DCA18CA007
2017-10-15 · Honolulu, Hawaii, United States · Serious · 1 aircraft · Status: Completed
Airport PHNL
Current FAA registration · N342AX
- Make / Model
- BOEING 767-328
- Year of manufacture
- 1993 · 24 years old at event
- Engine
- GE CF6-80C2B6F
- Seats / Engines
- 269 seats · 2 engines
- Last airworthiness date
- 20090807
- ADS-B equipped
- Yes — Mode-S A3C4D2
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
an inadvertent encounter of clear air turbulence.
Factual narrative
On October 15, 2017, at about 1022 universal coordinated time , Omni Air International, LLC, Boeing B-767-300ER, N342AX, was enroute to Daniel K. Inouye International Airport (DFS), Honolulu, Hawaii, when the flight encountered turbulence that caused serious injuries to one "deadheading" cabin crew member. None of the other 11 crew members were injured and the airplane was not damaged. The flight was conducted under the provisions of 14 Code of Federal Regulations Part 91 between Osan Air Base (OSN), Pyeongtaek, Republic of Korea, to DFS. As the flight was descending through about flight level 315 over the Pacific Ocean, approximately 117 miles from DFS, the airplane entered a thunderstorm cell and encountered severe turbulence that lasted about 30 seconds. When the turbulence was encountered, an off duty "deadheading" cabin crew member was in the aisle near the aft lavatory and was thrown to the floor injuring her right ankle. After being notified of the injury, the flight crew contacted telemedical advisory services via voice satellite communications and was provided medical direction to stabilize the injured crew member. Emergency medical personnel met the airplane on arrival and the injured crew member was transported to a local hospital where she was diagnosed with fractures in the right lateral and medial malleolus. Analysis of digital flight data retrieved from the Aeromechanical Systems Airborne Flight Information Reporting System (AFIRS) indicated that the airplane experienced vertical accelerations up to 1.78 g's and as low as 0.46 g's, with a change in rate of descent ranging from +240 feet per minute to -4,080 feet per minute. The flight crew reported no indication of precipitation or wind shear on the installed radar. The operator indicated that review of recorded telemetry reported by four other aircraft in the area equipped with The Weather Company Turbulence Auto-PIREP System (TAPS) showed no evidence of turbulence at the time of the accident. On October 15, 2017, at about 1022 universal coordinated time , Omni Air International, LLC, Boeing B-767-300ER, N342AX, was enroute to Daniel K. Inouye International Airport (DFS), Honolulu, Hawaii, when the flight encountered turbulence that caused serious injuries to one "deadheading" cabin crew member. None of the other 11 crew members were injured and the airplane was not damaged. The flight was conducted under the provisions of 14 Code of Federal Regulations Part 91 between Osan Air Base (OSN), Pyeongtaek, Republic of Korea, to DFS. As the flight was descending through about flight level 315 over the Pacific Ocean, approximately 117 miles from DFS, the airplane entered a thunderstorm cell and encountered severe turbulence that lasted about 30 seconds. When the turbulence was encountered, an off duty "deadheading" cabin crew member was in the aisle near the aft lavatory and was thrown to the floor injuring her right ankle. After being notified of the injury, the flight crew contacted telemedical advisory services via voice satellite communications and was provided medical direction to stabilize the injured crew member. Emergency medical personnel met the airplane on arrival and the injured crew member was transported to a local hospital where she was diagnosed with fractures in the right lateral and medial malleolus. Analysis of digital flight data retrieved from the Aeromechanical Systems Airborne Flight Information Reporting System (AFIRS) indicated that the airplane experienced vertical accelerations up to 1.78 g's and as low as 0.46 g's, with a change in rate of descent ranging from +240 feet per minute to -4,080 feet per minute. The flight crew reported no indication of precipitation or wind shear on the installed radar. The operator indicated that review of recorded telemetry reported by four other aircraft in the area equipped with The Weather Company Turbulence Auto-PIREP System (TAPS) showed no evidence of turbulence at the time of the accident. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Environmental issues-Conditions/weather/phenomena-Turbulence-Clear air turbulence-Effect on personnel - C
Verbatim from NTSB's published report. Source file
NTSB_2017_DCA18CA007.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (wind shear, stall, turbulence, thunderstorm). All research papers
- NASA NTRS 2019 · Contractor Report (CR) An Examination of Aviation Accidents Associated with Turbulence, Wind Shear and Thunderstorm
The focal point of the study reported here was the definition and examination of turbulence, wind shear and thunderstorm in relation to aviation accidents.
- NASA NTRS 2019 · Reprint (Version printed in journal) Observations of severe turbulence near thunderstorm tops
Data derived from the flight tapes of two airliners that experienced severe turbulence near thunderstorm tops are used to produce quantitative descriptions of the turbulence and its environment.
- Embry-Riddle Scholarly Commons 2021 · Journal article (IJAAA) Comparative Study on the Prediction of Aerodynamic Characteristics of Mini - Unmanned Aerial Vehicle with Turbulence Models
When dealing with CFD simulations the turbulent nature is seen on most of the engineering flows and these flows need to be solved.
- arXiv 2020 · arXiv preprint Numerical Simulation of Iced Wing Using Separating Shear Layer Fixed Turbulence Models
Aerodynamic prediction of glaze ice accretion on airfoils and wing is studied using the Reynolds-averaged Navier-Stokes method.
- NASA NTRS 2019 · Conference Paper Optimal recovery from microburst wind shear
The flight path of a twin-jet transport aircraft is optimized in a microburst encounter during approach to landing. The objective is to execute an escape maneuver that maintains safe ground clearance …
- NASA NTRS 2019 · Conference Proceedings Operational evaluation of thunderstorm penetration test flights during project Storm Hazards '80
The National Aeronautics and Space Administration is conducting a research project called Storm Hazards '80 in order to study the prediction, detectability and avoidance of the hazards of severe storm…