LAX92LA009
1991-10-05 · RIVERSIDE, California, United States · None · 1 aircraft · Status: Completed
Airport RAL
Current FAA registration · N9517T
- Make / Model
- CESSNA 210
- Year of manufacture
- 1960 · 31 years old at event
- Engine
- CONT MOTOR I0-470 SERIES (260 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19600409
- ADS-B equipped
- Yes — Mode-S AD3BBD
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE FAILURE OF A HYDRAULIC GEAR RETURN LINE, WHICH CAUSED THE AIRCRAFT'S MAIN LANDING GEAR TO COLLAPSE DURING LANDING TOUCHDOWN.
Factual narrative
SHORTLY AFTER TAKEOFF AFTER ATTEMPTING TO RETRACT THE LANDING GEAR, THE PILOT NOTED AN UNSAFE GEAR INDICATION. THE PILOT ESTABLISHED COMMUNICATIONS WITH CONTROL TOWER PERSONNEL AT A LARGER, NEARBY AIRPORT. HE REPORTED THE PROBLEM TO TOWER PERSONNEL AND REQUESTED LANDING INSTRUCTIONS. THE PILOT WAS CLEARED TO LAND. UPON TOUCHDOWN, THE MAIN LANDING GEAR COLLAPSED CAUSING THE AIRCRAFT TO COLLIDE WITH THE RUNWAY. POST-ACCIDENT EXAMINATION REVEALED THAT A HYDRAULIC GEAR RETURN LINE, CESSNA AIRCRAFT PART NUMBER 1280106-5, HAD RUPTURED. THE LINE WAS NOTED AS BEING 'BRITTLE.' LOG BOOK ENTRIES INDICATE THE LINE WAS INSTALLED ON THE AIRCRAFT ON JULY 19, 1991. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1991_LAX92LA009.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.
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Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
- NASA NTRS 2020 · Technical Memorandum (TM) Evaluation Issues for a Flight Deck Interface; CAST SE-210 Output 2: Report 4 of 6
This report is part of a series of reports that addresses flight deck design and evaluation, written as a response to loss of control accidents.
- 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…