NSN 6605-00-915-9319

Part Details | AIRCRAFT ATTITUDE COMPUTER

6605-00-915-9319 A computer that contains the follow-up servo for pitch and roll information from the platform, and the circuitry for computing vertical attack angles, climb angle, vertical velocity, and ground speed to altitude ratio.

Alternate Parts: 538701221271, 53-87012-21-271, 538701221, 53-87012-21, CP780ASN56, 637672, 637672, 637672, 6605-00-915-9319, 00-915-9319, 6605009159319, 009159319

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
66OCT 31, 196500-915-931953058 ( COMPUTER, AIRCRAFT ATTITUDE )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6605-00-915-9319
Part Number Cage Code Manufacturer
53-87012-21-27176301BOEING COMPANY, THEDBA BOEING
53-87012-2176301BOEING COMPANY, THEDBA BOEING
CP780ASN5680058JOINT ELECTRONICS TYPE DESIGNATIONSYSTEM
6376721XSM7L-3 COMMUNICATIONS AIS GP CORP
63767201255LITTON INDUSTRIES INC
63767206481NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS
Technical Data | NSN 6605-00-915-9319
Characteristic Specifications
INPUT INTELLIGENCE TYPE ALTITUDE, GENERAL DATA AND GROUND SPEED AND PITCH-ROLL SIGNAL DATA
INTELLIGENCE INPUT METHOD ELECTRICAL
OUTPUT INTELLIGENCE TYPE ANGLE OF ATTACK
POWER SOURCE EXTERNAL
MOUNTING TYPE BASE, SHOCK MOUNT
SPECIAL FEATURESADDITIONAL INFORMATION COMPUTED: CLIMB ANGLE, VERTICAL VELOCITY, GROUND SPEED TO ALTITUDE RATIO
UNPACKAGED UNIT LENGTH23.600 INCHES NOMINAL
UNPACKAGED UNIT WIDTH4.250 INCHES NOMINAL
UNPACKAGED UNIT HEIGHT9.740 INCHES NOMINAL
END ITEM IDENTIFICATIONAN/ASN-56 INERTIAL NAVIGATION SYS; RF4C AIRCRAFT
FUNCTIONAL DESCRIPTIONCONTAINS THE FOLLOW-UP SERVOS FOR PITCH AND ROLL INFORMATION FROM THE INERTIAL NAVIGATION SET STABLE PLATFORM, AND CIRCUITRY FOR COMPUTING VERTICAL ATTACK ANGLE, CLIMB ANGLE, VERTICAL VELOCITY, AND GROUND SPEED TO ALTITDE RATIO
TYPE/MODEL DESIGNATIONCP-780/ASN-56
RELATIONSHIP TO SIMILAR EQUIPMENTREPLACES 6605-00-919-2698
REFERENCE DATA AND LITERATURETECH ORDER 5N16-2-6-4 AND DD FORM 61