NTSB Prelim: Fokker DR1 (Really!) | 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-06.17.24

Airborne-NextGen-06.18.24

Airborne-Unlimited-06.12.24 Airborne-FltTraining-06.13.24

Airborne-Unlimited-06.14.24

Sat, Oct 17, 2020

NTSB Prelim: Fokker DR1 (Really!)

About 1,500 Ft Mean Sea Level, The Engine Suddenly Lost All Power

Location: Wake, VA Accident Number: ERA21LA005
Date & Time: October 1, 2020, 11:25 Local Registration: N512FH
Aircraft: FOKKER DR1 Injuries: 1 None
Flight Conducted Under:

On October 1, 2020, at 1125 eastern daylight time, an experimental Fokker DR1 airplane, N512FH, was substantially damaged when it was involved in an accident near Wake, Virginia. 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, prior to the flight he “topped off” the fuel tank adding about 6 gallons of fuel. He departed the Hummel Field Airport (W75), Saluda, Virginia, for a local flight at 1100. About 25 minutes after takeoff while in cruise flight, about 1,500 ft mean sea level, the engine suddenly lost all power.

There were no precursor indications, it did not “surge, sputter or misfire.” The propeller remained windmilling. The pilot attempted to restart the engine but was unsuccessful. As the airplane slowed to about 60 knots, the propeller stopped windmilling. While descending for a forced landing to a field, the airplane struck a wire, and slowed “substantially.” During landing the airplane impacted the edge of a bean field and nosed over into the adjacent grass field. After the airplane came to rest, the pilot noticed fuel leaking from the fuel tank filler neck.
 
Examination of the accident site by a Federal Aviation Administration inspector revealed that the airplane sustained substantial damage to the upper wing, 3 ft inboard of the wingtip. The fuselage structure was deformed near the right landing gear strut attach point. Continuity of the flight controls was confirmed. The engine controls were exercised and operated normally. Fuel sampled from the fuel tank was blue and absent of contaminants. The fuel inlet line was disconnected from the carburetor, and no fuel ran out from the line. First responders reported to the inspector that “several gallons” of fuel had leaked from the fuel filler neck onto the ground. A fuel sample taken from the airport fueling station was blue in color and absent of contaminants.

The wreckage was retained for further examination.

FMI: www.ntsb.gov

Advertisement

More News

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>[...]

Aero-News: Quote of the Day (06.12.24)

“The legislation now includes a task force with industry representation ensuring that we have a seat at the table and our voice will be heard as conversations about the futur>[...]

ANN's Daily Aero-Linx (06.12.24)

Aero Linx: Waco Museum The WACO Historical Society, in addition to preserving aviation's past, is also dedicated and actively works to nurture aviation's future through its Learnin>[...]

ANN's Daily Aero-Term (06.12.24): Adcock Range

Adcock Range National low-frequency radio navigation system (c.1930-c.1950) replaced by an omnirange (VOR) system. It consisted of four segmented quadrants broadcasting Morse Code >[...]

Airborne Affordable Flyers 06.06.24: 200th ALTO, Rotax SB, Risen 916iSV

Also: uAvionix AV-Link, Does Simming Make Better Pilots?, World Games, AMA National Fun Fly Czech sportplane manufacturer Direct Fly has finished delivering its 200th ALTO NG, the >[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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