No fatalities

2005-08-28: Cessna 441 Conquest (N77SA) — Security Aviation — Anchorage-Ted Stevens Intl, United States of America

Anchorage-Ted Stevens Intl, United States of AmericaLanding (descent or approach)

On August 28, 2005, a Cessna 441 Conquest (registration N77SA) operated by Security Aviation was involved in an aviation accident near Anchorage-Ted Stevens Intl, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The pilot's failure to lower the airplane's landing gear during landing, which resulted in an inadvertent wheels up landing. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 3 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781199372Data APIEditorial standards

A retractable-gear turboprop landed with gear down but retracted after touchdown, causing a wheels-up landing, runway excursion, and fire. Investigation found no preaccident mechanical malfunction.

Introduction

An airline transport pilot was landing a turboprop airplane equipped with retractable landing gear on a 10,900-foot-long, 150-foot-wide paved runway. The landing occurred under clear conditions, but a sequence of events after touchdown led to a significant accident.

Accident Sequence

According to the pilot, during the approach to land, he selected 10 degrees of wing flaps and then moved the landing gear selector switch to the down position. This was followed by the illumination of three green lights, indicating that the landing gear was down, locked, and safe for landing. However, after touchdown during the initial landing roll, the landing gear retracted, causing the airplane to slide on the underside of the fuselage. The aircraft then veered to the right of the runway centerline, and the right wing struck numerous runway edge lights. A post-crash fire ensued when the right wing's fuel tank was breached.

Damage and Marks

The airplane sustained structural damage to the underside of the fuselage, and the right wing was destroyed. Propeller strike marks originated near the touchdown point and extended approximately 2,200 feet to the airplane's final resting position. The fire consumed the right wing and further damaged the aircraft.

Investigation

A postaccident inspection was conducted by the Investigator-in-Charge (IIC) and another NTSB air safety investigator. The inspection revealed no evidence of any preaccident mechanical malfunction of the landing gear assembly or its associated operating systems. The airplane was placed on jack stands, and hydraulic pressure was supplied to the system using a ground power unit. The landing gear retraction system was cycled numerous times, and no mechanical anomalies were noted.

Probable Cause

The National Transportation Safety Board determined the probable cause of this accident to be the pilot's failure to lower the airplane's landing gear during landing, which resulted in an inadvertent wheels-up landing. Despite the pilot's indication of having received landing gear down indications, no mechanical issues were found to explain the gear retraction.