1 fatality

2001-08-01: Mitsubishi MU-2 Marquise (N1VY) — Bankair — Hilton Head, United States of America

Hilton Head, United States of AmericaLanding (descent or approach)

On August 1, 2001, a Mitsubishi MU-2 Marquise (registration N1VY) operated by Bankair was involved in an aviation accident near Hilton Head, United States of America during landing or approach. One person was killed. Investigators recorded the probable cause as: Improper maintenance/installation and inadequate inspection of the airplane's flap torque tube joints during routine maintenance by company maintenance personnel, which resulted in the right flap torque tube assembly coupler becoming detached and the flaps… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 5 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781202528Data APIEditorial standards

An airplane on approach to Hilton Head Airport suddenly rolled right and descended, impacting trees and ground. Investigation revealed the right flap was extended to about 20 degrees while the left was at 40 degrees, due to a disconnected torque tube assembly with an improperly installed cotter pin during prior maintenance.

Accident Sequence

The airplane was on final approach to land at Hilton Head Airport when, according to witnesses, it suddenly rolled to the right and descended. It initially impacted trees at about the 70-foot level, then struck the ground. A fire ensued upon ground impact, and the debris field spanned approximately 370 feet along an azimuth of about 082 degrees.

Examination Findings

Examination of the wreckage revealed that the left wing flap actuator and jack nut measurements were consistent with the wing flaps being extended to 40 degrees. In contrast, the right wing flap jack nut and actuator measurements were consistent with the right flap being extended to about 20 degrees. Additionally, the right flap torque tube assembly between the flap motor and the flap stop assembly had disconnected. The female coupler of the flap torque tube assembly, which attaches to the male spline end of the flap motor and flap stop assembly, was found with a cotter pin installed through the female coupler of the flap stop assembly. However, the cotter pin had not been placed through the spline and the coupler consistent with normal installation as per Mitsubishi's maintenance manual or as specified in Airworthiness Directive 88-23-01. Instead, the cotter pin had missed the male spline on the flap motor. Furthermore, the flap coupler on the opposite side of the flap motor was also found without a cotter pin installed.

Maintenance Records

Company maintenance records showed that on April 3, 2001, about 87 flight hours before the accident, the airplane was inspected per Airworthiness Directive (AD) 88-23-01, which required the disassembly, inspection, and reassembly of the flap torque tube joints. On July 9, 2001, the airplane was given a phase 1 inspection, and Bankair records showed that a company authorized maintenance person performed the applicable maintenance items and certified the airplane for return to service.

Probable Cause

The official probable cause was improper maintenance/installation and inadequate inspection of the airplane's flap torque tube joints during routine maintenance by company maintenance personnel, which resulted in the right flap torque tube assembly coupler becoming detached and the flaps developing asymmetrical lift when extended, which resulted in an uncontrolled roll, a descent, and an impact with a tree during approach to land.