NTSB CAROL · Event
Event MIA95LA081
Registry · N47U
FAA Aircraft Registry record.
Make / Model
CESSNA R182
Year of manufacture
1980 · 15 years old at event
Engine
LYCOMING 0-540 SERIES (250 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19800314
ADS-B equipped
Yes — Mode-S A5C083
Registrant of record
ALECO 182 LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the failure of the pilot-in-command to insure the landing gear was extended before landing.
Factual narrative
On March 4, 1995, about 2016 eastern standard time, a Cessna R182, N47U, registered to Aleco Inc., landed gear up at Orlando International Airport, Orlando, Florida, while on a 14 CFR Part 91 business flight. Visual meteorological conditions prevailed at the time and an instrument flight rules flight plan was filed. The airplane sustained substantial damage and the pilot and two passengers were not injured. The flight originated from Birmingham, Alabama, on March 4, 1995, about 1700. The pilot stated he visually inspected the landing gear and verified he had a gear down light on final approach. As the aircraft touched down he felt a shimmy from the nose and the aircraft settled to the runway. Examination by FAA inspectors indicated that scrape marks and propeller damage from the aircraft extended for about 1,000 feet on the runway. The aircraft's belly had sustained substantial damage due to sliding on the runway. The aircraft's landing gear, landing gear doors, and landing gear tires had no scuff marks or damage. The FAA inspectors stated all the areas checked during their inspection indicated that the landing gear was in the full retracted position throughout the entire landing. The right front seat passenger stated she found the landing gear handle in the up position after landing. The rear seat passenger stated that during landing he heard a horn sounding and observed a red light on the instrument panel. After the accident the aircraft was raised. The landing gear handle was placed in the gear down position and the gear extended and locked. Further retraction testing of the landing gear system revealed no evidence to indicate precrash failure or malfunction of the landing gear system. The pilot stated he visually verified the landing gear was extended and observed a gear down light before landing. During landing the nose began to shimmy and the aircraft settled to the runway. The right front seat passenger stated the landing gear handle was in the up position after the aircraft came to rest. The rear seat passenger stated he heard a warning horn and observed a red light illuminated on the instrument panel during the landing. FAA inspectors stated the aircraft had damage which was consistent with the landing gear being retracted during the entire landing sequence. Damage on the runway caused by the aircraft extended 1,000 feet. After the aircraft was raised the landing gear extended normally and locked. Further testing of the landing gear indicated it operated normally after the accident. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_MIA95LA081.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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