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LAX06CA027

2005-11-04 · Tucson, Arizona, United States · None · 1 aircraft · Status: Completed

Airport RYN

Current FAA registration · N515AB

Make / Model
LEE ROGER MARK III CLASSIC
Year of manufacture
2001 · 4 years old at event
Engine
ROTAX 912ULS SERIES (100 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20051028
ADS-B equipped
Yes — Mode-S A67404

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

the fatigue failure of the attachment that secured the horizontal stabilizer to the fuselage.

Factual narrative

On November 4, 2005, about 0830 mountain standard time, an experimental Lee Kolb Mark III Classic, N515AB, suffered an in-flight right horizontal stabilizer attachment failure at Ryan Airfield Airport (RYN), Tucson, Arizona. The pilot operated the borrowed airplane under the provisions of 14 CFR Part 91. The airline transport certified flight instructor (CFI) pilot, and the student pilot undergoing instruction (PUI) were not injured; the airplane sustained substantial damage. The instructional flight departed RYN about 0830. Visual meteorological conditions prevailed, and no flight plan had been filed. In a written statement to the National Transportation Safety Board, the pilot stated that the accident occurred on the downwind to landing phase of the traffic pattern. The instructional flight departed with the intention of practicing takeoffs and landings. On the right downwind leg they heard a "loud bang." The airplane lurched nose up, then nose down. The flight instructor took control of the aircraft and informed the tower he had a "serious" control problem. The pilot was able to land the aircraft using cross control inputs. After landing, the CFI was able to taxi safely to parking. Upon inspection of the airplane by the CFI, it was determined that the right horizontal stabilizer had separated from the fuselage due to a stainless steel "L" bracket failure. In the CFI's Description of Damage to Aircraft and Other Property section of his written report, he indicated that a bolt in the "L" bracket was found slightly loose, "which allowed a slight vibration and this caused metal fatigue over its 545 [hours] of flight [time]."

ADDITIONAL INFORMATION

As a result of the accident, the pilot recommended to other Kolb owners (via the Kolb Kolb owner website) to replace the "L" brackets at the 250-hour inspection and to install a second set of stabilizer cables on the horizontal stabilizer. The airplane made a forced landing after the horizontal stabilizer attachment failed in flight. The instructional flight departed with the intention of practicing takeoffs and landings. On the downwind leg, the pilots heard a loud bang. The airplane lurched nose up, then nose down. The flight instructor took control of the aircraft and informed the tower he had a flight control problem. He was able to land the aircraft using cross control inputs. The instructor inspected the airplane and determined that the right horizontal stabilizer had separated from the fuselage due to a stainless steel "L" bracket failure. The instructor attributed the failure to a loose bolt in the "L" bracket that allowed a vibration and caused metal fatigue of the component. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2005_LAX06CA027.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

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