Al Fashir - Sarif-Umra
Flight / Schedule
Al Fashir - Sarif-Umra
Aircraft
PZL-Mielec AN-28Registration
ST-TYB
MSN
1AJ006-02
Year of Manufacture
1988
Operator
Eldinder AviationDate
July 6, 2009 at 09:50 AM
Type
CRASHFlight Type
Cargo
Flight Phase
Landing (descent or approach)
Crash Site
Airport (less than 10 km from airport)
Crash Location
Sarif-Umra North Darfur (<U+0634><U+0645><U+0627><U+0644> <U+062F><U+0627><U+0631><U+0641><U+0648><U+0631>)
Region
Africa • Sudan
Crash Cause
Weather
Narrative Report
On July 6, 2009 at 09:50 AM, Al Fashir - Sarif-Umra experienced a crash involving PZL-Mielec AN-28, operated by Eldinder Aviation, with the event recorded near Sarif-Umra North Darfur (<U+0634><U+0645><U+0627><U+0644> <U+062F><U+0627><U+0631><U+0641><U+0648><U+0631>).
The flight was categorized as cargo and the reported phase was landing (descent or approach) at a airport (less than 10 km from airport) crash site.
2 people were known to be on board, 0 fatalities were recorded, 2 survivors were identified or estimated. This corresponds to an estimated fatality rate of 0.0%.
Crew on board: 2, crew fatalities: 0, passengers on board: 0, passenger fatalities: 0, other fatalities: 0.
The listed crash cause is weather. The flight progress strip at Al Fashir aerodrome control tower illustrate that on the 6th of July 2009 – ST-TYB, AN-28 departed Al Fashir at time 0601 UTC, estimated time to arrive destination Sarif-Umra was 0650 UTC, persons on board were two (crew only), intended flight level was 085 (VFR) re-cleared later FL105, fuel endurance was 3,5 hours, load on board as indicated on the cargo manifest was 1511 k.gm (food stuff) destined for the UNAMID forces. Aircraft center of gravity was organized. Calculated actual take off weight was 6335 k.gm and the actual landing weight was 6035 k.gm as reported by the pilot. The aircraft proceeded normally to destination at FL 105, when it reached the airfield, the pilot stated that, they started descend gradually at a speed of 250 km/h willing to check the strip serviceability and to specify the direction of landing from the located wind sock. They detected that, the strip was clear, dry and the wind was favorable to the direction of 23 (strip 23/05). As the crew established a speed of 210 km/h at an altitude of 60 meters on final approach, they saw a dust devil storm on their right crossing the air strip, to avoid this phenomena, they decided to go around for another approach. Eye witnesses confirmed the occurrence of the storm at the time the aircraft commenced the final approach. The crew reported that, they started a right turn and applied full power to gain height, but they felt that there was no response from the engines and the aircraft was influenced by a wind shear and began to sink. The crew managed to control the aircraft, but in few minutes its altitude decreased rapidly. At time 0650 UTC the aircraft impacted with the ground and rolled, there after struck a small rock and bounced, finally the aircraft impacted the ground by the left main gear and nose, and stopped at a distance of 1,850 meters from the beginning of strip 05 coordinates N 13 29.527 <U+0640><U+0640><U+0640><U+0640><U+0640><U+0640><U+0640> E 023 16.794. Crews (2) were safe and the aircraft sustained substantial damage.
Aircraft reference details include registration ST-TYB, MSN 1AJ006-02, year of manufacture 1988.
Fatalities
Total
0
Crew
0
Passengers
0
Other
0
Crash Summary
The flight progress strip at Al Fashir aerodrome control tower illustrate that on the 6th of July 2009 – ST-TYB, AN-28 departed Al Fashir at time 0601 UTC, estimated time to arrive destination Sarif-Umra was 0650 UTC, persons on board were two (crew only), intended flight level was 085 (VFR) re-cleared later FL105, fuel endurance was 3,5 hours, load on board as indicated on the cargo manifest was 1511 k.gm (food stuff) destined for the UNAMID forces. Aircraft center of gravity was organized. Calculated actual take off weight was 6335 k.gm and the actual landing weight was 6035 k.gm as reported by the pilot. The aircraft proceeded normally to destination at FL 105, when it reached the airfield, the pilot stated that, they started descend gradually at a speed of 250 km/h willing to check the strip serviceability and to specify the direction of landing from the located wind sock. They detected that, the strip was clear, dry and the wind was favorable to the direction of 23 (strip 23/05). As the crew established a speed of 210 km/h at an altitude of 60 meters on final approach, they saw a dust devil storm on their right crossing the air strip, to avoid this phenomena, they decided to go around for another approach. Eye witnesses confirmed the occurrence of the storm at the time the aircraft commenced the final approach. The crew reported that, they started a right turn and applied full power to gain height, but they felt that there was no response from the engines and the aircraft was influenced by a wind shear and began to sink. The crew managed to control the aircraft, but in few minutes its altitude decreased rapidly. At time 0650 UTC the aircraft impacted with the ground and rolled, there after struck a small rock and bounced, finally the aircraft impacted the ground by the left main gear and nose, and stopped at a distance of 1,850 meters from the beginning of strip 05 coordinates N 13 29.527 <U+0640><U+0640><U+0640><U+0640><U+0640><U+0640><U+0640> E 023 16.794. Crews (2) were safe and the aircraft sustained substantial damage.
Cause: Weather
Occupants & Outcome
Crew On Board
2
Passengers On Board
0
Estimated Survivors
2
Fatality Rate
0.0%
Known people on board: 2
Operational Details
Schedule / Flight
Al Fashir - Sarif-Umra
Operator
Eldinder AviationFlight Type
Cargo
Flight Phase
Landing (descent or approach)
Crash Site
Airport (less than 10 km from airport)
Region / Country
Africa • Sudan
Aircraft Details
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