NTSB Prelim: Boeing A75 | 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-04.29.24

Airborne-NextGen-04.30.24

Airborne-Unlimited-05.01.24 Airborne-AffordableFlyers--05.02.24

Airborne-Unlimited-05.03.24

Thu, Oct 07, 2021

NTSB Prelim: Boeing A75

While Inverted, The Airplane Entered Another Flat Spin And Did Not Recover

Location: Delta, CO Accident Number: CEN21FA424
Date & Time: September 17, 2021, 08:00 Local Registration: N19BB
Aircraft: Boeing A75 Injuries: 1 Fatal
Flight Conducted Under: Part 91: General aviation - Personal

On September 17, 2021, about 0800 central daylight time (CDT), a Boeing A75 airplane, N19BB, was destroyed when it was involved in an accident near Delta, Colorado. The commercial pilot sustained fatal injuries. The personal local flight was conducted under the provisions of Title 14 Federal Code of Regulations Part 91.

The airplane took off from runway 3 at Blake Field Airport (AJZ), Delta, Colorado. Two witnesses observed the airplane climb out and begin aerobatic maneuvers about 5 miles to the northeast of AJZ. Both witnesses stated that the airplane began a loop maneuver, and at the top of the loop while inverted, the airplane entered a flat spin. They observed the airplane recover from that spin. The airplane then gained altitude and they observed the airplane begin another loop maneuver. At the top of the loop, while inverted, the airplane entered another flat spin and did not recover. The airplane impacted rugged sloped terrain about 5 miles to the northeast of AJZ. First responders located the airplane wreckage and notified authorities. There were no radio or distress calls heard from the pilot.

The wreckage was found resting inverted on a 45-degree slope. The fuselage was oriented downslope and crushed from impact forces. The engine was partially separated from its fuselage mounts. The empennage section was bent rearward, the upper wings were bent upward, and lower wings were separated from their respective mounting braces, consistent with a flat impact. Flight control continuity was confirmed from the cockpit to all flight control surfaces. The engine throttle control was found in the idle position. Engine rotation continuity (compression resistance) was confirmed. The smell of fuel was present. The airplane was not equipped with inverted fuel or oil supply systems.

According to an acquaintance of the pilot, he and the pilot flew the airplane to AJZ  a few days prior to the accident flight. The acquaintance stated that the airplane operated normally.

FMI: www.ntsb.gov

Advertisement

More News

ANN's Daily Aero-Linx (05.02.24)

Aero Linx: Model Aeronautical Association of Australia MAAA clubs are about fun flying, camaraderie and community. For over 75 years, the MAAA has been Australia’s largest fl>[...]

ANN's Daily Aero-Term (05.02.24): Touchdown Zone Lighting

Touchdown Zone Lighting Two rows of transverse light bars located symmetrically about the runway centerline normally at 100 foot intervals. The basic system extends 3,000 feet alon>[...]

Aero-News: Quote of the Day (05.02.24)

“Discovery and innovation are central to our mission at Virgin Galactic. We’re excited to build on our successful record of facilitating scientific experiments in subor>[...]

ANN FAQ: Contributing To Aero-TV

How To Get A Story On Aero-TV News/Feature Programming How do I submit a story idea or lead to Aero-TV? If you would like to submit a story idea or lead, please contact Jim Campbel>[...]

NTSB Final Report: Cirrus Design Corp SR20

Student Pilot Reported That During Rotation, “All Of A Sudden The Back Of The Plane Kicked To The Right..." Analysis: The student pilot reported that during rotation, “>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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