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-05.20.24

Airborne-NextGen-05.21.24

Airborne-Unlimited-05.15.24 Airborne-AffordableFlyers-05.16.24

Airborne-Unlimited-05.17.24

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

ANN's Daily Aero-Term (05.19.24): Back-Taxi

Back-Taxi A term used by air traffic controllers to taxi an aircraft on the runway opposite to the traffic flow. The aircraft may be instructed to back-taxi to the beginning of the>[...]

Aero-News: Quote of the Day (05.19.24)

“Our WAI members across the nation are grateful for the service and sacrifice of the formidable group of WASP who served so honorably during World War II. This group of brave>[...]

Aero-News: Quote of the Day (05.20.24)

“Many aspiring pilots fall short of their goal due to the cost of flight training, so EAA working with the Ray Foundation helps relieve some of the financial pressure and mak>[...]

ANN's Daily Aero-Term (05.20.24): Blind Speed

Blind Speed The rate of departure or closing of a target relative to the radar antenna at which cancellation of the primary radar target by moving target indicator (MTI) circuits i>[...]

ANN's Daily Aero-Linx (05.20.24)

Aero Linx: International Airline Medical Association (IAMA) The International Airline Medical Association, formerly known as the Airline Medical Directors Association (AMDA) was fo>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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