NTSB Final Report: Quicksilver Aeronautics LLC L-S2S | 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, May 19, 2025

NTSB Final Report: Quicksilver Aeronautics LLC L-S2S

Postaccident Inspection Of The Aircraft Revealed A Missing Cooling System Expansion Tank Cap And A Low Coolant Level

Location: Geyserville, California Accident Number: WPR25LA095
Date & Time: February 17, 2025, 12:20 Local Registration: N14QK
Aircraft: Quicksilver Aeronautics LLC L-S2S Aircraft Damage: Substantial
Defining Event: Loss of engine power (total) Injuries: 2 None
Flight Conducted Under: Part 91: General aviation - Personal

Analysis:: During cruise flight, the pilot reported that he noticed a temperature alarm, and a short time later, the engine sustained a complete loss of power. The pilot initiated a forced landing to a dirt road located in a vineyard. During the landing roll, the airplane veered to the right and struck a pole, which resulted in substantial damage to the right wing. A postaccident inspection of the aircraft revealed a missing cooling system expansion tank cap and a low coolant level. The piston faces also showed high heat signatures from red discoloration and scoring along the cylinder walls. The pilot reported that he removed the cooling system tank cap during the preflight inspection to check the water level and did not resecure it. During the flight, the engine likely lost cooling fluid and overheated, which resulted in a complete loss of engine power.

Probable Cause and Findings: The National Transportation Safety Board determines the probable cause(s) of this accident to be -- The pilot’s failure to secure the coolant cap during the preflight inspection, which resulted in a total loss of engine power due to overheating and a subsequent forced landing.

FMI: www.ntsb.gov

Advertisement

More News

ANN's Daily Aero-Term (11.16.25): NonApproach Control Tower

NonApproach Control Tower Authorizes aircraft to land or takeoff at the airport controlled by the tower or to transit the Class D airspace. The primary function of a nonapproach co>[...]

Aero-News: Quote of the Day (11.16.25)

“This shutdown inflicted real damage. Beyond disrupting operations and adding risk into the aviation system… it hindered essential career growth opportunities and stal>[...]

ANN's Daily Aero-Linx (11.16.25)

Aero Linx: The Mooney Mite Site Dedicated to the Mooney M-18 Mite, "The Most Personal Airplane," and to supporting Mite owners everywhere. The Mooney M-18 Mite is a single-place, l>[...]

NTSB Final Report: Vans Aircraft Inc RV-12

Pilot’s Improper Installation Of The Control Stick Pushrod Assemblies, Which Resulted In Separation Of The Left Pushrod And A Total Loss Of Roll Control Analysis: While retur>[...]

ANN FAQ: How Do I Become A News Spy?

We're Everywhere... Thanks To You! Even with the vast resources and incredibly far-reaching scope of the Aero-News Network, every now and then a story that should be reported on sl>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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