What was found
AIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF HYDRAULIC LEAK AND LOW PRESSURE INDICATION. DURING REVISION WAS DETECTED A CRACK ON THE LEFT FUSE ASSEMBLY HYDRAULIC QUANTITY MEASURE. IT WAS CHANGED IAW MM, TEST OK.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF HYDRAULIC LEAK AND LOW PRESSURE INDICATION. DURING REVISION WAS DETECTED A CRACK ON THE LEFT FUSE ASSEMBLY HYDRAULIC QUANTITY MEASURE. IT WAS CHANGED IAW MM, TEST OK.