| AKPV |
MOUNTING FACILITY QUANTITY |
4 SINGLE GROUP |
| ADAQ |
BODY LENGTH |
2.250 INCHES NOMINAL |
| BPLC |
WINDING FUNCTION AND QUANTITY |
1 PRIMARY SINGLE COMPONENT AND 3 SECONDARY SINGLE COMPONENT |
| CRBZ |
WINDING OPERATING CURRENT |
2.0 AMPERES NOMINAL B AND BETTER DROP SIDING SINGLE COMPONENT 3RD SECONDARY |
| AXGY |
MOUNTING METHOD |
FLANGE SINGLE GROUP AND UNTHREADED HOLE SINGLE GROUP |
| AARG |
RELIABILITY INDICATOR |
NOT ESTABLISHED |
| ADAT |
BODY WIDTH |
2.250 INCHES NOMINAL |
| TTQY |
TERMINAL TYPE AND QUANTITY |
7 TAB, SOLDER LUG |
| AKNA |
INCLOSURE TYPE |
HERMETICALLY SEALED |
| CWJS |
WINDING OPERATING VOLTAGE |
6.30 AC POUNDS PER HOUR WET SINGLE COMPONENT 3RD SECONDARY |
| ADAU |
BODY HEIGHT |
2.750 INCHES NOMINAL |
| AARD |
DUMMY TERMINAL QUANTITY (NON-CORE) |
2 |
| CQLC |
WINDING TAP LOCATION (NON-CORE) |
CENTER TAP SINGLE COMPONENT 1ST SECONDARY |
| FEAT |
SPECIAL FEATURES |
WEAPON SYSTEM ESSENTIAL |
| ACZB |
FREQUENCY RATING |
400.0 HERTZ NOMINAL SINGLE COMPONENT |
| ACZC |
INPUT-OUTPUT PHASE RELATIONSHIP |
SINGLE PHASE TO SINGLE PHASE SINGLE COMPONENT |
| AGAV |
END ITEM IDENTIFICATION |
AIRCRAFT, PHANTOM F-4; SUBMARINE AUXILLARY AND MISCELLANEOUS SYSTEMS; AIRCRAFT, EAGLE F-15; TRIDENT HULL STRUCTURE; RADAR AND IFF SYSTEMS; COMMUNICATIONS AND DATA SYSTEMS; SSBN MK-118 FIRE CONTROL SYS; NAVIGATIONAL SYSTEMS; SHIP, OHIO CLASS SSN (TRIDENT); AIRCRAFT, HERCULES C-130 |
| CRBZ |
WINDING OPERATING CURRENT |
3.0 AMPERES NOMINAL B AND BETTER DROP SIDING SINGLE COMPONENT 2ND SECONDARY |
| ABKR |
CENTER TO CENTER DISTANCE BETWEEN MOUNTING FACILITIES PARALLEL TO WIDTH |
1.740 INCHES NOMINAL SINGLE MOUNTING FACILITY SINGLE CENTER GROUP |
| CRTL |
CRITICALITY CODE JUSTIFICATION |
FEAT |
| ABKQ |
CENTER TO CENTER DISTANCE BETWEEN MOUNTING FACILITIES PARALLEL TO LENGTH |
1.740 INCHES NOMINAL SINGLE MOUNTING FACILITY SINGLE CENTER GROUP |