Casualties unknown

2018-08-30: Boeing 747-47UF (N415MC) — Abnormal Runway Contact of Boeing 747-47UF at Hong Kong International Airport, HK

Abnormal Runway Contact of Boeing 747-47UF at Hong Kong International Airport, HK

On August 30, 2018, a Boeing 747-47UF (registration N415MC) was involved in an aviation accident near Abnormal Runway Contact of Boeing 747-47UF at Hong Kong International Airport, HK. Investigators recorded the probable cause as: The damage to the underside of the inlet cowl, fan cowl and reverser translating cowl of No.3 and No.4 engines was due to the combined effects of a sharp right yaw and significant right roll corresponding to the exaggerated inputs to the flight controls made… This summary draws on records from the Air Accident Investigation Authority of Hong Kong (AAIA); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Air Accident Investigation Authority of Hong Kong (AAIA)Primary reportUpdated 1785027978Data APIEditorial standards
Aircraft registered N415MC
Aircraft registered N415MC. Photo: YSSYguy at en.wikipedia / CC BY-SA 3.0, via Wikimedia Commons

On 30 August 2018, a Boeing 747-47UF veered and rolled on landing, causing No.3 and No.4 engine nacelles to contact the runway. Damage occurred; no fire. The pilot's exaggerated flight control inputs led to a sharp yaw and roll.

History of the Flight

On 30 August 2018, Atlas Air flight GTI 8086, a Boeing 747-47UF registered as N415MC, operated from Al Maktoum International Airport, Dubai (OMDW) to Hong Kong International Airport (VHHH). Shortly after touchdown on Runway 25R, the aircraft veered to the right and then to the left of the runway centreline. About five seconds later, it reversed abruptly towards the centreline.

Damage

As the aircraft veered right, it rolled such that the bottom of the No.3 and No.4 engine nacelles made contact with the runway. The lower section of the engine nacelles and the No.4 engine were damaged. No engine fire or abnormal indications on engine instruments were observed. The aircraft taxied to a cargo parking stand.

Investigation Findings

The investigation identified that the damage to the underside of the inlet cowl, fan cowl, and reverser translating cowl of the No.3 and No.4 engines was due to the combined effects of a sharp right yaw and a significant right roll. These movements corresponded to exaggerated inputs to the flight controls made by the pilot flying. The investigation resulted in one safety recommendation.

Probable Cause

The damage to the engine nacelles was due to the combined effects of a sharp right yaw and significant right roll corresponding to the exaggerated inputs to the flight controls made by the pilot flying.