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Printed page 28. PDF page 28.
Those invalid variations were probably due to channel reconfiguration in the ECU 2. Engine No. 2 Fire Warning triggered during 7 s. This included an ECAM Alert, Master Warning Red light flashing, and CRC Aural Alert. There were N1 vibrationOpen official document at PDF page 28Final investigation report: PIA 8303, AP-BLD
Printed page 146. PDF page 146.
physically at MAX REV) and several Engine No. 2 parameters showed invalid variations for 4 s. Engine No. 2 Fire Warning triggered for 7 s. There were N1 vibration on Engine No. 2 above 5 CU. At 09:34:41, both TLAOpen official document at PDF page 146Final investigation report: PIA 8303, AP-BLD
Printed page 155. PDF page 155.
with a single chime Aural Alert and Master Caution Amber light. 3.1.3.31 Aircraft both Engine nacelles made contact with R/W. Engine No. 2 Fire Alert triggered with associated Master Warning. After R/W contact aircraft again got airborne. 3.1.3.32 During R/WOpen official document at PDF page 155Final investigation report: PIA 8303, AP-BLD