As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) GENERAL VIBRATION AND BUZZING DURING AND AFTER ENGINE START CYCLE. #2 ENGINE HYDRAULIC PRESSURE AT 1100 TO 1200 PSI ONLY. CAUTION LIGHT ON. LH INBOARD GROUND SPOILER ACTUATOR FAILED. SB 8-27-62 COVERS MODIFICATION OF THIS P/N UNIT.