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DEN04LA016

2003-10-26 · Watkins, Colorado, United States · None · 1 aircraft · Status: Completed

Airport FTG

Current FAA registration · N9794G

Make / Model
CESSNA 180J
Year of manufacture
1972 · 31 years old at event
Engine
CONT MOTOR O-470 SERIES (230 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
19721117
ADS-B equipped
Yes — Mode-S ADA7FF

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's failure to maintain aircraft control resulting in the ground loop. Factors contributing to the accident were the crosswind and the gusts.

Factual narrative

On October 26, 2003, at approximately 1400 mountain standard time, a Cessna 180J, N9794G, was substantially damaged when it ground looped during landing roll on runway 26 (8,000 feet by 100 feet, dry asphalt) at the Front Range Airport, (FTG) Watkins, Colorado. The commercial pilot, the sole occupant on board the airplane, was not injured. The personal flight was being conducted under the provisions of Title 14 CFR Part 91 without a flight plan. Visual meteorological conditions prevailed at the time of the accident. The cross-country flight originated at Montrose, Colorado, at 1200, and was en route to FTG. In his written statement, the pilot said he entered the traffic pattern for runway 26. He said his approach was normal and that he had 10 to 15 degrees of right crab to keep the airplane aligned with the runway centerline. The pilot said he touched down "on the center line at normal speeds for a 3-point landing." The pilot said, "After flap retraction and brief braking, I lost directional control." The pilot said he was too slow to make a go-around. An examination of the airplane showed the left wing tip broken aft, and the outboard portion of the left wing and the left aileron bent aft and upward. The left main landing gear leg was bent aft. The forward fuselage showed bends and skin wrinkles. Flight control continuity was confirmed. An examination of the engine, engine controls, and other airplane systems showed no anomalies. At 1353, the reported wind conditions at FTG were 340 degrees at 16 knots, gusting to 20 knots. The pilot said he entered the traffic pattern for runway 26. He said his approach was normal and that he had 10 to 15 degrees of right crab to keep the airplane aligned with the runway centerline. The pilot said he touched down "on the center line at normal speeds for a 3-point landing." The pilot said, "After flap retraction and brief braking, I lost directional control." The pilot said the airspeed was inadequate to make a go-around. The airplane ground looped causing substantial damage to the left wing, left main landing gear, and forward fuselage. An examination of the airplane revealed no anomalies. The reported wind conditions approximately 7 minutes before the accident were 340 degrees at 16 knots, gusting to 20 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2003_DEN04LA016.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

Matched on aircraft type or causal vocabulary (go-around). All research papers