Helicopter Rotor Blades, Drive Mechanisms and Components: HTC-H53-12DB-02H, IT-2123, K11352-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| HTC-H53-12DB-02H HTCH5312DB02H | 1615-01-531-6374 | Dampener, Vibration, Drive Shaft | III End Item Identification: H-53M/J helicopter Special Features: Is a heavy duty version, and replaces nsn 1615-01-465-0647, P/N HTC-H53-12DB-02 III Part Name Assigned By Controlling Agency: Vibration absorber H-53M/J | Hood Technology Corporation (0YRF8) | |
| ID2352 | 1615-01-296-3786 | Detector, Metallic Particle | Special Features: Accessory gearbox assy;oil flow 7 gpm at 40 psig;temp range -65/+295 deg f;fluids per MIL-L-7809 or MIL-L-23699;1.246 in. O/a dia End Item Identification: CH-53E acft Overall Length: 4.188 inches nominal | Eaton Aerospace LLC (97484) | |
| IELBSP2M | 1615-00-463-5444 | Ring Connector | IEC Corporation (16071) | ||
| IL2980-1 IL29801 | 1615-01-205-9407 | Lock Assembly, Helicopter | Marathonnorco Aerospace Inc. (08844) | ||
| IPTE-51GF-1000-100D IPTE51GF1000100D | 1615-01-563-0791 | Transducer, Torque P | Schweizer Aircraft Corp. (78103) | ||
| IT-2123 IT2123 | 1615-00-436-0523 | Tube, Oil Transfer, Oil Cooler | End Item Identification: H-53 aircraft Part Name Assigned BY Controlling Agency: Oil transfer tube, oil cooler, nose gearbox General Characteristics Item Description: C/O liner, nylon, 3.130 in. lg;cover, 3-PLY nylon, 3.130 in. LG;2 cuffs, 0.700 in. lg, 6-PLY NYLON;3 rings, cres, 0.060 in. dia located along lg of interior cover, 0.650 in. apart APPROX;1 flange, alum, 0.180 in. thk by 2.200 in. od by 0.794 in. id W/three 0.261 in. dia holes on 2.250 in. dia bolt CIRCLE;1 flange, alum, 0.794 in. id W/two holes 1.106 in. from center;exterior coating, silicone rubber, 3.130 in. LG;3.490 in. lg O/A;150.000 psi proof PRESSURE;300.000 psi burst pressure;temp range MINUS65.0 deg F to plus 350.0 deg F | Industrial Tube Company LLC (26831) | |
| J-1105 J1105 | 1615-01-221-5868 | Sleeve, Wear | Federal-Mogul Corp. (01212) | ||
| J-15256-14 J1525614 | 1615-01-157-1283 | No Item Name Available | III End Item Identification: AH-64 apache airframe | Lord Corporation (76005) | |
| J16822-1 J168221 | 1615-01-063-1268 | Strap, Tension, Main | End Item Identification: OH-58A and/or C, rotary wing aircraft | Lord Corporation (76005) | |
| J-16822-14 J1682214 | 1615-01-063-1268 | Strap, Tension, Main | End Item Identification: OH-58A and/or C, rotary wing aircraft | Lord Corporation (76005) | |
| J-16822-5 J168225 | 1615-01-063-1268 | Strap, Tension, Main | End Item Identification: OH-58A and/or C, rotary wing aircraft | Lord Corporation (76005) | |
| J-16881-1 J168811 | 1615-01-164-3758 | Support Assy, Rotor | Lord Corporation (76005) | ||
| J-17235-10 J1723510 | 1615-01-063-4015 | Strap Assembly | III End Item Identification: AH-1, rotary wing aircraft | Jonal Laboratories Incorporated (24664) | |
| J6410-7 J64107 | 1615-00-103-0559 | Damper Assy | Lord Corporation (76005) | ||
| JA14TA28-122-E9534 JA14TA28122E9534 | 1615-00-921-0665 | Roller Assembly, Droop Stop | General Characteristics Item Description: Aluminum alloy WW-T-785 or QQ-A-268 body, steel, corrosion resisting QQ-S-763 or AMS5630 roller, passivated per HP4-8, heat treated to rockwell hardness C scale 55 to 59, teflon, reinforced liner, dim., 0.875 in. nom body od, 1.400 in. nom od crown radius, 0.4375 in. min, 0.4385 in. max id, 0.376 in. min, 0.377 in. max O/a W, max surface finish, left and right ends 32 microinches aa, all other surfaces 125 microinches aa, item used on hub assembly, main rotor | RBC Aircraft Products Inc. (3NPS1) Timken Aerospace Inc. (21335) | |
| JASC0 | 1615-00-765-2407 | Plate, Coupling Retainer | General Characteristics Item Description: Aluminum alloy QQ-A-225/6 comp 2024-T4, anodized bps FW4001, dim., 0.590 in. nom lg, 1.360 in. nom left flange od by 0.140 in. thk, 1.080 in. nom bodyod, 0.266 in. nom id, 0.680 in. right idcounterbore by 0.355 in. deep, right end od reduced to 0.805 in. min, 0.810 in. max od by 0.150 in. lg, left end counterbored to 0.940 in. dia by 0.095 in.deep, item used on tail rotor drive | Steuby Mfg Co. Inc. (05116) | |
| JEHA1875750L | 1615-01-201-9620 | Lee jet | III End Item Identification: Aircraft model H-46 General Characteristics Item Description: Steel 17-4PH; 750 lohm rate; 0.800 in. lg | The LEE Company (92555) | |
| K10001 | 1615-01-320-6620 | Disc Pack Repair kit | III End Item Identification: Acft CH-53E | Miba Hydramechanica Corp. (66951) | |
| K1001 | 1615-01-320-6620 | Disc Pack Repair kit | III End Item Identification: Acft CH-53E | Miba Hydramechanica Corp. (66951) | |
| K11352-1 K113521 | 1615-01-424-3605 | Modification kit, Aircraft Components | Hamilton Sundstrand Corporation (73030) United Technologies Corp. (07148) |