1 fatality

1990-06-26: Piper PA-46 (Malibu/Meridian/Mirage/Matrix/M-Class) (N315RC) — D & M express — Lakeville, United States of America

Lakeville, United States of AmericaFlight

On June 26, 1990, a Piper PA-46 (Malibu/Meridian/Mirage/Matrix/M-Class) (registration N315RC) operated by D & M express was involved in an aviation accident near Lakeville, United States of America in flight. One person was killed. Investigators recorded the probable cause as: The pilot's failure to use the airplane's ice protection equipment, which resulted in a performance loss due to induction icing, propeller icing, or both, while flying in convective instrument meteorological conditions (IMC) at and above the freezing level. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781212807Data APIEditorial standards

During IFR departure, the aircraft entered a steep descent after stalling due to induction or propeller icing. The pilot failed to use ice protection equipment, and pitot tube icing caused erroneous airspeed indications.

Introduction

The accident occurred during an IFR departure when the pilot received progressive altitude clearances to climb to 15,000 feet. The aircraft, with the pilot as the sole occupant, experienced a loss of control leading to an inflight breakup. The pilot was killed.

Flight History

At 1607 EDT, the pilot was vectored for 'a good rate of climb' through 14,000 feet with clearance to proceed on course after leveling at 14,000 feet for 15,000 feet. Radar data indicated a steady climb until the aircraft was above 13,000 feet. As it climbed from 13,300 feet to 13,900 feet (the maximum recorded altitude), its speed slowed from about 115 knots to below 80 knots. At 1613 EDT, the pilot was cleared to proceed direct and change frequency.

Radar Data

Radar data showed that after reaching 13,900 feet, the aircraft deviated from course and entered a steep descent. Radar contact was lost and an inflight breakup occurred.

Wreckage

Pieces of wings and stabilizers were found up to 1.5 miles from the fuselage. A trajectory study disclosed the breakup occurred between 6,000 feet and 9,000 feet MSL. Examination of fractures on major components revealed characteristics typical of overstress; no preexisting cracks were found. No autopilot failure or bird strike was found.

Weather

Clouds were layered to 20,000 feet; the freezing level was about 12,500 feet. There was evidence the aircraft was in or near convective precipitation above the freezing level for about 1.5 minutes before the rapid descent.

Examination

The Pitot heat switch was found 'off' and the induction air door in its primary position.

Probable Cause

The official probable cause was the pilot's failure to use the airplane's ice protection equipment, which resulted in a performance loss due to induction icing, propeller icing, or both, while flying in convective instrument meteorological conditions (IMC) at and above the freezing level. The performance loss led to a stall, the recovery from which probably was exacerbated by the pilot's improper response to erroneous airspeed indications that resulted from blockage of the pitot tube by atmospheric icing.