2 fatalities

2015-07-29: Socata TBM-700 (N425KJ) — Trustey Management Corporation — Milwaukee-Lawrence J. Timmerman, United States of America

Milwaukee-Lawrence J. Timmerman, United States of AmericaLanding (descent or approach)

On July 29, 2015, a Socata TBM-700 (registration N425KJ) operated by Trustey Management Corporation was involved in an aviation accident near Milwaukee-Lawrence J. Timmerman, United States of America during landing or approach. 2 people were killed. Investigators recorded the probable cause as: The pilot's improper pitch control during the landing, which resulted in the propeller striking the runway, and his failure to maintain adequate airspeed during the subsequent go-around, which resulted in the airplane exceeding its critical angle of attack… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 9 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781192918Data APIEditorial standards

An airline transport pilot performed a go-around after a landing with a propeller strike. During the subsequent climb, the airplane stalled and descended into terrain. Investigation attributed the accident to improper pitch control and failure to maintain airspeed.

Sequence of Events

The airline transport pilot was landing at the destination airport after a cross-country flight in visual meteorological conditions. The tower controller observed that the airplane's landing gear appeared to be extended during final approach and that the airplane landed within the runway's touchdown zone. The controller reported that, although the airplane made a normal landing, he heard a squealing noise that continued longer than expected. The pilot subsequently transmitted "go-around," which the controller acknowledged and cleared the pilot to enter a left traffic pattern.

The controller then heard the engine speed accelerate while the airplane maintained a level attitude over the runway until it passed midfield. He then saw the airplane pitch up and enter a climbing left turn. The controller stated that the airplane appeared to enter an aerodynamic stall before it descended into terrain in a left-wing-down attitude. Another witness reported seeing the airplane, with its landing gear extended, in a steep left turn before it descended rapidly into terrain.

Examination Findings

A postaccident examination did not reveal any evidence of flight control, landing gear, or engine malfunction. Examination of the runway revealed numerous propeller slash marks that began about 215 feet past the runway's touchdown zone; however, there was no evidence that any portion of the airframe had impacted the runway during the landing. Additionally, measurement of the landing gear actuators confirmed that all three landing gear were fully extended at the accident site.

Based on the evidence, the pilot likely did not adequately control the airplane's pitch during the landing, which allowed the propeller to contact the runway. Due to the propeller strikes, the propeller was likely damaged and unable to provide adequate thrust during the go-around. Further, based on witness accounts, the pilot likely did not maintain adequate airspeed during the climbing left turn, which resulted in the airplane exceeding its critical angle of attack and experiencing an aerodynamic stall at a low altitude.

Probable Cause

The official probable cause is: The pilot's improper pitch control during the landing, which resulted in the propeller striking the runway, and his failure to maintain adequate airspeed during the subsequent go-around, which resulted in the airplane exceeding its critical angle of attack and experiencing an aerodynamic stall at a low altitude.