What was found
NR 1 ENGINE SYS FAULT ILLUMINATED. PERFORMED TSM 75-32-00-810-844-A. REPLACED THE LT ENGINE ACTIVE HPC BLEED VALVE CONTROL SOLENOID IAW AMM 75-32-03-400-801-A. TEST 3 IDLE & LEAK CHECKED GOOD. OK FOR SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 ENGINE SYS FAULT ILLUMINATED. PERFORMED TSM 75-32-00-810-844-A. REPLACED THE LT ENGINE ACTIVE HPC BLEED VALVE CONTROL SOLENOID IAW AMM 75-32-03-400-801-A. TEST 3 IDLE & LEAK CHECKED GOOD. OK FOR SERVICE.