Helicopter Rotor Blades, Drive Mechanisms and Components: 204-011-438-1, 204-011-450-105, 204-011-701-23
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
204-011-438-1 2040114381 | 1615-00-830-9754 | Lever Assembly, Pylo | Bell Helicopter Textron Inc. (97499) | ||
204-011-450-105 204011450105 | 1615-01-362-0406 | Mast Assy, Main Roto | Bell Helicopter Textron Inc. (97499) | ||
204-011-450-7 2040114507 | 1615-01-434-0780 | Mast, Rotor, Helicopter | End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
204-011-451-001 204011451001 | 1615-00-970-1262 | Trunnion Assembly, Swashplate | General Characteristics Item Description: Steel, comp 52100 inner and outer race and rollers, steel, comp 9310 or 3312 rod end and housing, beryllium copper retainer, core rockwell hardnessrating C scale 35 to 40, casehardened outer race of shank, inner race of eye and rod end rockwell hardness C scale 60 min, cadmium-plated QQ-P-416 cl 2 TY1 exposed surfaces, dim., 2.850 in. max O/a lg, 1.559 in. min, 1.564 in. max housing lg, 2.260 in. max lg bore- center to housing end, 1.2495 in. min, 1.2500 in. max housing od, 1.140 in. min, 1.180 in. max rod end od, 0.3119 in. min, 0.3122 in. max rod end id, 0.750 in. min, 0.765 in. max outer member W, 0.872 in. min, 0.875 in. max inner member W, tapered roller bearing data, rbec 2 tolerance, 0.0005 in. tightto 0.0005 in. loose internal radial clearance, 13 rollers 0.210 in. lg, 33 short rollers 0.150 in. lg, rod end fitted W/2 shafer G3 grease fittings and bearing prelubricated MIL-G-25537 grease, housing drilled thru W/two holes 0.155 in. min, 0.161 in. max dia 180 deg apart 0.790 in. nom from housing end, | Bell Helicopter Textron Inc. (97499) | |
204-011-451-1 2040114511 | 1615-00-970-1262 | Trunnion Assembly, Swashplate | General Characteristics Item Description: Steel, comp 52100 inner and outer race and rollers, steel, comp 9310 or 3312 rod end and housing, beryllium copper retainer, core rockwell hardnessrating C scale 35 to 40, casehardened outer race of shank, inner race of eye and rod end rockwell hardness C scale 60 min, cadmium-plated QQ-P-416 cl 2 TY1 exposed surfaces, dim., 2.850 in. max O/a lg, 1.559 in. min, 1.564 in. max housing lg, 2.260 in. max lg bore- center to housing end, 1.2495 in. min, 1.2500 in. max housing od, 1.140 in. min, 1.180 in. max rod end od, 0.3119 in. min, 0.3122 in. max rod end id, 0.750 in. min, 0.765 in. max outer member W, 0.872 in. min, 0.875 in. max inner member W, tapered roller bearing data, rbec 2 tolerance, 0.0005 in. tightto 0.0005 in. loose internal radial clearance, 13 rollers 0.210 in. lg, 33 short rollers 0.150 in. lg, rod end fitted W/2 shafer G3 grease fittings and bearing prelubricated MIL-G-25537 grease, housing drilled thru W/two holes 0.155 in. min, 0.161 in. max dia 180 deg apart 0.790 in. nom from housing end, | Bell Helicopter Textron Inc. (97499) Ruag Aerospase Services GMBH (D0216) | |
204-011-454-001 204011454001 | 1615-00-860-9508 | Lock, Plate, Scissors | Bell Helicopter Textron Inc. (97499) | ||
204-011-454-1 2040114541 | 1615-00-860-9508 | Lock, Plate, Scissors | Bell Helicopter Textron Inc. (97499) | ||
204-011-458 204011458 | 1615-00-060-1065 | Plate, Swashplate | General Characteristics Item Description: Aluminum alloy 2024, cond T3 per QQ-A-250/5;O/A dim 4.000 in. O/a LG;1.530 in. W, one END;0.720 in. W, other END;0.125 in. HT;4 mounting HOLES;3.280 in. min. and 3.290 in. max. center to center distance between HOLES;0.645 in. min. and 0.655 in. distance between holes along WIDTH;0.720 in. center to center distance between HOLES;3 of the mounting holes 0.256 in. min. and 0.263 in. max. dia, the other mounting hole 0.256 in. min. and 0.272 in. max. dia;break edges 45.0 degrees by 0.025 in. typ | Bell Helicopter Textron Inc. (97499) | |
204-011-458 204011458 | 1615-00-854-8331 | Plate, Swashplate | Special Features: First leg lg 1.500 in.; second leg lg 3.000 in; 2 bolt holes 0.259 in. dia spaced 0.650 in. C to c; cham 45.0 deg 3 places Material: Aluminum alloy | Bell Helicopter Textron Inc. (97499) | |
204-011-458-003 204011458003 | 1615-00-060-1065 | Plate, Swashplate | General Characteristics Item Description: Aluminum alloy 2024, cond T3 per QQ-A-250/5;O/A dim 4.000 in. O/a LG;1.530 in. W, one END;0.720 in. W, other END;0.125 in. HT;4 mounting HOLES;3.280 in. min. and 3.290 in. max. center to center distance between HOLES;0.645 in. min. and 0.655 in. distance between holes along WIDTH;0.720 in. center to center distance between HOLES;3 of the mounting holes 0.256 in. min. and 0.263 in. max. dia, the other mounting hole 0.256 in. min. and 0.272 in. max. dia;break edges 45.0 degrees by 0.025 in. typ | Bell Helicopter Textron Inc. (97499) | |
204-011-458-005 204011458005 | 1615-00-060-1067 | Plate, Swashplate | Bell Helicopter Textron Inc. (97499) | ||
204-011-458-007 204011458007 | 1615-00-854-8331 | Plate, Swashplate | Special Features: First leg lg 1.500 in.; second leg lg 3.000 in; 2 bolt holes 0.259 in. dia spaced 0.650 in. C to c; cham 45.0 deg 3 places Material: Aluminum alloy | Bell Helicopter Textron Inc. (97499) | |
204-011-458-1 2040114581 | 1615-00-854-8475 | Plate, Swashplate | Bell Helicopter Textron Inc. (97499) | ||
204-011-458-3 2040114583 | 1615-00-060-1065 | Plate, Swashplate | General Characteristics Item Description: Aluminum alloy 2024, cond T3 per QQ-A-250/5;O/A dim 4.000 in. O/a LG;1.530 in. W, one END;0.720 in. W, other END;0.125 in. HT;4 mounting HOLES;3.280 in. min. and 3.290 in. max. center to center distance between HOLES;0.645 in. min. and 0.655 in. distance between holes along WIDTH;0.720 in. center to center distance between HOLES;3 of the mounting holes 0.256 in. min. and 0.263 in. max. dia, the other mounting hole 0.256 in. min. and 0.272 in. max. dia;break edges 45.0 degrees by 0.025 in. typ | Bell Helicopter Textron Inc. (97499) | |
204-011-458-5 2040114585 | 1615-00-060-1067 | Plate, Swashplate | Bell Helicopter Textron Inc. (97499) | ||
204-011-458-7 2040114587 | 1615-00-854-8331 | Plate, Swashplate | Special Features: First leg lg 1.500 in.; second leg lg 3.000 in; 2 bolt holes 0.259 in. dia spaced 0.650 in. C to c; cham 45.0 deg 3 places Material: Aluminum alloy | Bell Helicopter Textron Inc. (97499) | |
204-011-701-023 204011701023 | 1615-00-990-3101 | Hub, Tail Rotor | Bell Helicopter Textron Inc. (97499) | ||
204-011-701-11 20401170111 | 1615-00-017-9616 | Hub, Rotor, Helicopter | Bell Helicopter Textron Inc. (97499) | ||
204-011-701-13 20401170113 | 1615-00-933-6825 | Hub, Tail Rotor | Bell Helicopter Textron Inc. (97499) Lockheed Martin Corporation (80070) | ||
204-011-701-19 20401170119 | 1615-00-933-6825 | Hub, Tail Rotor | Bell Helicopter Textron Inc. (97499) Ruag Aerospase Services GMBH (D0216) | ||
204-011-701-23 20401170123 | 1615-00-990-3101 | Hub, Tail Rotor | Bell Helicopter Textron Inc. (97499) |