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| Part number | Description | Category | Details |
113346 | CLIP, SWITCH | | |
CA302 | COUPLING, DEAD RECKONING | GENERAL CHARACTERISTICS ITEM DESCRIPTION | SPUR GEAR 1,BUSHING 1,SHAFT EXTENSION 1,TORSION SPRING 1,SHAFT COLLAR 1,0.780 IN LG,0.4424 IN MIN AND 0.4444 IN MAX DIA |
537-200-022 | ELECTRONIC CHASSIS | | |
2555105 | PARTS KIT, OVERHAUL, | | |
2555105 | PARTS KIT, OVERHAUL, | | |
629743 | POWER SUPPLY, INERTI | | |
FDW31 | FLIGHT SLIDE RULE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | CIRCULAR,ALUMINUM MATERIAL,COMPUTES TIME,AIR SPEED,DENSITY ALTITUDE,DISTANCE,RATE OF FUEL CONSUMPTION,TRUE,ABSOLUTE AND PRESSURE ALTITUDE,CONVERTS NAUTICAL MILES TO STATUTE MILES,FARENHEIT TO CELSIUS TEMPERATURE READINGS,KILOMETERS TO EITHER STATUTE OR NAUTICAL MILES,INCLUDES SCALE OF TEMPERATURE CORRECTIONS VS TRUE AIR SPEED AND PROTRACTOR,4.000 IN. O/A DIA,0.047 IN. O/A H |
FDW31 | FLIGHT SLIDE RULE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | CIRCULAR,ALUMINUM MATERIAL,COMPUTES TIME,AIR SPEED,DENSITY ALTITUDE,DISTANCE,RATE OF FUEL CONSUMPTION,TRUE,ABSOLUTE AND PRESSURE ALTITUDE,CONVERTS NAUTICAL MILES TO STATUTE MILES,FARENHEIT TO CELSIUS TEMPERATURE READINGS,KILOMETERS TO EITHER STATUTE OR NAUTICAL MILES,INCLUDES SCALE OF TEMPERATURE CORRECTIONS VS TRUE AIR SPEED AND PROTRACTOR,4.000 IN. O/A DIA,0.047 IN. O/A H |
MARK8C | FLIGHT SLIDE RULE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | CIRCULAR,ALUMINUM MATERIAL,COMPUTES TIME,AIR SPEED,DENSITY ALTITUDE,DISTANCE,RATE OF FUEL CONSUMPTION,TRUE,ABSOLUTE AND PRESSURE ALTITUDE,CONVERTS NAUTICAL MILES TO STATUTE MILES,FARENHEIT TO CELSIUS TEMPERATURE READINGS,KILOMETERS TO EITHER STATUTE OR NAUTICAL MILES,INCLUDES SCALE OF TEMPERATURE CORRECTIONS VS TRUE AIR SPEED AND PROTRACTOR,4.000 IN. O/A DIA,0.047 IN. O/A H |
6528000283 | INTEGRATED CIRCUIT | | |
569-21-000 | STROBE ASSEMBLY, RED | III END ITEM IDENTIFICATION | AIRCRAFT MODEL S-2E |
569-22-000 | STROBE ASSEMBLY, GREEN | III END ITEM IDENTIFICATION | AIRCRAFT MODEL S-2E |
569-3-025 | SOLENOID AND FLAG | III END ITEM IDENTIFICATION | AIRCRAFT MODEL S-2E |
569-13-000 | TIMER ASSY | | |
3308-950 | SERVOMECHANISM, DRIVE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | C/O CAM CLUSTER 1 P/N 3450-610,CAM SUBASSEMBLY 1 P/N 3318-674,SPUR GEAR CLUSTER 1 P/N 3318-508,SPUR GEAR CLUSTER 3 P/N 3318-507,GEARSHAFT AND GEAR SUBASSEMBLY 2 P/N 3318-505 AND 3318-506,GEAR CLUSTER AND SHAFT SUBASSEMBLY 1 P/N 3318-504,GEAR AND SHAFT SUBASSEMBLY 1 P/N 3318-503,RELAY 1 P/N 3158-309,RESISTOR 1 P/N 3318-543 |
3308-970 | SERVOMECHANISM, DRIVE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | O/A DIM. 4.59375 IN. LG,2.6875 IN. W |
3306-761 | BRACKET, FUSE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | C/O OVAL HEAD TUBULAR RIVET (0.123 IN. DIA,0.156 IN. LG) P/N MS16535-53; BRACKET P/N 3450-627; ELECTRICAL CLIP |
3158-185 | BRACKET, TEST POINT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | C/O TERMINAL 18,JACK,TIP 1,TERMINAL BRACKET 28 |
3318-504 | GEARS AND SHAFT ASSEMBLY | GENERAL CHARACTERISTICS ITEM DESCRIPTION | MATL CADMIUM PLATED,QQ-P-416,TYPE II,CLASS 3; C/O GEAR,SPUR,60T P/N 3318-525,GEAR,CLUSTER P/N 3318-520,SHAFT,SHOULDERED |
3318-674 | CAM, ASSEMBLY | GENERAL CHARACTERISTICS ITEM DESCRIPTION | CONSISTS OF CONTROL CAM,3318-335,1; CAM HUB,3318-533,1; LOCK WASHER,1710-00,1; SURFACE TREATMENT PASSIVATED |
3450-628 | BEARING MAIN PLATE | | |
3306-774 | RIDER RIM AND MOVER | | |
3306-773 | RIDER RIM AND MOVER | GENERAL CHARACTERISTICS ITEM DESCRIPTION | C/O RIDER RIM 1 P/N 3158-180; HUB 1 P/N 3306-757; GEAR SPUR (30T)1 P/N 3306-768; GEAR SPUR,PARTIAL(2T)1 P/N 3306-771; SPRING PIN 1 P/N MS51923-122 |
158-300 | TERMINAL BRACKET AS | GENERAL CHARACTERISTICS ITEM DESCRIPTION | C/O TERMINAL BRACKET 1 P/N 3158-301; TERMINAL BOARD SUBASSEMBLY 1 P/N 3158-301 |
3158-300 | TERMINAL BRACKET AS | GENERAL CHARACTERISTICS ITEM DESCRIPTION | C/O TERMINAL BRACKET 1 P/N 3158-301; TERMINAL BOARD SUBASSEMBLY 1 P/N 3158-301 |