369162: IGNITER,SPARK,GAS TURBINE ENGINE.
IGNITER,SPARK,GAS TURBINE ENGINE. Key specifications include material: COPPER ALLOY OVERALL, ring_style: CONTRACTING CONCENTRIC, joint_style: DIAGONAL JOINT, overall_width: 0.3130 INCHES NOMINAL IN, inside_diameter: 2.062 INCHES MINIMUM AND 2.063 INCHES MAXIMUM IN, fsc_application_data: PUMP,ROTARY. This part is cataloged in the U.S.
Government catalog under NSN 2920-00-776-4482, 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.
| material | COPPER ALLOY OVERALL |
| ring_style | CONTRACTING CONCENTRIC |
| joint_style | DIAGONAL JOINT |
| overall_width | 0.3130 INCHES NOMINAL IN |
| inside_diameter | 2.062 INCHES MINIMUM AND 2.063 INCHES MAXIMUM IN |
| fsc_application_data | PUMP,ROTARY |
| radial_wall_thickness | 0.4300 INCHES MINIMUM AND 0.4320 INCHES MAXIMUM IN |
| cross-sectional_shape_style | PLAIN RECTANGULAR, STRAIGHT FACE |
| NSN | 2920-00-776-4482 |
| MOUNTING FACILITY SIZE | TWO 0.322 IN. DIA HOLES 1.510 IN. C TO C IN |
| LENGTH | 4.730 INCHES NOMINAL IN |
| MOUNTING METHOD | FLANGE |
| POLARIZATION FEATURE | NOT INCLUDED |
| HEIGHT | 1.375 INCHES NOMINAL IN |
| SPECIAL FEATURES | SUPPORTS GRUMMAN A-10 AIRCRAFT |
| WIDTH | 0.781 INCHES NOMINAL IN |
| PLUG DESIGN | STRAIGHT |