FSC 1615 Helicopter Rotor Blades, Drive Mechanisms and Components: 1615-00-471-3324, 1615-00-472-7294, 1615-00-475-0805

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NSNMFG SKUItem NameDetailsManufacturer (CAGE)RFQ
1615-00-471-3324
1615004713324
65351-11282-047Filler Neck and capIII End Item Identification: OH-54B
Special Features: Tube, filler assembly, main gear box
Sikorsky Aircraft Corporation (78286)

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1615-00-471-3325
1615004713325
369A1600-21Hub and Blade AssemMcDonnell Douglas Helicopter Co. Inc. (02731)
Boeing Company, The (8V613)

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1615-00-471-5918
1615004715918
212-010-403-5
212-010-403-005
Lever, Main RotorGeneral 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)

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1615-00-472-7292
1615004727292
114D3303-4Shaft Assembly, fanThe Boeing Company (77272, 81205)

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1615-00-472-7294
1615004727294
114R3131-8Seal Assembly, Slider ShaftGeneral 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)

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1615-00-472-7306
1615004727306
204-040-003-29Gearbox Assembly, Tail Rotor DrivIII 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)

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1615-00-472-7308
1615004727308
204-011-702-15
204-011-702-015
Blade, Rotary RudderIII End Item Identification: UH-1 series helicopters
Bell Helicopter Textron Inc. (97499)

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1615-00-472-7310
1615004727310
204-011-400-7Swashplate, ControllableSpecial Features: C/O approx 257 parts
End Item Identification: UH-1 series helicopters
Bell Helicopter Textron Inc. (97499)

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1615-00-472-7312
1615004727312
204-011-173-003
204-011-173-3
Counterweight, Main RotorGeneral 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)

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1615-00-474-0859
1615004740859
65358-07000-046Shaft Assy, PitchSikorsky Aircraft Corporation (78286)

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1615-00-474-8469
1615004748469
204-040-506-1Adapter, GearboxBell Helicopter Textron Inc. (97499)

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1615-00-474-9137
1615004749137
204-011-113-1
204-011-113-001
Strap set, Main RotorGeneral 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)

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1615-00-474-9139
1615004749139
204-011-115-1
204-011-115-001
Fitting, Strap RetenBell Helicopter Textron Inc. (97499)

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1615-00-474-9151
1615004749151
204-011-403-001
204-011-403-1
Ring Assembly, OuterGeneral 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)

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1615-00-474-9223
1615004749223
204-011-102-1
204-011-102-001
Yoke Assembly, MainBell Helicopter Textron Inc. (97499)

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1615-00-474-9224
1615004749224
204-011-105-1
204-011-105-001
Trunnion AssemblyGeneral 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)

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1615-00-474-9227
1615004749227
204-011-108-1BlockBell Helicopter Textron Inc. (97499)

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1615-00-474-9228
1615004749228
204-011-107-1RINGBell Helicopter Textron Inc. (97499)

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1615-00-475-0276
1615004750276
214-040-190-1Adapter, FlangeBell Helicopter Textron Inc. (97499)

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1615-00-475-0805
1615004750805
214-040-131-1Screen Assy, Pump inBell Helicopter Textron Inc. (97499)

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