What was found
THE A-HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. MANUALLY EXTENDED THE LANDING GEAR AND RETURNED TO STL. REPLACED THE O/B FLAP DRIVE MOTOR DUE TO LEAKAGE. CHECK-C 8-24-98 MCI.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE A-HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. MANUALLY EXTENDED THE LANDING GEAR AND RETURNED TO STL. REPLACED THE O/B FLAP DRIVE MOTOR DUE TO LEAKAGE. CHECK-C 8-24-98 MCI.