NTSB CAROL · Event
Event BFO84IA004
Registry · N72TM
FAA Aircraft Registry record.
Make / Model
BEECH 95-B55 (T42A)
Year of manufacture
1976 · 8 years old at event
Engine
CONT MOTOR I0-470 SERIES (260 hp)
Seats / Engines
6 seats · 2 engines
Last airworthiness date
19761013
ADS-B equipped
Yes — Mode-S A9A2E8
Registrant of record
TANGO SIERRA LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
THE PLT MADE AN EMERGENCY LANDING ON RWY 18 FOLLOWING A LOSS OF POWER IN THE RT ENG & A SUBSEQUENT IN-FLIGHT FIRE. INVESTIGATION REVEALED A CRACK IN THE #1 CYL THAT ORIGINATED AT THE EXHAUST PORT, DOWNSTREAM OF THE VALVE. THE CRACK PROPAGATED THROUGH FATIQUE TO THE TOP SPARK PLUG HOLE. EVENTUALLY, IT PROGRESSED TO THE POINT THAT THE FLAME PATH (DURING THE COMBUSITION CYCLES), TORCHED THROUGH NEAR THE SPARK PLUG HOLE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1984_BFO84IA004.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type. Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2011 · Conference Paper
Joint thunderstorm operations using the NASA F-106B and FAATC/AFWAL Convair 580 airplanes
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
American Airlines 587 (A300-605R) Belle Harbor, NY, November 12, 2001 — 265 fatalities. Investigation of the post-takeoff in-flight breakup of American 587 over Belle Harbor.
- 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…
- NASA NTRS 2016 · Conference Paper
An overview of SAE ARP 1587: Aircraft gas turbine engine monitoring system guide
A systematic approach to developing an engine monitoring system (EMS) is outlined. An extensive shopping list of EMS capabilities and benefits are included.
- arXiv 2025 · arXiv preprint
Numerical Investigation of Discontinuous Ice Effects on Swept Wings
This study investigates the aerodynamic performance and flow structures of infinite swept wings with artificially simulated discontinuous ice using an enhanced delayed detached-eddy simulation.
Browse the full corpus — academia portal ↗