2195000-17: CYLINDER ASSEMBLY,ACTUATING,LINE.
CYLINDER ASSEMBLY,ACTUATING,LINE. Key specifications include extended_length: 33.830 INCHES MINIMUM AND 33.870 INCHES MAXIMUM IN, compressed_length: 24.250 INCHES NOMINAL IN, body_outside_diameter: 2.560 INCHES MINIMUM AND 2.570 INCHES MAXIMUM IN, design_characteristics: DOUBLE ACTING SINGLE CYLINDER, end_item_identification: F101-GE-102 ENGINE,B1-B AIRCRAFT, first_end_outside_diameter: UNABLE TO DECODE. This part is cataloged in the U.S.
Government catalog under NSN 1650-01-147-9117, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| extended_length | 33.830 INCHES MINIMUM AND 33.870 INCHES MAXIMUM IN |
| special_features | INCL SENSOR W/ELEC CONNECTOR PER GE M50TF3018,CL-B,TY 10-5-P10,LOCATED AT END OF MTG FACILITY 2.50 IN. CEN-TO-END; ASSY FOR EXHAUST NOZZLE-LVDT IN |
| compressed_length | 24.250 INCHES NOMINAL IN |
| body_outside_diameter | 2.560 INCHES MINIMUM AND 2.570 INCHES MAXIMUM IN |
| design_characteristics | DOUBLE ACTING SINGLE CYLINDER |
| end_item_identification | F101-GE-102 ENGINE,B1-B AIRCRAFT |
| first_end_outside_diameter | UNABLE TO DECODE |
| first_piston_rod_end_style | UNABLE TO DECODE |
| mounting_type_and_location | RING CYLINDER HEAD END |
| integral_valve_operation_method | HYDRAULIC |
| reference_number_differentiating_characteristics | AS DIFFERENTIATED BY SOURCE CONTROL NO. 9338M42 |
| NSN | 1650-01-147-9117 |
| COMPRESSED LENGTH | 24.250 INCHES NOMINAL IN |
| EXTENDED LENGTH | 33.830 INCHES MINIMUM AND 33.870 INCHES MAXIMUM IN |
| DESIGN CHARACTERISTICS | DOUBLE ACTING SINGLE CYLINDER |
| BODY OUTSIDE DIAMETER | 2.560 INCHES MINIMUM AND 2.570 INCHES MAXIMUM IN |
| FIRST PISTON ROD END STYLE | UNABLE TO DECODE |
| SPECIAL FEATURES | INCL SENSOR W/ELEC CONNECTOR PER GE M50TF3018,CL-B,TY 10-5-P10,LOCATED AT END OF MTG FACILITY 2.50 IN. CEN-TO-END; ASSY FOR EXHAUST NOZZLE-LVDT IN |
| END ITEM IDENTIFICATION | F101-GE-102 ENGINE,B1-B AIRCRAFT |
| INTEGRAL VALVE OPERATION METHOD | HYDRAULIC |
| MOUNTING TYPE AND LOCATION | RING CYLINDER HEAD END |
| FIRST END OUTSIDE DIAMETER | UNABLE TO DECODE |