| AJAG |
UNPACKAGED UNIT WIDTH |
6.50 INCHES NOMINAL |
| AGAV |
END ITEM IDENTIFICATION |
F110-GE100 ENGINE F-16C/D ACFT |
| RDAL |
REFERENCE DATA AND LITERATURE |
TO 5E1-2-12-1 |
| AWZJ |
POWER SOURCE |
EXTERNAL OR SELF-CONTAINED |
| AJAF |
UNPACKAGED UNIT LENGTH |
10.00 INCHES NOMINAL |
| ZZZV |
FSC APPLICATION DATA |
ENGINE MONITORING SYSTEM COMPUTER (EMSC)SUPPGBATTERY NOT INCLUDED |
| 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 |
| ACUR |
DIRECT CURRENT VOLTAGE RATING IN VOLTS |
28.0 |
| ADTV |
CASE MATERIAL |
ALUMINUM ALLOY |
| 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 |
| AJAH |
UNPACKAGED UNIT HEIGHT |
5.00 INCHES NOMINAL |
| AXQJ |
INTELLIGENCE INPUT METHOD |
ELECTRICAL |