NIIN Output Data
Definition:
A TRANSFORMER CONSISTING OF ONE OR MORE PRIMARY WINDING(S) AND ONE OR MORE SECONDARY WINDING(S). IT MAY BE DESIGNED FOR DIRECT CONNECTION TO AN ALTERNATING CURRENT SOURCE FOR PURPOSES OF CHANGING THE SECONDARY VOLTS AND AMPERES OR DESIGNED TO ELIMINATE METALLIC INTERCONNECTION BETWEEN CIRCUITS IN AN OVERALL ONE TO ONE VOLTAGE RATIO, WITH OR WITHOUT ADDITIONAL OUTPUT WINDINGS, OR ITEMS DESIGNED TO AUTOMATICALLY MAINTAIN A CONSTANT OUTPUT VOLTAGE WITHIN SPECIFIED LIMITS UNDER VARYING INPUT OR LOAD CONDITIONS. ALSO INCLUDES ITEMS HAVING A PROVISION FOR MECHANICALLY CHANGING THE TURNS RATIO OR INDUCTIVE COUPLING IN PROGRESSIVE INCREMENTS BY MEANS OF VOLTAGE TAPS, RATIO ADJUSTER, OR DEVICES OE SIMILAR DESIGN. FOR TRANSFORMERS HAVING WINDING(S) COMMON TO BOTH INPUT AND OUTPUT CIRCUITS, SEE TRANSFORMER (1), POWER, AUTOTRANSFORMER. EXCLUDES TRANSFORMER (1), PULSE.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| CPD-307 | 80223 | A | 5 | 2 | 5 | ZZ | ||
| CPD-307 | 1L8V1 | A | 3 | 2 | 5 | ZZ | ||
| J103 | 26522 | A | 3 | 2 | 5 | KE | ||
| 7109256-001 | 93322 | A | 1 | 2 | 1 | KE |
CAGE Information
| Code | Company |
|---|---|
| 1L8V1 | MAGNETIKA INC DBA MANUFACTURING BRAN |
| 80223 | UNITED TRANSFORMER CORP SUB OF OPT I |
| 26522 | B G LABORATORIES INC. |
| 93322 | GE AVIATION SYSTEMS LLC DBA GE AVIAT |
Federal Supply Class
Title
COILS AND TRANSFORMERS
Inclusions:
INCLUDES COILS, EXCEPT IGNITION AND MAGNETO; COIL ASSEMBLIES; REACTORS; TRANSFORMERS.
Exclusions:
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| ADAR | BODY OUTSIDE DIAMETER | 3.000 INCHES MAXIMUM |
| ABTB | MOUNTING HOLE DIAMETER | 0.209 INCHES NOMINAL SINGLE GROUP |
| TTQY | TERMINAL TYPE AND QUANTITY | 30 TURRET |
| AKNA | INCLOSURE TYPE | HERMETICALLY SEALED |
| BPLC | WINDING FUNCTION AND QUANTITY | 7 PRIMARY SINGLE COMPONENT AND 12 SECONDARY SINGLE COMPONENT |
| ADAQ | BODY LENGTH | 1.286 INCHES MAXIMUM |
| AXGY | MOUNTING METHOD | UNTHREADED HOLE SINGLE GROUP |
| FEAT | SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
| ACZC | INPUT-OUTPUT PHASE RELATIONSHIP | SINGLE PHASE TO SINGLE PHASE SINGLE COMPONENT |
| AKPV | MOUNTING FACILITY QUANTITY | 1 SINGLE GROUP |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| AGAV | END ITEM IDENTIFICATION | AIRCRAFT, HORNET F/A-18 |