NTSB Prelim: Pool Cessna 172 | 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-06.23.25

Airborne-NextGen-06.24.25

AirborneUnlimited-06.25.25

Airborne-AffordableFlyers-06.26.25

AirborneUnlimited-06.27.25

Mon, May 15, 2023

NTSB Prelim: Pool Cessna 172

Pilot’s Family Notified Local Authorities That The Flight Was Overdue

Location: Victor, CO Accident Number: CEN23FA174
Date & Time: May 6, 2023, 10:00 Local Registration: N15188
Aircraft: Pool Cessna 172 Injuries: 4 Fatal
Flight Conducted Under: Part 91: General aviation - Personal

On May 6, 2023, about 1000 mountain daylight time, a Pool-Cessna airplane, N15188, was destroyed when it was involved in an accident near Victor, Colorado. The pilot and 3 passengers were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to the airport manager, the flight departed the Fremont County Airport (1V6), Canon City, Colorado, about 0920, with an intended destination of Centennial Airport (APA), Centennial, Colorado. Later in the day, the pilot’s family notified local authorities that the flight was overdue. The accident site was subsequently located in mountainous terrain early the following morning.

The accident site was located in mountainous terrain about 15 miles north of the departure airport. The airplane impacted trees and terrain on an approximate 300° heading. The right wing was separated near the root and was suspended in a tree about 35 ft southeast of the site. The main wreckage consisted of the fuselage, left wing, empennage, engine, and propeller. The airplane came to rest inverted and a postimpact fire ensued. A majority of the fuselage from the cockpit to the aft fuselage was consumed.

A preliminary airframe examination established flight control continuity from the rudder and elevator to the cockpit, and from the left aileron to the cockpit. An examination of the right aileron control is pending recovery from the tree. The engine was located under the forward fuselage/cockpit. Both propeller blades were located with the engine; one blade remained secured to the hub and the second blade was separated from the hub and located adjacent to the engine. A detailed postrecovery engine examination is planned.

FMI: www.ntsb.gov

Advertisement

More News

ANN's Daily Aero-Term (06.30.25): Ground Stop (GS)

Ground Stop (GS) The GS is a process that requires aircraft that meet a specific criteria to remain on the ground. The criteria may be airport specific, airspace specific, or equip>[...]

ANN's Daily Aero-Linx (06.30.25)

Aero Linx: Australian Transport Safety Bureau (ATSB) The Australian Transport Safety Bureau (ATSB) improves safety and public confidence in aviation, marine and rail transport thro>[...]

Aero-News: Quote of the Day (06.30.25)

“The Palo Alto stopover confirmed—yet again—that flight schools and aero-clubs are no longer just curious about electric training; they are ready to buy. In just >[...]

NTSB Final Report: ICON A5

Pilot’s Failure To Maintain Clearance From The Water While Flying At A Low Altitude Analysis: The flight of two airplanes was in cruise flight on a north heading about 50 ft >[...]

Airborne Affordable Flyers 06.26.25: PA18 Upgrades, ‘Delta Force’, Rhinebeck

Also: 48th Annual Air Race Classic, Hot Air Balloon Fire, FAA v Banning 100LL, Complete Remote Pilot The news Piper PA-18 Super Cub owners have been waiting for has finally arrived>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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