What was found
ENGINE NR 2 COMPRESSOR STALL WHEN ON POSITION RUNNING UP THE ENGINES AT 80 PERCENT, HIGH CROSSWIND COMPONENT. INSPECTED NR 2 ENGINE FAN, NO DEFECTS NOTED. ACCESS HATCH SECURED IAW M/M 71-00 PAGE 608.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ENGINE NR 2 COMPRESSOR STALL WHEN ON POSITION RUNNING UP THE ENGINES AT 80 PERCENT, HIGH CROSSWIND COMPONENT. INSPECTED NR 2 ENGINE FAN, NO DEFECTS NOTED. ACCESS HATCH SECURED IAW M/M 71-00 PAGE 608.