CHI82DA257
1982-07-18 · YPSILANTI, Michigan, United States · None · 1 aircraft · Status: Completed
Airport YIP
Current FAA registration · N52GS
- Make / Model
- BEECH 36
- Year of manufacture
- 1968 · 14 years old at event
- Engine
- CONT MOTOR IO 520 SERIES (285 hp)
- Seats / Engines
- 6 seats · 1 engine
- Last airworthiness date
- 19681112
- ADS-B equipped
- Yes — Mode-S A6873C
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
AFTER THE ENGINE WAS STARTED, THE PILOT FOUND THAT HE NEEDED A NEW MICROPHONE. HE STATED THAT HE LEANED OVER TO THE RIGHT TO HELP THE PASSENGER OPEN THE DOOR AND APPARENTLY BUMPED THE THROTTLE. THE AIRCRAFT MOVED AND STRUCK A PARKED GRUMMAN AMERICAN AA-5A, N9929U. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1982_CHI82DA257.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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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. All research papers
- arXiv 2022 · arXiv preprint Zero Touch Coordinated UAV Network Formation for 360° Views of a Moving Ground Target in Remote VR Applications
Unmanned aerial vehicles (UAVs) with on-board cameras are widely used for remote surveillance and video capturing applications.
- Embry-Riddle Scholarly Commons 2021 · Journal article (IJAAA) Internet of Things 36-rotor Multicopter for Ionizing Radiation Surveying
This paper presents an Internet of things 36-rotor unmanned aerial vehicle suitable for radiological surveying of buildings and facilities.
- NASA NTRS 2019 · Other - NACA Research Memorandum Ditching Tests of Two Models of the Army B-36 Airplane
The ditching characteristics of the Army B-36 airplane were determined by testing 1/20- and 1/30-scale dynamic models in calm water in Langley tank no. 2 and at the outdoor catapult.
- NASA NTRS 2019 · Other Differential Pressures on a Pitot-venturi and a Pitot-static Nozzle over 360 Degrees Pitch and Yaw
Measurements of the differential pressures on two navy air-speed nozzles, consisting of a Zahm type Pitot-Venturi tube and a SQ-16 two-pronged Pitot-static tube, in a tunnel air stream of fixed speed …
- NASA NTRS 2019 · Technical Memorandum (TM) Flutter clearance of the Schweizer 1-36 deep-stall sailplane
A Schweizer 1-36 sailplane was modified for a controlled, deep-stall flight program. This modification allowed the horizontal stabilizer to pivot as much as 70 deg leading edge down.
- arXiv 2026 · arXiv preprint Observability of Finite-Depth Double-Diffusive Exchange from Sparse Temperature-Salinity Measurements
Double-diffusive interfaces can support exchange histories that are spatially organized but only sparsely observed. A resolved three-dimensional calculation contains the route by which scalar gradient…