ASN logo
Accident
Last updated: 22 November 2017
Status:Schlussbericht
Datum:Donnerstag 16 Mai 2013
Zeit:08:33
Flugzeugtyp:Silhouette image of generic DHC6 model; specific model in this crash may look slightly different
de Havilland Canada DHC-6 Twin Otter 300
Fluggesellschaft:Nepal Airlines
Kennzeichen: 9N-ABO
Werknummer: 638
Baujahr: 1979-08-24 (33 years 9 months)
Betriebsstunden:32291
Anzahl Zyklen der Zelle:54267
Triebwerk: 2 Pratt & Whitney Canada PT6A-27
Besatzung:Todesopfer: 0 / Insassen: 3
Fluggäste:Todesopfer: 0 / Insassen: 18
Gesamt:Todesopfer: 0 / Insassen: 21
Sachschaden: schwer beschädigt
Konsequenzen: Written off (damaged beyond repair)
Unfallort:Jomsom Airport (JMO) (   Nepal)
Flugphase: Landung (LDG)
Betriebsart:Inländischer planmäßiger Passagierflug
Flug von:Pokhara Airport (PKR/VNPK), Nepal
Flug nach:Jomsom Airport (JMO/VNJS), Nepal
Unfallbericht:
A DHC-6 Twin Otter passenger plane sustained substantial damage in a landing accident at Jomsom Airport (JMO), Nepal. Two crew members and one passenger sustained serious injuries.
The airplane departed Pokhara Airport (PKR) at 08:10 on a domestic flight to Jomsom. While descending towards the destination airport, the Jomsom controller reported that there was a south-westerly 8-12 knot wind with runway 24 in use.
During the approach the pilot in command took over the communication function of the copilot and contacted Jomsom Tower, requesting to use runway 06 instead of runway 24, despite the advice of the tower controller to use runway 24 to avoid tail wind effect in runway 06.
The tailwind component, exceeded the five knot tailwind limit stipulated in the company’s standard operating procedure.
The airplane touched down 776 feet past the threshold of the 2,424-foot-long runway 06. It covered a distance of 194 feet on the airstrip and veered towards the grassland.
During the landing roll, when the aircraft was decelerating, the co-pilot had raised the flaps as per the existing practice of carrying out the after the landing checks."
The pilot in command added power to re-enter the runway. After running 705 feet on the grassland the airplane entered the runway again. Without making his intentions clear to the copilot, the pilot in command continued adding power for go around.
The accelerating aircraft gained insufficient speed and lift to take off and ran out of the runway 24 end, continued towards the river, hit the barbed fence and gabion wall with an initial impact and finally fell down onto the banks of Kaligandaki River.

Probable Cause:

The most probable cause of the accident is the inappropriate conduct of STOL procedure and landing technique carried out by the PIC, during the landing-phase and an endeavour to carry out take off again with no sufficient airspeed, no required lifting force and non availability of required runway length to roll.
Contributory factors to the occurrence is the absence of proper CRM in terms of communication, coordination and briefing in between crew members on intention and action being taken by PIC during pre and post landing phase.

Informationsquelle:
» eKantipur
» Hemant Arjyal
» The Himalayan Times


Sicherheitsempfehlungen

Nepal AAIC issued 12 Safety Recommendations

Show all AD's and Safety Recommendations

Fotos

photo of de Havilland Canada DHC-6 Twin Otter 300 9N-ABO
Add your photo of this accident or aircraft
 

Video, social media

Map
This map shows the airport of departure and the intended destination of the flight. The line between the airports does not display the exact flight path.
Distance from Pokhara Airport to Jomsom Airport as the crow flies is 69 km (43 miles).

This information is not presented as the Flight Safety Foundation or the Aviation Safety Network’s opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.
languages: languages

Share