Helicopter Rotor Blades, Drive Mechanisms and Components: 204-040-206-9, 204-040-237-009, 204-040-288-011
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 204-040-206-9 2040402069 | 1615-00-133-7364 | Quill Assy | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-207-013 204040207013 | 1615-00-795-0661 | Quill Assembly, Tail | III End Item Identification: UH-1 rotary wing aircraft | Bell Helicopter Textron Inc. (97499) | |
| 204-040-207-13 20404020713 | 1615-00-795-0661 | Quill Assembly, Tail | III End Item Identification: UH-1 rotary wing aircraft | Bell Helicopter Textron Inc. (97499) Lockheed Martin Corporation (80070) Textron Systems Corporation (04614) | |
| 204-040-207-15 20404020715 | 1615-00-867-5738 | Transmission, Mechanical, Helicopt | Special Features: Quill assy, tail rotor drive End Item Identification: H-1 aircraft | Bell Helicopter Textron Inc. (97499) Lockheed Martin Corporation (80070) | |
| 204-040-207-9 2040402079 | 1615-00-792-6408 | Quill Assembly | Bell Helicopter Textron Inc. (97499) Lockheed Martin Corporation (80070) | ||
| 204-040-234-001 204040234001 | 1615-00-701-9879 | Plug, Oil, Transmission | General Characteristics Item Description: Aluminum alloy QQ-A-225/6 comp 2024-T4, anodized bps FW4001, dim., 2.690 in. nom O/a lg, 2.246 in. min, 2.248 in.max od by 1.890 in. nom body lg, left end center extention 0.800 in. lg by 0.600 in. od, 1.820 in. nom id by 1.720IN. lg, counterbored 2.040 in. dia by 1.150 in. lg, extension center drilled and tapped W/0.375-24 unf class 2B threads 0.620 in. deep, one hole 0.250 in.dia drilled thru od wall 0.270 in. from right end, one od groove 0.187 in. W, 2.026 in. od located 0.380 in. from left end | Bell Helicopter Textron Inc. (97499) | |
| 204-040-234-1 2040402341 | 1615-00-701-9879 | Plug, Oil, Transmission | General Characteristics Item Description: Aluminum alloy QQ-A-225/6 comp 2024-T4, anodized bps FW4001, dim., 2.690 in. nom O/a lg, 2.246 in. min, 2.248 in.max od by 1.890 in. nom body lg, left end center extention 0.800 in. lg by 0.600 in. od, 1.820 in. nom id by 1.720IN. lg, counterbored 2.040 in. dia by 1.150 in. lg, extension center drilled and tapped W/0.375-24 unf class 2B threads 0.620 in. deep, one hole 0.250 in.dia drilled thru od wall 0.270 in. from right end, one od groove 0.187 in. W, 2.026 in. od located 0.380 in. from left end | Bell Helicopter Textron Inc. (97499) | |
| 204-040-237-009 204040237009 | 1615-00-624-5245 | Screen Assy, Pump Inlet | General Characteristics Item Description: Steel, screen 16X16 mesh, 23 gauge W and m, steel, MIL-T-6736 comp 4130 cond D sleeve, steel, MIL-S-6758 comp 4130 cond G4 plug, dim., 3.750 in. nom O/a lg, 0.870 in. nom screen od, 0.980 in. right end sleeve od by 0.250 in. lg, 1-380 in. width across hex flats on left end plug, 0.250 in. hex thk, 0.720 in. nom plug lg, 0.875 in. plug id, 1.125-12 unf class 2A plug od threads by 0.370 in. lg, screen brazed to plug and sleeve id, item used on pump inlet, trans | Bell Helicopter Textron Inc. (97499) Lynn David Machine Inc. (3K464) | |
| 204-040-237-1 2040402371 | 1615-00-624-5245 | Screen Assy, Pump Inlet | General Characteristics Item Description: Steel, screen 16X16 mesh, 23 gauge W and m, steel, MIL-T-6736 comp 4130 cond D sleeve, steel, MIL-S-6758 comp 4130 cond G4 plug, dim., 3.750 in. nom O/a lg, 0.870 in. nom screen od, 0.980 in. right end sleeve od by 0.250 in. lg, 1-380 in. width across hex flats on left end plug, 0.250 in. hex thk, 0.720 in. nom plug lg, 0.875 in. plug id, 1.125-12 unf class 2A plug od threads by 0.370 in. lg, screen brazed to plug and sleeve id, item used on pump inlet, trans | Lockheed Martin Corporation (80070) | |
| 204-040-237-9 2040402379 | 1615-00-624-5245 | Screen Assy, Pump Inlet | General Characteristics Item Description: Steel, screen 16X16 mesh, 23 gauge W and m, steel, MIL-T-6736 comp 4130 cond D sleeve, steel, MIL-S-6758 comp 4130 cond G4 plug, dim., 3.750 in. nom O/a lg, 0.870 in. nom screen od, 0.980 in. right end sleeve od by 0.250 in. lg, 1-380 in. width across hex flats on left end plug, 0.250 in. hex thk, 0.720 in. nom plug lg, 0.875 in. plug id, 1.125-12 unf class 2A plug od threads by 0.370 in. lg, screen brazed to plug and sleeve id, item used on pump inlet, trans | Bell Helicopter Textron Inc. (97499) | |
| 204-040-250-11 20404025011 | 1615-00-757-5778 | Sleeve Assembled, Bushing, Tail Ro | III End Item Identification: 1560-00-488-4921 General Characteristics Item Description: Alum alloy per QQ-A-601 comp 3 temp T51 or QQ-A-596 temp T51;9.894 in. lg approx by 1.410 in. thk O/a by 5.470 in. wd APPROX;1 2.750 in. dia hole W/8 HOLES-2 W/0.312-18 UNC-2B thd on 4.937 in. dia bolt circle located on upper PART;1 5.180 in. dia hole W/6 0.284IN. dia HOLE-1 W/0.312-18 UNC-2B thd on 7.380 in. dia bolt circle located onlower PART;2 bushings included, steel per MIL-S-6736 comp 4130, 1-6.00 in. od by 5.500 in. id by 1.200 in. lg, 1-3.00 in. od by 2.500 in. id by 1.700 in. lg | Bell Helicopter Textron Inc. (97499) Lockheed Martin Corporation (80070) | |
| 204-040-257-001 204040257001 | 1615-00-691-2163 | Liner, Transmission | General Characteristics Item Description: Steel, AMS6381 or AMS6413 or AMS6415, black oxide coated bps FW4084, dim., 4.990 in. nom flange od, 0.300 in. nom flange W, 4.3300 in. min, 4.3309 in. maxbody od by 0.570 in. lg, 4.140 in. nom id, flange internal spline data, 45 teeth 0.260 in. lg, 30.0 deg pressure angle, 10120 diametral pitch, 4.5000 in. pitch dia, 4.403 in. nom minor dia, 4.700 in. max major dia, item used as liner forinner lower bearing planetary support, transmission | Bell Helicopter Textron Inc. (97499) | |
| 204-040-257-1 2040402571 | 1615-00-691-2163 | Liner, Transmission | General Characteristics Item Description: Steel, AMS6381 or AMS6413 or AMS6415, black oxide coated bps FW4084, dim., 4.990 in. nom flange od, 0.300 in. nom flange W, 4.3300 in. min, 4.3309 in. maxbody od by 0.570 in. lg, 4.140 in. nom id, flange internal spline data, 45 teeth 0.260 in. lg, 30.0 deg pressure angle, 10120 diametral pitch, 4.5000 in. pitch dia, 4.403 in. nom minor dia, 4.700 in. max major dia, item used as liner forinner lower bearing planetary support, transmission | Bell Helicopter Textron Inc. (97499) | |
| 204-040-261-013 204040261013 | 1615-00-898-6884 | Jet Lubricator, Transmission | General Characteristics Item Description: Steel, MIL-S-6758, comp 4130 cond D4 tube steel, MIL-S-18729 comp 4130 cond N, dim 5.585 in. nom O/a lg, O.430 in. min and 0.432 in. max flange od, 0.337 in. nom base od, 0.285 in. nom tube od, 0.190 in. nom id by 5.430 in. lg, 10-32 nf class 2B internal threads on base id 0.370 in lg, 17 slots 0.031 in. W, 0.094 in. deep equally spaced and staggered on top and bottom of tube within 2.080 in. from right flange face, one hole 0.040 in. dia drilled thru tube wall 3.304 in. from right flange face, jet orfice 0.040 in. dia drilled in tip at 43.0 deg angle above horizontal center line, mounting plate dim., 1.234 in. O/a lg 0.750 in. wide 0.100 in. thk two mounting holes drilled in plate, first hole 0.339 in. dia, second hole 0.271 in dia W/0.624 in. center to center distance between holes, plate marked no. 4 | Bell Helicopter Textron Inc. (97499) | |
| 204-040-261-13 20404026113 | 1615-00-898-6884 | Jet Lubricator, Transmission | General Characteristics Item Description: Steel, MIL-S-6758, comp 4130 cond D4 tube steel, MIL-S-18729 comp 4130 cond N, dim 5.585 in. nom O/a lg, O.430 in. min and 0.432 in. max flange od, 0.337 in. nom base od, 0.285 in. nom tube od, 0.190 in. nom id by 5.430 in. lg, 10-32 nf class 2B internal threads on base id 0.370 in lg, 17 slots 0.031 in. W, 0.094 in. deep equally spaced and staggered on top and bottom of tube within 2.080 in. from right flange face, one hole 0.040 in. dia drilled thru tube wall 3.304 in. from right flange face, jet orfice 0.040 in. dia drilled in tip at 43.0 deg angle above horizontal center line, mounting plate dim., 1.234 in. O/a lg 0.750 in. wide 0.100 in. thk two mounting holes drilled in plate, first hole 0.339 in. dia, second hole 0.271 in dia W/0.624 in. center to center distance between holes, plate marked no. 4 | Bell Helicopter Textron Inc. (97499) | |
| 204-040-262-021 204040262021 | 1615-00-069-3312 | Jet Lubricator, Transmission | General Characteristics Item Description: Steel, MIL-S-6736, comp 4130, D1M., 3.239 in. nom O/a lg, 0.430 in. min and 0.432 in. max flange od, 0.337 in. nom base od, 0.285 in. nom tube od, 0.190 in. nom id by 3.125 in. lg, 10-32 unf class 2B internal threads on base 0.370 in. lg, 14 slots 0.031 in. W, 0.094 1N. deep equally spaced and staggered on top and bottom of tube within 0.780 in. section 1.128 in. from right flange face, one jet orfice 0.052 in. dia drilled in tip on horizontal centerline, one jet orfice 0.040 in. dia drilled at 30.0 deg angle above and below horizontal centerline 3.000 in. from flange face, mounting plate dim., 1.422 in.O/a lg, 0.750 1N. wide, 0.100 in. thick, two mounting holes drilled in plate, first hole 0.338 in. dia, second hole 0.209 in. dia with 0.807 in. min and 0.817 in. max center to center distance between holes, plate marked no. 2 | Bell Helicopter Textron Inc. (97499) | |
| 204-040-262-13 20404026213 | 1615-00-989-3775 | Nozzle, Lubricant, Tr | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-262-17 20404026217 | 1615-00-989-3775 | Nozzle, Lubricant, Tr | Bell Helicopter Textron Inc. (97499) | ||
| 204-040-262-21 20404026221 | 1615-00-069-3312 | Jet Lubricator, Transmission | General Characteristics Item Description: Steel, MIL-S-6736, comp 4130, D1M., 3.239 in. nom O/a lg, 0.430 in. min and 0.432 in. max flange od, 0.337 in. nom base od, 0.285 in. nom tube od, 0.190 in. nom id by 3.125 in. lg, 10-32 unf class 2B internal threads on base 0.370 in. lg, 14 slots 0.031 in. W, 0.094 1N. deep equally spaced and staggered on top and bottom of tube within 0.780 in. section 1.128 in. from right flange face, one jet orfice 0.052 in. dia drilled in tip on horizontal centerline, one jet orfice 0.040 in. dia drilled at 30.0 deg angle above and below horizontal centerline 3.000 in. from flange face, mounting plate dim., 1.422 in.O/a lg, 0.750 1N. wide, 0.100 in. thick, two mounting holes drilled in plate, first hole 0.338 in. dia, second hole 0.209 in. dia with 0.807 in. min and 0.817 in. max center to center distance between holes, plate marked no. 2 | Bell Helicopter Textron Inc. (97499) | |
| 204-040-288-011 204040288011 | 1615-00-898-6883 | Jet Lubricator, Transmission | General Characteristics Item Description: Steel, MIL-S-6736, comp 4130, dim., 3.500 in. nom O/a lg, 0.430 in. min and 0.432 in. max flange od, 0.337 in. nom base od, 0.275 in. min and 0.285 in. max tube od, 0.124 in. min and 0.130 in. max id by 3.340 in. deep, tap 10-32 nf class 2B internal threads on base id 0.370 in. lg, 15 slots 0.027 in. nom W, 0.094 in. deep equally spaced and staggered on top and bottom of tube within 1.300 in. from right flange face, one hole 0.020 in. dia drilled thru tube wall 3.125 in. from right flange face, jet slot on tube top 0.020 min to 0.025 max in. wide by 0.095 min to 0.115 max in. deep, 0.275 in. from tip, mounting plate dim., 1.300 in O/a lg, 0.750 in. W, 0.054 in. thk, two mounting holes drilled in plate, first hole 0.298 in. nom dia, second hole 0.336 in. nom dia W/0.685 in. center to center distance between holes, plate marked no. 5 | Bell Helicopter Textron Inc. (97499) |