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| Part number | Description | Category | Details |
1615-00-050-6195 | RETAINER, HELICAL COMPRESSION SPRING | MATERIAL | ALUMINUM ALLOY, QQ-A-225/6, ALLOY 2024 |
1615-00-050-6196 | SUPPORT, TRANSMISSION | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL,MIL-S-5000 COMP 4340,SURFACE TREATMENT BLACK OXIDE MIL-C-13924 CLASS 1 GRADE A,ROCKWELL HARDNESS RATIMG C SCALE 50 TO 53,SHAPE,MODIFIED L,DIM.,1.190 IN. NOM O/A HT,0.880 IN. NOM O/A BOTTOM LG,0.600 IN. NOM FOOT LG,0.481 IN. MIN,0.491 IN. MAX W,0.100 IN. NOM MATERIAL THK,ONE MOUNTING HOLE 0.213 IN. MIN,0.219 IN. MAX DIA DRILLED THRU UPPER LEG 0.446 IN. FROM TOP ON VERTICAL CENTERLINE,45.0 DEG CORNER ANGLE BEGINNING 0.904 IN. FROM TOP BY 0.280 IN. LG,FLUORESCENT AND MAGNETIC PARTICLE INSPECTED PER BAC 5424 CLASS A |
1615-00-050-6199 | SCREEN ASSEMBLY, TRANSMISSION | GENERAL CHARACTERISTICS ITEM DESCRIPTION | BRASS,QQ-B-613 COMP 2 1/2 HARD FRAME,BRASS SCREEN 10 X 10 MESH 0.075 IN. OPENING,NO. 10 WIRE 0.028 IN. DIA,SCREEN SILVER SOLDERED MIL-B-7883 TO FRAME OR SILVER SOLDER MIL-B-15395 CLASS 7,DIM.,5.923 IN. NOM O/A LG,4.000 IN. NOM O/A W,0.780 IN. NOM O/A HT,0.063 IN. NOM MATERIAL THK,2.880 IN. NOM SCREEN W,4.188 IN. NOM SCREEN LG,TWO MOUNTING HOLES 0.257 IN. NOM DIA ON FRAME LG TOP AND BOTTOM,2.500 IN. DISTANCE BETWEEN CENTERS ON LG,4.000 IN. DISTANCE BETWEEN CENTERS ON W,ONE SLOT ONCENTER TAB RIGHT END 0.380 IN. LG BY 0.260 IN. W,ONE CENTER GUIDE SLOT ON LEFT END 0.180 IN. LG BY 0.256 IN. W |
1615-00-051-1596 | | | |
1615-00-051-1685 | | | |
1615-00-051-1689 | DRIVE SHAFT ASSEMBLY, TAIL ROTOR | III END ITEM IDENTIFICATION | H-53 HELICOPTER |
1615-00-051-3646 | CROSSHEAD ASSEMBLY | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY QQ-A-268 COMP 2024-T4,SURFACE TREATMENT ANODIZED BPS FW4001,DIM.,6.000 IN. NOM O/A LG,1.250 IN. NOM CENTER HT BY 1.300 IN. SQUARE CENTER,0.960 IN. NOM LEFT AND RIGHT ARM HT,1.062 IN. MIN,1.064 IN. MAX LEFT AND RIGHT ARM W,0.750 IN. MIN,0.752 IN. MAX LEFT AND RIGHT ARM END SLOT W,1.120 IN. NOM LEFT AND RIGHT ARM END SLOT DEPTH,TWO HOLES IN-LINE ON LEFT ANO RIGHT SLOT ENDS 0.3750 IN. DIA 2.500 IN. FROM CENTER,NO. 204-010-794-1 BUSHING INSTALLED IN EACH HOLE,0.900 IN. ID DRILLED IN BOTTOM CENTER BY 1.130 IN. DEEP AND COUNTERBORED 1.0236 IN. MIN,1.0241 IN. MAX DIA BY 0.605 IN. DEEP,ONE LUB FITTING NAS516-1 INSTALLED IN TOP CENTER THRU 0.1235 IN. DIA HOLE,ONE MOUNTING HOLE DRILLED ON TOP 1.063 IN. EACH SIDE OF CENTER 0.259 IN. DIA,ITEM USED ON TAIL ROTOR |
1615-00-051-4822 | HARNESS ASSEMBLY, WIRING | III END ITEM IDENTIFICATION | AIRCRAFT MODEL H-53 |
1615-00-051-4888 | HARNESS ASSY, WIRING | III END ITEM IDENTIFICATION | H-53 AIRCRAFT |
1615-00-051-4942 | CABLE ASSY, ROTOR | | |
1615-00-051-5007 | CABLE ASSY, ROTOR | | |
1615-00-051-5143 | ADAPTER, SPRING ASSEMBLY | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY QQ-A-268 COMP 2024-T4,ANODIZED MIL-A-8625 TYPE 1,DIM.,2.137 IN. NOM O/A LG,0.750 IN. NOM LEFT END FLANGE OD,0.062 IN. NOM FLANGE W,0.500 IN. NOM OD BY 1.637 IN.LG,0.312-24 UNF CLASS 3A EXTERNAL THREADS ON LEFT END OD BY 0.375 IN. LG NAS1394C3L INSERT INSTALLED IN RIGHT END ID,USED ON TRIM ACTUATOR |
1615-00-051-5630 | GEAR ASSEMBLY, TRANSMISSION | | |
1615-00-051-9586 | RETAINER, BALL BEARI | | |
1615-00-051-9587 | SWASH PLATE, ASSY RO | | |
1615-00-051-9599 | SWASH PLATE ASSY, AF | | |
1615-00-052-0408 | BLADE, ROTARY WING | | |
1615-00-052-4455 | GEAR ROTOR | | |
1615-00-052-4457 | GEAR ROTOR | | |
1615-00-053-3954 | ADJUSTER ASSEMBLY, ANTI-TORQUE CO NTROLS | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ASSEMBLY CONSIST OF 56 COMPONENTSU/O ANTI-TORQUE CONTROL SYSTEM |
1615-00-054-3534 | BRACKET, VERNIER SCALE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY AMS 4260 OR QQ-A-225/8 T6 OR QQ-A-200/8 COMP 6061-T6,ANODIZED PER MIL-A-8625,DIM.,2.330 IN. NOM O/A LG,1.500 IN. NOM W,0.120 IN. NOM MATERIAL THK,FIRST VERTICAL SECTION 0.480 IN. LG W/2.400 IN. SPHERICAL OD RADIUS,2ND SECTION BENT UPWARD AT 45.0 DEG ANGLE 1.000 IN. LG,3RD SECTION BENT DOWNWARD AT 55.0 DEG ANGLE 0.850 IN. LG,FIRST SECTION DRILLED W/ONE MOUNTING HOLE 0.200 IN. MIN,0.215 IN. DIA 10.0 DEG EACH SIDE OF VERTICAL CENTERLINE AND 0.168 IN. FROM TOP,ITEM USED ON TAIL ROTOR SLEEVE AND SPINDLE ASSEMBLY |
1615-00-054-3535 | SPINDLE ASSEMBLY, RO | GENERAL CHARACTERISTICS ITEM DESCRIPTION | CONSISTS OF THE FOLLOWING PARTS,2 WASHERS P/N 65112-07016-101;1 SPACER P/N 65112-07015-102;2 BUSHINGS P/N 20DU20;1 PLUG P/N 156102;1 SPINDLE P/N 65112-07001-104;1 SPACER P/N 6410-33335-102;1 BRACKET,VERNIER P/N 65112-07012-103 |
1615-00-054-3536 | SPACER ASSY, ROTARY | | |
1615-00-054-4729 | JET, OIL, GEARBOX | | |
1615-00-054-4733 | GEARBOX, INTERMEDIAT | | |