Casualties unknown

Engine Test Flight Ends in Crash During Night Icing Conditions (N5LN)

Rock, KS, US

On November 5, 1998, a Mitsubishi MU-2B-60 (registration N5LN) was involved in an aviation accident near Rock, KS. Investigators recorded the probable cause as: the pilot failed to maintain control of the aircraft and made an improper evaluation of the weather. Additional factors were flying a test flight at night with the icing conditions in the clouds. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

A test flight for an overhauled left engine's Negative Torque Sensing (NTS) check resulted in an accident. The aircraft deviated from assigned altitude and heading, descending into terrain. Both engines were operating at impact.

Overview

An aircraft with registration N5LN was conducting a test flight to perform an in-flight Negative Torque Sensing (NTS) check on its left engine, which had recently been overhauled. The check required shutting down the left engine during the flight. The test took place at night.

Weather and Briefing

The pilots were briefed that icing conditions existed, with moderate rime icing mixed below 15,000 feet in clouds and precipitation. Cloud bases were reported between 2,500 and 2,900 feet above ground level (agl).

Flight Sequence

After departure, the pilot reported to air traffic control (ATC) that the aircraft was clear of clouds and on top of the cloud layer at approximately 6,500 feet mean sea level (msl). ATC assigned N5LN a heading of 180 degrees at an assigned altitude of 8,000 feet. Without notifying ATC, N5LN subsequently turned to a southeast heading, descended from 7,700 feet to about 5,500 feet, and decelerated from approximately 182 knots to about 138 knots.

ATC then assigned N5LN a block altitude of 6,000 to 8,000 feet and a VFR-On-Top clearance. ATC instructed the flight to turn right to remain within the assigned airspace. N5LN turned right but continued to descend from about 5,500 feet to the last radar indication of 4,500 feet.

Impact and Wreckage Examination

The airplane impacted the ground in a steep attitude. Examination of the wreckage revealed that the landing gear was down, the right rudder trim was at full deflection, and the elevator trim was set to approximately six degrees nose-up. Examination of both engines indicated they were rotating and operating at the time of impact. Inspection of the airframe and propellers found no pre-existing anomalies that would have precluded normal operation.

Probable Cause

No probable cause was stated in the investigation source.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X11373. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.