"AIR FRAME MOUNTED UNIT,LITHIUM BATTERY BACKUP,NORMAL OPERATING TEMP -65TO 160 DEG F, NORMAL OPERATING POWER 50 WATTS"
FTLD
FUNCTIONAL DESCRIPTION
RECEIVES DIGITAL SIGNALS ON ENGINE PERFORMANCE FROM ENGINE MONITORING SYSTEM PROCESS AND AIRCRAFT MULTIPLEXERBUS. SIGNALS ARE COMPARED AGAINST PREDETERMINED LIMIT STORED IN THE EMSC
RDAL
REFERENCE DATA AND LITERATURE
TP5-E1-12-1
RTSE
RELATIONSHIP TO SIMILAR EQUIPMENT
"RETROFIT OF F110-GE-100/100B ENGINE MONITORING SYSTEM COMPUTER WITH NEWSOFTWARE, NSN 6610-01-429-9115"