NTSB CAROL · Event
Event MIA05LA013
Aircraft involved
Probable cause & findings
The pilot-in-command's failure to maintain airspeed while on base to final leg, which resulted in an inadvertent stall/mush and subsequent impact with the runway.
Factual narrative
On October 25, 2004, about 1615 Atlantic standard time, a Piper PA-23-250, N62711, registered to Florida Flying Leasing & Services Inc. and operated by Premier Airways Inc, as a Title 14 CFR Part 91 personal flight, impacted into the runway on approach to the Fernando Luis Ribas Dominicci Airport, San Juan, Puerto Rico. Visual meteorological conditions prevailed and no flight plan was filed. The commercial-rated pilot and the five passengers received no injuries, and the airplane incurred substantial damage. The flight originated from Saint Croix, U.S. Virgin Islands, earlier that day, about 1545. The pilot stated that, on the downwind leg, the air traffic controller (ATC) instructed him to extend the downwind for 2 miles from the airport for traffic. Shortly after, ATC instructed him to fly straight to the runway for a short approach from the Capital building and to expedite due to inbound traffic at that time. The pilot questioned ATC about the short final instructions because of the ships at the port in close proximity to the approach. The pilot stated, "On short final the aircraft had no control" and he applied full power to the engines; however, the airplane impacted on the runway, left wing first. The controller at the Isla Grande Air Traffic Control stated that he told the pilot to remain two miles off the shoreline and report abeam the control tower for landing. The pilot then reported in at two miles NNE at an indicated altitude of 800 feet. The controller decided that he would be first to land, and gave him a short approach for landing. The pilot accepted the landing instructions and continued on the approach. The controller than issued a traffic advisory which the pilot acknowledged and was cleared to land. Shortly afterwards, the airplane crashed at the threshold of runway 9. Two witnesses stated they observed the accident airplane attempting a short final approach to runway 9, the airplane was in a 45 degree left turn and about at 150 feet, and was losing altitude. One of the witnesses stated they heard a rapid acceleration of the engines just before impact. Both witnesses observed the left wing impact the runway and the airplane sliding backwards before coming to a complete stop. A witness positioned about 1,000 feet from the approach end of runway 9, stated he observed the accident airplane over the inside pattern turning on a left turn for a short final approach for runway 9. The airplane continued the descent without any indication of recovery. He heard the engine speeding up before the left wing tip hit the surface and bounced back to the right hitting the nose and the right main gear, at this point both main landing gear separated. The airplane slid backwards for about 300 feet on the runway before coming to a stop. The six people onboard exited the airplane without assistance and appeared to have no injuries. The FAA Inspector that conducted the post-accident examination to the accident airplane's flight controls stated that continuity of the flight controls was established and the accident airplane's flight control systems were determined to be in operational condition. Runway 9 at Fernando Luis Ribas Dominicci Airport, is a published 100-foot wide by 5,317 foot long runway. The pilot stated that, on the downwind leg, the air traffic controller (ATC) instructed him to extend the downwind for 2 miles from the airport for traffic. Shortly after, ATC instructed him to fly straight to the runway for a short approach from the Capital building and to expedite due to inbound traffic at that time. The pilot questioned ATC about the short final instructions because of the ships at the port in close proximity to the approach. The pilot stated, "On short final the aircraft had no control" and he applied full power to the engines; however, the airplane impacted on the runway, left wing first. A witness positioned about 1,000 feet from the approach end of runway 9, stated he observed the accident airplane over the inside pattern turning on a left turn for a short final approach for runway 9. The airplane continued to descend without any indication of recovery. He heard the engine speeding up before the left wing tip hit the surface and bounced back to the right hitting the nose and the right main gear, at this point both main landing gear separated. The airplane slid backwards for about 300 feet on the runway before coming to a stop. The six people onboard exited the airplane without assistance and appeared to have no injuries. An FAA Aviation Safety Inspector that conducted the post-accident examination to the accident airplane's flight controls stated that continuity of the flight controls was established and the accident airplane's flight control systems were determined to be in operational condition. Runway 9 at Fernando Luis Ribas Dominicci Airport, is a published 100-foot wide by 5,317 foot long runway. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_MIA05LA013.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Beyond the agency record
Search this event elsewhere.
Pre-filled searches into the sources where news + community discussion of aviation events lives. External sources are reported, not agency. Treat them as signal that something happened, not as fact about what happened.
Entity-clustered aviation events in the press — last 24 hr + 30-day archive.
Official agency record + docket.
Investigative docket: factual reports, photos, transcripts.
Long-running aviation incident database (Flight Safety Foundation).
Community NTSB synthesis blog — often has photos and witness reports.
Gold-standard aviation incident blog.
Aviation industry news search.
GA pilot forum — informed but rumor-prone.
GA pilot subreddit search.
Tail-number page — flight history (free tier limited).
AOPA Air Safety Institute search.
Mainstream press coverage. Recent events only.
Privacy-preserving news search.
External links open in a new tab. We don't ingest their content; we deep-link search queries.
Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall). 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 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
Browse the full corpus — academia portal ↗