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MRC | Criteria | Characteristic |
---|---|---|
CHHK | MAXIMUM TILT FROM HORIZONTAL POSITION IN DEG | 40.0 |
CHHM | VERNIER TILTING SCALE | INCLUDED |
FTLD | III FUNCTIONAL DESCRIPTION | USED WITH ADAPTER 204-91950-1 TO MOUNT INERTIAL NAVIGATION SYSTEM IN ORDER TO PROVIDE SPECIFIC AIRPLANE ATTITUDE PITCH, ROLL AND ROLL (VERSINE) TO THE AUTOMATIC PILOT DURING MAINTENANCE AND REPAIR OF AUTOMATIC FLIGHT CONTROLS; ALSO USED TO MOUNT TWO VERTICAL GYROS OF ATTITUDE AND HEADING REFERENCE SYSTEM TO PROVIDE AIRPLANE ATTITUDE REFERENCE TO THE WEATHER RADAR ANTENNA OR FLIGHT DIRECTOR SYSTEM DURING MAINTENANCE |
CHHL | TABLE TOP LEVELING DEVICE | INCLUDED |
CHHN | VERNIER ANGULAR SCALE | INCLUDED |
AGAV | III END ITEM IDENTIFICATION | E-3A, E-4A, -4B AEROSPACE GROUND SUPPORT EQUIPMENT |
APGF | DESIGN TYPE | LEG |
RDAL | III REFERENCE DATA AND LITERATURE | TO 35-1-251-1; TO 33D-1-111 |
CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | INERTIAL NAVIGATION SYSTEM (INS) AND GYRO UNITS TILT TABLE |
SR-5 | DESIGN CONTROL REFERENCE | 2TSJ60B00002 |
MATL | MATERIAL | ALUMINUM AND STEEL |
SR-5 | MANUFACTURERS CODE | 81205 |
SR-5 | THE MANUFACTURERS DATA |
2TS1MSS | 2TS141-67 | 2TS1MSS | 2TS1 |
2TS-4 | 2TSJ25-22558-2 | 2TS-1M | 2TSJ60B00002-7 |
2TS3 | 2TS141-67 | 2TS2 | 2TSJ25-27412-1 |
2TSLCAMBER | 2TS-4 |
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