What was found
ON FINAL APPROACH, RIGHT HYDRAULIC SYSTEM FAILED WITH LOSS OF ALL HYDRAULIC FLUID WHEN FLAPS WERE SELECTED TO 5 DEGREES. FOUND A HYDRAULIC LINE IN THE RIGHT WING ROOT AREA LEAKING. INSTALLED A TEMPORARY FLEX LINE IAW SPM 29.01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ON FINAL APPROACH, RIGHT HYDRAULIC SYSTEM FAILED WITH LOSS OF ALL HYDRAULIC FLUID WHEN FLAPS WERE SELECTED TO 5 DEGREES. FOUND A HYDRAULIC LINE IN THE RIGHT WING ROOT AREA LEAKING. INSTALLED A TEMPORARY FLEX LINE IAW SPM 29.01.