MKC87LA008
1986-10-18 · MACON, Missouri, United States · None · 1 aircraft · Status: Completed
Airport K89
Current FAA registration · N1690K
- Make / Model
- LUSCOMBE 8E
- Engine
- LYCOMING 0-290 SERIES (140 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19560508
- ADS-B equipped
- Yes — Mode-S A1157F
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
THE PILOT STATED THAT HE ENCOUNTERED MORE SEVERE CROSSWINDS THAN PLANNED UPON LANDING AND THAT HE TRIED REMEDIAL ACTION, INCLUDING A REJECTED LANDING, BUT IT CAME TOO LATE. THE WIND WAS BLOWING FROM THE RIGHT ON THE LANDING ROLL AS HE SHUT DOWN THE ENGINE AND DEFLECTED FULL LEFT RUDDER TO TRY TO GROUND-LOOP THE AIRPLANE. THE AIRCRAFT CAME TO REST IN AN AREA OF BRAMBLES AND VEGETATION AT THE BOTTOM OF A HOLLOW. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1986_MKC87LA008.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type. All research papers
- NASA NTRS 2019 · Conference Paper Transonic Experimental Observations of Abrupt Wing Stall on an F/A-l8E Model
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.
- NASA NTRS 2019 · Conference Paper Transonic Experimental Observations of Abrupt Wing Stall on an F/A-18E Model (Invited)
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.