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MRC | Criteria | Characteristic |
---|---|---|
SR-5 | THE MANUFACTURERS DATA | |
SUPP | III SUPPLEMENTARY FEATURES | CONSISTS OF AN ELECTRICALLY DRIVEN ROTOR SITUATED IN A GIMBAL ARRANGEMENT TO PROVIDE ACCURATE ANGULAR DISPLACEMENT MEASUREMENT IS REFERENCED TO VERTICAL BY MEANS OF ELECTRICAL ERECTION IS VIBRATION ISOLATED. ITEM PART OF: CH-47 HELICOPTER ITEM USED WITH: ARU-12/A INDICATOR INTCHG STMT: TWO-WAY INTERCHANGEABLE. EXCEPT BY MAINTENANCE PARTS CN-811/ASN & CN-811A/ASN |
FREQ | FREQUENCY IN HERTZ | 400.0 |
ELEC | VOLTAGE IN VOLTS | 115.0 |
FAAZ | PHASE | SINGLE |
FEAT | SPECIAL FEATURES | MOUNTING DATA - PER SCS-413: DESIGN ACTIVITY DATA: JET ELECTRONICS AND TECHNOLOGY, INC. FSCM 25583, P/N 501-1332-01; AIRCRAFT INSTALLED. FUNCT DESC: GYROSCOPE DEVELOPS ELECTRICAL SIGNALS REPRESENTATIVE OF AIRCRAFT ATTITUDE THRU 360 DEG ROLL AND +/-82 DEG PITCH |
SR-5 | MANUFACTURERS CODE | 25583 |
ABMK | OVERALL WIDTH | 4.000 INCHES NOMINAL |
SR-5 | DESIGN CONTROL REFERENCE | 501-1332-01 |
APQB | UNIT TYPE | VERTICAL |
ABKW | OVERALL HEIGHT | 4.000 INCHES NOMINAL |
BBWH | AXIS DISPLACEMENT LIMITATION IN DEG | PORM 82 DEG FOR PITCH AXIS, 360 DEG ROLL ATTITUDE SENSING |
BBWD | WHEEL POWER METHOD | ELECTRIC |
ABHP | OVERALL LENGTH | 6.600 INCHES NOMINAL |
ACDC | CURRENT TYPE | AC |
501-00-0826 | 501-00-0825 | 501-00-0826 | 501-00-0827 |
501.000 | 501-00-0825 | 501.000 | 501-00-0827 |
501-00-0827 | 501-000 | 501-00-0310 | 501-00-0827 |
501-00-0215 | 501-00-0825 | 501-00-0826 | 501-000 |
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