FSC 1615 Helicopter Rotor Blades, Drive Mechanisms and Components: 1615-00-065-9155, 1615-00-068-6597, 1615-00-069-0093
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1615-00-065-9155 1615000659155 | S6135-66322-1 | Plug, Seal, Gear box | General Characteristics Item Description: Aluminum alloy QQ-A-225/6, anodized finish, 0.869 in. min 0.871 in. max O/a dia, 0.500 in. O/a lg, one end drilled 0.322 in. dia by 0.350 in. deep and tapped 3/8-24 UNF-3B by 0.287 in. deep | Sikorsky Aircraft Corporation (78286) | |
| 1615-00-065-9157 1615000659157 | S6137-66507-1 | Plug and Breather a | Sikorsky Aircraft Corporation (78286) | ||
| 1615-00-065-9158 1615000659158 | S6137-66507-3 | Breather | Special Features: Felt, MIL-F-5656, ty 5;FSC application data:gear box, transmission, helicopter Overall Height: 0.250 inches maximum Outside Diameter: 0.620 inches maximum | Sikorsky Aircraft Corporation (78286) | |
| 1615-00-065-9159 1615000659159 | S6137-66707-1 | Nut, Lock, Gear Assembly | General Characteristics Item Description: 4130 steel MIL-S-6758, 2.1875-16 thd, 3.312 in. od, 0.736 in. THK8 1/4-28 tapped holes equally spaced and parallel to bore | Sikorsky Aircraft Corporation (78286) McMellon Bros. Incorporated (05141) | |
| 1615-00-065-9165 1615000659165 | S6135-66658-1 | Adapter, Detector Plug | General Characteristics Item Description: Aluminum alloy, cadmium-plated, 0.734 in. min, 0.739 in. max O/a lg, hexagon shaped head 0.185 in. min, 0.190 in. max thk, 1.125 in. across flats, thd 3/4-16 unjf 3B, body 0.549 in. lg, thd 1-1/16-12 un 3A | Sikorsky Aircraft Corporation (78286) | |
| 1615-00-066-0285 1615000660285 | 114D3207-3 | Retainer Assembly, Bearing | General Characteristics Item Description: Steel, MIL-S-5000 comp 4340 cond F, cadmium-plated QQ-P-416 class 2, type 1 body, plastic, polycap inserts, dim., 1.000 in. nom O/a lg, 2.495 in. min, 2.496 in. max flange od, 0.380 in. nom flange W, 1.8125-16 unf class 3A external threads on body od by 0.620 in. lg, 0.515 in. square id, 1.520 in. nom id counterbore by 0.250 in. deep on left side, 8 slots equally spaced on flange face 0.125 in. W, two long lok inserts installed on od threads 90.0 deg apart, item used on engine and sync drive shafts | The Boeing Company (81205, 77272) | |
| 1615-00-068-3855 1615000683855 | 65101-11021-106 | Cover, Rotary Wing a | Sikorsky Aircraft Corporation (78286) | ||
| 1615-00-068-6565 1615000686565 | 114H6841-1 | Cover, Control Valve | III End Item Identification: CH-47 | The Boeing Company (77272) | |
| 1615-00-068-6574 1615000686574 | 114D1246-1 | Plug, Rotor Shaft | General Characteristics Item Description: Rubber, synthetic, molded MIL-R-6855 class 2, grade 80, dim., 3.940 in. nomod, 0.500 in. nom W, 3.340 in. nom id by 0.250 in. deep, od tapered to 3.840IN. nom dia, outside left and right corners rounded by 0.120 in. radius, inside corner rounded by 0.250 in. radius, all diameters on common centerlineconcentric to each other within 0.030 tir | The Boeing Company (77272) | |
| 1615-00-068-6585 1615000686585 | 114D6268-1 | Retainer, Pinion Bearing | General Characteristics Item Description: Steel AMS6359, comp 4340, surface treatment black oxide, MIL-C-13924, rockwell hardness rating C scale 50 TO53, dim., 6.132 in. nom O/a lg, 0.280 in.nom O/a thk, 1.050 in. nom O/a H, retainer bent 30 deg to left at 3.180 in. radius by 0.155 in. lg then rebentvertically, upper section drilled with two holes on 3.590 in. bolt circle radius, one hole 0.208 in. dia located 30 deg each side of vertical centerline, three holes located on 3.650 in. bolt circle radius, W/one hole 0.328 in. dia located on verticalcenterline and one hole 0.450 in. eachside of centerline | The Boeing Company (77272) | |
| 1615-00-068-6593 1615000686593 | 114D6269-1 | Retainer Assembly, Gear | General Characteristics Item Description: Magnesium alloy QQ-M-56 comp AZ91C-T6, surface treatment dichromate MIL-M-3171 type 3, dim., 7.560 in. nom O/a face W, 6.810 in. nom bolt circle dia 3.000 in. nom left side internal flange id, 0.160 in. nom internal flange W, 3.4985 in. min, 3.5015 in. max right side id, 1.460 in. nom O/a thickness, three holes 0.281 in. nom dia drilled at 0.0, 110.0 and 245.0 deg on 6.810 in. bolt circle dia, three pair of holes 0.281 in. dia for clinch nuts drilled at 65 and 80, 180 and 195, 295 and 315 deg on 6.810 in. bolt circle dia, retainer used on output gear, engine transmission | The Boeing Company (77272) | |
| 1615-00-068-6597 1615000686597 | A8299 | Vent, Breather | Eaton Aerospace LLC (97484) | ||
| 1615-00-068-6598 1615000686598 | 114D6253-1 | Deflector, Oil, Pinion Gear | General Characteristics Item Description: Steel, MIL-S-18729 comp 4130, shape modified l, dim., 4.200 in. nom O/a lg, 0.400 in. nom base W, 0.063 in. nom thk, 1.300 in. nom flat width, lower left and right corners cut at 28.0 degangle 0.400 in. from T0P W/center 1.380 in. lg, upper left and right corners cut inward toward center W/center 1.440 in. lg, one notch 0.620 in. from each end 0.240 in. W by 0.200 in. deepone hole 0.219 in. dia on each end 0.350 in. from front W/3.590 in. between centers, back bent upward at 0.570 in. from front at 120.0 deg angle | The Boeing Company (77272) | |
| 1615-00-068-6606 1615000686606 | 114D5249-1 | Baffle, Pinion Gear | General Characteristics Item Description: Aluminum alloy QQ-A-250/11 comp 6061-TO, surface treatment anodized per MIL-C-5541, shape, 270 deg conical collar, dim., 7.500 in. base od, 5.080 in. base id, 4.000 in. nom top id, 1.915 in. nom height, 0.063 in. material thickness, four mounting holes 0.218 in. min, 0.225 in. max dia drilled on 7.500 in. bolt circle dia, two holes on left side ofopening 50.0 deg above and below horizontal centerline, two holes adjacent to opening 60.0 deg above and below horizontal centerline, item used on combing transmission | The Boeing Company (77272) | |
| 1615-00-068-6607 1615000686607 | 114D5267-1 | Deflector, Oil, Pinion Gear | General Characteristics Item Description: Steel, MIL-S-18729 comp 4130, surface treatment black oxide MIL-C-13924, shape, modified l, dim., 4.350 in. nom O/a lg, 1.660 in. nom O/a flat W, 1.050 in. nom O/a bent W, 0.063 in. nom thk, 0.810 in. nom base width, two holes in base 0.218 in. min, 0.224 in. max dia 0.500 in. from front and 0.380 in. from each end W/3.594 in. distance between centers, upright section upwardat 0.810 in. from plate front at 115.0DEG angle, sides of upright section tapered at 45.0 deg angle W/2.250 in. W across top, base front center cut by 3.000 in. radius to 0.250 in. depth | The Boeing Company (77272) | |
| 1615-00-068-6618 1615000686618 | 114D5261-1 | Tube, Oil Transfer | General Characteristics Item Description: Aluminum alloy QQ-A-225/6 comp 2024-T4, surface treatment anodized per MIL-C-5541, dim., 0.875 in. min, 0.880 in. max lg, 0.623 in. min, 0.624 in. max od, 0.312 in. min, 0.319 in. max id, 0.150 in. nom od groove W both ends, 0.080 in. nom groove depth, 0.093 in. groove distance from each end, tube used on engine and combingng transmissions | The Boeing Company (77272) | |
| 1615-00-068-6624 1615000686624 | 540-011-119-23 | Plug, Retention Bolt | General Characteristics Item Description: Aluminum alloy QQ-A-225/6 comp 2024-T4, anodized MIL-A-8625, dim., 0.875IN. nom lg, 0.875-14 unf class 3A threads by 0.535 in. lg, 1.250 in. nom flange od, 0.090 in. nom flange W, 0.625IN. nom head od, 0.250 in. nom head height, 0.150 in. nom head slot depth by 0.080 in. W, one hole 0.190 in. dia drilled thru plug center, plug part of bolt, blade retention, main rotor | Bell Helicopter Textron Inc. (97499) | |
| 1615-00-068-6634 1615000686634 | 205-040-175-1 205-040-175-001 | 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) | |
| 1615-00-068-6635 1615000686635 | 205-040-004-003 205-040-004-3 | Driveshaft Assembly | Bell Helicopter Textron Inc. (97499) Ruag Aerospase Services GMBH (D0216) | ||
| 1615-00-069-0093 1615000690093 | 65110-07000-014 | Head, Rotary Rudder | III End Item Identification: HH-53B helicopter III Fsc Application Data: Helicopter drive mechanism III Reference Data and Literature: T.O. 3R1-3-4-4 | Sikorsky Aircraft Corporation (78286) |