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Printed page 32. PDF page 32.
only CVR recording resumed until end of the flight. 1.1.9.2. The events mentioned after 09:36:27 are only based on the analysis of the CVR (recording and spectral analysis). The Engine No. 1 N1 frequency could not be heard on CVROpen official document at PDF page 32Final investigation report: PIA 8303, AP-BLD
Printed page 53. PDF page 53.
reconfiguration phase of aircraft electrical system into EEC. CVR recovered after about 8 s at 09:36:27 due to RAT deployment and then remained available till end of flight at 09:40:18. Due to non- availability of DFDR recording after 09:36:17, bothOpen official document at PDF page 53Final investigation report: PIA 8303, AP-BLD
Printed page 143. PDF page 143.
was a transient CVR shutdown at 09:36:19. The CVR was then recovered (after 8 s) at 09:36:27 and remained powered until the ground impact. This is consistent with a nominal reconfiguration of the electrical system in EEC. Final Report -Open official document at PDF page 143Final investigation report: PIA 8303, AP-BLD