BFO93LA074
1993-05-08 · TOWANDA, Pennsylvania, United States · Serious · 1 aircraft · Status: Completed
Airport N27
Aircraft involved
Probable cause & findings
THE FAILURE OF THE AILERON CONTROL CABLE WHICH RESULTED IN LOSS OF CONTROL IN FLIGHT.
Factual narrative
SHORTLY AFTER TAKEOFF, THE LEFT AILERON CONTROL CABLE FAILED IN THE VICINITY OF THE RIGHT AFT DOOR POST IN THE LOCATION OF A PULLEY. THE PILOT STATED IT TOOK FULL RIGHT AILERON TO KEEP THE AIRPLANE FROM ROLLING. THE AIRPLANE REMAINED IN THE TRAFFIC PATTERN TO LAND. DURING THE BASE LEG, THE PILOT APPLIED FULL FLAPS. THE AIRPLANE CONTINUED TO ROLL LEFT AND THE AILERONS DID NOT RESPOND TO CONTROL INPUTS. THE AIRPLANE IMPACTED THE GROUND LEFT WING DOWN AND CAME TO REST INVERTED. A METALLURGICAL EXAMINATION OF THE FAILED CABLE REVEALED THAT IT WAS CORRODED IN THE AREA OF THE FAILURE. THE AIRPLANE HAD RECEIVED A 100 HOUR ANNUAL INSPECTION ON OCTOBER 3, 1992. SINCE THE INSPECTION, THE AIRPLANE HAD FLOWN ABOUT ONE HOUR. THE AIRPLANE WAS TIED DOWN OUTSIDE FOR MOST OF THE TIME SINCE PURCHASED IN THE YEAR 1958. THE FAILED AILERON CONTROL CABLE WAS AN ORIGINAL CABLE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1993_BFO93LA074.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 or causal vocabulary (loss of control). All research papers
- NASA NTRS 2023 · Reprint (Version printed in journal) Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft
The NASA Emergency Locator Transmitter Survivability and Reliability project was initiated in 2013 to assess the crash performance standards for the next generation of emergency locator transmitter (E…
- NASA NTRS 2019 · Conference Paper Crash Testing and Simulation of a Cessna 172 Aircraft: Pitch Down Impact Onto Soft Soil
During the summer of 2015, NASA Langley Research Center conducted three full-scale crash tests of Cessna 172 (C-172) aircraft at the NASA Langley Landing and Impact Research (LandIR) Facility.
- NASA NTRS 2019 · Technical Memorandum (TM) Simulating the Impact Response of Three Full-Scale Crash Tests of Cessna 172 Aircraft
During the summer of 2015, a series of three full-scale crash tests were performed at the Landing and Impact Research Facility located at NASA Langley Research Center of Cessna 172 aircraft.
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER) A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- SKYbrary (Eurocontrol) 2024 · SKYbrary article Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
- Semantic Scholar 2024 · Article (International Conference on Networking and Services) Risk Assessment of Loss of Control In-Flight Trajectories for Urban Air Mobility Safety
In Urban Air Mobility (UAM), maintaining a minimum separation between aircraft is a safety requirement, which becomes challenging amidst congested air traffic and off-nominal conditions, such as Loss …