Incident Overview

Date: Friday 22 January 1999
Aircraft Type: Beechcraft 1900D
Owner/operator: Colgan Air
Registration Number: N215CJ
Location: Hyannis-Barnstable Airport, MA (HYA) – ÿ United States of America
Phase of Flight: Landing
Status: Substantial, repaired
Casualties: Fatalities: 0 / Occupants: 4
Component Affected: Aircraft Control Systems (particularly the yoke and power levers).Aircraft Control Systems (particularly the yoke and power levers).
Investigating Agency: NTSBNTSB
Category: Accident
A Beech 1900D, N215CJ operated by Colgan Air experienced substantial damage during landing at Hyannis-Barnstable Airport (HYA) due to challenging nighttime conditions. The aircraft executed two missed approaches, culminating in a sinking and subsequent ground impact during the third approach. The captain initiated a ‘FI’ gate maneuver, positioning the aircraft with propellers aligned with the runway centerline, and subsequently lost control, resulting in a significant ground impact.A Beech 1900D, N215CJ operated by Colgan Air experienced substantial damage during landing at Hyannis-Barnstable Airport (HYA) due to challenging nighttime conditions. The aircraft executed two missed approaches, culminating in a sinking and subsequent ground impact during the third approach. The captain initiated a ‘FI’ gate maneuver, positioning the aircraft with propellers aligned with the runway centerline, and subsequently lost control, resulting in a significant ground impact.

Description

A Beech 1900D, N215CJ, operated by Colgan Air as flight 1070, was substantially damaged while landing at the Hyannis-Barnstable Airport (HYA), Massachusetts. Night instrument meteorological conditions prevailed for the positioning flight which had departed Boston, Massachusetts, at 16:00. At dusk, with a 100-foot ceiling in fog, the captain of the Beech 1900D had performed two missed approaches to the airport. On the third approach, both the captain and first officer visually acquired the runway. The first officer said the captain lined the airplane up with the runway centerline and requested landing flaps. The first officer further stated, ‘…the aircraft floated at appr. 20’ [feet] over the runway at a normal transition when I heard the captain taking the power levers over the ‘FI [flight idle] gate’ by the sound of the engine/props.’ This placed the propellers in the ‘BETA’ range. The airplane then started to sink, and the captain pulled back on the control yoke. The main landing gear struck the ground and were fractured during the +2.9G touchdown, which occurred about 2,500 feet beyond the approach end of the 5,252 foot long runway. The airplane departed the right side of the runway, about 4,700 feet beyond the approach end, and stopped. To place the throttles in BETA, it was necessary to lift the power levers over the flight idle stop. The captain’s improper placement of the power levers in the BETA position, while the airplane was inflight. Factors were the fog and dusk conditions.

Primary Cause

Poor coordination and improper use of control levers during the third approach, exacerbated by challenging nighttime conditions and a sudden loss of control.Poor coordination and improper use of control levers during the third approach, exacerbated by challenging nighttime conditions and a sudden loss of control.

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