AIRCRAFT HELICOPTER COMPONENTS Parts 1615-00-137-2911 through 1615-00-141-0080 |
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We solve sourcing challenges for parts like 1615-00-137-2911, 1615-00-137-2917, 1615-00-137-2920, 1615-00-138-8489, 1615-00-138-8495, 1615-00-138-9430, 1615-00-138-9431, 1615-00-138-9432, 1615-00-138-9437, 1615-00-138-9438 -- hard to find, long lead time, and obsolete part requirements.
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| Part number | Description | Category | Details |
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1615-00-137-2911 | GUIDE, SPECIAL | | |
1615-00-137-2917 | SHAFT, CONTROL | GENERAL CHARACTERISTICS ITEM DESCRIPTION | CRES,5.153 IN. LG,0.875 IN. DIA |
| 1615-00-137-2920 | GUIDE, SPECIAL | | |
| 1615-00-138-8489 | HEAD, ROTARY WING | III END ITEM IDENTIFICATION | AIRCRAFT MODEL H3-A |
| 1615-00-138-8495 | SOCKET, SWASHPLATE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 9.743 IN MIN,9.746 IN MAX,O/A LG,1.370IN NOM O/A H |
| 1615-00-138-9430 | BALANCE ASSY | | |
| 1615-00-138-9431 | FLANGE, COUPLING | | |
| 1615-00-138-9432 | BALANCE ASSY | | |
| 1615-00-138-9437 | HOUSING ASSEMBLY | | |
| 1615-00-138-9438 | | | |
| 1615-00-138-9484 | SHAFT ASSEMBLY, DRIV | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ZINC CHROMATE FINISH,FLANGE COUPLING,SHAFT DYNAMICALLY BALANCED |
| 1615-00-138-9486 | SHAFT ASSEMBLY, DRIV | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ZINC CHROMATE FINISH,FLANGE COUPLING,SHAFT DYNAMICALLY BALANCED |
| 1615-00-138-9507 | RETAINER, SPECIAL | | |
| 1615-00-139-1489 | GEAR BOX ASSEMBLY | | |
| 1615-00-139-1490 | GEARBOX, ACCESSORY DRIVE, TURBINE ENGINE | | |
| 1615-00-139-1513 | GEARBOX, ACCESSORY DRIVE, TURBINE ENGINE | | |
| 1615-00-139-6160 | AZIMUTH ASSEMBLY | | |
| 1615-00-139-6509 | | | |
| 1615-00-139-9302 | SPINDLE, HEAD, ROTARY WING | | |
| 1615-00-140-3015 | | | |
| 1615-00-140-4566 | CLIP-LOCK, MAIN ROTO | | |
| 1615-00-140-4595 | GEAR BOX ASSY, ROTOR | | |
| 1615-00-141-0078 | RETAINER, BALLAST, ROTARY WING BLADE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL,CORROSION RESISTANT,MIL-S-5059,COMP 301 OR 302,PASSIVATED PER BPS FW 4007,SHAPE,OCTAGON,DIM.,2.000 IN. O/A HT,1.800 IN. O/A WIDTH 0.140 IN. MATERIAL THK,0.320 IN. TOP WIDTH,0.500 IN. BOTTOM WIDTH,1.800 IN. MAX WIDTH 0.470 IN. FROM TOP,1.520 IN. NOM WIDTH 0.470 IN. FROM BOTTOM,ONE HOLE 0.320 IN. MIN,0.328 IN. MAX DIA ON VERTICAL CENTERLINE 0.500 IN. FROM TOP AND 0.500 IN. FROM BOTTOM W/1.100 IN. DISTANCE BETWEEN CENTERS,USED ON MAIN ROTOR OF HUB AND BLADE ASSEMBLY |
| 1615-00-141-0079 | RETAINER, WEIGHT, ROTARY WING BLADE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY QQ-A-250/4 COMP 2024-T3,CHEMICAL FILM TREATED BPS FW4182BELL HELICOPTER CO,DIM.,2.050 IN. NOM LG,1.650 IN. NOM W 1.280 IN. FROMBOTTOM,1.800 IN. NOM W 0.530 IN. FROM BOTTOM,0.160 IN. NOM THICK,LOWERCORNERS CHAMFERED 0.530 IN. LG BY 0.500 IN. DEEP,UPPER CORNERS CHAMFERED0.770 IN. LG BY 0.425 IN. DEEP,ONE THRU SLOT 0.650 IN. LG W/ENDS ROUNDED BY0.188 IN. RADIUS LOCATED ON VERTICAL CENTERLINE 0.100 IN. FROM BOTTOM,ONETHRU SLOT 0.750 IN. LG W/ENDS ROUNDED BY 0.188 IN. RADIUS LOCATED ONVERTICAL CENTERLINE 0.200 IN. FROM TOP |
| 1615-00-141-0080 | LOCK PLATE, RETAINER | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL,COMP 1010 THRU 1025,CADMIUM-PLATED QQ-P-416 CLASS 2 TYPE 2,DIM.,2.050 IN. NOM LG,0.800 IN. NOM W,0.032 IN. NOM THICK,TWO HOLES 0.380 IN. DIADRILLED THRU ON VERTICAL CENTERLINE AND 0.510 IN. FROM NOTCHED END W/1.100IN. CENTER TO CENTER DISTANCE,ONE NOTCH ON EACH SIDE OF VERTICAL CENTERLINE0.150 IN. W BY 0.330 IN. LG W/CENTER SECTION 0.500 IN. WIDE |
