NTSB CAROL · Event
Event BFO88FA063
Registry · N1021P
FAA Aircraft Registry record.
Make / Model
CESSNA T182T
Year of manufacture
2005
TCDS
3A13 · TEXTRON AVIATION INC
Engine
LYCOMING TI0-540 SER (310 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20050504
ADS-B equipped
Yes — Mode-S A00EAB
Registrant of record
YUROK TRIBE CONSTRUCTION CORP
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
SHORTLY AFTER TAKEOFF AT AN ALTITUDE OF 200 FT AGL, A POWER LOSS WAS EXPERIENCED ON THE LEFT ENGINE. ACCORDING TO THE PLT, WHEN THE THROTTLE WAS RETARDED TO VERIFY THE ENGINE FAILURE, THE ENGINE SEEMED TO 'COME BACK TO LIFE'. THE THROTTLE WAS ADVANCED AND ONCE AGAIN A LOSS OF POWER WAS EXPERIENCED. UNABLE TO GAIN ENOUGH ALTITUDE TO CLEAR THE SURROUNDING TERRAIN AND RETURN TO THE AIRPORT, THE PLT ELECTED TO MAKE A GEAR-UP FORCED LANDING IN A FIELD. THE AIRPLANE SLID FOR 333 FT BEFORE COMING TO REST. INSPECTION OF THE AIRPLANE, ENGINE AND ENGINE COMPONENTS FAILED TO REVEAL ANY MECHANICAL FAILURE/MALFUNCTION. THE ONLY DISCREPANCY FOUND WERE SEVERAL PIECES OF A SILICON RUBBER TYPE MATERIAL INSIDE THE LEFT MAIN FUEL TANK NEAR THE FUEL PICK-UP LINE SCREEN. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1988_BFO88FA063.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 or causal vocabulary (engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2022 · arXiv preprint
Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper
Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM)
A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum)
Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…
Browse the full corpus — academia portal ↗