Alvorlig luftfartshendelse Myanmar - Below par CRM - ASN

Status:	Final
Date:	Wednesday 8 May 2019
Time:	18:51
Type:	de Havilland Canada DHC-8-402Q Dash 8
Operator:	Biman Bangladesh Airlines
Registration:	S2-AGQ
C/n / msn:	4367
First flight:	2011
Total airframe hrs:	8115
Engines:	2 Pratt & Whitney Canada PW150A
Crew:	Fatalities: 0 / Occupants: 6
Passengers:	Fatalities: 0 / Occupants: 28
Total:	Fatalities: 0 / Occupants: 34
Aircraft damage:	Damaged beyond repair
Location:	Yangon-Mingaladon Airport (RGN) (   Myanmar)
Phase:	Landing (LDG)
Nature:	International Scheduled Passenger
Departure airport:	Dhaka-Shahjalal International Airport (DAC/VGHS), Bangladesh
Destination airport:	Yangon-Mingaladon Airport (RGN/VYYY), Myanmar
Flightnumber:	BG060

Narrative:
A Biman Bangladesh Airlines DHC-8-400 suffered an accident during an attempted landing on runway 21 at Yangon-Mingaladon Airport, Myanmar.
The aircraft departed Dhaka-Shahjalal International Airport, Bangladesh, as Biman flight 060 about 15:15 hours local time with destination Yangon-Mingaladon Airport in Myanmar. Weather at Yangon was poor due to the presence of a thunderstorm in the area.
While the flight crew was performing an ILS approach, the controller instructed them to go around as the airport was closed due to weather. When the weather condition got better, the flight was cleared for an RNP approach to runway 21 because only the localizer was available at that moment. The co-pilot was Pilot Flying and the captain was Pilot Monitoring. The aircraft was higher than the 3 degree approach path and the airspeed fluctuated between 136 and 151 kts, which was than the 122 kts target airspeed.
The captain said "continue, continue" to the copilot and the approach was continued. At an altitude of 22 feet over the runway, the captain began pushing the control column forward, while the PF was attempting to pull on the control column. The aircraft briefly skipped on the runway a few times before getting airborne again. The captain then stated: "I have control", which was confirmed by the co-pilot. While in the air, the captain applied the brake pedal several times. At a height of 44 feet, the captain put the propellers in beta range and reduced the power lever angle to 18 degrees. The aircraft sank again and collided with runway 03 and slid forward. It left the runway and came to a complete stop in the over-run area.
The aircraft fuselage broke in just behind the forward passenger door and just behind the rear service door. The undercarriage collapsed and the right hand wing broke at the attachment point with the fuselage. There was no fire. All occupants survived, but twelve suffered serious injuries.