Casualties unknown

2023-07-08: Bell Textron Bell 212 Helicopter (A6-ALD) — Close to ARAS Driller Rig, Umm Al Quwain, AE

Close to ARAS Driller Rig, Umm Al Quwain, AE

On July 8, 2023, a Bell Textron Bell 212 Helicopter (registration A6-ALD) was involved in an aviation accident near Close to ARAS Driller Rig, Umm Al Quwain, AE. Investigators recorded the probable cause as: Controlled flight into terrain (CFIT) most probably caused by spatial disorientation due to limited external visual references during night operations, resulting in degrading the pilots’ situational awareness and impairing their ability to maintain proper… This summary draws on records from the UAE Air Accident Investigation Sector (GCAA AAIS).

Sourcesthe UAE Air Accident Investigation Sector (GCAA AAIS)Primary reportUpdated 1784424886Data APIEditorial standards

On 7 September 2023, a Bell 212 helicopter operated by Aerogulf Services crashed into the sea during a night training flight near the ARAS Driller Rig, killing both pilots. The accident was attributed to controlled flight into terrain due to spatial disorientation.

Accident Overview

On 7 September 2023, at approximately 2008 local time, a Bell Textron Bell 212 helicopter, registration A6-ALD, operated by Aerogulf Services Co. (LLC), crashed into the sea near the ARAS Driller Rig offshore Umm Al Quwain, United Arab Emirates. The helicopter was conducting a non-revenue night training flight from Al Maktoum International Airport (OMDW) to the offshore rig. On board were two flight crewmembers: an instructor pilot in the left seat and a pilot undergoing route familiarization in the right seat. During the third circuit at the offshore helideck, shortly after takeoff, the helicopter entered a high rate of descent toward the sea and impacted the water approximately 600 meters northwest of the rig. Both pilots sustained fatal injuries, and the helicopter was destroyed.

Investigation Findings

The investigation, conducted by the UAE Air Accident Investigation Sector (AAIS), determined that the helicopter was airworthy before the flight, with maintenance and inspection records current. Both Pratt & Whitney PT6T-3B engines were operating normally at the time of impact, and examination at the manufacturer's facilities in Canada revealed no anomalies that could have contributed to power loss. SmartCycle data confirmed both engines were delivering high power and maintaining normal rotor speed up to impact. The helicopter was within weight and balance limits, and environmental conditions were within operational parameters. Extensive examination of the main rotor transmission and mast assembly at Bell Textron laboratories found no pre-existing fractures or mechanical defects; grease splatter consistent with approved lubricant indicated normal lubrication prior to impact.

Probable Cause

The accident was categorized as controlled flight into terrain (CFIT). The investigation determined that the most probable cause was spatial disorientation due to limited external visual references during night operations, which degraded the pilots' situational awareness and impaired their ability to maintain proper attitude and level-off maneuver. This degradation prevented them from recognizing the high rate of descent and taking timely recovery actions. A contributing factor was degraded cockpit performance during the dark night flight, compounded by the crew composition: an instructor who was not adequately rested under the applicable prescriptive scheme, and a pilot undergoing route familiarization to that location at night for the first time.

Safety Recommendations

Two safety recommendations were issued to Aerogulf Services to enhance flight training and operational oversight, ensuring effective risk controls for high-risk operations such as night offshore flights. The recommendations also called for review and strengthening of organizational controls and operational policies related to fatigue risk management and crew pairing in potential-risk helicopter operations.