NTSB CAROL · Event
Event CHI96LA127
Registry · N292RG
FAA Aircraft Registry record.
Make / Model
COMMANDER AIRCRAFT CO 114TC
Year of manufacture
1996 · 0 years old at event
Engine
LYCOMING IO-540 SER (300 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19960513
ADS-B equipped
Yes — Mode-S A2FE66
Registrant of record
WASHINGTON ROAD ASSOCIATES LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
fatigue fracture and subsequent failure of the gear door hinge bracket.
Factual narrative
On March 29, 1996, at 1733 central standard time, a Socata TBM-700, N292RG, operated by Chemrite Industries, Inc. sustained substantial damage while landing in Eau Claire, Wisconsin, with the right main landing gear in the retracted position. The commercial pilot and private pilot rated passenger reported no injuries. The 14 CFR Part 91, business flight originated in Rice Lake, Wisconsin at 1400 with a planned destination of Milwaukee, Wisconsin. Visual meteorological conditions prevailed. In his written statement, the pilot reported that an "unsafe gear door light" was displayed "shortly after departing." He recycled the landing gear. The right main landing gear did not extend. He performed several normal and emergency gear extension attempts with no success. He had several telephone patch conversations with the airplane manufacturer and flight safety. The right main landing gear could not be lowered. He orbited to burn down fuel, declared an emergency, and conducted a gear up landing. The airplane sustained substantial damage to the lower fuselage. Examination of the right main landing gear revealed the right inboard landing gear door, forward hinge bracket was fractured. The door was wedged in the wheel well. The fractured bracket was examined by a NTSB metallurgist. In his factual report, he stated "SEM inspections of the crack revealed fatigue progression features emanating from both surfaces of the mounting flange." The pilot reported that an 'unsafe gear door light' was displayed 'shortly after departing.' He recycled the landing gear. The right main landing gear did not extend. He performed several normal and emergency gear extension attempts with no success. He had several telephone patch conversations with the airplane manufacturer and flight safety. The right main landing gear could not be lowered. He orbited to burn down fuel, declared an emergency, and conducted a gear up landing. Examination of the right main landing gear revealed a fatigue fracture in the right inboard landing gear door forward hinge bracket. The door was wedged in the wheel well. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_CHI96LA127.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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