NTSB Final Report: Pitts Model 12 | 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-11.10.25

AirborneNextGen-
11.11.25

Airborne-Unlimited-11.12.25

Airborne-Unlimited-11.06.25

AirborneUnlimited-11.07.25

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

Wed, Apr 03, 2024

NTSB Final Report: Pitts Model 12

Pilot Elected To Return To The Airport, And About 1 Minute Later The Engine Sustained A Series Of Power Loss Fluctuations

Location: Conroe, Texas Accident Number: CEN23LA081
Date & Time: January 14, 2023, 14:25 Local Registration: N512P
Aircraft: Pitts Model 12 Aircraft Damage: Substantial
Defining Event: Sys/Comp malf/fail (non-power) Injuries: 1 Serious, 1 Minor
Flight Conducted Under: Part 91: General aviation - Personal

Analysis: The pilot and passenger were conducting a local flight to practice maneuvers and landings. About 3 to 4 minutes after takeoff, and 2,000 ft above ground level, the pilot noticed a master warning light on instrument panel but did not notice any anomalies or problems. The pilot elected to return to the airport, and about 1 minute later the engine sustained a series of power loss fluctuations. The pilot attempted to troubleshoot the problem but was unsuccessful and the engine lost total power. Unable to reach the airport or a field due to a high descent rate, the pilot performed a forced landing to a nearby roadway. During the landing, the airplane impacted a powerline and terrain before coming to rest inverted. The airplane sustained substantial damage to the wings, fuselage, and empennage.

Postaccident examination of the airplane revealed non-ferrous metallic debris throughout the entire fuel system; the source of the debris was unable to be determined. Due to a leak noted during a functional test, the engine-driven fuel pump was disassembled. Scratches and scoring marks were noted on the pressure relief valve seat, which allowed fuel into the air side cavity of the fuel pump. It is likely the fuel pump air cavity filled with fuel, which equalized the pump pressure and restricted fuel flow to the engine. The restricted fuel flow resulted in a total loss of engine power.

Probable Cause and Findings: The National Transportation Safety Board determines the probable cause(s) of this accident to be -- The failure of the engine-driven fuel pump, which resulted in a total loss of engine power. Contributing to the failure of the fuel pump was an unknown non-ferrous metallic debris that was noted throughout the airplane’s fuel system.

FMI: www.ntsb.gov

Advertisement

More News

NTSB Final Report: Piper PA-44-180

While On The Base Leg Of The Airport Traffic Pattern The Right Main Landing Gear Did Not Fully Extend Analysis: Both pilots reported that after performing airwork they returned to >[...]

Classic Aero-TV: The Bizarre Universe of Klyde Morris Cartoons

From 2023 (YouTube Edition): Putting the ANT in Antihero A Beech Starship speeds along at altitude. “Deflectors on!” a voice from within the aircraft cries. “Look>[...]

ANN's Daily Aero-Term (11.09.25): 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>[...]

Aero-News: Quote of the Day (11.09.25)

“Beginning this aircraft subsystem testing is the culmination of more than a decade of focused engineering and certification refinements. This is the moment where our intende>[...]

Classic Aero-TV: Falling for Para-Phernalia’s Softie Emergency Parachutes

From 2023 (YouTube Edition): The Best Option for A Pilots’ Worst Days Since its 1979 founding, Para-Phernalia, Inc. has designed and manufactured the Softie line of pilot eme>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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