AIRCRAFT HELICOPTER COMPONENTS Parts 1615-00-027-9531 through 1615-00-040-8125 |
|
|
| Leading Edge Sourcing Services |
 |
|
We solve sourcing challenges for parts like 1615-00-027-9531, 1615-00-029-9475, 1615-00-030-6488, 1615-00-030-6512, 1615-00-030-6515, 1615-00-030-6516, 1615-00-030-7199, 1615-00-030-9348, 1615-00-030-9419, 1615-00-031-5235 -- 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 |
|---|
1615-00-027-9531 | TAB, TAIL GEAR BOX | GENERAL CHARACTERISTICS ITEM DESCRIPTION | MATL STL PER MIL-S-18729,MIN TENSILE STRENGTH RC26-33 PER MIL-H-6875,CADMIUM PLATE PER QQ-P-416; OVAL SHAPE 0.090IN. THK,2.440IN. L,ONE HOLE 0.531IN. DIA,ONE HOLE 0.343IN. DIA |
1615-00-029-9475 | BLADE, FAN ENGINE | | |
| 1615-00-030-6488 | CABLE ASSEMBLY, TAIL | | |
| 1615-00-030-6512 | FORK WELD ASSEMBLY, | | |
| 1615-00-030-6515 | WEIGHT, TAIL ROTOR BLADE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL,FED STD 66 COMP 1010 OR MIL-S-7952 COMP 1020,DIM.,1.180 IN. NOMLG ARC SEGMENT OF 5.000 IN. ID,5.250 IN. OD BY 13.5 DEG W,0.250 IN. NOM W0.050 IN. NOM THICK,TWO HOLES 0.096 IN. DIA DRILLED THRU ON 5.125 IN. BOLTCIRCLE 0.250 IN. FROM EACH END,MAX SURFACE FINISH,ALL SURFACES 63MICROINCHES AA |
| 1615-00-030-6516 | WEIGHT, TAIL ROTOR BLADE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL,FED STD 66 COMP 1010,DIM.,1.180 IN. NOM LG ARC SEGMENT OF 5.000IN. ID,5.250 IN. OD BY 13.5 DEG W,0.250 IN. NOM W,0.025 IN. NOM THICK,TWOHOLES 0.096 IN. DIA DRILLED THRU ON 5.125 IN. BOLT CIRCLE 0.250 FROM EACHEND,MAX SURFACE FINISH,ALL SURFACES 63 MICROINCHES AA |
| 1615-00-030-7199 | RETAINER, MAIN ROTOR, TRUNNION | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY QQ-A-725/6 ALLOY 7024 TEMPER T351,ANODIZED PER PBSFW4001,BELL HELICOPTER CO,DIM.,3.380 IN. NOM O/A DIA,1.376IN. NOM W,0.250 IN. NOM THK ENDS,0.370 IN. MIN,0.380 IN. MAX THK RAISED CENTERSECTION,RAISED CENTERROUNDED ON 0.500 IN. RADIOS ON 2.620 IN. NOM DIA BOTHSIDES,FOUR BOLT HOLES 0.327 IN. MIN,0.333 IN. MAX DIA,BOLT HOLE CENTERTO CENTER DISTANCE ON LONGITUDINAL SIDE 1.115 IN. NOM,BOLT HOLE CENTER TOCENTER DISTANCE ON W SIDE 0.750IN. NOM,PENETRANT INSPECTED PER BPS FW4089BELL HELICOPTER CO |
| 1615-00-030-9348 | CAP, ROTARY WING HUB | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,4.940 IN. DIA,1.118 IN. LG |
| 1615-00-030-9419 | LINEAR, GEAR BOX | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL,4.930 IN. MIN,4.931 IN. MAX LG,1.045 IN. W |
| 1615-00-031-5235 | | | |
| 1615-00-032-5652 | PIN, WOBBLE RING | | |
| 1615-00-033-6313 | HUB, ROTOR, HELICOPTER | | |
| 1615-00-033-6314 | TRUNNION, MAIN ROTOR | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL,AMS6414 COMP 4340,CADMIUM- PLATED QQ-P-416 CLASS 2 TYPE 2 O/A EXCEPT SPLINES,DIM.,10.430 IN. NOM O/A LG,5.200 IN. NOM CENTER W,4.350 IN. NOM CENTER LG,1.848 IN. MIN,1.849 IN. MAX LEFT AND RIGHT ARM DIA,0.750 IN. NOM LEFT AND RIGHT ARM LG,0.625 IN. NOM LEFT AND RIGHT ARM ID,TRUNNION INTERNAL SPLINE DATA,FILLET ROOT SPLINE,SIDE BEARING SLIDING CLASS A FIT,38 TEETH,10/20 DIAMETRAL PITCH,30.0 DEG PRESSURE ANGLE,3.8000 IN. PITCH DIA,3.7000 IN. MIN,3.7025 IN. MAX MINOR DIA,3.9800 IN. MIN,3.9950 IN. MAX MAJOR DIA |
| 1615-00-033-8166 | PLATE, HOISTING | | |
| 1615-00-033-8172 | RING ASSEMBLY | | |
| 1615-00-033-8208 | FILTER ASSEMBLY, OIL | | |
| 1615-00-033-8247 | CAP, OIL PRESSURE | | |
| 1615-00-034-4141 | ROTOR ASSEMBLY | | |
| 1615-00-034-4142 | RING ASSEMBLY | | |
| 1615-00-040-8101 | FAIRING ASSEMBLY, RO | | |
| 1615-00-040-8106 | FAIRING ASSEMBLY, RO | | |
| 1615-00-040-8109 | FAIRING ASSEMBLY, RO | | |
| 1615-00-040-8115 | FAIRING ASSEMBLY, RO | | |
| 1615-00-040-8118 | FAIRING ASSEMBLY, RO | | |
| 1615-00-040-8125 | FAIRING ASSEMBLY, RO | | |
