Mfg Part Number: 53-87012-21
Alternate P/N: 538701221
NSN : 6605-00-915-9319
NIIN : 009159319
CAGE Code : 80058
Manufacturer: Joint Electronics Type Designation
Item Name : Computer Aircraft A
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MRC | Criteria | Characteristic |
---|---|---|
AAXX | MOUNTING TYPE | BASE, SHOCK MOUNT |
TMDN | III TYPE/MODEL DESIGNATION | CP-780/ASN-56 |
RTSE | III RELATIONSHIP TO SIMILAR EQUIPMENT | REPLACES 6605-00-919-2698 |
FTLD | III FUNCTIONAL DESCRIPTION | CONTAINS 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 |
AJAG | III UNPACKAGED UNIT WIDTH | 4.250 INCHES NOMINAL |
AJAF | III UNPACKAGED UNIT LENGTH | 23.600 INCHES NOMINAL |
AXQJ | INTELLIGENCE INPUT METHOD | ELECTRICAL |
AJAH | III UNPACKAGED UNIT HEIGHT | 9.740 INCHES NOMINAL |
AXQK | OUTPUT INTELLIGENCE TYPE | ANGLE OF ATTACK |
AXQH | INPUT INTELLIGENCE TYPE | ALTITUDE, GENERAL DATA AND GROUND SPEED AND PITCH-ROLL SIGNAL DATA |
RDAL | III REFERENCE DATA AND LITERATURE | TECH ORDER 5N16-2-6-4 AND DD FORM 61 |
FEAT | SPECIAL FEATURES | ADDITIONAL INFORMATION COMPUTED: CLIMB ANGLE, VERTICAL VELOCITY, GROUND SPEED TO ALTITUDE RATIO |
AGAV | III END ITEM IDENTIFICATION | AN/ASN-56 INERTIAL NAVIGATION SYS; RF4C AIRCRAFT |
AWZJ | POWER SOURCE | EXTERNAL |
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