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National Stock Number:
6910-00-907-1759
Federal Supply Class:
6910
National Item Identification Number:
009071759
Description:
TRAINING AID,FLIGHT *
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Manufacturer Information:
| 4027802-1 | 36659 | LOCKHEED MARTIN CORP LOCKHEED MARTIN AERONAUTICAL SYSTEMS BURBANK OPNS | | 4027802-1 | 92685 | LOCKHEED MARTIN CORPORATION DBA LM AERONAUTICS COMPANY | | 4027805-1 | 36659 | LOCKHEED MARTIN CORP LOCKHEED MARTIN AERONAUTICAL SYSTEMS BURBANK OPNS | | 4027808-1 | 36659 | LOCKHEED MARTIN CORP LOCKHEED MARTIN AERONAUTICAL SYSTEMS BURBANK OPNS | | 4027808-1 | 92685 | LOCKHEED MARTIN CORPORATION DBA LM AERONAUTICS COMPANY | | 4027805-1 | 92685 | LOCKHEED MARTIN CORPORATION DBA LM AERONAUTICS COMPANY | | 4027811-1 | 36659 | LOCKHEED MARTIN CORP LOCKHEED MARTIN AERONAUTICAL SYSTEMS BURBANK OPNS | | 4028303-1 | 36659 | LOCKHEED MARTIN CORP LOCKHEED MARTIN AERONAUTICAL SYSTEMS BURBANK OPNS | | TAU142E | 80049 | DEPARTMENT OF THE AIR FORCE | | TAU143E | 80049 | DEPARTMENT OF THE AIR FORCE | | TAU144E | 80049 | DEPARTMENT OF THE AIR FORCE | | TAU145E | 80049 | DEPARTMENT OF THE AIR FORCE | | 4028303-1 | 92685 | LOCKHEED MARTIN CORPORATION DBA LM AERONAUTICS COMPANY | | 4027811-1 | 92685 | LOCKHEED MARTIN CORPORATION DBA LM AERONAUTICS COMPANY |
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Techincal Specification:
| AC OPERATING VOLTAGE RATING IN VOLTS | 115.0 MINIMUM AND 208.0 MAXIMUM | | ALTERNATING CURRENT USAGE | REQUIRED | | FREQUENCY IN HERTZ | 60.0 MINIMUM AND 400.0 MAXIMUM | | INSTALLATION DESIGN | MOBILE | | PHASE | THREE | | POWER SOURCE | AC | | 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 | | TRAINING PHASE | OPERATION AND MAINTENANCE OF THE AIR VEHICLE |
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