2840-00-001-2117 through 2840-00-021-7488 SPACERS RETAINERS AND_MISCELLANEOUS HARDWARE ENGINES |
Parts listed on this page: SPACERS RETAINERS AND_MISCELLANEOUS HARDWARE ENGINES 2840-00-001-2117, 2840-00-001-8351, 2840-00-001-8352, 2840-00-003-9754, 2840-00-004-3966, 2840-00-004-4222, 2840-00-007-1436, 2840-00-008-2813, 2840-00-011-0698, 2840-00-011-5633, 2840-00-012-5039, 2840-00-015-1516, 2840-00-015-1660, 2840-00-015-1661, 2840-00-015-2165, 2840-00-015-2191, 2840-00-015-2203, 2840-00-015-2205, 2840-00-015-2213, 2840-00-018-3179, 2840-00-019-2573, 2840-00-021-3728, 2840-00-021-4545, 2840-00-021-4702, 2840-00-021-7488
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| Leading Edge Sourcing Services |
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We solve sourcing challenges for parts like 2840-00-001-2117,2840-00-001-8351,2840-00-001-8352,2840-00-003-9754 -- hard to find, long lead time, and obsolete part requirements.
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| Part number | Description | Category | Details |
2840-00-001-2117 | SLEEVE, DAMPER, TURBINE ENGINE | CRITICALITY CODE JUSTIFICATION | AGAV |
2840-00-001-8351 | PLATE, HIGH PRESSURE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL,AMS5545,IRREGULAR SHAPE,0.740 IN. MIN,0.750 IN. MAX,W,0.029IN. MIN,0.035 IN. MAX,THK,1.230 IN. APPROX LG,2 HOLES 0.150 IN. MIN,0.160 IN. MAX DIA,LOCATED 0.520 IN. APART,4 EMBOSSMENTS IRREGULARLY SHAPED |
2840-00-001-8352 | PLATE, SIDE, TURBINE | | |
2840-00-003-9754 | PLATE, COMPONENT MOUNTING, AIRCRAFT GAS TURBINE ENGI | MATERIAL | NICKEL ALLOY OVERALL |
2840-00-004-3966 | SHAFT AND COUPLING | | |
2840-00-004-4222 | COUPLING, SHAFT | | |
2840-00-007-1436 | COUPLING PRESSURE, PUMP | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL,5.515 IN. LG,1.9900 IN. DIA,SPUR GEAR ONE END 17 TEETH,0.9020 IN. DITCH DIA |
2840-00-008-2813 | RINGS, SEGMENTS, DRUM | | |
2840-00-011-0698 | PLATE, COMPONENT MOUNTING, AIRCRAFT GAS TURBINE ENGI | MATERIAL | STEEL CORROSION RESISTING OVERALL |
2840-00-011-5633 | SLEEVE, LINK SOCKET | GENERAL CHARACTERISTICS ITEM DESCRIPTION | NICKEL ALLOY AMS5663;2.925 MIN,2.975 MAX IN. LG |
2840-00-012-5039 | MANIFOLD ASSEMBLY, MAIN BEARING | GENERAL CHARACTERISTICS ITEM DESCRIPTION | THD INTERNAL TUBEFITTING ON EACH END |
2840-00-015-1516 | PLATE, MOUNTING STRA | | |
2840-00-015-1660 | PLATE, RETAINING TUB | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL AMS 5510,2.750 IN. BOLT CIRCLE,1.630 MIN IN. 1.635 MAX IN. DIA OF CENTER HOLE,0.090 MIN 0.110 MAX IN. W,0.276 MIN 0.286 MAX IN. DIA OF 3 HOLES EQ SP |
2840-00-015-1661 | PLATE, OIL TANK RETA | MATERIAL | STEEL |
2840-00-015-2165 | DAMPER, TURBINE FRONT BEARING | MATERIAL | STEEL CORROSION RESISTING |
2840-00-015-2191 | ADAPTER, TURBINE COUPLING | MATERIAL | STEEL CORROSION RESISTING |
2840-00-015-2203 | RING, INTERNAL SPLIN | CRITICALITY CODE JUSTIFICATION | AGAV |
2840-00-015-2205 | LOCK RING, RETAINING | CRITICALITY CODE JUSTIFICATION | AGAV |
2840-00-015-2213 | SPACER, TURBINE SHAFT, TURBINE ENGINE | MATERIAL | STEEL CORROSION RESISTING |
2840-00-018-3179 | RETAINER, SPRING, OIL | MATERIAL | STEEL CORROSION RESISTING |
2840-00-019-2573 | PLATE ASSY, OIL TANK | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 0.073 MIN,0.087 MAX IN. THK MATL;3.160 MIN,3.200 MAX IN. LG O/A;2.840 MIN,2.880 MAX IN. W O/A;ASSEMBLE FROM P/NS AN124972 RIVET,4,105B5366P3 PLATE,R401P2 NUT,R412P2 NUT |
2840-00-021-3728 | WEIGHT, COUNTER BALANCE, TURBINE ENGINE | | |
2840-00-021-4545 | PLATE, POSITIONING, C | | |
2840-00-021-4702 | PLATE, RETAINING, TUB | | |
2840-00-021-7488 | WEIGHT, COUNTER BALANCE, TURBINE ENGINE | | |
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