Part Details | POWER TRANSFORMER
5950-00-476-5583 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.
Alternate Parts: 515081220, 51508-1220, 515081220, 51508-1220, 316027, 3-16027, 5950-00-476-5583, 00-476-5583, 5950004765583, 004765583
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | MAR 23, 2006 | 00-476-5583 | 32496 ( TRANSFORMER, POWER ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5950-00-476-5583
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 51508-1220 | 31435 | LUCAS AEROSPACE POWER EQUIPMENTCORPORATION |
| 51508-1220 | 3CPE0 | SAFRAN POWER USA, LLC |
| 3-16027 | 00144 | TE CONNECTIVITY NETWORKS, INC.DIV ADC TELECOMMUNICATIONS SALES, |
Technical Data | NSN 5950-00-476-5583
| Characteristic | Specifications |
|---|---|
| TERMINAL TYPE AND QUANTITY | 12 PIN |
| INCLOSURE TYPE | FULLY INCLOSED |
| OVERALL LENGTH | 2.060 INCHES MAXIMUM |
| OVERALL HEIGHT | 1.380 INCHES MAXIMUM |
| OVERALL WIDTH | 0.880 INCHES MINIMUM |
| RELIABILITY INDICATOR | NOT ESTABLISHED |
| SPECIAL FEATURES | GWEAPON SYSTEM ESSENTIAL; WINDING FUNCTION AND QUANTITY 3 PRIMARY AND 3 SECONDARY SINGLE COMPONENT; THREAD CLASS 2B SINGLE GROUP; THREAD DIRECTION RIGHT-HAND SINGLE GROUP |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | USED ON CHINOOK F23 AIRCRAFT |