52-1102-001: FILTER ASSEMBLY,ELECTRICAL.
The FILTER ASSEMBLY,ELECTRICAL is a the manufacturer industrial component. Key specifications include end_item_identification: A10-C AIRCRAFT, criticality_code_justification: FEAT, part_name_assigned_by_controlling_agency: FILTER,POWER INPUT. This part is cataloged in the U.S.
Government catalog under NSN 5915-01-600-5246, 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.
| end_item_identification | A10-C AIRCRAFT |
| criticality_code_justification | FEAT |
| part_name_assigned_by_controlling_agency | FILTER,POWER INPUT |
| NSN | 5915-01-600-5246 |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| SPECIAL FEATURES | CRITICAL FUNCTIONS; REPAIR SUPPORT CENTRAL INTERFACE CONTROL UNIT; CASE MATERIAL AND FINISH: .050" THICK ALUMINUM, TIN PLATE PER MIL-F-14072, TYPE M217; ALL CORNERS SHALL HAVE .050" MINIMUM BREAK; MATERIAL AND FINISH SHALL BE COMPATIBLE WITH AN ALUMINUM MOUNTING SURFACE TREATED I/A/W MIL-C-5541, CHEMICAL FILM CLASS 3; CAUTION DECAL MATERIAL; ALUMINUM FOIL, PRESSURE SENSITIVE, DRY RELEASE, MIL-P-19834 APPLIES; ALL CHARACTERS SHALL BE GOTHIC .125" HIGH; COLORS: YELLOW PER FED STD-595 NUMBER 23655 AND BLACK PER FED-STD-595 NUMBER 27038; TEMPERATURE RANGE: -55 DEGREES CELSIUS TO +95 DEGREES CELSIUS (MOUNTING AND STILL AIR AMBIENT); NON-OPERATING: -55C TO +125C; ALTITUDE PER MIL-STD-202, METHOD 105 TO 15,000 FEETTEMPERATURE SHOCK PER MIL-STD-202, METHOD 107, TEST CONDITION BIMPACT SHOCK PER MIL-STD-202, METHOD 213, TEST CONDITION G; VIBRATION PER MIL-STD-202, METHOD 214, TEST CONDITION II C |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FILTER,POWER INPUT |
| END ITEM IDENTIFICATION | A10-C AIRCRAFT |
No substitute or cross-reference records for this part.