Part Details | FLIGHT DIRECTOR COMPUTER
6610-00-042-8461 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: CPU65A, CPU-65/A, MILC38286, MIL-C-38286, 5224174003, 522-4174-003, 6610-00-042-8461, 00-042-8461, 6610000428461, 000428461
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | MAY 15, 1968 | 00-042-8461 | 28374 ( COMPUTER, FLIGHT DIRECTOR ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6610-00-042-8461
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CPU-65/A | 80058 | JOINT ELECTRONICS TYPE DESIGNATIONSYSTEM |
| MIL-C-38286 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 522-4174-003 | 13499 | ROCKWELL COLLINS, INC.DBA GOVERNMENT SYSTEMS |
Technical Data | NSN 6610-00-042-8461
| Characteristic | Specifications |
|---|---|
| INPUT INTELLIGENCE TYPE | ALTITUDE DATA AND HORIZONTAL |
| INTELLIGENCE INPUT METHOD | ELECTRICAL |
| OUTPUT INTELLIGENCE TYPE | HORIZONTAL |
| 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 | A8113-20A41PSP$$A8113-22A55PSPA5 |
| CONNECTOR MANUFACTURER CODE | 97814 |
| TERMINAL LOCATION | BACK |
| MOUNTING TYPE | RACK |
| UNPACKAGED UNIT LENGTH | 9.467 INCHES NOMINAL |
| UNPACKAGED UNIT WIDTH | 5.290 INCHES NOMINAL |
| UNPACKAGED UNIT HEIGHT | 7.594 INCHES NOMINAL |
| END ITEM IDENTIFICATION | C-130E, C-141A, & F111 AIRCRAFT |
| FUNCTIONAL DESCRIPTION | SUPPLIES SIGNALS TO REMOTE FLIGHT DIRECTOR INDICATORS SUCH AS ARU-11/A AND ARU-2B/A ATTITUDE DIRECTOR INDICATORS. CALCULATES SIGNALS FOR EDISPLAY ON THE STTITUDE DIRECTOR TO ENABLE THE PILOT TO PERFORM PROPER CONTROL ACTIONS TO INTERCEPT AND MAINTAIN THE DESIRED COURSE OF THE FLLIGHT PATH FOR THE MAJOR MODES OF VOR, TACAN, DOPLER, DATALINK, ILS. |
| TYPE/MODEL DESIGNATION | CPU-65/A |
| REFERENCE DATA AND LITERATURE | 5F505-7-4, DD FORM 61, & MIL-SPEC |