Helicopter Rotor Blades, Drive Mechanisms and Components: 204-011-127-3, 204-011-154-003, 204-011-164-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 204-011-127-3 2040111273 | 1615-01-291-3142 | Link Assembly Main | Bell Helicopter Textron Inc. (97499) | ||
| 204-011-128-001 204011128001 | 1615-00-829-6855 | Universal, Control l | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 204-011-128-1 2040111281 | 1615-00-829-6855 | Universal, Control l | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) NP Precision Inc. (3PQR2) Ruag Aerospase Services GMBH (D0216) U S Army Aviation and Missile (81996) | |
| 204-011-134-1 2040111341 | 1615-00-898-0046 | Lock, Inner Race | III End Item Identification: UH-1 rotary wing aircraft | Bell Helicopter Textron Inc. (97499) Imperial Tooling and Mfg Inc. (30333) Rotair Industries Inc. (54878) | |
| 204-011-139-001 204011139001 | 1615-00-856-9367 | Plate, Fitting, Main | Bell Helicopter Textron Inc. (97499) | ||
| 204-011-139-1 2040111391 | 1615-00-856-9367 | Plate, Fitting, Main | Bell Helicopter Textron Inc. (97499) | ||
| 204-011-141-1 2040111411 | 1615-00-716-8568 | Fitting, Drag Brace | Bell Helicopter Textron Inc. (97499) | ||
| 204-011-150-001 204011150001 | 1615-00-868-2754 | Weight, Rotor hub | General Characteristics Item Description: Steel MIL-S-18729 comp 4130 cond C4 or MIL-S-7952 comp 1020 cond C4, surface treatment cadmium plated, QQ-P-416, class I type 1, dim., 3.000 in. nom O/a dia, 0.063 in. nom thk, one hole 0.374 in. min, 0.381 in. max dia drilled in center of weight, max surface finish 125 micro inches aa | Bell Helicopter Textron Inc. (97499) | |
| 204-011-150-1 2040111501 | 1615-00-868-2754 | Weight, Rotor hub | General Characteristics Item Description: Steel MIL-S-18729 comp 4130 cond C4 or MIL-S-7952 comp 1020 cond C4, surface treatment cadmium plated, QQ-P-416, class I type 1, dim., 3.000 in. nom O/a dia, 0.063 in. nom thk, one hole 0.374 in. min, 0.381 in. max dia drilled in center of weight, max surface finish 125 micro inches aa | Bell Helicopter Textron Inc. (97499) Lockheed Martin Corporation (80070) | |
| 204-011-151-001 204011151001 | 1615-00-830-9736 | Bolt Assembly, Main Rotor | General Characteristics Item Description: Steel, MIL-S-5000 comp 4340 cond C1 bolt, cadmium-plated QQ-P-416 type 2, class 1, aluminum alloy QQ-A-225/6 comp 2024-T6 plug, dim., 10.450 in. nom O/a lg, 3.210 in. min, 3.211 in. max left flange od, 0.250 in. nom flange thickness, 2.4992 in. min, 2.4999 in. max bolt od, 1.240 in. min, 1.255 in. max W/across hexagon flats, 0.500 in. nom hex head height, 0.875-14 unf 3B hex internal threads by 1.000 in. lg, 2-12 un 2A right end external threads by 1.360 in. lg, 2.000 in. nom bolt id by 7.200 in. lg, 1.5002 in. right end id, plug for right end, 1.5012 in. O, 0.750 in. lg, 0.120 in. lg left end chamfer by 30.0 deg, used as bolt, blade, main rotor | Bell Helicopter Textron Inc. (97499) | |
| 204-011-151-1 2040111511 | 1615-00-830-9736 | Bolt Assembly, Main Rotor | General Characteristics Item Description: Steel, MIL-S-5000 comp 4340 cond C1 bolt, cadmium-plated QQ-P-416 type 2, class 1, aluminum alloy QQ-A-225/6 comp 2024-T6 plug, dim., 10.450 in. nom O/a lg, 3.210 in. min, 3.211 in. max left flange od, 0.250 in. nom flange thickness, 2.4992 in. min, 2.4999 in. max bolt od, 1.240 in. min, 1.255 in. max W/across hexagon flats, 0.500 in. nom hex head height, 0.875-14 unf 3B hex internal threads by 1.000 in. lg, 2-12 un 2A right end external threads by 1.360 in. lg, 2.000 in. nom bolt id by 7.200 in. lg, 1.5002 in. right end id, plug for right end, 1.5012 in. O, 0.750 in. lg, 0.120 in. lg left end chamfer by 30.0 deg, used as bolt, blade, main rotor | Bell Helicopter Textron Inc. (97499) U S Army Aviation and Missile (81996) | |
| 204-011-154-003 204011154003 | 1615-00-864-3476 | Bolt, Drag Brace, Mai | Bell Helicopter Textron Inc. (97499) | ||
| 204-011-154-3 2040111543 | 1615-00-864-3476 | Bolt, Drag Brace, Mai | Bell Helicopter Textron Inc. (97499) | ||
| 204-011-157-007 204011157007 | 1615-00-183-4422 | Static Stop, Main Rotor | General Characteristics Item Description: Aluminum alloy QQ-A-225/6 comp 2024-T4, anodized bps FW4001, dim., 4.000 in. nom lg, 2.760 in. nom W, 1.200 in. nom ht, 0.310 in. nom material thk, right side center extension 0.800 in. lg by 1.250 in. wide W/two end tangs 0.280 in. lg by 0.245 in. W and 0.150 in. thk, two holes 0.396 in. min, 0.403 in. maxdia drilled on vertical centerline 0.500 in. from right edge W/3.000 in. center to center distance, two threaded holes 0.250-28 unf class 3B tapped on center extension 0.500 in. from vertical centerline W/0.750 in. center to center distance, left side concaved by 3.670 in. radius W/tang on each end 1.200 in. high | Bell Helicopter Textron Inc. (97499) | |
| 204-011-157-1 2040111571 | 1615-00-830-9739 | Static Stop, Main Ro | Bell Helicopter Textron Inc. (97499) | ||
| 204-011-157-7 2040111577 | 1615-00-183-4422 | Static Stop, Main Rotor | General Characteristics Item Description: Aluminum alloy QQ-A-225/6 comp 2024-T4, anodized bps FW4001, dim., 4.000 in. nom lg, 2.760 in. nom W, 1.200 in. nom ht, 0.310 in. nom material thk, right side center extension 0.800 in. lg by 1.250 in. wide W/two end tangs 0.280 in. lg by 0.245 in. W and 0.150 in. thk, two holes 0.396 in. min, 0.403 in. maxdia drilled on vertical centerline 0.500 in. from right edge W/3.000 in. center to center distance, two threaded holes 0.250-28 unf class 3B tapped on center extension 0.500 in. from vertical centerline W/0.750 in. center to center distance, left side concaved by 3.670 in. radius W/tang on each end 1.200 in. high | Bell Helicopter Textron Inc. (97499) | |
| 204-011-159-001 204011159001 | 1615-00-898-0048 | Spacer, Main Rotor Grip | General Characteristics Item Description: Aluminum alloy WW-T-785 comp 2024-T3, anodized bps FW4001, dim., 5.995 in.min, 6.005 in. max lg, 6.620 in. min, 6.623 in. max left end flange od, 5.370 in. min, 5.373 in. max body od, 5.190 in. left end id, 5.000 in. right end internal flange id, left end flange grooved 0.135 in. W, 5.461 in. dia 0.090 in. from end, right end grooved 0.135 in. W, 5.211 in. dia 0.094 in. from end | Bell Helicopter Textron Inc. (97499) | |
| 204-011-159-1 2040111591 | 1615-00-898-0048 | Spacer, Main Rotor Grip | General Characteristics Item Description: Aluminum alloy WW-T-785 comp 2024-T3, anodized bps FW4001, dim., 5.995 in.min, 6.005 in. max lg, 6.620 in. min, 6.623 in. max left end flange od, 5.370 in. min, 5.373 in. max body od, 5.190 in. left end id, 5.000 in. right end internal flange id, left end flange grooved 0.135 in. W, 5.461 in. dia 0.090 in. from end, right end grooved 0.135 in. W, 5.211 in. dia 0.094 in. from end | Bell Helicopter Textron Inc. (97499) | |
| 204-011-164-001 204011164001 | 1615-00-758-2828 | Stop, Inboard Fitting | General Characteristics Item Description: Rubber, MIL-R-7362 comp a type 2 molded, dim., 0.174 in. nom lg, 0.500 in.min, 0.530 in. max W, 0.200 in. min, 0.230 in. max thk, bottom lg rounded by 2.000 in. radius, bottom side concaved by 3.670 in. radius, item usedon hub assy, main rotor | Bell Helicopter Textron Inc. (97499) | |
| 204-011-164-1 2040111641 | 1615-00-758-2828 | Stop, Inboard Fitting | General Characteristics Item Description: Rubber, MIL-R-7362 comp a type 2 molded, dim., 0.174 in. nom lg, 0.500 in.min, 0.530 in. max W, 0.200 in. min, 0.230 in. max thk, bottom lg rounded by 2.000 in. radius, bottom side concaved by 3.670 in. radius, item usedon hub assy, main rotor | Bell Helicopter Textron Inc. (97499) Lockheed Martin Corporation (80070) |