NTSB CAROL · Event
Event LAX91FA342
Registry · N5277L
FAA Aircraft Registry record.
Make / Model
CESSNA T206H
Seats / Engines
6 seats · 1 engine
ADS-B equipped
Yes — Mode-S A6A647
Registrant of record
M2C2 AIR LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
FAILURE OF THE PILOT TO MAINTAIN PROPER AIRSPEED BY EMPLOYING AN EXCESSIVE ANGLE OF ATTACK DURING THE TAKEOFF CLIMB DURING A GO-AROUND RESULTING IN AN AERODYNAMIC STALL AND SUBSEQUENT INFLIGHT LOSS OF CONTROL. CONTRIBUTING TO THE ACCIDENT WAS THE PILOT'S POOR APPROACH PLANNING, COMPENSATION FOR WIND CONDITIONS AND A HIGH DENSITY ALTITUDE.
Factual narrative
A PIPER PA 28-180 COLLIDED WITH PORTABLE BUILDINGS ON THE AIRPORT AFTER AN IN FLIGHT LOSS OF CONTROL. THE PILOT REPORTED HAVING PROBLEMS RECEIVING RADIO TRANSMISSIONS. THE AIR TRAFFIC CONTROL TOWER CLEARED THE PILOT TO LAND ON THE RWY MOST INTO THE WIND. THE AIRPLANE CONTINUED PAST THE ACTIVE RWY AND APPROACHED A PERPENDICULAR RWY RESULTING IN A QUARTERING TAILWIND. THE AIRPLANE OVERSHOT THE FINAL APPROACH COURSE OF THE PERPENDICULAR RWY AND INITIATED A GO-AROUND. DURING THE GO-AROUND WITNESSES OBSERVED THE AIRPLANE NOT GAINING ALTITUDE AND AT A SLOW AIRSPEED. THE WITNESSES ALSO INDICATED THE SOUND OF THE ENGINE APPEARED NORMAL. THE AIRPLANE THEN TURNED RIGHT, INTO A QUARTERING HEADWIND, STALLED, AND DESCENDED VERTICALLY TO THE GROUND. THE WIND VELOCITY AT THE TIME OF THE ACCIDENT WAS 13 KTS. THE DENSITY ALTITUDE WAS COMPUTED TO BE ABOUT 7,500 FEET MSL. ACCORDING TO THE PILOT OPERATING HANDBOOK FOR THE PIPER PA 28-180, THE AIRPLANE SHOULD HAVE BEEN CAPABLE OF A 375 FOOT PER MINUTE RATE OF CLIMB. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1991_LAX91FA342.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 (stall, loss of control, go-around). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NTSB Aircraft Accident Reports 2021 · Accident report
Crash of Atlas Air Flight 3591, Boeing 767-300 (N1217A)
Atlas Air 3591 crashed into Trinity Bay, Texas, February 23, 2019. Investigation of the in-flight loss-of-control crash of Atlas Air 3591 into Trinity Bay, Texas.
- Semantic Scholar 2016 · Article (Interacción)
Trajectory Recovery System: Angle of Attack Guidance for Inflight Loss of Control
This paper describes the design and development of an ecological display to aid pilots in the recovery of an In-Flight Loss of Control event due to a Stall (ILOC-S).
- NTSB Aircraft Accident Reports 2010 · Accident report
Loss of Control on Approach — Colgan Air Flight 3407
Colgan Air 3407 / Continental Connection (Q400) Buffalo NY, February 12, 2009 — 50 fatalities. Definitive investigation of the Colgan 3407 stall-stick-pusher crash on approach to Buffalo.
- 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 …
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- NASA NTRS 2025 · Conference Paper
A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
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