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Pakistan International Airlines 8303

Printed page 24. PDF page 24.

was 5,300 ft/min. G/S signal was corresponding to ~ 4� G/S and decreasing. 1 s later, Landing Gears were selected UP, and 3 s later Speed Brakes were retracted. 14 s later, Landing Gears were recorded Uplocked. 13 s interval
Open official document at PDF page 24Final investigation report: PIA 8303, AP-BLD

Pakistan International Airlines 8303

Printed page 132. PDF page 132.

PULL UP 09:32:57 � No Go-Around triggered at "PULL UP" activation - � ROD 5,300 ft/min Landing Gears were selected UP 09:32:58 - Karachi Approach: Pakistan 8303 clear land 25L 09:32:59 - Speed Brakes were retracted 09:33:02 � Pitch attitude
Open official document at PDF page 132Final investigation report: PIA 8303, AP-BLD

Pakistan International Airlines 8303

Printed page 133. PDF page 133.

Investigation Board of Pakistan 2.2.2.24 Landing Gears and Speed Brakes Retracted - At 09:32:57, Landing Gears were selected UP, and 2 s later Speed Brakes were retracted. 14 s later, Landing Gears were recorded Uplocked which is consistent with a
Open official document at PDF page 133Final investigation report: PIA 8303, AP-BLD

Pakistan International Airlines 8303

Printed page 154. PDF page 154.

did not call out GPWS Caution. 3.1.3.24 At 1,600 ft baro altitude, 5 NM from R/W 25L, Landing Gears were selected UP, and Speed Brakes were retracted. Retraction of Landing Gears and Speed Brakes were not verbalized. 3.1.3.25 At 1,100
Open official document at PDF page 154Final investigation report: PIA 8303, AP-BLD

Pakistan International Airlines 8303

Printed page 30. PDF page 30.

Aircraft Accident Investigation Board of Pakistan 1.1.8.6. At 09:34:57, 140 ft RA, Landing Gears were selected DOWN and then UP, FDs Lateral MODE changed to NAV. During the transient selection of the Landing Gears to the DOWN position, no change
Open official document at PDF page 30Final investigation report: PIA 8303, AP-BLD

Pakistan International Airlines 8303

Printed page 93. PDF page 93.

(climbing away after R/W contact) and the aircraft CAS was between 168 kts and 187 kts. The Landing Gears was selected DOWN transiently for 1 sample then UP again at 9:34:57, and was therefore UP at the time of the
Open official document at PDF page 93Final investigation report: PIA 8303, AP-BLD