NTSB Prelim: Bell 206B | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-07.14.25

Airborne-NextGen-07.15.25

AirborneUnlimited-07.16.25

Airborne-FlightTraining-07.17.25

AirborneUnlimited-07.11.25

Mon, Oct 18, 2021

NTSB Prelim: Bell 206B

At 40 Knots And 175 Ft AGL, The Helicopter Started To Yaw To The Right

Location: Gonzales, LA Accident Number: CEN22LA009
Date & Time: October 6, 2021, 14:15 Local Registration: N373SP
Aircraft: Bell 206B Injuries: 1 Minor
Flight Conducted Under: Public aircraft

On October 6, 2021, about 1415 central daylight time, a Bell 206B helicopter, N373SP, sustained substantial damage when it was involved in an accident near Gonzales, Louisiana. The commercial pilot sustained minor injuries. The helicopter was operated as a public aircraft flight.

The pilot of the Louisiana State Police Air Support Unit helicopter reported that while on the downwind leg to land to runway 35 at the Louisiana Regional Airport (REG), Gonzales, Louisiana, he completed the before landing checks. The pilot then reduced the power and began to slow the helicopter to about 60 knots. After completing the base leg, he maneuvered the helicopter for final while at 400 ft agl. The pilot applied a small amount of power to sustain the  desired approach angle. While at 40 knots and 175 ft agl, the helicopter started to yaw to the right. The pilot applied left pedal and the helicopter continued to yaw to the right.

The pilot observed the trim indicator and confirmed that the helicopter was in trim, however he still had to apply left pedal. Shortly thereafter, the helicopter “aggressively” yawed to the right. The pilot applied forward cyclic input and the helicopter rolled to the left while it continued to rotate “very aggressively” to the right. The pilot attempted to regain control using cyclic input, however he was unable. The pilot decreased the throttle to idle, the helicopter began to settle, and he applied collective input to cushion the landing. The helicopter came to rest partially upright on the grass, with the skids split, about 200 ft short of the approach end of the runway. The pilot performed an emergency shutdown and was able to egress from the helicopter without further incident.

The helicopter sustained substantial damage to the main rotor system, the fuselage, the tailboom, and the tail rotor system. The wreckage was recovered for a future examination of the airframe and engine.

FMI: www.ntsb.gov

Advertisement

More News

ANN's Daily Aero-Term (07.15.25): Charted Visual Flight Procedure Approach

Charted Visual Flight Procedure Approach An approach conducted while operating on an instrument flight rules (IFR) flight plan which authorizes the pilot of an aircraft to proceed >[...]

Aero-News: Quote of the Day (07.15.25)

“When l became the Secretary of Defense, I committed to rebuild our military to match threats to capabilities. Drones are the biggest battlefield innovation in a generation, >[...]

ANN's Daily Aero-Linx (07.15.25)

Aero Linx: Stearman Restorers Association Welcome to the Stearman Restorers Association. The Stearman Restorers Association is an independent “Not for Profit” 501C-3 Co>[...]

NTSB Final Report: Kjelsrud Gary Kitfox

Airplane Exhibited A Partial Loss Of Engine Power When It Was About Halfway Down The Runway Analysis: The pilot of the experimental amateur-built airplane was departing from his pr>[...]

NTSB Prelim: Cessna A150L

The Flight Path Was Consistent With Low-Altitude Maneuvering On June 18, 2025, about 0922 mountain standard time, a Cessna A150L airplane, N6436F, was substantially damaged when it>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2025 Web Development & Design by Pauli Systems, LC