NTSB Prelim: ZENITH CH 750 | 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-05.13.24

Airborne-NextGen-05.07.24

Airborne-Unlimited-05.08.24 Airborne-FlightTraining-05.09.24

Airborne-Unlimited-05.10.24

Sun, Sep 27, 2020

NTSB Prelim: ZENITH CH 750

Engine Restart Was Unsuccessful, And The Pilot Initiated A Forced Landing

Location: Montrose, MO Accident Number: CEN20LA412
Date & Time: 09/20/2020, 1145 CDT Registration: N210WP
Aircraft: ZENITH CH 750 Injuries: 1 None
Flight Conducted Under: Part 91: General Aviation - Personal

On September 20, 2020, about 1145 central daylight time, a William Prosch Zenith 750 airplane, N210WP, was substantially damaged when it was involved in an accident near Montrose, Missouri. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to the pilot, while en route to his destination airport, the engine momentarily lost power. He immediately selected the alternate fuel pump and engine control unit (ECU), and the engine regained power. About 5 minutes later, the engine lost total power, and the pilot attempted to restart the engine. The engine restart was unsuccessful, and the pilot initiated a forced landing to a field. During the forced landing, the airplane's landing gear contacted the high vegetation, and the nose impacted terrain. The airplane nosed over and came to rest inverted. The airplane's left wing leading edge was crushed, and the rudder was bent.

Postaccident examination of the airplane revealed the main fuse block, located behind and under the instrument panel, was discolored and exhibited internal thermal damage. An automotive blade-type fuse, that connected to both primary and secondary fuel pumps and primary and back up ECUs, displayed arching signatures and had failed.

According to the engine manufacturer, who responded to the accident site, the primary and secondary ECUs should have been wired directly to the main buss and should not have contained a fuse. After bypassing the failed electrical system, an engine test run was performed. The engine started and operated normally with no mechanical issues noted.

The engine manufacturer has a service bulletin that recommends an ECU wiring upgrade. The upgrade removes the ECU select switch in order to operate on a single computer only. The service bulletin had not been completed on the accident experimental airplane, nor was it required to be completed.

FMI: www.ntsb.gov

Advertisement

More News

Sierra Space Repositions Dream Chaser for First Mission

With Testing Soon Complete, Launch Preparations Begin in Earnest Sierra Space's Dream Chaser has been put through the wringer at NASA's Glenn Armstrong Test Facility in Ohio, but w>[...]

ANN's Daily Aero-Term (05.10.24): Takeoff Roll

Takeoff Roll The process whereby an aircraft is aligned with the runway centerline and the aircraft is moving with the intent to take off. For helicopters, this pertains to the act>[...]

Aero-News: Quote of the Day (05.10.24)

“We’re proud of the hard work that went into receiving this validation, and it will be a welcome relief to our customers in the European Union. We couldn’t be mor>[...]

Aero-News: Quote of the Day (05.11.24)

"Aircraft Spruce is pleased to announce the acquisition of the parts distribution operations of Wag-Aero. Wag-Aero was founded in the 1960’s by Dick and Bobbie Wagner in the >[...]

ANN's Daily Aero-Term (05.11.24): IDENT Feature

IDENT Feature The special feature in the Air Traffic Control Radar Beacon System (ATCRBS) equipment. It is used to immediately distinguish one displayed beacon target from other be>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2024 Web Development & Design by Pauli Systems, LC