NSN 6615-01-125-6581 · NIIN 011256581 · FSC 6615
NO DASHES 6615011256581
In Stock
GYROSCOPE,DISPLACEMENT
Automatic Pilot Mechanisms and Airborne Gyro Components
Technical characteristics
12 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| ABHP | OVERALL LENGTH | INCHES NOMINAL 6.600 |
| ABKW | OVERALL HEIGHT | INCHES NOMINAL 4.000 |
| ABMK | OVERALL WIDTH | INCHES NOMINAL 4.000 |
| ACDC | CURRENT TYPE | AC |
| APQB | UNIT TYPE | VERTICAL |
| BBWD | WHEEL POWER METHOD | ELECTRIC |
| BBWH | AXIS DISPLACEMENT LIMITATION IN DEG | PORM 82 DEG FOR PITCH AXIS, 360 DEG ROLL ATTITUDE SENSING |
| 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 |
| FREQ | FREQUENCY IN HERTZ | 400.0 |
| SUPP | 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 |