Sun, Nov 09, 2025
While On The Base Leg Of The Airport Traffic Pattern The Right Main Landing Gear Did Not Fully Extend
Location: Pompano Beach, Florida Accident Number: ERA25LA096
Date & Time: January 10, 2025, 11:15 Local Registration: N555HF
Aircraft: Piper PA-44-180 Aircraft Damage: Substantial
Defining Event: Sys/Comp malf/fail (non-power) Injuries: 2 None
Flight Conducted Under: Part 91: General aviation - Flight test

Analysis: Both pilots reported that after performing airwork they returned to the departure airport where multiple uneventful full stop landings were performed. They then departed and while on the base leg of the airport traffic pattern the right main landing gear did not fully extend. At that point the designated pilot examiner (DPE) took the controls from the pilot applicant, and during the course of 90 minutes, made multiple attempts to fully lower the right main landing gear that were ultimately unsuccessful. The DPE then elected to land with the landing gear retracted rather than with two landing gear down and one retracted. After touchdown the airplane came to rest near the runway centerline. The underside of the fuselage was substantially damaged during the landing.
After raising the airplane from the runway, the right main landing gear was manually pulled out of the wheel well and during that process it was discovered that the hardware that secured the upper and lower torque links were not in position and could not be located. Since the hardware could not be found, no determination could be made as to the reason for the separation of the hardware. A review of the airplane’s maintenance records revealed that the hardware securing the right main landing gear torque links was replaced last on about 11 months before the accident. At the time of the accident, the airplane had accrued about 324 flight hours since the hardware replacement. The mechanic who performed the last 100-Hour inspection, about 6 months and 46 hours before the accident, reported that he did not notice any abnormality or defects with the torque link bolts at that time.
Probable Cause and Findings: The National Transportation Safety Board determines the probable cause(s) of this accident to be -- The separation of the securing hardware for the right main landing gear upper and lower torque links for undetermined reasons, which prevented extension of the right main landing gear.
More News
Also: AFE25 Tickets!, Jamaica Recovery, E-Aircraft at Boeing Fld, Diamond DA50 RG Cert Elon Musk is once again promising the impossible…this time, in the form of a Tesla tha>[...]
Also: Louisville UPS Crash Aftermath, Taiwan Boosts Pilot Pool, Spartan Acquires, DON’T MISS the MOSAIC Town Hall! This three-day Affordable Flying Expo brings together indoo>[...]
“Our strategic partnership with AutoFlight, backed by their substantial technological expertise and tangible advancements in eVTOL airworthiness, represents a significant mil>[...]
Aero Linx: British Gliding Association (BGA) The British Gliding Association is the governing body for the sport of gliding in the UK and members are the 76 clubs that provide glid>[...]
While Descending Toward ASN, He Advanced The Throttle, But The Engine Did Not Respond On October 2, 2025, at 1126 central daylight time, a Cirrus SR22, N812SE, was substantially da>[...]