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MRC | Criteria | Characteristic |
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FTLD | Functional Description | RECEIVES DIGITAL ENGINE PERFORMANCE SIGNALS FROM THE ENGINE MONITORING SYSTEM PROCESSOR AND AIRCRAFT PARAMETERS FROM THE MUX;THESE SIGNALS ARE COMPARED AGAINST PREDETERMINED LIMITS STORED IN THE EMSC;EXCEEDENCES AND FAULTS ARE TRANSMITTED TO REMOTE AIRCRAFT SYSTEMS;ALSO MONITORS THE DEC AND ITS OWN PERFORMANCES AND TRANSMITTS DATA TO THE PILOT DISPLAYS;DETECTS ENGINE CONTROL LOOP FAILURES AND COMPRESSOR STALLS |
AJAF | Unpackaged Unit Length | 10.00 INCHES NOMINAL |
ACUR | Direct Current Voltage Rating In Volts | 28 |
MRC | Decoded Requirement | Clear Text Reply |
ZZZV | Fsc Application Data | ENGINE MONITORING SYSTEM COMPUTER (EMSC)SUPPGBATTERY NOT INCLUDED |
AJAG | Unpackaged Unit Width | 6.50 INCHES NOMINAL |
AJAH | Unpackaged Unit Height | 5.00 INCHES NOMINAL |
FEAT | Special Features | AMBIENT OPERATING TEMPERATURE -65 TO +160 DEG F.;DOWNLOAD OPERATING POWER 20 WATTS;NORMAL OPERATING POWER 50 WATTS;THE EMSC IS AN AIRFRAME MOUNTED UNIT;BATTERY BACKUP |
AXQJ | Intelligence Input Method | ELECTRICAL |
RDAL | Reference Data And Literature | TO 5E1-2-12-1 |
AGAV | End Item Identification | F110-GE100 ENGINE F-16C/D ACFT |
AWZJ | Power Source | EXTERNAL OR SELF-CONTAINED |
ADTV | Case Material | ALUMINUM ALLOY |
Guaranteed on-time |
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Customized and |
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Over 5100 |
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Complete Purchasing |