Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)

Modification of a Rockwell Collins, Inc. AHC-85( ) (AHRS) installation. FAA STC ST01713WI

Reduction in maximum zero fuel weight to 23,218 lbs. to reduce payload to FAR 135 limit of 7,500 lbs. For model EMB-120FC.