NTSB Prelim: Embraer EMB-145LR | 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-12.01.25

AirborneNextGen-
12.02.25

Airborne-Unlimited-12.03.25

Airborne-FltTraining-12.04.25

AirborneUnlimited-12.05.25

AFE 2025 LIVE MOSAIC Town Hall (Archived): www.airborne-live.net

Thu, Jun 20, 2024

NTSB Prelim: Embraer EMB-145LR

The Flight Crew Described A Feeling That There Was Something Wrong

Location: Houston, TX Accident Number: DCA24FA179
Date & Time: May 3, 2024, 18:00 Local Registration: N942JX
Aircraft: Embraer EMB-145LR Injuries: 1 Minor, 23 None
Flight Conducted Under: Part 135: Air taxi & commuter - Non-scheduled

On May 3, 2024, about 1800 central daylight time (CDT), Delux Public Charter, doing business as JSX flight 284, an Embraer EMB-145LR experienced a left main landing gear (LMLG) collapse during landing at Houston Hobby International Airport (HOU), Houston, Texas. Of the 3 crew and 21 passengers onboard, one crew member sustained minor injuries. The aircraft was substantially damaged. The flight was a public charter sold by JSX, as the charter operator (subject to provisions of Title 14 Code of Federal Regulations (CFR) Part 380) and operated by Delux Public Charter, LLC as the direct air carrier (operating under the provisions of Title 14 CFR Part 135) as a nonscheduled passenger flight from Dallas Love Field airport (DAL), Dallas, Texas to HOU.

The flight crew described an uneventful takeoff, climb, cruise, and descent. The flight data indicated the airspeed, vertical speed, and glide path were stabilized during the majority of the final approach. Surface winds during the approach at HOU were reported from 130 degrees at 16 knots, gusting to 24 knots. As the aircraft flew over the threshold of runway 4 at HOU, the flight crew described a feeling that there was something wrong, and the captain, who was the pilot flying, called for a go-around. The aircraft landed hard shortly thereafter. While the crew did not recall initiating the go-around, flight data showed an increase in throttle lever angle consistent with commanding go-around thrust that began shortly before impact. 

Flight data indicated that the vertical load factor during the touchdown was 3.9 gravitational constants (g). As the aircraft continued down the runway, the LMLG collapsed and punctured through the left-wing upper skin. The aircraft came to a stop on the left side of the runway about 567 ft from the end. Emergency personnel responded to the accident and assisted the passengers as they deplaned through the main cabin door (L1). The first officer was transported to a local hospital for minor injuries.

Visual inspection of the LMLG showed structural damage and deformation, in addition to hydraulic fluid leakage. The left wing spar III, a principal structural element, was bent and fractured through at 2 locations and partially fractured at 3 additional locations. While there was damage to some of the left wing’s structural components, the fuel tank was not compromised during the event. Most of the structural damage to the inboard section of the wing was consistent with a strong upward force from the LMLG. Damage to the outboard section of the wing was consistent with the wing scraping the runway surface and impacting runway lights.

The following NTSB specialists were assigned to investigate the accident: Airworthiness, Operations, Human Performance, Cockpit Voice Recorder (CVR), and Flight Data Recorder (FDR). The Federal Aviation Administration (FAA) and Delux Public Charter are parties to the investigation. The airplane was designed and manufactured in Brazil, and pursuant to International Civil Aviation Organization Annex 13, Centro de Investigação e Prevenção de Acidentes Aeronáuticos (CENIPA) assigned an Accredited Representative to the investigation and designated Embraer as a technical advisor.

The CVR and FDR were removed from the aircraft by NTSB investigators and were shipped to NTSB headquarters in Washington, DC where they were successfully downloaded. The aircraft wreckage was documented during the on-scene portion of the investigation and flight crew interviews were conducted via video conference on May 5, 2024. 

The investigation continues.

FMI: www.ntsb.gov

Advertisement

More News

ANN's Daily Aero-Term (12.04.25): Cooperative Surveillance

Cooperative Surveillance Any surveillance system, such as secondary surveillance radar (SSR), wide-area multilateration (WAM), or ADS-B, that is dependent upon the presence of cert>[...]

ANN's Daily Aero-Linx (12.04.25)

Aero Linx: OX5 Aviation Pioneers Incorporated in 1955 as a Pa 501 (c)(3) Not for Profit Corporation, the OX5 Aviation Pioneers is dedicated to bringing before the public the accomp>[...]

NTSB Prelim: Extra Flugzeugproduktions EA 300/SC

The Pilot Appeared To Regain Control After Six Rotations And Attempted To “Fly Out” Inverted But Had Insufficient Altitude On November 8, 2025, at 1038 eastern standard>[...]

Classic Aero-TV: The Bally Bomber - The All Time Ultimate Warbird Replica?

From 2018 (YouTube Edition): Aero-News Talks With The Airplane's Builder One of the many unique airplanes at AirVenture 2018 was a 1/3-scale B-17 bomber built by Jack Bally, who ta>[...]

ANN's Daily Aero-Linx (12.05.25)

Aero Linx: Society of U.S. Army Flight Surgeons (SoUSAFS) The Society of US Army Flight Surgeons (SoUSAFS) serves to advance the science and art of Aerospace Medicine and its allie>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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