Boeing 767 36N N768NA

Summary

On 20 June 2014 at about 19:37 local time, a Boeing 767 36N registered N768NA, operated by Omni Air International Inc, was involved in an accident near Kabul, Afghanistan. 81 people were on board and 4 had minor injuries. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

20 June 2014 at 19:37

Classification

Accident

Location

Kabul, Afghanistan

Nearest airport

Kabul International Airport (OAKB)

Coordinates

34.5617, 69.2289

Aircraft

Boeing 767 36N

Registration

N768NA

Category

Airplane

Year built

1999

Engines

2

Operator

Omni Air International Inc

Operating rule

Part 121: Air Carrier

Phase of flight

Not recorded

Route

Bucharest → Kabul

Aircraft damage

Substantial

Weather

VMC

Light

Dusk

NTSB number

DCA14FA122

4 people had minor injuries.

the early reduction of engine thrust that resulted in an excessive sink rate and nose high pitch attitude during the landing flare. Contributing to the accident was a significant change in the vertical and horizontal wind components just prior to touchdown.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The flight experienced a tailstrike on landing resulting in substantial damage to the fuselage and aft pressure bulkhead. There were no injuries to the passengers; however, four of the 16 crewmembers received minor injuries. According to the flight crew statements and recorder data, the landing reference speed for the approach was 145 knots.  Due to the weather conditions, the flight crew added 10 knots to this for their approach speed due to the gusty weather conditions and conducted a visual approach using the visual approach slope indicator as guidance. As a result of the weather and gusty winds, airspeed fluctuated during the approach between 162 knots and 138 knots and engine thrust varied accordingly between about 86% N1 and 40% N1 on approach. The captain stated that the flight was on speed and glide path at 500 feet above the ground but at about 200 feet above the ground, the flight started to move above the glide path and airspeed started to increase. To compensate, the captain reduced engine power and then heard a "sink rate" aural alert when passing through about 50 feet. Flight recorder data indicated the engine N1 decreased to 40%, with throttles at forward idle position, at about 110 feet above the ground, and remained there until after touchdown.  The airplane touched down at 140 knots and a nose up pitch attitude of 8.9 °, increasing to 9.5° immediately after touchdown.  Guidance included in the operator's training manuals indicated that normal touchdown attitude should be between 4 and 6 degrees nose up. Additionally, guidance indicated that thrust should be managed on approach to maintain reference speed, plus any wind additive, until the beginning of the flare. After reaching the flare, thrust levers should be retarded smoothly to idle with main gear touchdown ideally occurring simultaneously with thrust levers reaching idle. An analysis of calculated vertical and horizontal wind effect indicated an existing updraft transitioned to a downdraft and a headwind component transitioned to a tailwind component during the last 5 seconds prior to touchdown.

Quoted verbatim from the NTSB record.