NYC88LA140
1988-05-15 · ROCHESTER, New York, United States · None · 1 aircraft · Status: Completed
Airport ROC
Current FAA registration · N2047K
- Make / Model
- LUSCOMBE 8E
- Engine
- CONT MOTOR C85 SERIES (85 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19600927
- ADS-B equipped
- Yes — Mode-S A1A436
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
THE LUSCOMBE 8E EXPERIENCED A FAILURE OF THE RIGHT MAIN LANDING GEAR AXLE DURING A BOUNCED LANDING. THE FAILURE OCCURRED AT THE WELD WHERE THE AXLE ATTACHES TO THE LANDING GEAR STRUT. EXAMINATION OF THE FRACTURE REVEALED A PRE-EXISTING CRACK THAT WAS NOT DETECTED PRIOR TO THE ACCIDENT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1988_NYC88LA140.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.