As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ENGINE EXCEED ON TAKE OFF N2 INDICATE 103. MAX THRUST TAKE OF EPR 1.75. EXCEEDANCE HAPPENED IN LOW SPEED ON TAKE OFF. BELOW 80 KTS. NO HOT BRAKES. ADD EMP:U374916 EXCEED RECORDED ON #1 ENG N2 103% FOR 8 SECONDS. RR ENGINEERING REQUESTED BVCU TEST FOR #1 ENG EXCEEDANCE. BVCU REPORTS FAULT 12 FOR ALL RECORDED FLIGHT LEGS. (IP STAGE 1 BLEED VALVE SOLENOID OPEN CIRCUIT ON COIL A OR B, OR THE TWO COILS A&B). FLAGGING FOR SDR PERFORMED TEST 3 REF AMM 71-00-00-715-049-R03. BLEED VALVE WITHIN OPERATIONAL TEST LIMITS PER TABLE 502.