NTSB Final: RANS S21 | 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-06.02.25

Airborne-NextGen-06.03.25

AirborneUnlimited-06.04.25

Airborne-AffordableFlyers-06.05.25

AirborneUnlimited-06.06.25

Sun, May 12, 2024

NTSB Final: RANS S21

Postaccident Examination Of The Engine Revealed That The Fuel Filter B-Nut Fitting Was Not Properly Torqued

Location: Fairfield, Utah Accident Number: WPR22LA211
Date & Time: June 9, 2022, 10:45 Local Registration: N46JH
Aircraft: RANS S21 Aircraft Damage: Substantial
Defining Event: Fuel starvation Injuries: 1 Minor
Flight Conducted Under: Part 91: General aviation - Personal

Analysis: The pilot was conducting a test flight following recent maintenance when, shortly after departing, the engine began to lose power. He performed a forced landing on airport property, during which the airplane landed hard and sustained substantial damage.

Postaccident examination of the engine revealed that the fuel filter b-nut fitting was not properly torqued, which likely introduced air into the fuel system. Additionally, there was no restricted bypass line between the inlet (pressure side of the fuel pump module) and the return line and no vent line from the header tank, both of which would have allowed the venting of air from the fuel system. Based on this evidence, it is likely that the loose fuel filter b-nut allowed the air into the fuel system that could not be properly vented due to the lack of a restricted bypass line and vent line, which ultimately resulted in the loss of engine power.

Probable Cause and Findings: The National Transportation Safety Board determines the probable cause(s) of this accident to be -- The owner’s (pilot) failure to properly torque a fuel filter b-nut fitting, which likely introduced air into the fuel system and resulted in a loss of engine power. Contributing to the loss of power was a missing restricted bypass line and a header tank vent line, which would have allowed the venting of air from the fuel system.

FMI: www.ntsb.gov

Advertisement

More News

ANN's Daily Aero-Term (06.02.25): Minimum Friction Level

Minimum Friction Level The friction level specified in AC 150/5320-12, Measurement, Construction, and Maintenance of Skid Resistant Airport Pavement Surfaces, that represents the m>[...]

ANN's Daily Aero-Linx (06.02.25)

Aero Linx: Airpower Museum The APM owns 30 acres on Antique Airfield, including the south half of the N-S runway. It consists of three hangars, an annex, and a library. The museum >[...]

NTSB Prelim: Champion 7ECA

Patient Told The First Responders That The “Man Who Was In The Plane Was Flying At The Time Of The Accident And Had Overshot The Runway They Were Attempting To Land On.&rdquo>[...]

Classic Klyde Morris (From 06.10.22)

Klyde Just Can't Believe This Has Gotten To This Point... FMI: www.klydemorris.com>[...]

Airborne 05.30.25: Anti-Helicopter Bill, PW Strike Done, All-Electric Bristell

Also: Duffy Wants $$$, KS Airports, Morningside U’s Aviation School, New Airstrip In ID After 6 were killed in a helicopter crash over the Hudson River, several US Representa>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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