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| Part number | Description | Category | Details |
1560-00-001-2559 | SUPPORT, STRUCTURAL COMPONENT, AIRCRAFT | | |
1560-00-003-1605 | FITTING, SUPPORT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,ANODIZED,8.172 IN. LG,1.750 IN. W,GM20153FSCM26512 |
1560-00-003-1606 | FITTING, SUPPORT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,ANODIZED,8.172 IN. LG,1.750 IN. W,GM20153FSCM26512 |
1560-00-003-1614 | FITTING, COVE SUPPORT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL,AMS5643,PASSIVATE MIL-S-5002,3.797 IN. LG,IRREGULAR SHAPED |
1560-00-003-1615 | FITTING, COVE SUPPORT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL,AMS5643,PASSIVATE MIL-S-5002,3.797 IN. LG,IRREGULAR SHAPED |
1560-00-003-2027 | SUPPORT, STRUCTURAL COMPONENT, AIRCRAFT | AIRCRAFT MISSION DESIGN SERIES | KC-135 |
1560-00-003-7324 | BOSS, IDLER SUPPORT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL,4340,MIL-S-5000 |
1560-00-004-1433 | SUPPORT, STRUCTURAL COMPONENT, AIRCRAFT | MATERIAL | STEEL |
1560-00-004-1435 | SUPPORT, STRUCTURAL COMPONENT, AIRCRAFT | MATERIAL | ALUMINUM ALLOY 2024 |
1560-00-004-1436 | SUPPORT, STABILIZER, HORIZONTAL | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 39.300 IN. O/A LG |
1560-00-004-3046 | SUPPORT, PROBE, FUEL QUANTITY | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,0.850 IN. THK |
1560-00-004-3065 | SUPPORT, HARNESS | GENERAL CHARACTERISTICS ITEM DESCRIPTION | POLYAMIDE GM4104BFA FSCM 26512,0.750 IN. LG,0.938 IN. W,0.500 IN. THK |
1560-00-004-3066 | SUPPORT, HARNESS | GENERAL CHARACTERISTICS ITEM DESCRIPTION | POLYAMIDE GM4104BFA FSCM 26512,0.750 IN. LG,0.938 IN. W,0.500 IN. THK |
1560-00-004-3067 | SUPPORT, HARNESS | GENERAL CHARACTERISTICS ITEM DESCRIPTION | POLYAMIDE GM4104BFA FSCM 26512,1.125 IN. LG,0.938 IN. W,0.500 IN. THK |
1560-00-004-3068 | SUPPORT, HARNESS | GENERAL CHARACTERISTICS ITEM DESCRIPTION | POLYAMIDE GM4104BFA FSCM 26512,1.750 IN. LG,0.938 IN. W,0.500 IN. THK |
1560-00-004-5517 | SUPPORT, TUBING | GENERAL CHARACTERISTICS ITEM DESCRIPTION | PLASTIC,THERMOSETTING,1.113 IN. LG,0.450 IN. W,0.408 IN. H ON LHEND,0.555 IN. H ON RH END,0.217 IN. MIN,0.226 IN. MAX DIA OF HOLE FORBOLT ON RH END,0.313 IN. MIN,0.315 IN. MAX RADIUS OF CONTOUR FOR TUBING,P6073-1,FSCM 81755 |
1560-00-004-5518 | SUPPORT, TUBING | GENERAL CHARACTERISTICS ITEM DESCRIPTION | PLASTIC,THERMOSETTING,1.113 IN. LG,0.450 IN. W,0.408 IN. H,0.217IN. MIN,0.226 IN. MAX DIA HOLE FOR BOLT ON RH END,0.313 IN. MIN,0.315IN. MAX RADIUS OF CONTOUR FOR TUBING,P6073-1,FSCM 81755 |
1560-00-005-0130 | CHANNEL, FLAP SUPPORT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY QQ-A-250/5 |
1560-00-005-1811 | SUPPORT, STRUCTURAL COMPONENT, AIRCRAFT | | |
1560-00-005-1821 | SUPPORT, STRUCTURAL COMPONENT, AIRCRAFT | | |
1560-00-005-1825 | SUPPORT, STRUCTURAL COMPONENT, AIRCRAFT | MATERIAL | ALUMINUM ALLOY |
1560-00-005-1834 | SUPPORT, STRUCTURAL COMPONENT, AIRCRAFT | MATERIAL | ALUMINUM ALLOY 6061 |
1560-00-005-3714 | SUPPORT, STRUCTURAL COMPONENT, AIRCRAFT | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-367 FED SPEC SINGLE MATERIAL RESPONSE |
1560-00-005-3715 | SUPPORT, BELLCRANK | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,QQ-A-367,CONDITION T411,ANODIZED |
1560-00-005-6795 | SUPPORT, STRUCTURAL COMPONENT, AIRCRAFT | MATERIAL | ALUMINUM ALLOY 2024 |