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FTW96LA082

1995-12-30 · DURANGO, Colorado, United States · None · 1 aircraft · Status: Completed

Airport DRO

Current FAA registration · N7356V

Make / Model
BELLANCA 17-30
Year of manufacture
1969 · 26 years old at event
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19690218
ADS-B equipped
Yes — Mode-S A9E0DC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

the failure of the nose wheel steering mechanism which rendered the aircraft uncontrollable on the ground. A factor was the rough and uneven terrain.

Factual narrative

On December 30, 1995, at 1315 mountain standard time, a Bellanca 17-30, N7356V, departed the side of the runway during landing at La Plata County Airport, Durango, Colorado. The CFI and student pilot were not injured and the aircraft sustained substantial damage. Visual meteorological conditions prevailed for this Title 14 CFR Part 91 local area instructional flight and no flight plan was filed. According to the flight instructor, the owner/student was performing touch-and-go landings and the landing which preceded the accident was smooth and on center line. The flight instructor said that when the nose wheel was lowered to the runway, the aircraft immediately veered to the right. He said he got on the rudder with the student and had full left rudder applied without effect. As the aircraft departed the side of the runway the landing gear collapsed in the rough terrain and the aircraft slid to a stop. There was no fire. Examination of the aircraft provided evidence of a fractured left nose wheel steering rod. Examination of the rod provided evidence that the rod fractured at the adjustment nut. According to the attached metallurgist's report, the fracture surface exhibited features typical of an overstress separation. During landing roll, when the nose wheel was lowered to the runway, the aircraft veered right and departed the side of the runway into rough terrain. During this excursion, the landing gear collapsed. Examination of the aircraft provided evidence of a failure of the left nose wheel steering rod. The fracture surface on the rod displayed evidence of overstress. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1995_FTW96LA082.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.