Sunday, June 4, 2017

Cessna 172R Skyhawk, N118ET, L & W Leasing LLC: Accident occurred March 20, 2016 at John C. Tune Airport (KJWN), Nashville, Davidson County, Tennessee

Aviation Accident Final Report - National Transportation Safety Board: https://app.ntsb.gov/pdf

Investigation Docket - National Transportation Safety Board: https://dms.ntsb.gov/pubdms

Aviation Accident Data Summary - National Transportation Safety Board: https://app.ntsb.gov/pdf


Additional Participating Entity:

Federal Aviation Administration / Flight Standards District Office; Nashville, Tennessee

L & W Leasing LLC: http://registry.faa.gov/N118ET 

NTSB Identification: GAA16CA157
14 CFR Part 91: General Aviation
Accident occurred Sunday, March 20, 2016 in Nashville, TN
Probable Cause Approval Date: 05/03/2016
Aircraft: CESSNA 172, registration: N118ET
Injuries: 4 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.

The pilot reported that during landing in crosswind conditions, the airplane began to drift to the right over the runway lights in the landing flare. The pilot further reported that he determined "it was not safe to land" and applied full power to go-around and subsequently retracted the flaps from 30 degrees to zero degrees. During the go-around, he reported that the airplane was unable to gain airspeed or altitude and touched down in the grass next to the runway and aborted the go-around. Subsequently, the pilot taxied back onto the runway and proceeded to the ramp.

A postaccident examination revealed substantial damage to elevator and rudder. The pilot reported that "he did not realize the angle of attack was severe enough" to cause a tail strike during the go-around.

The Cessna 172R (180 HP) Pilot's Operating Handbook in part states: "In a balked landing (go-around) climb, reduce the flap setting to 20 degrees immediately after full power is applied. If obstacles must be cleared during the go-around climb, reduce the wing flap setting to 10 degrees and maintain a safe airspeed until the obstacles are cleared." 

The pilot reported that there were no mechanical malfunctions or failures with the airplane that would have precluded normal operation.

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

The pilot's excessive pitch up and incorrect action of selecting flaps to zero degrees, which resulted in a tail strike during a go-around in crosswind conditions.

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