Helicopter Rotor Blades, Drive Mechanisms and Components: 114D1200-15, 114D2161-1, 114D2164-2
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 114D1200-15 114D120015 | 1615-01-112-5841 | Transmission, Mechanical, Helicopt | End Item Identification: CH-47C, cargo, hel | The Boeing Company (77272) | |
| 114D1200-18 114D120018 | 1615-01-449-0857 | Transmission, Helicopter | III End Item Identification: CH-47 series helicopter General Characteristics Item Description: Spare parts | The Boeing Company (77272) | |
| 114D1200-19 114D120019 | 1615-01-138-2579 | Transmission, Rotor | The Boeing Company (77272) | ||
| 114D1200-20 114D120020 | 1615-01-244-4970 | Transmission, Mechanical, Helicopt | End Item Identification: CH-47C, cargo, hel | The Boeing Company (77272) | |
| 114D1200-6 114D12006 | 1615-00-009-5405 | Transmission, Helico | The Boeing Company (77272) | ||
| 114D1200-7 114D12007 | 1615-00-092-4661 | Transmission, Mechanical, Helicopt | End Item Identification: CH-47C, cargo, hel | The Boeing Company (77272) | |
| 114D1200-9 114D12009 | 1615-00-621-1853 | Transmission, Mechanical, Helicopt | End Item Identification: CH-47C, cargo, hel | The Boeing Company (77272) | |
| 114D1246-1 114D12461 | 1615-00-068-6574 | Plug, Rotor Shaft | General Characteristics Item Description: Rubber, synthetic, molded MIL-R-6855 class 2, grade 80, dim., 3.940 in. nomod, 0.500 in. nom W, 3.340 in. nom id by 0.250 in. deep, od tapered to 3.840IN. nom dia, outside left and right corners rounded by 0.120 in. radius, inside corner rounded by 0.250 in. radius, all diameters on common centerlineconcentric to each other within 0.030 tir | The Boeing Company (77272) | |
| 114D2071-3 114D20713 | 1615-00-176-1185 | Carrier, Planet, Tran | The Boeing Company (77272) | ||
| 114D2088-3 114D20883 | 1615-00-111-2872 | Liner, Housing, Transmission | General Characteristics Item Description: Steel, MIL-S-5000 comp 4340 cond E, black oxide coated MIL-C-13924, dim., 1.510 in. nom O/a lg, 11.428 in. min, 11.448 in. max id, 11.959 in. min, 11.961IN. max od, right side counterbored to 11.750 in. nom dia by 0.820 in. DEEP14.120 in. nom flange od, 0.100 in. nom flange W, 8 mounting holes 0.344 in.dia, 4 located left of vertical centerline 2 above and below horizontalcenterline 2.535, 6.121 in. from vertical, 2.535, 6.121 in. from horizontalcenterline, 4 holes located right of vertical centerline 2 above and belowhorizontal centerline 2.535, 6.171 from vertical and 2.410, 6.121 fromhorizontal centerline, 6 lubrication holes 0.078 in. dia at 50 deg drilledthru od groove at 30, 120, 165, 210, 300 and 345 deg, 4 lubrication holes 0.060IN. dia at 55 deg drilled thru od groove at 75, 100, 255 and 280 deg, twolubrication holes 0.040 in. dia at 65 deg drilled thru od groove at 60 AND240 deg, inside left corner chamfered 0.100 in. lg by 30 deg, max surfacefinish, id, od and right surface of flange 80 microinc | The Boeing Company (77272) | |
| 114D2098-2 114D20982 | 1615-01-253-0379 | Liner, Seal Retainer | The Boeing Company (77272) | ||
| 114D2122-1 114D21221 | 1615-00-895-9437 | Dowel, Housing Assembly | Material: Steel Overall Length: 0.750 inches nominal | The Boeing Company (77272,81205) | |
| 114D2151-3 114D21513 | 1615-00-956-9913 | Window, Sump Sight Gage | General Characteristics Item Description: Plastic, kel-F, AMS3650 or AMS3650A, dim., 5.090 in. nom O/a lg, 3.570 in. nom O/a W, 0.125 in. nom material thk, six holes three per side 0.311 in. min, 0.319 in. max dia located 0.420 in. from top and 0.410 in. from each side middle holes located 2.125 in. C to C distance from top and bottom holes, oneadditional hole located at bottom on vertical centerline | The Boeing Company (77272,81205) | |
| 114D2153-1 114D21531 | 1615-00-830-9771 | Cover, Hydraulic Pump | General Characteristics Item Description: Aluminum alloy QQ-A-267 comp 2024-T4, anodized MIL-C-5541, dim., 0.750 in.nom W, 5.720 in. min, 5.740 in. max flange od, 0.130 in. nom flange thk, 3.998 in. min, 3.999 in. max body od by 0.620IN. lg, one od groove 0.190 in. W by 0.115 in. deep located 0.150 in. from right end, right end drilled W/3.500 in. dia hole by 0.620 in. deep, left flangeface drilled thru W/four equally spaced holes 0.344 in. dia on 5.000 in. bolt circle dia, max surface finish groovesurfaces 80 microinches aa, all other surfaces 125 microinches aa, item used on aft transmission | The Boeing Company (77272,81205) | |
| 114D2155-1 114D21551 | 1615-00-895-9439 | Jet Lubricator, Transmission | General Characteristics Item Description: Aluminum alloy QQ-A-325 comp 6061, T6, surface treatment oxide film MIL-C-5541, dim., 3.400 in. nom O/a lg, 2.220 in. nom flange lg, 1.250 in. nom flange W, 0.120 in. nom flange thk, 0.686 in. nom base od, 0.500-20 unf 3B base internal threads 0.438 in. deep, 2.680 in. nom nozzle lg, 0.425 in. nom nozzle od, 0.187 in. min, 0.192 in. max nozzleid, nozzle top beveled at 34.0 deg with two jet holes 0.039 in. min, 0.042 in. max perpindicular to bevel, two mounting holes drilled in flange 0.230IN. nom dia with 1.594 in. center to center distance, one thru hole 0.250 in. nom dia 0.660 in. from flange face | The Boeing Company (77272,81205) | |
| 114D2155-3 114D21553 | 1615-01-210-6506 | Jet, Lubricator, Tran | The Boeing Company (77272) | ||
| 114D2161-1 114D21611 | 1615-00-895-9444 | Jet Lubricator, Transmission | General Characteristics Item Description: Aluminum alloy QQ-A-325 comp 6061, T6, surface treatment oxide film MIL-C-5541, dim., 2.960 in. nom O/a lg, 2.220 in. nom flange lg, 1.180 in. nom flange W, 0.120 in. nom flange thk, 0.874 in. nom base od, 0.500-20 unf 3B base internal threads 0.438 in. deep, 2.360 in. nom nozzle lg, 0.555 in. nom nozzle od, 0.311 in. min, 0.319 in. max nozzle id, nozzle tip chamfered 30.0 deg W/one hole 0.039 in. min, 0.042 in.max dia drilled perpendicular to chamfer, one hole 0.039 in. min, 0.042 in. max dia drilled on bottom of tube at 70.0 deg angle 2.150 in. from flange face, two mounting holes drilledin flange 0.230 in. nom dia W/1.594 in. center to center distance, one thruhole 0.312 in. dia 0.730 in. from flange face | The Boeing Company (77272,81205) | |
| 114D2164 | 1615-00-895-9445 | Jet Lubricator, Transmission | Special Features: 2.220 in. nom flange lg, 1.250 in. nom flange W, 0.120 in. nom flange thk; 0.920 in. nom base od; 0.500 IN.-20 UNF-3B base internal threads; 0.438 in. deep, 2.250 in. nom nozzle lg, 0.555 in. nom nozzle od, 0.470 in. nom nozzle id, one center nozle top hole 0.059 in. min and 0.062 in. max dia; two mounting holes drilled in flange 0.230 in. nom dia with 1.594 in. center to center distance, one thru hole 0.312 in. dia, 0.730 in. from flange to face Material: Aluminum alloy Overall Length: 3.150 inches nominal | The Boeing Company (77272) | |
| 114D2164-1 114D21641 | 1615-00-895-9445 | Jet Lubricator, Transmission | Special Features: 2.220 in. nom flange lg, 1.250 in. nom flange W, 0.120 in. nom flange thk; 0.920 in. nom base od; 0.500 IN.-20 UNF-3B base internal threads; 0.438 in. deep, 2.250 in. nom nozzle lg, 0.555 in. nom nozzle od, 0.470 in. nom nozzle id, one center nozle top hole 0.059 in. min and 0.062 in. max dia; two mounting holes drilled in flange 0.230 in. nom dia with 1.594 in. center to center distance, one thru hole 0.312 in. dia, 0.730 in. from flange to face Material: Aluminum alloy Overall Length: 3.150 inches nominal | The Boeing Company (77272,81205) | |
| 114D2164-2 114D21642 | 1615-01-210-6510 | Jet, Lubricator, Tran | The Boeing Company (77272) |