CHI91LA155
1991-05-11 · CRESTON, Iowa, United States · None · 1 aircraft · Status: Completed
Airport CSQ
Current FAA registration · N88441
- Make / Model
- PIPER J3C-65
- Year of manufacture
- 1946 · 45 years old at event
- Engine
- CONT MOTOR C90 SERIES (95 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19951005
- ADS-B equipped
- Yes — Mode-S AC2FAF
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
ICING IN THE INDUCTION AIR CONTROL SYSTEM.
Factual narrative
THE ACCIDENT AIRPLANE COLLIDED WITH ROUGH UNEVEN TERRAIN DURING A FORCED LANDING, AFTER LOSING PARTIAL ENGINE POWER DURING A PERSONAL FLIGHT. THE EXPERIMENTAL (EXHIBITION) CERTIFICATED AIRPLANE WAS SUBSTANTIALLY DAMAGED. THE ACCIDENT AIRPLANE HAD BEEN EXTENSIVELY MODIFIED BY REDUCING THE WINGSPAN AND THE INSTALLATION OF AN ENGINE MODIFIED FOR FUEL INJECTED OPERATION. NO PROVISIONS FOR INDUCTION SYSTEM HEATING OR A MEANS OF PROVIDING AN ALTERNATE AIR SOURCE WERE INCLUDED IN THE MODIFICATION. NO DEFECTS WERE DISCOVERED IN THE AIRFRAME OR POWERPLANT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1991_CHI91LA155.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 ↗
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- Pilots of America Community ↗
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Related research
Matched on aircraft type or causal vocabulary (icing, stall). All research papers
- 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 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…
- NASA NTRS 2019 · Contractor Report (CR) An Evaluation of an Analytical Simulation of an Airplane with Tailplane Icing by Comparison to Flight Data
This report presents the assessment of an analytical tool developed as part of the NASA/FAA Tailplane Icing Program. The analytical tool is a specialized simulation program called TAILSM4 which was de…
- NASA NTRS 2019 · Technical Publication (TP) NASA/FAA Tailplane Icing Program: Flight Test Report
This report presents results from research flights that explored the characteristics of an ice-contaminated tailplane using various simulated ice shapes attached to the leading edge of the horizontal …
- NASA NTRS 2019 · Other [Tail Plane Icing]
The Aviation Safety Program initiated by NASA in 1997 has put greater emphasis in safety related research activities. Ice-contaminated-tailplane stall (ICTS) has been identified by the NASA Lewis Icin…
- Embry-Riddle Scholarly Commons 2019 · Journal article (IJAAA) Airport Policing in Pakistan: Structure, Training, and Issue
Airports are strategically and economically important installations of any country. Airports are the gateway of any country and any incidents at these gateways may harm the very aspects of a country i…