LAX95LA251
1995-07-13 · SANTA MONICA, California, United States · None · 1 aircraft · Status: Completed
Airport SMO
Current FAA registration · N200CT
- Make / Model
- MOONEY M20M
- Year of manufacture
- 1989 · 6 years old at event
- Engine
- LYCOMING TI0-540 SER (310 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19891108
- ADS-B equipped
- Yes — Mode-S A19247
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's improper remedial action during an aborted takeoff due to an improperly installed pitot line to the airspeed indicator.
Factual narrative
QcOn July 13, 1995, at 0727 hours Pacific daylight time, a Mooney M-20-M, N200CT, was substantially damaged during an aborted takeoff at Santa Monica, California. The pilot and passenger were not injured. Visual meteorological conditions prevailed for the departure, and an instrument flight plan was filed. The flight was originating as a personal cross-country flight destined for Abilene, Texas. The pilot stated that during the takeoff roll on runway 21, he realized that he had no airspeed indication. He chose to abort the takeoff at that point. At the west end of the runway, skid marks indicated that the airplane went sideways and the left landing gear collapsed. The left wing settled to the ground and fuel ignited from the wing fuel vent area. The brief fire burnt into the wing structure. The wing was also damaged from ground contact. The pilot had contracted for repairs to the vacuum/instrument system while at Santa Monica. According to a Federal Aviation Administration (FAA) inspector, examination of the airspeed plumbing revealed that the plastic pitot tube was not connected at the airspeed indicator. Further examination of the tube failed to reveal a crush imprint from the "B" nut cone. The cone was found on the cockpit floor. An airspeed repair date of January 23, 1995, was affixed to the airspeed instrument case. The pilot stated that the M20 brakes are not adequate to stop a TLS model, near gross weight, down hill with a slight tailwind. He stated that the brakes should have been enlarged with the gross weight increase. He further stated that he now has the double puck brakes and that they are much more effective. DURING THE TAKEOFF ROLL THE PILOT REALIZED THAT HE HAD NO AIRSPEED INDICATION AND CHOSE TO ABORT. THE AIRCRAFT SKIDDED OFF THE END OF THE RUNWAY COLLAPSING A MAIN LANDING GEAR RESULTING IN A FIRE AT THE MID-WING FUEL VENT AREA. THE PILOT HAD CONTRACTED FOR INSTRUMENT REPAIRS IN ANOTHER AREA OF THE INSTRUMENT PANEL JUST PRIOR TO DEPARTURE. POSTACCIDENT EXAMINATION REVEALED THAT THE PITOT LINE TO THE AIRSPEED INDICATOR HAD BEEN IMPROPERLY INSTALLED AND WAS SUBSEQUENTLY PULLED OUT OF THE INSTRUMENT WHILE OTHER WORK WAS BEING PREFORMED NEAR IT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_LAX95LA251.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
- 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…