NSN 6930-00-907-1759
Part Details | AIRCRAFT INSTRUMENT AND FLIGHT DIRECTOR SYSTEM TRAINER
6930-00-907-1759 The trainer will be used to instruct and familiarize maintenance and operating personnel on the instrument and flight director systems as pertains to the operation, location, recognition, installation, aircrew operation, servicing, adjustment, trouble shooting, and inspection.
Alternate Parts: TAU143E, 40278111, 4027811-1, 40278111, 4027811-1, 6930-00-907-1759, 00-907-1759, 6930009071759, 009071759
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 69 | JAN 01, 1960 | 00-907-1759 | 26379 ( TRAINER, INSTRUMENT AND FLIGHT DIRECTOR SYSTEM, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6930-00-907-1759
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| TAU143E | 80049 | DEPARTMENT OF THE AIR FORCE |
| 4027811-1 | 92685 | LOCKHEED MARTIN CORPORATIONDBA LM AERONAUTICS COMPANY |
| 4027811-1 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
Technical Data | NSN 6930-00-907-1759
| Characteristic | Specifications |
|---|---|
| TRAINING PHASE | OPERATION AND MAINTENANCE OF THE AIR VEHICLE |
| INSTALLATION DESIGN | MOBILE |
| POWER SOURCE | AC |
| AC OPERATING VOLTAGE RATING IN VOLTS | 115.0 MINIMUM AND 208.0 MAXIMUM |
| FREQUENCY IN HERTZ | 60.0 MINIMUM AND 400.0 MAXIMUM |
| PHASE | THREE |
| ALTERNATING CURRENT USAGE | REQUIRED |
| SPECIAL FEATURES | DWG NAME,TRAINER,FLIGHT DIRECTOR SYSTEM,AIRCRAFT; DIRECT CIRRENT,28V,REQUIRED; LENGTH,84 IN; WIDTH, 42IN; HEIGHT; MAJOR COMPONENTS C/O, RATE OF TURN SENSOR,TRU-2A/A; GYRO,MD-1; RATE SWITCHING GYRO,MC-1; HORIZONTAL SITUATION INDICATOR AQU-2/A; ATTITUDE DIRECTOR INDICATOR ARU-28/A; COMPUTER CPU-27/A; SPECIAL FEATURES,THE SILHOUETTE SHALL BE SUPPORTED BY A ONE-PIECE COLUMN AND UNIVERSAL ACTION TYPE OF BALL JOINT ASSEMBLY, PITCH AND ROLL MOVEMENT OF THE SILHOUETTE SHALL BE RESTRICTED TO PLUS AND MINUS 20 DEGREES; THE CONTROL CONSOLE SHALL NOT EXTEND ABOVE THE HORIZONTAL BASE OF THE SILHOUETTE; THE COMPASS SIMULATOR SHALL BE INCORPORATED INTO THE BASE OF THE SUPPORT COLUMN; DD61 N., USAF-65-21 |
