Helicopter Rotor Blades, Drive Mechanisms and Components: 205-040-004-021, 205-040-124-1, 205-040-136-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 205-040-004-021 205040004021 | 1615-01-014-6005 | Drive Assembly, Inpu | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 205-040-004-101 205040004101 | 1615-01-318-5677 | Drive Shaft, Helicop | Bell Helicopter Textron Inc. (97499) | ||
| 205-040-004-19 20504000419 | 1615-01-433-6233 | Drive Shaft Assembly, Rotary Wing | III End Item Identification: AH-1 , rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 205-040-004-21 20504000421 | 1615-01-014-6005 | Drive Assembly, Inpu | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 205-040-004-3 2050400043 | 1615-00-068-6635 | Driveshaft Assembly | Bell Helicopter Textron Inc. (97499) Ruag Aerospase Services GMBH (D0216) | ||
| 205-040-004-5 2050400045 | 1615-01-434-0781 | Drive Shaft Assembly, Rotary Wing | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 205-040-004-7 2050400047 | 1615-00-103-7298 | Drive Shaft Assembly, Tail Rotor | General Characteristics Item Description: Drive shaft 1;SPRING 4;NUT 2;4 packing PREFORM;4 COUPLING;4 RETAINER;2 LUBRICANT;2 RING;2 BOOT;16 BOLT;16 WASHER;2 plate;lockwire and adhesive | Bell Helicopter Textron Inc. (97499) | |
| 205-040-110-001 205040110001 | 1615-00-077-8762 | Cap, Idler Gearshaft | General Characteristics Item Description: Aluminum alloy QQ-A-225/6, ANOD1ZED bps FW4001, dim., 1.300 in. nom head dia, 0.200 in. nom head thk, 0.648 in. min, 0.658 in. max body od, 0.520 in.nom body id by 0.200 in. lg, center hole drilled in head 0.266 in. dia thru 0.200 in. deep, cap used on generator drive, transmissions | Bell Helicopter Textron Inc. (97499) | |
| 205-040-110-003 205040110003 | 1615-00-077-8758 | Cap, Idler Gearshaft | Bell Helicopter Textron Inc. (97499) | ||
| 205-040-110-1 2050401101 | 1615-00-077-8762 | Cap, Idler Gearshaft | General Characteristics Item Description: Aluminum alloy QQ-A-225/6, ANOD1ZED bps FW4001, dim., 1.300 in. nom head dia, 0.200 in. nom head thk, 0.648 in. min, 0.658 in. max body od, 0.520 in.nom body id by 0.200 in. lg, center hole drilled in head 0.266 in. dia thru 0.200 in. deep, cap used on generator drive, transmissions | Bell Helicopter Textron Inc. (97499) | |
| 205-040-110-3 2050401103 | 1615-00-077-8758 | Cap, Idler Gearshaft | Bell Helicopter Textron Inc. (97499) | ||
| 205-040-124-001 205040124001 | 1615-00-944-7287 | Adapter, cap Assembl | Bell Helicopter Textron Inc. (97499) | ||
| 205-040-124-1 2050401241 | 1615-00-944-7287 | Adapter, cap Assembl | Bell Helicopter Textron Inc. (97499) | ||
| 205-040-125-11 20504012511 | 1615-00-488-5021 | Plate, Shim | Bell Helicopter Textron Inc. (97499) | ||
| 205-040-134-001 205040134001 | 1615-00-888-3160 | Housing Assembly, Pl | III End Item Identification: UH-1 rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 205-040-134-1 2050401341 | 1615-00-888-3160 | Housing Assembly, Pl | III End Item Identification: UH-1 rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 205-040-135-001 205040135001 | 1615-00-475-2533 | Jet Lubricator, Transmission | General Characteristics Item Description: Steel, MIL-S-6758, cadmium-plated QQ-P-416 type 2 class 2, dim., jet tube, 1.370 in. nom lg, 0.513 in. nom base od, 0.678 in. nom flange od, 0.350 in. nom flange W, 0.132 in. nom flange center-groove W, 0.750 in. nom tip lg, 0.285 in. nom tip od, 0.125 in. nom tip id, 0.312 in. nom base id, tip chamfered 0.150 in. lg by 60.0 deg, two holes 0.042 in. nom dia drilled 180.0 deg apart on tip chamfer, one hole 0.053 in. nom dia drilled thru tip center, steel bar adapter 1.045 in. lg by 0.750 in. nom od W/left top section chamfered 45.0 deg by 0.707 in. lg, bottom drilled for 0.250 in. tube fitting 0.640 in. deep, boss per AND10050, top right od, opposite chamfer, drilled 0.500 in. dia by 0.156 in. deep, jet silver-brazed to top opening | Bell Helicopter Textron Inc. (97499) | |
| 205-040-135-1 2050401351 | 1615-00-475-2533 | Jet Lubricator, Transmission | General Characteristics Item Description: Steel, MIL-S-6758, cadmium-plated QQ-P-416 type 2 class 2, dim., jet tube, 1.370 in. nom lg, 0.513 in. nom base od, 0.678 in. nom flange od, 0.350 in. nom flange W, 0.132 in. nom flange center-groove W, 0.750 in. nom tip lg, 0.285 in. nom tip od, 0.125 in. nom tip id, 0.312 in. nom base id, tip chamfered 0.150 in. lg by 60.0 deg, two holes 0.042 in. nom dia drilled 180.0 deg apart on tip chamfer, one hole 0.053 in. nom dia drilled thru tip center, steel bar adapter 1.045 in. lg by 0.750 in. nom od W/left top section chamfered 45.0 deg by 0.707 in. lg, bottom drilled for 0.250 in. tube fitting 0.640 in. deep, boss per AND10050, top right od, opposite chamfer, drilled 0.500 in. dia by 0.156 in. deep, jet silver-brazed to top opening | Bell Helicopter Textron Inc. (97499) | |
| 205-040-136-001 205040136001 | 1615-00-992-6473 | Cap Assembly, Transmission | III End Item Identification: UH-1 airframe unit powertrain III Part Name Assigned By Controlling Agency: Cap oil filler extension transmission assembly of | Bell Helicopter Textron Inc. (97499) | |
| 205-040-136-1 2050401361 | 1615-00-992-6473 | Cap Assembly, Transmission | III End Item Identification: UH-1 airframe unit powertrain III Part Name Assigned By Controlling Agency: Cap oil filler extension transmission assembly of | Bell Helicopter Textron Inc. (97499) |