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| Part number | Description | Category | Details |
|---|
1560-00-031-4185 | FITTING ASY | | |
1560-00-031-4268 | FITTING ASSEMBLY | GENERAL CHARACTERISTICS ITEM DESCRIPTION | CONSISTS ONE FITTING MADE OF STEEL 4340 MIL-S-5000 P/N 89WM10395-7; ONE BUSHING P/N 89WM10407-1 |
| 1560-00-031-4272 | FITTING | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL; 14.910 INCH LENGTH; 12 HOLES 0.185 INCH NOMINAL DIA SPACED EQUALLY IN 8.250 INCH LENGTH |
| 1560-00-032-3529 | FITTING, HINGE, FUSE | III END ITEM IDENTIFICATION | H-3 HELICOPTER |
| 1560-00-032-3823 | FITTING, STRUCTURAL COMPONENT, AIRCRAFT | MATERIAL | ALUMINUM ALLOY |
| 1560-00-032-4272 | FITTING, STRUCTURAL COMPONENT, AIRCRAFT | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225/6 FED SPEC SINGLE MATERIAL RESPONSE |
| 1560-00-032-6630 | FITTING, STRUCTURAL COMPONENT, AIRCRAFT | AIRCRAFT MISSION DESIGN SERIES | C-141 |
| 1560-00-033-8095 | FITTING, DOOR, LANDING GEAR | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,7075-T73,MIL-A-22771,7.020 IN. LG,3.225 IN. W. |
| 1560-00-034-5108 | FITTING, STRUCTURAL COMPONENT, AIRCRAFT | III PART NAME ASSIGNED BY CONTROLLING AGENCY | SUPPORT ASSEMBLY, AILERON FEEL MECHANISM, UPPER-MID FUS SECT |
| 1560-00-034-6204 | FITTING, ARRESTING | GENERAL CHARACTERISTICS ITEM DESCRIPTION | IRONAMS 5735 COMP A286,2.150 IN. LG,2.350 ID |
| 1560-00-034-7603 | PLUG, PYLON HOIST FITTING | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,QQ-A-225/6,0.50 IN. THK,0.879 IN. DIA |
| 1560-00-034-9259 | FITTING ASSEMBLY, TAB | | |
| 1560-00-034-9382 | FITTING, CARRIAGE INBOARD FLAP | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,75S-T6,AMS4139 |
| 1560-00-034-9383 | FITTING, CARRIAGE INBOARD FLAP | | |
| 1560-00-034-9384 | FITTING ASSEMBLY, AILERON | | |
| 1560-00-034-9992 | FITTING, ENGINE MOUNT | | |
| 1560-00-035-0004 | FITTING, ANTIDRAG RING | | |
| 1560-00-035-0467 | FITTING ASSEMBLY, BO | | |
| 1560-00-035-2148 | FITTING, FORWARD CARGO DOOR LATCH | GENERAL CHARACTERISTICS ITEM DESCRIPTION | MAGNESIUM ALLOY,QQ-M-56 COMP AZ63A COND T6,2.710 IN. O/A LG,1.760 IN. O/A W,1.500 IN. O/A H,2 HOLES IN LINE 0.249 IN. MIN,0.257 IN. MAX DIA |
| 1560-00-035-2353 | FITTING, INNER WING DRAG | | |
| 1560-00-035-2382 | FITTING, STRUCTURAL COMPONENT, AIRCRAFT | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-367 FED SPEC SINGLE MATERIAL RESPONSE |
| 1560-00-035-3841 | FITTING, OPERATING CYLINDER | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,QQ-A-367 CLASS 5,15.312 IN. EFFECTIVE LG |
| 1560-00-035-3882 | FITTING, ROLLER SUPP | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY 356-T6,QQ-A-601,2 EA 0.625 IN. DIA IN LINE HOLES,1.125 IN. W CLEVIS GAP,2.312 IN. H CLEVIS CENTER |
| 1560-00-035-3888 | FITTING ASSEMBLY, AUXILIARY | | |
| 1560-00-035-4160 | FITTING ASSEMBLY, ENGINE TRUNNION | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL,MIL-S-6758 |
