NTSB Final Report: Hagerty Glasair Super IIS-TD | 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-05.19.25

Airborne-NextGen-05.20.25

AirborneUnlimited-05.21.25

Airborne-AffordableFlyers-05.22.25

AirborneUnlimited-05.23.25

Mon, Apr 22, 2024

NTSB Final Report: Hagerty Glasair Super IIS-TD

During The Climb, About 4,500 Ft Mean Sea Level, The Engine Began To Run Rough, And Shortly Thereafter Lost All Power

Location: Jasper, Georgia Accident Number: ERA23LA063
Date & Time: November 4, 2022, 15:00 Local Registration: N430JV
Aircraft: Hagerty Glasair Super IIS-TD Aircraft Damage: Substantial
Defining Event: Sys/Comp malf/fail (non-power) Injuries: 1 None
Flight Conducted Under: Part 91: General aviation - Personal

Analysis: The pilot reported that during the climb, about 4,500 ft mean sea level, the engine began to run rough, and shortly thereafter lost all power. The pilot immediately turned back toward the departure airport, which was about 5 miles from his position. He began troubleshooting the loss of power, but power was not restored. The pilot was able to glide to the airport; however, in a right turn to align with the runway, the pilot felt the onset of an aerodynamic stall. He leveled the wings, the airplane overshot the runway, descended abruptly, and impacted a grass area hard next to the runway. The left wing and fuselage sustained substantial damage. 

A postaccident test run of the engine revealed it produced normal power with the electric fuel pump on, but would not operate with only the engine-driven fuel pump. Further examination and disassembly of the engine-driven fuel pump revealed no anomalies that would have explained its inability to pump fuel.

The pilot reported that in the climb he turned off the electric fuel pump and, after the loss of power, he did not turn the pump back on, despite the owner’s manual instructing pilots to use the electric fuel pump following a loss of engine power. Had the pilot turned the electric fuel pump on, power likely would have been restored.

Probable Cause and Findings: The National Transportation Safety Board determines the probable cause(s) of this accident to be -- The loss of engine power due to the failure of the engine-driven fuel pump and the pilot’s failure to use the electric fuel pump, which resulted in a forced, hard landing. 

FMI: www.ntsb.gov

Advertisement

More News

ANN's Daily Aero-Term (05.29.25): Terminal Radar Service Area

Terminal Radar Service Area Airspace surrounding designated airports wherein ATC provides radar vectoring, sequencing, and separation on a full-time basis for all IFR and participa>[...]

ANN's Daily Aero-Term (05.30.25): Very High Frequency (VHF)

Very High Frequency (VHF) The frequency band between 30 and 300 MHz. Portions of this band, 108 to 118 MHz, are used for certain NAVAIDs; 118 to 136 MHz are used for civil air/grou>[...]

Aero-News: Quote of the Day (05.30.25)

“From approximately November 2021 through January 2022, Britton-Harr, acting on behalf of AeroVanti, entered into lease-purchase agreements for five Piaggio-manufactured airc>[...]

Airborne 05.23.25: Global 8000, Qatar B747 Accepted, Aviation Merit Badge

Also: Virtual FLRAA Prototype, IFR-Capable Autonomous A/C, NS-32 Crew, Golden Dome Missile Defense Bombardier announced that the first production Global 8000 successfully completed>[...]

ANN's Daily Aero-Linx (05.30.25)

Aero Linx: The 1-26 Association (Schweizer) The Association’s goal is to foster the helpfulness, the camaraderie, and the opportunity for head-to-head competition that is fou>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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