Helicopter Rotor Blades, Drive Mechanisms and Components: 114H6816-1, 114H6825-2, 114R1502-48
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 114H6816-1 114H68161 | 1615-00-076-1491 | Tank, Fluid, Shock Ab | The Boeing Company (77272) | ||
| 114H6821-1 114H68211 | 1615-00-069-3299 | Sleeve, Cylinder | General Characteristics Item Description: Aluminum alloy QQ-A-200/2 comp 2014-T6, chromium-plated id QQ-C-320 class 2, chemical film MIL-C-5541 type 2 class 1 grade C all other surfaces, dim., 5.812 in. nom lg, 3.373 in. min, 3.375 in. max od, 3.608 in. min, 3.616 in. max flange od, 0.438 in. lg left flange W, 0.847 in. lg center flange W, 0.531 in. lg right flange W, 0.225 in. flange W by 3.375 in. dia W/one grooveper left and right flanges and two grooves on center flange, twelve holes 0.081 in. dia equally spaced 1.185 in.from left end W/2ND row of twelve holes 0.209 in. distance between centers offset 15.0 deg, similar set of twelve holes 0.633 in. from right end, sleeve used on blade lag shock absorber | Aero Components Inc. (59213) Associated Aircraft Manufacturing (56540) Creative Precision Inc. (0F3N2) Essner Manufacturing L.P. (2B834) Lehigh Machine and Tool Co. (7H884) The Boeing Company (77272) Transaero Inc. (27541) Triumph Actuation Systems (33068) | |
| 114H6824-1 114H68241 | 1615-00-021-2720 | End Cover, Shock Absorber | General Characteristics Item Description: Phosphor bronze astm B139-5B comp a or QQ-B-750 comp a temper hard, dim., 3.615 in. min, 3.616 in. max left end flange od, 0.501 in. nom flange lg, 3.114 in. min, 3.115 in. max right end body od, 0.552 in. nom body lg, 1.365 in. nom O/a lg, 1.937 in. nom left end body od, 0.312 in. nom left end body lg, 1.2490 in. min, 1.2495 in. max td, 1.636 in. nom left end counterbore dia.by 0.156 in. deep, left end flange center-grooved 0.188 in. W by 3.375 in. nom dia, right end body center-grooved 0.225 in. W by 2.875 in. nom dia, nine holes on right face 0.375 in. dia by 0.680 in. deep equally spaced on 2.250 in. bolt circle dia, item used as end cover for blade lag shock absorber | Creative Precision Inc. (0F3N2) The Boeing Company (77272) Transaero Inc. (27541) Triumph Actuation Systems (33068) | |
| 114H6825-2 114H68252 | 1615-01-279-0251 | Retainer, End Cover, Rotor Blades | III End Item Identification: 1520-00-871-7308 | Delta Machine & Tool Company (9N156) The Boeing Company (77272) | |
| 114H6828-2 114H68282 | 1615-00-759-8304 | Retainer, Shock Absorber | General Characteristics Item Description: Aluminum alloy QQ-A-225/6 comp 2024-T4, anodized MIL-A-8625 type 1 dyed black no. 37038 overall, dim., 1.470 in.nom lg, 1.050 in. nom body od, threaded flange 0.250 in. from right end W/1.250-16 un class 3A threads 0.550 in. lg, one od groove 0.315 in. from left end 0.141 in. W by 0.878 in. od, 0.685 in. left end od by 0.150 in. lg W/four equally spaced notches 0.060 in. W by 0.060 in. deep, 0.500 in. id by 0.080 in. deep, 0.690 in. nom right end id by 1.060 in. deep, 0.876 in. sq wrenching flats on right end od W/two 0.046 in. dialockwire holes 180.0 deg apart, item used on blade lag shock absorber | The Boeing Company (77272) | |
| 114H6831-2 114H68312 | 1615-00-813-0543 | Plate, Check Valve | General Characteristics Item Description: Steel, corrosion resisting AMS5643COMP 17-4PH, dim., 0.210 in. nom O/a lg, 0.863 in. min, 0.867 in. flange od, 0.060 in. nom flange thk, 0.685 in. nom body od, 0.150 in. nom body lg, max surfacefinish, right flange face 16 microinches aa, all other surfaces 125 microinches aa, magnetic particle inspected per BAC5424 class b, item used on blade lagshock absorber | The Boeing Company (77272) | |
| 114H6832 | 1615-00-763-7563 | Check Valve Seat, Shock Absorber | General Characteristics Item Description: Steel, corrosion resisting AMS5643COMP 17-4PH, dim., 0.729 in. nom O/a lg, 1.053 in. min, 1.054 in. max flange od by 0.093 in. W located 0.157 and 0.404IN. from right end, one center groove between flange 0.120 in. W by 0.870 in. W by 0.870 in. od, 0.865 in. min, 0.870 in. max body od, 0.500 in. thru id W/right end counterbored to 0.625 in. dia by 0.340 in. deep W/60.0 deg valve seat, 0.750 in. left end od, four slots equally spaced on left end od 0.060 in. deep and wide | The Boeing Company (77272) | |
| 114H6832-2 114H68322 | 1615-00-763-7563 | Check Valve Seat, Shock Absorber | General Characteristics Item Description: Steel, corrosion resisting AMS5643COMP 17-4PH, dim., 0.729 in. nom O/a lg, 1.053 in. min, 1.054 in. max flange od by 0.093 in. W located 0.157 and 0.404IN. from right end, one center groove between flange 0.120 in. W by 0.870 in. W by 0.870 in. od, 0.865 in. min, 0.870 in. max body od, 0.500 in. thru id W/right end counterbored to 0.625 in. dia by 0.340 in. deep W/60.0 deg valve seat, 0.750 in. left end od, four slots equally spaced on left end od 0.060 in. deep and wide | The Boeing Company (77272) | |
| 114H6834-1 114H68341 | 1615-00-073-5278 | Retainer, Valve Check | General Characteristics Item Description: Aluminum alloy QQ-A-225/6 comp 2024-T4, surface treatment anodized per MIL-A-8625 and black lusterless dye no. 37038 O/a, dim., 2.900 in. nom O/a lg, 1.2500-16 un class 3A external threads on left end od by 0.700 in. lg, 1.0625-16 un class 3B internal threads on left end id by 1.057 in. lg, raised hexagon surface 2.000 in. from right end by 0.500 in. lg W/1.250 in. distance across flats, 1.054 in. nom right od by 0.593 in. lg, one groove 0.094 in. by 0.943 in. dia 0.250 in. from right end, 1.1875-16 un class 3A threads W/0.750 in. lg threads beginning 0.593 in. from from right end, 0.790 in. nom right end id W, four equally spaced slots 0.125 in. W by 0.065 in. deep, four equally spaced slots 0.078 in. W by 0.562 in. deep on left end, item used on blade lag shock absorber | The Boeing Company (77272) | |
| 114H6835-1 114H68351 | 1615-00-050-6195 | Retainer, Helical Compression Spr | Style Designator: Irregular Special Features: Raised center on id base 0.450 in. dia by 0.190 in. high, 1.062-16 un class 3A threads on flange od, flange vase center drilled 0.312 in. dia by 0.312 in. deep and four equally spaced holes 0.125 in. dia by 0.125 in. deep on 0.620 in. bolt circle dia, three equally spaced holes 0.076 in. dia drilled thru flange od 0.250 in. from end, item used on blade lag shock absorber Overall Height: 1.921 inches nominal | The Boeing Company (77272) | |
| 114H6841-1 114H68411 | 1615-00-068-6565 | Cover, Control Valve | III End Item Identification: CH-47 | The Boeing Company (77272) | |
| 114R1002-102 114R1002102 | 1615-00-187-3943 | Blade, Rotary Wing | The Boeing Company (77272) | ||
| 114R1502-33 114R150233 | 1615-00-176-2106 | Blade, Rotary Wing | Special Features: Left hand blade assembly | The Boeing Company (77272) | |
| 114R1502-34 114R150234 | 1615-00-001-6443 | Blade, Rotary Wing | Material: Steel Aircraft Model Number: CH-47C | The Boeing Company (77272) | |
| 114R1502-35 114R150235 | 1615-00-172-2102 | Blade, Rotary Wing | The Boeing Company (77272) | ||
| 114R1502-36 114R150236 | 1615-00-001-6443 | Blade, Rotary Wing | Material: Steel Aircraft Model Number: CH-47C | The Boeing Company (77272) | |
| 114R1502-43 114R150243 | 1615-00-172-2099 | Blade, Rotary Wing | III End Item Identification: Blade assembly, droop snoot, rotary wing | The Boeing Company (77272) | |
| 114R1502-44 114R150244 | 1615-00-001-6443 | Blade, Rotary Wing | Material: Steel Aircraft Model Number: CH-47C | The Boeing Company (77272) | |
| 114R1502-47 114R150247 | 1615-00-172-2102 | Blade, Rotary Wing | The Boeing Company (77272) | ||
| 114R1502-48 114R150248 | 1615-00-001-6443 | Blade, Rotary Wing | Material: Steel Aircraft Model Number: CH-47C | The Boeing Company (77272) |