NTSB Final Report: 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-05.13.24

Airborne-NextGen-05.07.24

Airborne-Unlimited-05.08.24 Airborne-FlightTraining-05.09.24

Airborne-Unlimited-05.10.24

Mon, Apr 29, 2024

NTSB Final Report: RANS S21

Owner’s (Pilot) Failure To Properly Torque A Fuel Filter B-Nut Fitting, Which Likely Introduced Air Into The Fuel System

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 (05.10.24): Takeoff Roll

Takeoff Roll The process whereby an aircraft is aligned with the runway centerline and the aircraft is moving with the intent to take off. For helicopters, this pertains to the act>[...]

Aero-News: Quote of the Day (05.10.24)

“We’re proud of the hard work that went into receiving this validation, and it will be a welcome relief to our customers in the European Union. We couldn’t be mor>[...]

Aero-News: Quote of the Day (05.11.24)

"Aircraft Spruce is pleased to announce the acquisition of the parts distribution operations of Wag-Aero. Wag-Aero was founded in the 1960’s by Dick and Bobbie Wagner in the >[...]

ANN's Daily Aero-Term (05.11.24): IDENT Feature

IDENT Feature The special feature in the Air Traffic Control Radar Beacon System (ATCRBS) equipment. It is used to immediately distinguish one displayed beacon target from other be>[...]

ANN's Daily Aero-Linx (05.11.24)

Aero Linx: Pararescue Air Force Pararescuemen, also known as PJs, are the only DoD elite combat forces specifically organized, trained, equipped, and postured to conduct full spect>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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