NSN 6610-01-359-6555
Part Details | FLIGHT DIRECTOR COMPUTER
6610-01-359-6555 An airborne analog computer used to combine signals from various navigational aids, gyroscopic controls, and landing systems in order to provide flight director steering signals to the pilot. Excludes COMPUTER, AIR NAVIGATION; COMPUTER, AZIMUTH; COMPUTER, COURSE-DISTANCE; COMPUTER, DESTINATION PRESET; and COMPUTER, HEADING.
Alternate Parts: 1395601, 139560-1, ES1410, CPU65AA, CPU-65A/A, MILC38286, MIL-C-38286, 6610-01-359-6555, 01-359-6555, 6610013596555, 013596555
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | JUN 10, 1992 | 01-359-6555 | 28374 ( COMPUTER, FLIGHT DIRECTOR ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6610-01-359-6555
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 139560-1 | 10138 | ASTRONAUTICS CORPORATION OF AMERICA |
| ES1410 | 10138 | ASTRONAUTICS CORPORATION OF AMERICA |
| CPU-65A/A | 80058 | JOINT ELECTRONICS TYPE DESIGNATIONSYSTEM |
| MIL-C-38286 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 6610-01-359-6555
| Characteristic | Specifications |
|---|---|
| INPUT INTELLIGENCE TYPE | PITCH-ROLL SIGNAL DATA AND COURSE AND HEADING ERROR |
| INTELLIGENCE INPUT METHOD | ELECTRICAL |
| OUTPUT INTELLIGENCE TYPE | PITCH-ROLL SIGNAL DATA AND WARNING |
| COMPUTATION TYPE | GREAT CIRCLE |
| POWER SOURCE | EXTERNAL |
| DIRECT CURRENT VOLTAGE RATING IN VOLTS | 28.0 |
| ALTERNATING CURRENT VOLTAGE RATING IN VOLTS | 115.0 |
| FREQUENCY IN HERTZ | 400.0 |
| PHASE | SINGLE |
| TERMINAL TYPE | CONNECTOR, RECEPTACLE |
| TERMINAL QUANTITY | 2 |
| CONNECTOR MANUFACTURER PART NUMBER | AMS3124E-20-41P$$AMS3124E-20-55P |
| CONNECTOR MANUFACTURER CODE | 96906 |
| TERMINAL LOCATION | BACK |
| MOUNTING TYPE | RACK |
| SPECIAL FEATURES | NON-HERMETICALLY SEALED |
| UNPACKAGED UNIT LENGTH | 8.470 INCHES NOMINAL |
| UNPACKAGED UNIT WIDTH | 5.510 INCHES NOMINAL |
| UNPACKAGED UNIT HEIGHT | 7.500 INCHES NOMINAL |
| END ITEM IDENTIFICATION | C-130 ACFT COMMON-ALL SERIAL NUMBERS |
| FUNCTIONAL DESCRIPTION | THE FLIGHT DIRECTOR COMPUTER FDC ACCEPTS INPUTS FROM C130 ACFT SENSORS,INSTRUMENTS,MODE SELECT PANELS,AND NAVIGATION SETS TO PERFORM SIGNAL SWITCHING AND COMPUTATION OF PITCH AND ROLL STEERING COMMANDS WHICH DRIVE COCKPIT DISPLAYS;ASSISTS PILOT IN INTERCEPTING AND MAINTAINING A SELECTED FLIGHT PATH |
| TYPE/MODEL DESIGNATION | CPU-65A/A |