NTSB Prelim: Mooney M20E | 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-05.14.24

Airborne-Unlimited-05.15.24 Airborne-AffordableFlyers-05.16.24

Airborne-Unlimited-05.17.24

Mon, Jul 11, 2022

NTSB Prelim: Mooney M20E

Airplane Experienced A Partial Loss Of Engine Power

Location: Stillwater, OK Accident Number: CEN22LA255
Date & Time: June 18, 2022, 09:45 Local Registration: N5895Q
Aircraft: Mooney M20E Injuries: 2 None
Flight Conducted Under: Part 91: General aviation - Personal

On June 18, 2022, about 0945 central daylight time, a Mooney M20E airplane, N5895Q, sustained substantial damage when it was involved in an accident near  Stillwater, Oklahoma. The pilot and passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that about 20 to 25 minutes into the flight, while in cruise about 4,500 ft, the airplane experienced a partial loss of engine power. The power had been set to 2,400 RPM and 24” of manifold pressure and it decreased to 2,000 RPM and between 11 and 12” of manifold pressure. The pilot manipulated the throttle control, but the engine did not respond. He moved the fuel selector through all positions while moving the throttle, but there was still no response from the engine. Unable to maintain level flight, he set up for a forced landing to a highway. As he was about to land, he became distracted with avoiding a vehicle and did not extend the landing gear. After a soft touch down, he turned slightly left to keep the propeller from impacting the vehicle; the left wing impacted a barrier.

The airplane sustained substantial damage to the left wing. A post-accident examination by a Federal Aviation Administration air safety inspector did not reveal any anomalies with the engine control system and throttle control continuity was established from the cockpit controls to the engine. The inspector did find that the induction air filter was oil soaked and felt “tacky” to the touch. The source of the oil could not be determined due to the disposition of the wreckage.

A detailed examination is pending.

FMI: www.ntsb.gov

Advertisement

More News

ANN's Daily Aero-Term (05.17.24): Very High Frequency

Very High Frequency 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/ground voi>[...]

ANN's Daily Aero-Linx (05.17.24)

Aero Linx: Aviation Suppliers Association Established February 25, 1993, the Aviation Suppliers Association (ASA), based in Washington, D.C., is a not-for-profit association, repre>[...]

ANN FAQ: Submit a News Story!

Have A Story That NEEDS To Be Featured On Aero-News? Here’s How To Submit A Story To Our Team Some of the greatest new stories ANN has ever covered have been submitted by our>[...]

Classic Aero-TV: ANN Visits Wings Over The Rockies Exploration Of Flight

From 2021 (YouTube Version): Colorado Campus Offers aVariety Of Aerospace Entertainment And Education Wings over the Rockies Exploration of Flight is the second location for the Wi>[...]

Airborne Affordable Flyers 05.16.24: PRA Runway, Wag-Aero Sold, Young Eagles

Also: Paramotor Champ's, Electric Ultralight, ICON BK Update, Burt Rutan at Oshkosh! The Popular Rotorcraft Association is reaching out for help in rebuilding their private runway >[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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