Ge Aircraft Computer Engine 7148m74p02 Nsn 6620-01-341-9128 on 2040-parts.com

G.E. AIRCRAFT COMPUTER ENGINE MONITORING P/N 7148M74P02 NSN 6620-01-341-9128
NOS CONDITION. BELIEVED TO FULLY FUNCTIONAL. NOT TESTED
14 DAY WARRANTY FOR COMPLETE REFUND.
DATE CODE 8/19/1984

• NO EXPORT

Name    Value
DIRECT CURRENT VOLTAGE RATING IN VOLTS    28.0
CASE MATERIAL    ALUMINUM ALLOY
END ITEM IDENTIFICATION    F110-GE-129 ENGINE F16 ACFT
UNPACKAGED UNIT LENGTH    10.00 INCHES NOMINAL
UNPACKAGED UNIT WIDTH    6.50 INCHES NOMINAL
UNPACKAGED UNIT HEIGHT    5.00 INCHES NOMINAL
UNPACKAGED UNIT WEIGHT    13.50 POUNDS
POWER SOURCE    EXTERNAL OR SELF-CONTAINED
INTELLIGENCE INPUT METHOD    ELECTRICAL
SPECIAL FEATURES    OPERATING TEMP -65 TO 160 DEG F, MAX 30 MINUTES AT 203 DEG F; DOWNLOAD OPERATING POWER 20 WATTS; NORMAL OPERATING POWER 50 WATTS; DOWNLOAD OPERATING VOLTAGE 28 VDC; THE EMSC IS AN AIRFRAME MOUNTED UNIT CONTAINING A BATTERY (EXCEPT FOR AIR SHIPMENT), A FLEX/CONNECTOR ASSY AND 4 ELECTRONIC COMPONENT ASSEMBLIES INCLUDING DIGITAL PROGRAMMED CPU BOARD
FUNCTIONAL DESCRIPTION    RECEIVES DIGITAL ENGINE PERFORMANCE SIGNALS FROM THE DIGITAL ELECTRONIC CONTROL (DEC) AND ACFT PARAMETERS FROM THE ACFT MUX BUS; THESE SIGNALS ARE COMPARED AGAINST PREDETERMINED LIMITS STORED IN THE EMSC; EXCEEDENCES AND FAULTS ARE TRANSMITTED TO REMOTE ACFT SYSTEMS; ALSO MONITORS THE DEC AND ITS OWN PERFORMANCE AND TRANSMITS DATA TO THE PILOT DISPLAY; DETECTS ENGINE CONTROL LOOP FAILURES AND COMPRESSOR STALLS
PROPRIETARY CHARACTERISTICS    PACS
REFERENCE DATA AND LITERATURE    T.O. 5E1-2-12-1, -4
SUPPLEMENTARY FEATURES    BATTERY IS NOT INCLUDED FOR AIR SHIPMENT; BATTERY POWER 3.67 VDC AND IS MOUNTED IN THE FRONT PANEL OF THE EMSC
FSC APPLICATION DATA    ENGINE MONITORING SYSTEM COMPUTER EMSC