- Date
- January 29, 2020, 09:00 local (15:00 UTC)
- Place
- Chilton, WI
- Injuries
- 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Landing
- Aircraft
- N425GZMitsubishi MU 2B-40
- Defining event
- Landing: Loss of control on ground
- Weather
- Visual (VMC) · Day
- Status
- Completed
- Report
- Approved by Office Director
- Investigation class
- Class 3
- NTSB office
- Central Region
- Parties
- Honeywell Aerospace, Hartzell Propeller Inc, Flight Standards District Office, Mitsubishi Heavy Industries America, Inc.
- FAA report
- 20200129000939A
- Case key
- 101087
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
The pilot's decision to land on the turf runway with insufficient landing performance and his subsequent loss of control during the landing roll.
Findings · 5
NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.
Sequence of events
The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.
Analysis
The pilot was landing the turbine-powered airplane on a 2,500-ft-long frozen, turf runway. The pilot reported to the manufacturer that, during the landing roll, the airplane yawed left and the right wing contacted the ground, resulting in substantial damage. Examination of the airplane did not reveal any anomalies that would have resulted in a directional control issue. According to the pilot operating handbook, the airplane’s landing distance over a 50-ft for a dry, hard surface runway was about 2,500 ft. The manufacturer estimated that this distance for a wet or turf runway were about 4,250 ft. The pilot did not respond to requests for information regarding his flight planning or estimated landing distance. The pilot's decision to land on a runway that provided an inadequate distance likely resulted in an inability to maintain control of the airplane during the landing roll.
Factual narrative
The flight manual contained landing distance information for a dry, hard surface runway. Landing distance information for a turf runway was not available to the pilot. Investigators calculated airplane landing performance based on ambient temperature, calm wind, zero runway slope, an airplane weight of 500 lbs above empty weight, flaps at 20°, and no use of reverse thrust. Estimated landing distance over a 50 ft obstacle and ground roll were 2,500 and 1,500 ft, respectively. The airplane manufacturer estimated the landing distance over a 50 ft obstacle and ground roll for a turf (or wet) runway to be about 4,250 and 3,250 ft, respectively. The pilot did not respond to requests for additional information, such as expected landing distance, runway braking condition, touchdown location, actions taken after touchdown, and where the airplane departed the runway surface. According to the pilot, the turf runway was 2,500 ft x 85 ft; publicly available information indicated the turf runway was 1,000 x 60 ft. On January 29, 2020, about 0900 central standard time, a Mitsubishi MU-2B-40 airplane, N425GZ, was substantially damaged when it was involved in an accident at Flying Feathers Airport (11Y), Chilton, Wisconsin. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 personal flight. The National Transportation Safety Board (NTSB) was informed of the accident on March 12, 2020, by the airframe manufacturer; it was not reported to the NTSB by the pilot. The pilot stated that while landing at his private turf airstrip, the airplane yawed left and the right wing was substantially damaged when it contacted the ground. On December 14, 2019, the pilot completed an initial MU-2 training course, which included 14.9 flight hours and 20 hours of ground training as required 14 CFR Part 91 Subpart N. An examination of the airplane, which included engine rigging, propellers, and flight control continuity, did not reveal an anomaly that would have resulted in a directional control issue.
Aircraft
- Registration
- N425GZ
- Reported as
- Mitsubishi MU 2B-40
- Category
- Airplane
- Serial number
- 425 S.A.
- Built
- 1980
- Airframe hours
- 4,723
- Engines
- Honeywell TPE-33110511M, 940 horsepower, turbo propHoneywell TPE-33110511M, 940 horsepower, turbo prop
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Airworthiness certificate
- Standard, Normal
- Last inspection
- 100 hour · August 9, 2019 · 49 hours before
- Departed
- 8D1 · New Holstein, WI
- Destination
- 11Y · Chilton, WI
- Airport
- 11Y · Flying Feathers, runway 18, 2,500 × 85 ft, grass/turf
Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.
Flight crew
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 48
- Injuries
- None
- Certificate
- Airline transport
- Airplane ratings
- Single-engine land, Multi-engine land
- Instrument ratings
- Airplane
- Medical
- Class 1, With waivers/limitations
- Last flight review
- December 14, 2019
- Seat
- Left
- Restraint
- 4-point
- Flight hours
- 21,000 total · 93 in this make and model · 53 in the last 90 days · 27 in the last 30 days · 0 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- Calm
- Visibility
- 10 statute miles
- Lowest ceiling
- 2,800 ft overcast
- Temperature
- 25 °F, dew point 18 °F
- Altimeter
- 30.20 inHg
- Observed at
- KOSH, 16 nm away
Docket · 7
The files NTSB released with the investigation on November 19, 2020, on NTSB’s docket system: statements, records, photos and specialists’ reports. 6.2 MB in all.
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.