AIRCRAFT HELICOPTER COMPONENTS Parts 1615-00-434-8200 through 1615-00-437-7535 |
|
|
| Leading Edge Sourcing Services |
 |
|
We solve sourcing challenges for parts like 1615-00-434-8200, 1615-00-434-8291, 1615-00-434-8294, 1615-00-434-8336, 1615-00-434-8342, 1615-00-434-8345, 1615-00-434-8363, 1615-00-434-8411, 1615-00-434-8421, 1615-00-434-8467 -- hard to find, long lead time, and obsolete part requirements.
|
 |
|
|
1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 >>>
|
| Part number | Description | Category | Details |
1615-00-434-8200 | BAR, LINK, PITCH CONT | | |
1615-00-434-8291 | GEAR, TRANSMISSION F | | |
1615-00-434-8294 | RETAINER | | |
1615-00-434-8336 | GEAR ASSEMBLY, GENER | | |
1615-00-434-8342 | SLEEVE | | |
1615-00-434-8345 | GEAR ASSEMBLY, GENER | | |
1615-00-434-8363 | HOUSING, TRANSMISSIO | | |
1615-00-434-8411 | CASE ASSEMBLY, TRANS | | |
1615-00-434-8421 | GUIDE, FREE WHEEL RO | | |
1615-00-434-8467 | YOKE, TAIL ROTOR DRI | | |
1615-00-434-8469 | PLUG, TAIL ROTOR DRIVE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY QQ-A-354 COMP 24S-T4 COND T,DIM.,0.493 IN. MIN,0.498 IN.MAX BODY OD,0.625 IN. NOM BODY LG,0.248 IN. MIN,0.250 IN. MAX CENTEREXTENSION OD,0.500 IN. NOM CENTER EXTENSION LG,0.156 IN. CHAMFER LG BY 15DEG ON EXTENSION END,1.125 IN. NOM O/A LG,BODY OD DRILLED THRU BY 0.312IN. DIA HOLE 0.256 IN. FROM EXTENSION END |
1615-00-434-8514 | SHAFT ASSEMBLY, TAIL | | |
1615-00-434-8517 | SHAFT ASSEMBLY, TAIL | | |
1615-00-434-8521 | SHAFT ASSEMBLY, TAIL | | |
1615-00-434-8541 | CAP, TAIL ROTOR DRIV | | |
1615-00-434-8542 | CAP, TAIL ROTOR DRIV | | |
1615-00-434-8682 | STRAINER, TRANSMISSI | | |
1615-00-435-0247 | YOKE, MAIN ROTOR ASSEMBLY | GENERAL CHARACTERISTICS ITEM DESCRIPTION | SUPPORT ASSEMBLY YOKE |
1615-00-436-0523 | TUBE, OIL TRANSFER, OIL COOLER | GENERAL CHARACTERISTICS ITEM DESCRIPTION | C/O LINER,NYLON,3.130 IN. LG;COVER,3-PLY NYLON,3.130 IN. LG;2 CUFFS,0.700 IN. LG,6-PLY NYLON;3 RINGS,CRES,0.060 IN. DIA LOCATED ALONG LG OF INTERIOR COVER,0.650 IN. APART APPROX;1 FLANGE,ALUM,0.180 IN. THK BY 2.200 IN. OD BY 0.794 IN. ID W/THREE 0.261 IN. DIA HOLES ON 2.250 IN. DIA BOLT CIRCLE;1 FLANGE,ALUM,0.794 IN. ID W/TWO HOLES 1.106 IN. FROM CENTER;EXTERIOR COATING,SILICONE RUBBER,3.130 IN. LG;3.490 IN. LG O/A;150.000 PSI PROOF PRESSURE;300.000 PSI BURST PRESSURE;TEMP RANGE MINUS65.0 DEG F TO PLUS 350.0 DEG F |
1615-00-436-0557 | GEARBOX, ACCESSORY DRIVE, TURBINE ENGINE | | |
1615-00-436-0559 | SEAL AND HOUSING AS | | |
1615-00-436-0560 | JET ASSEMBLY, GEARBO | | |
1615-00-436-1835 | SCISSORS AND SLEEVE | III END ITEM IDENTIFICATION | UH-1, ROTARY WING AIRCRAFT |
1615-00-437-2621 | PLATE, LOCK | | |
1615-00-437-7535 | STOP, ROTARY RUDDER | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL,CORROSION RESISTING AMS5355COMP 17-4PH,PASSIVATED BPS FW4007,SHAPE,FLANGED SLEEVE,DIM.,2.750 IN. NOM O/A FLANGE LG,0.640 IN. NOM FLANGE W ON EACH END,1.620 IN. NOM O/A CENTER W,0.290 IN. NOM FLANGE THK AT CENTER,0.250FLANGE THK AT ENDS,1.530 IN. NOM BODY OD BY 0.580 IN. LG,ID INVOLUTE SPLINE DATA,FLAT ROOT SPLINE SIDE BEARING SLIDING CLASS A FIT,40 TEETH THEORETICAL W/MASTER TOOTH LOCATED AT 90.0 DEG,32/64 DIAMETRAL PITCH,30.0 DEG PRESSURE ANGLE,1.2500 IN. PITCH DIA,1.2188 IN. MIN,1.2203 IN. MAX MINOR DIA,1.2915 IN. MIN,1.2996 IN. MAX MAJOR DIA |