NTSB CAROL · Event
Event MIA99LA127
Registry · N959DF
FAA Aircraft Registry record.
Make / Model
CONSOLIDATED AERONAUTICS INC. LAKE LA-4-200
Year of manufacture
1980 · 19 years old at event
Engine
LYCOMING I0360 SER A&C (200 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19800813
ADS-B equipped
Yes — Mode-S AD5667
Registrant of record
AEROLOGIC LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's inability to maintain directional control due to failure of the main landing gear, and partial electrical system failure for undetermined reasons.
Factual narrative
On April 14, 1999, about 1129 central daylight time, a Lake LA-4-200, N959DF, registered to an individual, ran off the runway while landing at Pensacola Regional Airport, Pensacola, Florida, while on a Title 14 CFR Part 91 instructional flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft received substantial damage and the airline transport-rated pilot and commercial-rated dual student were not injured. The flight originated from Pensacola, Florida, the same day, about 0945. The instructor stated that while practicing water landings they noticed the electrical power was at 10 volts and the electrical system was discharging. They terminated the flight training and contacted Air Traffic Control for a return to Pensacola Regional Airport. They were cleared for a straight in approach to runway 8. The hydraulic pressure was showing 700-800 pounds and they lowered the landing gear. The main landing gear appeared to lock down; however, the nose landing gear did not lock. The instructor took control of the aircraft and informed the ATC controller that he would bounce the aircraft in an attempt to lock the nose landing gear. Upon touchdown the nose gear did lock, but the aircraft began to drift to the left. Attempts to correct the left drift were unsuccessful and the aircraft ran off the runway to the left, hit a runway sign, and stopped after a 160/170-degree turn to the left. He believes the left drift was caused by the left main landing gear collapsing during landing roll out. Postcrash examination of the aircraft and runway was conducted by an FAA inspector. A visual inspection of the runway did not reveal any signs of aircraft parts or heavy tire marks. Examination of the aircraft showed the left main landing gear had come through the top of the left wing. The nose of the aircraft was damaged due to hitting a runway sign. (See FAA Inspector Statement) While on an instructional flight, the flightcrew noticed the electrical power was at 10 volts and discharging. They returned to the departure airport for landing. When the landing gear was lowered they noticed an unsafe indication for the nose landing gear. They bounced the aircraft during landing and the nose gear then locked down. During rollout, the aircraft veered to the left and they could not control it. The aircraft went off the runway, collided with a sign, and spun around about 160-170 degrees. Post crash examination showed no heavy tire marks or aircraft parts on the touchdown area of the runway. The left main landing gear had collapsed and had penetrated the wing. The reason for the electrical system failure was not determined. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1999_MIA99LA127.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (icing). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Contractor Report (CR)
Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
- NASA NTRS 2025 · Presentation
NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
- arXiv 2024 · arXiv preprint
An energy-stable phase-field model for droplet icing simulations
A phase-field model for three-phase flows is established by combining the Navier-Stokes (NS) and the energy equations, with the Allen-Cahn (AC) and Cahn-Hilliard (CH) equations and is demonstrated ana…
- NASA NTRS 2024 · Presentation
NASA Icing Update – Oct 2024
This presentation provides a status update on select NASA icing research activities for the SAE AC-9C Icing Technical Committee Meeting on Oct 21, 2024.
Browse the full corpus — academia portal ↗