NSN 6615-01-110-6322
Part Details | AUTOMATIC PILOT FLIGHT CONTROLLER
6615-01-110-6322 A controller designed to control an aircraft through an automatic pilot in pitch, yaw, roll and coordinated turns.
Alternate Parts: HM02070620100, HM020706-201-00, HM02070610100, HM020706-101-00, HM02070600100, HM020706-001-00, APU5BB, APU-5B/B, 6615-01-110-6322, 01-110-6322, 6615011106322, 011106322
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | APR 03, 1981 | 01-110-6322 | 03365 ( CONTROLLER, FLIGHT, AUTOMATIC PILOT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6615-01-110-6322
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| HM020706-201-00 | 51215 | BOEING COMPANY, THEDBA BOEING |
| HM020706-101-00 | 51215 | BOEING COMPANY, THEDBA BOEING |
| HM020706-001-00 | 51215 | BOEING COMPANY, THEDBA BOEING |
| APU-5B/B | 80058 | JOINT ELECTRONICS TYPE DESIGNATIONSYSTEM |
Technical Data | NSN 6615-01-110-6322
| Characteristic | Specifications |
|---|---|
| POWER SOURCE | EXTERNAL |
| MAXIMUM VOLTAGE RATING IN VOLTS | 115.0 AC AND 28.0 DC |
| FREQUENCY IN HERTZ | 400.0 |
| PHASE | SINGLE |
| CURRENT RATING IN AMPS | B0.2$$B0.7 |
| CASE MATERIAL | ALUMINUM |
| MAXIMUM OVERALL LENGTH | 9.800 INCHES |
| MAXIMUM OVERALL WIDTH | 4.200 INCHES |
| MAXIMUM OVERALL HEIGHT | 4.200 INCHES |
| SPECIAL FEATURES | GUIDED BOMB AUTOMATIC PILOT; HAS ANALOG INPUTS FOR PITCH AND YAW, MIDCOURSE GUIDANCE DEVICE, INTERTIAL SENSORS, LINE OF SIGHT RATE COMMANDS; ANALOG OUTPUTS FOR FLIGHT CONTROL SYSTE; DISVRETE INPUTS AND OUTPUTS FOR ACFT COMMAMNDS, DATA LINK COMMANDS, IDENTIFIERS, TIME DELAY, WEAPON COMMANDS, WEAPON READY STATUS; DESIGNED FOR AIRBORNE GUIDED BOMB INSTALLATION; INSTALLED IN THE COMMON CONTROL MODULE BY MEANS OF 4 SOCKET HEAD CAP SCREWS; A SINGLE 158 CONTACT CONNECTOR ATTACHES TO THE COMMON CONTROL MODULE WIRING HARNESS |
| END ITEM IDENTIFICATION | MODULAR GUIDED BOMB GBU-15(V)1/B AND 2/B |
| FUNCTIONAL DESCRIPTION | RELAYS COMMANDS RECVD FROM THE ACFT DIRECTLY OR INDIRECTLY THROUGH THE REMOTE CONTROL SUBSYSTEM DATA LINK TO THE TARGET DETECTING DEVICE FOR DETECTING, DESIGNATING AND TRACKING TARGETS; ALSO PROCESSES GUIDANCE AND INERTIAL STABILIZATION SIGNALS RECVD FROM THE MIDCOURSE GUIDANCE DEVICE, TARGET DETECTING DEVICE AND INERTIAL SENSORS INTO POSITION COMMANDS FOR THE FLIGHT CONTROL SURFACE ACTUATORS IN ORDER TO CONTROL THE FLIGHT PATH OF THE GBU-15(V) |