DEN05IA092
2005-06-26 · Grand Junction, Colorado, United States · None · 1 aircraft · Status: Completed
Airport GJT
Current FAA registration · N240GL
- Make / Model
- BEECH 1900D
- Year of manufacture
- 1996 · 9 years old at event
- Engine
- P&W PT6A SER (750 hp)
- Seats / Engines
- 19 seats · 2 engines
- Last airworthiness date
- 19960921
- ADS-B equipped
- Yes — Mode-S A230A0
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the flight crew's diverted attention while the number 2 engine was operating and failure to maintain aircraft control which resulted in an inadvertent taxi of the airplane into an airport security fence.
Factual narrative
On June 26, 2005, at 1010 mountain daylight time, a Beech 1900D, N240GL, owned and operated by Great Lakes Aviation, LTD., sustained minor damage when it struck an airport security fence while taxiing at the Walker Field Airport, Grand Junction, Colorado. The captain, first officer, and 17 passengers on board were not injured. Visual meteorological conditions prevailed, and an instrument flight rules flight plan was filed for the Title 14 Code of Federal Regulations Part 121 scheduled domestic passenger flight. The flight was originating at the time of the incident and was destined for Denver, Colorado. According to the captain, the number 2 engine (right) was operating and he had given the ground marshals clearance to remove the wheel chocks. The first officer closed the cabin door and had completed the passenger safety briefing. After the first officer had completed the briefing, the captain turned in his seat to demonstrate to the first officer how to secure a component of the cabin door from "rattling" in-flight. During the captain's demonstration, the first officer was standing in the forward cabin. While the flight crew's attention was diverted, the airplane taxied forward, rolled onto a curb, and struck an airport security fence. Examination of the aircraft by airport personnel revealed the right propeller blades were separated near the hub, the right engine cowling and the radome were punctured. The number 2 engine (right) was operating and the captain had given the ground marshals clearance to remove the wheel chocks. The first officer closed the cabin door and had completed the passenger safety briefing. After the first officer had completed the briefing, the captain turned in his seat to demonstrate to the first officer how to secure a component of the cabin door from "rattling" in-flight. During the captain's demonstration, the first officer was standing in the forward cabin. While the flight crew's attention was diverted, the airplane taxied forward, rolled onto a curb, and struck an airport security fence. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_DEN05IA092.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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