What was found
ENGINE 2 BLEED FAULT IN FLIGHT DUE TO PNEUMATIC AIR LEAK WAS REMOVED AND REPLACED THE SENSE LINE BTW THE PRV AND THE PYLON INTERFACE ON ENGINE #2 I.A.W AMM 36-11-49-000/400-026-A REV 71 REV DATE 01-FEB-2025 AND PERFORMED LEAK CHECK I.W.A AMM 36-11-52-790-001-A REV 71 REV DATE 01-FEB-2025, NOT FOUND LEAKS ON THE SENSE LINE ENGINE 2 BLEED FAULT IN FLIGHT PERFORMED LEAK TEST OF THE BLEED PRESSURE REGULATOR VALVE WITH THE ENGINE IN OPERATION IAW AMM 36-11-52-790-001-A REV 71 REV DATE 01 FEB 2025 TEST PASS OK