NTSB Identification: ERA12CA128
14 CFR Part 91: General Aviation
Accident occurred Wednesday, December 28, 2011 in Picayune, MS
Probable Cause Approval Date: 11/26/2012
Aircraft: MITSUBISHI MU-2B-20, registration: N800BY
Injuries: 3 Uninjured.

NTSB investigators used data provided by various entities, including, but not limited to, the Federal Aviation Administration and/or the operator and did not travel in support of this investigation to prepare this aircraft accident report.

According to the pilot, the wind was calm at the time of the accident. The airplane entered the traffic pattern on a left base leg at 120 knots with the landing gear extended and flaps extended to 20 degrees. The pilot turned the airplane onto final approach, and when the runway was assured, extended the flaps to 40 degrees and confirmed the landing gear were down and locked. Upon landing, the airplane suddenly pitched nose down, and the pilot realized there was a discrepancy with the nose landing gear. He applied full thrust reverse, stopped, and secured the airplane on the runway. Postaccident examination of the airplane revealed that the nose landing gear was collapsed, the left main landing gear tire was separated from the wheel, and the wheel assembly was separated from the landing gear. Wrinkles in the fuselage skin near the forward pressure bulkhead were noted on both sides of the airplane. Additionally, the left and right upper and lower wing spars were distorted, and the fuel tanks at the wingtips were dislodged and loose from their mountings, consistent with substantial damage. The pilot reported no mechanical malfunctions or anomalies with the airplane, but the damage was consistent with a hard landing.

The National Transportation Safety Board determines the probable cause(s) of this accident to be:

The pilot's excessive rate of descent during the landing flare/touchdown, which resulted in a hard landing.

Full narrative available

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