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-11.17.25

AirborneNextGen-
11.11.25

Airborne-Unlimited-11.12.25

Airborne-FltTraining-11.13.25

AirborneUnlimited-11.14.25

LIVE MOSAIC Town Hall (Archived): www.airborne-live.net

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

Aero-News: Quote of the Day (11.18.25)

“Setting eight speed records this quickly following its August entry into service is a powerful testament to the tremendous capabilities of this aircraft. We are already seei>[...]

ANN's Daily Aero-Term (11.18.25): On-Course Indication

On-Course Indication An indication on an instrument, which provides the pilot a visual means of determining that the aircraft is located on the centerline of a given navigational t>[...]

ANN's Daily Aero-Linx (11.18.25)

Aero Linx: WW1 Aeroplanes, Inc. WORLD WAR 1 AEROPLANES was founded by Leo Opdycke in 1961 and incorporated as a federally recognized 501 (c) (3) not-for-profit corporation in 1979,>[...]

NTSB Final Report: Shoemaker Ronald R Pazmany PL-2

Pilot Reported That He Purchased The Airplane Earlier That Day Analysis: The pilot reported that he purchased the airplane earlier that day and completed a condition inspection tha>[...]

Airborne-NextGen 11.18.25: Dream Chaser Preps, Joby eTurbine, UAE Flt Test

Also: Abu Dhabi’s 1st Vertiport Network, Anduril-EDGE Partner, Vertical Permit/eVTOL Regs Sierra Space’s Dream Chaser spaceplane has cleared another round of pre-flight>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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