Part Details | AIRCRAFT COCKPIT LIGHT
6220-00-507-4740 A light specifically designed to be permanently installed in aircraft for map reading or cockpit illumination. It may contain dimming features, switches, filters, and/or cables or coiled cables to permit portability within the length of the cable. If provided with cables or coiled cables, the mounting base must remain fixed to the aircraft and include a snap-in or similar locking device to permit detachment and attachment of the light. For items that supply general illumination for other compartments of an aircraft, see LIGHT, DOME. Excludes LIGHT (1), EXTENSION.
Alternate Parts: B2930A, B-2930-A, 6220-00-507-4740, 00-507-4740, 6220005074740, 005074740
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 62 | JAN 01, 1963 | 00-507-4740 | 22778 ( LIGHT, COCKPIT, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6220-00-507-4740
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| B-2930-A | 72914 | GRIMES AEROSPACE COMPANYDBA HONEYWELL |
Technical Data | NSN 6220-00-507-4740
| Characteristic | Specifications |
|---|---|
| VOLTAGE RATING IN VOLTS | 28.0 DC NOMINAL |
| LAMP TYPE ACCOMMODATED AND QUANTITY | 1 INCANDESCENT |
| LAMP BASE TYPE ACCOMMODATED | DOUBLE CONTACT BAYONET CANDELABRA INDEXING |
| OVERALL DIAMETER | 1.625 INCHES MAXIMUM |
| OVERALL LENGTH | 3.500 INCHES MAXIMUM |
| LENS TRANSPARENCY | TRANSPARENT |
| MOUNTING METHOD | BASE |
| TERMINAL TYPE AND QUANTITY | 2 SOLDER LUG |
| WIRING PROVISION METHOD | CABLE ASSEMBLY |
| HAZARDOUS LOCATIONS/ENVIRONMENTAL PROTECTION | |
| FURNISHED ITEMS AND QUANTITY | 1 LAMP |
| FEATURES PROVIDED | DIMMING DEVICE AND SWITCH AND ADJUSTABLE LIGHT BEAM SPREAD |