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Pakistan International Airlines 8303

Printed page 15. PDF page 15.

Go-Around. Both Engines were damaged during the contact with the R/W. The resultant loss of Engine oil and subsequent lack of lubrication resulted in failure of both Engines. Around 2,000 ft, flight crew announced that they have lost Engines, followed
Open official document at PDF page 15Final investigation report: PIA 8303, AP-BLD

Pakistan International Airlines 8303

Printed page 146. PDF page 146.

punctured wall (hole in the casing) allowing Oil leakage. This resulted in the total loss of Engine Oil on both Engines, and the triggering of the OIL LOW PRESSURE Red Warnings. Subsequent to the loss of lubrication, both Engines failed
Open official document at PDF page 146Final investigation report: PIA 8303, AP-BLD

Pakistan International Airlines 8303

Printed page 152. PDF page 152.

were damaged during contact with the R/W, particularly AGBs and TGBs. The resultant loss of Engine Oil and subsequent lack of lubrication resulted in failure of both Engines in sequence (Engine No. 1, followed by Engine No. 2). 3.1.1.8 ELT
Open official document at PDF page 152Final investigation report: PIA 8303, AP-BLD

Pakistan International Airlines 8303

Printed page 158. PDF page 158.

where both Engines' nacelle made contact with R/W. Both Engines were damaged causing loss of Engine Oil and lubrication which resulted in failure of both Engines during Go-Around. 3.1.1.2 Non-adherence to SOPs and disregard of ATC instructions during the event
Open official document at PDF page 158Final investigation report: PIA 8303, AP-BLD

Pakistan International Airlines 8303

Printed page 73. PDF page 73.

of the Outer End Gear Teeth: Cylindrical Cut View Shape Figure 79 - Oil Distribution: Loss of Oil due to TGB (Possibly TGB and Pipes) Housing Hole Figure 80 - Fuel Filter Cover with Figure 81 - Fuel Filter cover
Open official document at PDF page 73Final investigation report: PIA 8303, AP-BLD

Pakistan International Airlines 8303

Printed page 74. PDF page 74.

lower part showed marks of friction with hard flat surface, material displacement and loss of material. Damages on TGB along with punctured wall allowed Oil leakage. It was consistent with the lower part of the Nacelle and Engine No. 2
Open official document at PDF page 74Final investigation report: PIA 8303, AP-BLD