1560-00-000-0047 through 1560-00-001-6972 AIRCRAFT STRUCTURAL |
Parts listed on this page: AIRCRAFT STRUCTURAL 1560-00-000-0047, 1560-00-000-0105, 1560-00-001-1849, 1560-00-001-1850, 1560-00-001-1851, 1560-00-001-2478, 1560-00-001-2479, 1560-00-001-2480, 1560-00-001-2481, 1560-00-001-2483, 1560-00-001-2484, 1560-00-001-2485, 1560-00-001-2486, 1560-00-001-2500, 1560-00-001-2501, 1560-00-001-3925, 1560-00-001-3926, 1560-00-001-5501, 1560-00-001-5570, 1560-00-001-6883, 1560-00-001-6885, 1560-00-001-6886, 1560-00-001-6887, 1560-00-001-6892, 1560-00-001-6972
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| Leading Edge Sourcing Services |
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We solve sourcing challenges for parts like 1560-00-000-0047,1560-00-000-0105,1560-00-001-1849,1560-00-001-1850 -- hard to find, long lead time, and obsolete part requirements.
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| Part number | Description | Category | Details |
1560-00-000-0047 | MODIFICATION KIT, AIRFRAME | COMPONENT QUANTITY | 4 |
1560-00-000-0105 | CAP, FILLER OPENING | | |
1560-00-001-1849 | GYRO BOX ASSEMBLY | III END ITEM IDENTIFICATION | AIRCRAFT MODEL TA-4J |
1560-00-001-1850 | RADOME | RADOME FLEXIBILITY | RIGID |
1560-00-001-1851 | RADOME | RADOME FLEXIBILITY | RIGID |
1560-00-001-2478 | HINGE, LEADING EDGE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,MMS158 COMP 7075 TEMPER T7351 |
1560-00-001-2479 | HINGE, LEADING EDGE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL |
1560-00-001-2480 | HINGE, LEADING EDGE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL |
1560-00-001-2481 | HINGE, LEADING EDGE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL |
1560-00-001-2483 | HINGE, LEADING EDGE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,MMS158,COMP 7075,TEMPER T7351,20.298 IN. O/A LG,2.855 IN. O/A W,1.640 IN. O/A H,67 HOLES FOR 0.250 IN. TAPER-LOK MATED TO EXISTING HOLES IN AIRFRAME |
1560-00-001-2484 | HINGE, LEADING EDGE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,MMS158 COMP 7075 TEMPER T7351 |
1560-00-001-2485 | HINGE, LEADING EDGE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL |
1560-00-001-2486 | HINGE, LEADING EDGE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL |
1560-00-001-2500 | WEIGHT, COUNTERBALANCE | | |
1560-00-001-2501 | WEIGHT, COUNTERBALANCE | | |
1560-00-001-3925 | HEAT SHIELD ASSEMBLY | III END ITEM IDENTIFICATION | AIRCRAFT MODEL AV-8A |
1560-00-001-3926 | HEAT SHIELD ASSEMBL | III END ITEM IDENTIFICATION | AIRCRAFT MODEL AV-8A |
1560-00-001-5501 | GRIP, ENGINE QUADRANT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,A356-T6,MIL-A-21180 |
1560-00-001-5570 | STRAP, BONDING, OUTBOARD PYLON | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 17.800 IN. LG,3.620 IN. W |
1560-00-001-6883 | GUARD, CABLE PULLEY, PYLON | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,QQ-A-250/5,2024 TEMPER T3,1.760 IN. LG,1.740 IN. W,0.750 IN. H,W/2 HOLES IN LINE,2 PLACES,0.190 IN. MIN,0.196 IN. MAX DIA SPACED 1.300 IN. APART CENTER TO CENTER,2 HOLES IN LINE 0.251 IN. MIN,0.258 IN. MAX DIA |
1560-00-001-6885 | LOCK, ECCENTRIC BUSHING, PYLON TO WING | GENERAL CHARACTERISTICS ITEM DESCRIPTION | CRES,17-4PH,AMS5604,TEMPER H1025,3.000 IN. LG,3.000 IN. W,0.312 IN. THK,W/NAS580-16-35 SPLINE,2 MTG HOLES 0.280 IN. MIN,0.287 IN. MAX DIA SPACED 1.250 IN. CENTER TO CENTER |
1560-00-001-6886 | LOCK, ECCENTRIC BUSHING, PYLON TO WING | GENERAL CHARACTERISTICS ITEM DESCRIPTION | CRES,17-4PH,AMS5604,TEMPER H1025,4.700 IN. LG,3.000 IN. W,0.312 IN. THK,W/NAS580-8-29 SPLNE,2 MTG HOLES 0.280 IN. MIN,0.287 IN. MAX DIA SPACED 1.250 IN. CENTER TO CENTER |
1560-00-001-6887 | FLOOR, AIRCRAFT | MATERIAL | ALUMINUM ALLOY |
1560-00-001-6892 | FLOOR, AIRCRAFT | MATERIAL | ALUMINUM ALLOY 7075 |
1560-00-001-6972 | ADAPTER, PRESSURE FUEL SERVICING | SHAPE | CYLINDRICAL |
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