NTSB CAROL · Event
Event BFO88FA010
Registry · N23AZ
FAA Aircraft Registry record.
Make / Model
CESSNA A185F
Year of manufacture
1974 · 13 years old at event
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
19981027
ADS-B equipped
Yes — Mode-S A2063F
Registrant of record
NIX JACOB DBA
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
THE ACFT HAD DESCENDED THROUGH A CLOUD LAYER ENROUTE FOR THE SCHEDULED LNDG AT IAD AND ACCORDING TO THE CREW HAD PICKED UP SOME TRACE RIME ICE ON ITS WING SURFACES. ALTHOUGH PITOT AND SAS (STALL AVOIDANCE SYSTEM) HEAT WERE USED THE CAPTAIN ELECTED NOT TO USE ENGINE INLET ANTI-ICE. JUST INSIDE THE OUTER MARKER THE LEFT ENGINE LOST POWER FOLLOWED SHORTLY BY THE RIGHT ENGINE. THE CAPTAIN WAS ABLE TO SET THE ACFT DOWN IN AN OPEN FIELD WHERE THE GEAR COLLAPSED DURING THE LANDING ROLL. THE ENGINES WERE SUCCESSFULLY RUN-UP AT THE GARRETT FACILITY. THE FLT MANUAL CONTAINS A WARNING AND A NOTE STATING THAT ENGINE HEAT AND CONTINUOUS IGNITION MUST BE USED AFTER LEAVING ICING CONDITIONS UNTIL THE PLT IS CONFIDENT THAT ANY SIGNIFICANT RESIDUAL ICE WILL NOT BE INJESTED INTO THE ENGINES. ICE WAS FOUND LYING BENEATH THE RT WING WHICH MATCHED THE CURVATURE OF THE LEADING EDGE OF THE WING. A ROUND CONICAL SHAPED PIECE OF ICE WAS FOUND ALONG THE WRECKAGE PATH WHICH MATCHED THE NOSE OF THE PROPELLER SPINNER. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1987_BFO88FA010.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 (icing, stall). 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 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- NASA NTRS 2019 · Contractor Report (CR)
An Evaluation of an Analytical Simulation of an Airplane with Tailplane Icing by Comparison to Flight Data
This report presents the assessment of an analytical tool developed as part of the NASA/FAA Tailplane Icing Program. The analytical tool is a specialized simulation program called TAILSM4 which was de…
- NASA NTRS 2019 · Technical Publication (TP)
NASA/FAA Tailplane Icing Program: Flight Test Report
This report presents results from research flights that explored the characteristics of an ice-contaminated tailplane using various simulated ice shapes attached to the leading edge of the horizontal …
- NASA NTRS 2019 · Other
[Tail Plane Icing]
The Aviation Safety Program initiated by NASA in 1997 has put greater emphasis in safety related research activities. Ice-contaminated-tailplane stall (ICTS) has been identified by the NASA Lewis Icin…
- Embry-Riddle Scholarly Commons 2019 · Journal article (IJAAA)
Airport Policing in Pakistan: Structure, Training, and Issue
Airports are strategically and economically important installations of any country. Airports are the gateway of any country and any incidents at these gateways may harm the very aspects of a country i…
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