced on plate 0.312 in. dia W/no. 2 locating hole 0.834 in. left of vertical centerline and 4.731 in. above horizontal centerline | The Boeing Company (81205, 77272) | |
1615-00-472-7306 1615004727306 | 204-040-003-29 | Gearbox Assembly, Tail Rotor Driv | III End Item Identification: UH-1 airframe unit power train III Part Name Assigned By Controlling Agency: Gear box assembly 42 tail rotor drive | Bell Helicopter Textron Inc. (97499) | |
1615-00-472-7308 1615004727308 | 204-011-702-15 204-011-702-015 | Blade, Rotary Rudder | III End Item Identification: UH-1 series helicopters | Bell Helicopter Textron Inc. (97499) | |
1615-00-472-7310 1615004727310 | 204-011-400-7 | Swashplate, Controllable | Special Features: C/O approx 257 parts End Item Identification: UH-1 series helicopters | Bell Helicopter Textron Inc. (97499) | |
1615-00-472-7312 1615004727312 | 204-011-173-003 204-011-173-3 | Counterweight, Main Rotor | General Characteristics Item Description: Steel, QQ-S-633 comp 1018 cond B4 or cold finished or comp 1112 cond byor cold finished, cadmium-plated QQ-P-416, dim., 3.970 in. min, 3.990 in. max OD0.880 in. min, 0.900 in. max id, 1.810 in. min, 1.830 in. max O/a lg, idcounterbored to 2.000 in. dia by 0.570 in. deep, counterbore chamfered 0.300IN. deep by 45 deg, id chamfered 0.090 in. deep by 45 deg both sides, odreduced to 1.850 in. dia by 0.100 in. deep on side opposite counterboremax surface finish, all surfaces 125 microinches aa | Bell Helicopter Textron Inc. (97499) | |
1615-00-474-0859 1615004740859 | 65358-07000-046 | Shaft Assy, Pitch | Sikorsky Aircraft Corporation (78286) | ||
1615-00-474-8469 1615004748469 | 204-040-506-1 | Adapter, Gearbox | Bell Helicopter Textron Inc. (97499) | ||
1615-00-474-9137 1615004749137 | 204-011-113-1 204-011-113-001 | Strap set, Main Rotor | General Characteristics Item Description: Steel, corrosion resisting, MIL-S-5059 comp 301, 2B or 2D finish, laminated, dim., 1.000 in. nom O/a thk, 0.600 in. nom inner thk, 0.020 in. nom thk lamination, 20 no. 204-011-113-5 outer laminations, 18.275 in. nom O/a lg W/1.660 in. end radius, 2.260 in. nom center W, 32 no. 204-011-113-3 inner laminations, 19.320 in. nom O/a lg W/1.137 in. end radius, 2.890 in. nom center W, 1.1250 in. min, 1.1255 in. max dia hole drilled thru each end 16.000 in. nom C to C distance | Bell Helicopter Textron Inc. (97499) | |
1615-00-474-9139 1615004749139 | 204-011-115-1 204-011-115-001 | Fitting, Strap Reten | Bell Helicopter Textron Inc. (97499) | ||
1615-00-474-9151 1615004749151 | 204-011-403-001 204-011-403-1 | Ring Assembly, Outer | General Characteristics Item Description: Aluminum alloy QQ-A-601 alloy 356-T6, anodized bps FW4001, dim., 14.500 in. nom O/a od, 3.072 in. nom O/a lg, 10.427 in. min, 10.430 in. max top id, 10.250 in. min, 10.252 in. max top liner id no. 204-011-425-1, two thru holes 1.2495 in. min, 1.2510 in. max dia drilled thru od 1.025 in. from bottom at 45 AND225.0 deg, top face drilled and tapped W/12 0.312-18 unc class 3B threads on 11.125 in. bolt circle dia, no. SF101-93A11A studs threaded into holes | Bell Helicopter Textron Inc. (97499) U S Army Aviation and Missile (81996) | |
1615-00-474-9223 1615004749223 | 204-011-102-1 204-011-102-001 | Yoke Assembly, Main | Bell Helicopter Textron Inc. (97499) | ||
1615-00-474-9224 1615004749224 | 204-011-105-1 204-011-105-001 | Trunnion Assembly | General Characteristics Item Description: Steel, MIL-S-5000 comp 4340, cadmium-plated QQ-P-416 class 1 type 2, dim., 9.000 in. nom O/a lg, 5.200 in. nom center W, 3.000 in. nom center ht, 2.2499 in. min, 2.2505 in. max left and right emd od by 1.600 in. nom od lg, 1.125 in. nom left and right end id by 1.780 in. lg, 1.501 in. nom left and right end id counterbore dia by 1.000 in. lg, center involute spline data, fillet root spline, side bearing sliding class a fit, 38 teeth, 10/20 diametral pitch, 30.0 deg pressure angle, 3.800 in. pitch dia, 3.9800 in. min, 3.9950 in. max major dia, 3.7000 in. min, 3.7025 in. max major dia, one external slot parallel to splines on each side on center saction 1.000 in. W by 0.315 in. deep | Bell Helicopter Textron Inc. (97499) | |
1615-00-474-9227 1615004749227 | 204-011-108-1 | Block | Bell Helicopter Textron Inc. (97499) | ||
1615-00-474-9228 1615004749228 | 204-011-107-1 | RING | Bell Helicopter Textron Inc. (97499) | ||
1615-00-475-0276 1615004750276 | 214-040-190-1 | Adapter, Flange | Bell Helicopter Textron Inc. (97499) | ||
1615-00-475-0805 1615004750805 | 214-040-131-1 | Screen Assy, Pump in | Bell Helicopter Textron Inc. (97499) |