Helicopter Rotor Blades, Drive Mechanisms and Components: 204-011-025-1, 204-011-039-5, 204-011-055-025
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 204-011-025-1 2040110251 | 1615-00-401-6192 | Weight, Rotary Wing Blade | General Characteristics Item Description: Lead, QQ-L-201 grade b, dim., 2.000 in. nom lg, 1.800 in. nom W at one END1.580 in. nom W at opposite end, 0.120 in. nom thick, small end tapered fromhorizontal centerline to sides 0.210 in. deep, largest end tapered fromhorizontal centerline to sides 0.470 and 0.500 in. respectively, cornersrounded by 0.250 in. radius, two holes 0.285 in. nom dia drilled thru onhorizontal centerline 0.500 and 1.600 in. from widest end, max surface finishall surfaces 250 microinches aa | Bell Helicopter Textron Inc. (97499) | |
| 204-011-025-3 2040110253 | 1615-00-495-6558 | Weight, Main Rotor Blade | General Characteristics Item Description: Lead, QQ-L-201 grade D, dim., 2.000 in. nom lg, 1.800 in. nom W at 0.470IN. from top, 1.580 in. nom W at 0.210 in. from bottom, 0.125 in. nom materialthickness, top tapered either side of vertical centerline to 0.470 in. onedge, bottom tapered either side of vertical centerline to 0.210 in. on edgetwo holes 0.343 in. dia drilled thru on vertical centerline 0.500 and 1.600IN. from top W/1.100 in. distance between centers | Bell Helicopter Textron Inc. (97499) | |
| 204-011-039-001 204011039001 | 1615-00-830-9729 | Tab, Trim, Aircraft | Bell Helicopter Textron Inc. (97499) | ||
| 204-011-039-1 2040110391 | 1615-00-830-9729 | Tab, Trim, Aircraft | Bell Helicopter Textron Inc. (97499) | ||
| 204-011-039-107 204011039107 | 1615-01-143-7337 | Tab, Trim, Aircraft | Bell Helicopter Textron Inc. (97499) | ||
| 204-011-039-5 2040110395 | 1615-01-223-4602 | Stabilizer Plate, up | Bell Helicopter Textron Inc. (97499) | ||
| 204-011-042-009 204011042009 | 1615-00-984-5533 | Cover, Tip End, Rotor | Bell Helicopter Textron Inc. (97499) | ||
| 204-011-042-9 2040110429 | 1615-00-984-5533 | Cover, Tip End, Rotor | Bell Helicopter Textron Inc. (97499) | ||
| 204-011-043 204011043 | 1615-00-239-3807 | Retainer, Blade Ballast | General Characteristics Item Description: Aluminum alloy, QQ-A-250/4; octogonal shape 1.960 in. W, one side 1.750IN. l, one side 1.880 in. l; 2 0.260 min 0.267 max in. holes | Bell Helicopter Textron Inc. (97499) | |
| 204-011-043-003 204011043003 | 1615-00-497-1956 | Retainer, Blade Ballast | General Characteristics Item Description: Aluminum alloy QQ-A-250/4 temper T3 or QQ-A-250/5, dim., 2.320 in. nom LG2.080 in. nom W right end by 0.700 in. nom lg, 1.000 in. nom W by 0.980 in.nom lg center section, 2.300 in. nom W by 0.740 in. nom lg left end, 0.125 in.nom material thickness, two holes 0.260 in. min, 0.267 in. max dia drilledthru on horizontal centerline 0.380 AND1.480 in. from left end W/1.100 in.distance between centers, max surface finish, all surfaces 125 microinches aa | Bell Helicopter Textron Inc. (97499) | |
| 204-011-043-005 204011043005 | 1615-00-239-3807 | Retainer, Blade Ballast | General Characteristics Item Description: Aluminum alloy, QQ-A-250/4; octogonal shape 1.960 in. W, one side 1.750IN. l, one side 1.880 in. l; 2 0.260 min 0.267 max in. holes | Bell Helicopter Textron Inc. (97499) | |
| 204-011-043-007 204011043007 | 1615-00-497-1955 | Retainer, Blade Ballast | General Characteristics Item Description: Aluminum alloy QQ-A-250/4 temper T3 or QQ-A-250/5, dim., 2.320 in. nom LG0.920 in. nom W right end, 1.030 in. nom W at 0.320 in. from right end, 0.790IN. nom W at 0.560 in. from left end, 0.500 in. nom W left end, 0.125 in. nommaterial thickness, two holes 0.260 in. min, 0.267 in. max dia drilled thru onhorizontal centerline 0.820 and 1.920 in. from left end W/1.100 in. distancebetween centers, max surface finish, all surfaces 125 microinches aa | Bell Helicopter Textron Inc. (97499) | |
| 204-011-043-009 204011043009 | 1615-00-488-7588 | Retainer, Blade Ballast | General Characteristics Item Description: Aluminum alloy QQ-A-250/4 temper T3 or QQ-A-250/5, dim., 2.320 in. nom LG1.000 in. nom W right end, 1.100 in. nom W 0.320 in. from right end, 0.860 in.nom W 0.560 in. from left end, 0.500 in. nom W left end, two holes 0.260 in.min, 0.267 in. max dia drilled thru on horizontal centerline 0.820 and 1.920IN. from left end W/1.100 in. distance between centers, 0.125 in. nommaterial thickness, max surface finish, all surfaces 125 microinches aa | Bell Helicopter Textron Inc. (97499) | |
| 204-011-043-3 2040110433 | 1615-00-497-1956 | Retainer, Blade Ballast | General Characteristics Item Description: Aluminum alloy QQ-A-250/4 temper T3 or QQ-A-250/5, dim., 2.320 in. nom LG2.080 in. nom W right end by 0.700 in. nom lg, 1.000 in. nom W by 0.980 in.nom lg center section, 2.300 in. nom W by 0.740 in. nom lg left end, 0.125 in.nom material thickness, two holes 0.260 in. min, 0.267 in. max dia drilledthru on horizontal centerline 0.380 AND1.480 in. from left end W/1.100 in.distance between centers, max surface finish, all surfaces 125 microinches aa | Bell Helicopter Textron Inc. (97499) | |
| 204-011-043-5 2040110435 | 1615-00-239-3807 | Retainer, Blade Ballast | General Characteristics Item Description: Aluminum alloy, QQ-A-250/4; octogonal shape 1.960 in. W, one side 1.750IN. l, one side 1.880 in. l; 2 0.260 min 0.267 max in. holes | Bell Helicopter Textron Inc. (97499) | |
| 204-011-043-7 2040110437 | 1615-00-497-1955 | Retainer, Blade Ballast | General Characteristics Item Description: Aluminum alloy QQ-A-250/4 temper T3 or QQ-A-250/5, dim., 2.320 in. nom LG0.920 in. nom W right end, 1.030 in. nom W at 0.320 in. from right end, 0.790IN. nom W at 0.560 in. from left end, 0.500 in. nom W left end, 0.125 in. nommaterial thickness, two holes 0.260 in. min, 0.267 in. max dia drilled thru onhorizontal centerline 0.820 and 1.920 in. from left end W/1.100 in. distancebetween centers, max surface finish, all surfaces 125 microinches aa | Bell Helicopter Textron Inc. (97499) | |
| 204-011-043-9 2040110439 | 1615-00-488-7588 | Retainer, Blade Ballast | General Characteristics Item Description: Aluminum alloy QQ-A-250/4 temper T3 or QQ-A-250/5, dim., 2.320 in. nom LG1.000 in. nom W right end, 1.100 in. nom W 0.320 in. from right end, 0.860 in.nom W 0.560 in. from left end, 0.500 in. nom W left end, two holes 0.260 in.min, 0.267 in. max dia drilled thru on horizontal centerline 0.820 and 1.920IN. from left end W/1.100 in. distance between centers, 0.125 in. nommaterial thickness, max surface finish, all surfaces 125 microinches aa | Bell Helicopter Textron Inc. (97499) | |
| 204-011-052-005 204011052005 | 1615-00-239-3808 | Support Assy, Weight | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 204-011-052-5 2040110525 | 1615-00-239-3808 | Support Assy, Weight | III End Item Identification: UH-1, rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 204-011-055-025 204011055025 | 1615-00-941-8742 | Block, Nose, Main Rotor Blade | General Characteristics Item Description: Aluminum alloy QQ-A-267 comp 2024T4, finished per no. 204-947-002 drawing, dim., semi-circular bar, 18.000 in. nom lg, 0.6495 in. min, 0.6645 in. ht, twisted zero deg 41 minutes over lg | Bell Helicopter Textron Inc. (97499) |