Event ERA17LA130

Factual narrative

On February 25, 2017, about 1115 eastern standard time, a Socata TB20, N2519T, was substantially damaged during a gear up landing at Melbourne International Airport (MLB), Melbourne, Florida. The private pilot was not injured. The personal flight was conducted under the provisions of Title 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed and no flight plan was filed for the flight, which departed Key West International Airport (EYW), Key West, Florida, about 1012.The pilot reported that during his cross-country flight he noticed the alternator warning light flash and the battery began to discharge. He contacted air traffic control, but did not declare an emergency, and began a slow descent while initiating the emergency gear extension. After multiple unsuccessful attempts the pilot performed a gear up landing. An examination of the airplane by a Federal Aviation Administration Inspector revealed that the main landed gear was extended but not fully locked. The nose landing gear did not extend and remained in the wheel well. Examination of the airframe revealed that the bottom forward bulkhead was damaged during landing sequence. An examination of the nose gear assembly revealed the circlip on the nose landing gear strut was dislodged from the nose landing gear leg assembly, which allowed the strut to extend further than usual. The circlip used to retain the nose gear strut inside the nose gear assembly had paint on the outer portion of the circlip, which should have been fully set inside the groove used to keep the circlip in place. An examination of the circlip groove revealed that it was in serviceable condition with no corrosion or other deformation within the groove. A review of the maintenance records showed that the nose strut was disassembled and repaired on July 15, 2015, and the airplane was completely repainted on April 5, 2016. Further review of the maintenance records revealed that since the disassembly of the nose gear, a total of 75 hours of flight time had accumulated since the maintenance. According to the airplane's maintenance manual the, nose landing gear strut retaining circlip should have been fully installed in the groove. After it is installed, the landing gear should be rotated several times to confirm proper installation. During a personal flight, the airplane's alternator warning light flashed and the battery began to discharge, so the pilot conducted a precautionary landing. The nose landing gear did not fully deploy, and the pilot performed a gear-up landing. Examination of the landing gear system revealed the nose landing gear was jammed within the wheel well because the nose strut had overextended. Further, the circlip that held the strut inside the gear assembly was dislodged from the groove. Paint was identified on the outer portion of the circlip. Review of the maintenance records revealed that the nose landing gear was disassembled and repaired more than 2 years and 75 flight hours before the accident flight. The airplane was fully painted after that maintenance. According to the airplane maintenance manual, the circlip should have been fully installed in the groove, and the landing gear should be rotated several times to confirm proper installation. If the circlip had been properly installed inside the nose strut housing groove at the time paint was applied, paint would not have been on the outer surface of the circlip. It is likely that the circlip was improperly installed when the nose landing gear was repaired; it eventually became dislodged sufficiently to cause the internal strut to overextend and the gear to become jammed within the wheel well. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).

• C Personnel issues-Task performance-Maintenance-Repair-Maintenance personnel - C
• C Aircraft-Aircraft systems-Landing gear system-Nose/tail gear strut/axle-Incorrect service/maintenance - C