CHI85LA195
1985-05-07 · TERRE HAUTE, Indiana, United States · None · 1 aircraft · Status: Completed
Airport HUF
Current FAA registration · N29CP
- Make / Model
- BEECH 58
- Year of manufacture
- 1970 · 15 years old at event
- Engine
- CONT MOTOR IO 520 SERIES (285 hp)
- Seats / Engines
- 6 seats · 2 engines
- Last airworthiness date
- 19700611
- ADS-B equipped
- Yes — Mode-S A2F361
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
THE PLT WAS PRACTICING TOUCH-&-GO LANDINGS ON RWY 13, THEN ELECTED TO MAKE ANOTHER ON RWY 5. HE STATED THAT THE GEAR WAS EXTENDED ON DOWNWIND & A SAFE GEAR INDICATION WAS RECEIVED. HOWEVER, THE ACFT WAS LANDED WITH THE GEAR RETRACTED. THE PLT STATED THAT THERE WAS NO WARNING HORN WHEN THE THROTTLES WERE RETARDED TO IDLE JUST BEFORE TOUCHDOWN. AN EXAM OF THE ACFT REVEALED NO PREIMPACT GEAR PROBLEMS, EXCEPT THE WARNING HORN WAS INOP DUE TO A BAD MICRO-SWITCH & A BROKEN ELECTRICAL WIRE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1985_CHI85LA195.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 (icing). All research papers
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During the 1985 thunderstorm season, three joint thunderstorm research flights were conducted within 100 n.mi. of NASA Langley by the NASA Storm Hazards F-106B and the FAA/USAF CV-580 research airplan…
- NTSB Aircraft Accident Reports 2004 · Accident report In-Flight Separation of Vertical Stabilizer — American Airlines Flight 587
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- NASA NTRS 2024 · Presentation American Airlines Flight 587 Crash Investigation: NASA Langley Research Center Participation and Perspective
- NASA NTRS 2019 · Other Documentation for Three Wake Vortex Model Data Sets from Simulation of Flight 587 Wake Vortex Encounter Accident Case
This document contains a general description for data sets of a wake vortex system in a turbulent environment. The turbulence and thermal stratification of the environment are representative of the co…
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A systematic approach to developing an engine monitoring system (EMS) is outlined. An extensive shopping list of EMS capabilities and benefits are included.
- NASA NTRS 2019 · Conference Paper Icing research tunnel test of a model helicopter rotor
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