As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING 'L' CHECK IT WAS NOTICED THAT NR 2 ENGINE POWER LEVER APPEARED TO NOT MAKE FULL FORWARD TRAVEL. UPON INVESTIGATION, FOUND POWER LEVER BINDING AT FULL PWR SETTING DUE TO HMU TO PCU POWER LEVER ROD ASSEMBLY INSTALLED ON WRONG SIDE OF HMU PWR LEVER. POWER LEVER ROD ASSEMBLY REINSTALLED ON CORRECT SIDE IAW DASH 8 MM CH 76-10-00 FIG 206 PG 218.