AIRCRAFT STRUCTURAL Parts 1560-00-000-0047 through 1560-00-001-6972 |
|
|
| Leading Edge Sourcing Services |
 |
|
We solve sourcing challenges for parts like 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 -- hard to find, long lead time, and obsolete part requirements.
|
 |
|
|
1 2 3 3 4 5 6 7 8 9 11 12 14 15 16 17 18 19 20 20 21 22 23 23 24 25 26 27 28 29 31 32 34 35 36 37 38 39 40 40 41 42 43 43 44 45 46 46 47 48 49 51 52 54 55 1 4 6 7 9 10 12 13 15 18 21 24 26 27 29 30 32 33 35 38 41 44 47 49 50 52 53 55 56 57 58 59 60 62 63 64 65 66 67 68 70 71 73 74 76 77 79 80 82 83 84 85 86 87 88 90 91 93 94 96 97 99 100 5 8 11 14 17 25 28 31 34 37 45 48 51 54 57 58 60 61 63 64 65 66 67 68 69 71 72 74 75 77 78 80 81 83 84 86 87 88 89 90 91 92 94 95 97 98 100 61 69 72 75 78 81 89 92 95 98 2 10 13 16 19 22 30 33 36 39 42 50 53 56 59 62 70 73 76 79 82 85 93 96 99 >>>
|
| 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 |