Part Details | FLIGHT DIRECTOR COMPUTER
6610-00-056-5889 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: CPU27A, CPU27/A, 1511493901, 1511493-901, MILC27522, 6610-00-056-5889, 00-056-5889, 6610000565889, 000565889
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
66 | JAN 01, 1963 | 00-056-5889 | 28374 ( COMPUTER, FLIGHT DIRECTOR ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6610-00-056-5889
Part Number | Cage Code | Manufacturer |
---|---|---|
CPU27/A | 80058 | JOINT ELECTRONICS TYPE DESIGNATIONSYSTEM |
1511493-901 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
MILC27522 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 6610-00-056-5889
Characteristic | Specifications |
---|---|
INPUT INTELLIGENCE TYPE | COURSE AND HEADING ERROR AND INFRARED LOG SIGNAL STRENGTH AND PITCH-ROLL SIGNAL DATA |
INTELLIGENCE INPUT METHOD | ELECTRICAL |
OUTPUT INTELLIGENCE TYPE | COURSE RANGING AND WARNING |
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 |
CONNECTOR MANUFACTURER PART NUMBER | APT1H-20-41P$$APT1H-22-55P |
CONNECTOR MANUFACTURER CODE | 77820 |
MOUNTING TYPE | RACK |
SPECIFICATION/STANDARD DATA | 81349 - MIL-C-27522 GOVERNMENT SPECIFICATION |
UNPACKAGED UNIT LENGTH | 9.480 INCHES NOMINAL |
UNPACKAGED UNIT WIDTH | 5.480 INCHES NOMINAL |
UNPACKAGED UNIT HEIGHT | 7.530 INCHES NOMINAL |
END ITEM IDENTIFICATION | C130E,F111 |
TYPE/MODEL DESIGNATION | CPU-27/A |
REFERENCE DATA AND LITERATURE | 5F5-5-4-4 |