NSN 6615-01-701-7635 · NIIN 017017635 · FSC 6615
NO DASHES 6615017017635
In Stock
COMPUTER,FLIGHT CONTROL
Automatic Pilot Mechanisms and Airborne Gyro Components
Technical characteristics
13 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 |
|---|---|---|
| AXQH | INPUT INTELLIGENCE TYPE | AIR DATA AND AUTOMATIC PILOT STEERING |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | FLIGHT CONTROL COMPUTER |
| FEAT | SPECIAL FEATURES | DISTRIBUTED ARCHITECTURE INCORPORATING FOUR INCEPTOR INTERFACE MODULES (IIMS), TWO FCCS AND EIGHT REMOTE ELECTRONIC UNITS (REUS). FCS PERFORMS CONTROL AND MONITORING OF ALL THE PRIMARY CONTROL SURFACES; AILERONS, RUDDER AND ELEVATORS, AS WELL AS THE MULTIFUNCTION SPOILERS (MFS) AND GROUND SPOILERS. IT ALSO PROVIDES SECONDARY FLIGHT CONTROL FOR THE HORIZONTAL STABILIZER TRIM, FLAPS AND SPEED BRAKES. THE FCC INTERFACES WITH OTHER AIRCRAFT SYSTEMS TO PROVIDE FUNCTIONS TO SUPPORT AUTOPILOT, AIR DATA AND INERTIAL REFERENCE AUGMENTATION, FAULT LOGGING AND CENTRAL MAINTENANCE. 2X +28 V DC TYPE IV AIRCRAFT SUPPLY. WEIGHT: 6.25 KG MAX. PASSIVELY COOLED. |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |
| AEEF | CONNECTOR MANUFACTURER PART NUMBER | ARINC 600 CONNECTOR |
| AJAF | UNPACKAGED UNIT LENGTH | MILLIMETERS MINIMUM 387.096 AND MILLIMETERS MAXIMUM 389.128 |
| AWZJ | POWER SOURCE | EXTERNAL |
| AXQK | OUTPUT INTELLIGENCE TYPE | AIR DATA AND AUTOMATIC PILOT STEERING |
| CBBL | FEATURES PROVIDED | ELECTROSTATIC SENSITIVE |
| AXQJ | INTELLIGENCE INPUT METHOD | ELECTRICAL |
| AJAH | UNPACKAGED UNIT HEIGHT | MILLIMETERS NOMINAL 199.39 |
| ACUR | DIRECT CURRENT VOLTAGE RATING IN VOLTS | 28.0 |
| AJAG | UNPACKAGED UNIT WIDTH | MILLIMETERS NOMINAL 127.0 |