N410UE - Aircraft Aircraft Registration

JS31

Aircraft Description

Model Year

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Manufacturer

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Model

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Type Aircraft

Fixed Wing Multi Engine

ICAO Type Code

JS31Jetstream 31

Airworthiness Date

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Classification

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Type Registration

Unknown

Status

N-Number Assigned – but has not yet been registered

Cert Issue Date

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Registered Owner

The registered owner has requested to keep this data private under Title 49 of the United States Code, Section 44114.

Powerplant & Avionics

Engine Type

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Number of Engines

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Mode S Code (Oct)

51152747

Mode S Code (Hex)

A4D5E7

NTSB Accident History (1)

Date	NTSB #	Damage	Highest Injury	Probable Cause
Dec 27, 1989	DCA90MA011	Destroyed	Fatal	THE FLIGHTCREW'S DECISION TO CONTINUE AN UNSTABILIZED INSTRUMENT LANDING SYSTEM (ILS) APPROACH THAT LED TO A STALL, MOST LIKELY OF THE HORIZONTAL STABILIZER, AND LOSS OF CONTROL AT LOW ALTITUDE. CONTRIBUTING TO THE ACCIDENT WAS THE AIR TRAFFIC CONTROLLER'S IMPROPER VECTORS THAT POSITIONED THE AIRPLANE INSIDE THE OUTER MARKER WHILE IT WAS STILL WELL ABOVE THE GLIDESLOPE. CONTRIBUTING TO THE STALL AND LOSS OF CONTROL WAS THE ACCUMULATION OF AIRFRAME ICE THAT DEGRADED THE AERODYNAMIC PERFORMANCE OF THE AIRPLANE.

Dec 27, 1989DCA90MA011

Destroyed

Fatal

THE FLIGHTCREW'S DECISION TO CONTINUE AN UNSTABILIZED INSTRUMENT LANDING SYSTEM (ILS) APPROACH THAT LED TO A STALL, MOST LIKELY OF THE HORIZONTAL STABILIZER, AND LOSS OF CONTROL AT LOW ALTITUDE. CONTRIBUTING TO THE ACCIDENT WAS THE AIR TRAFFIC CONTROLLER'S IMPROPER VECTORS THAT POSITIONED THE AIRPLANE INSIDE THE OUTER MARKER WHILE IT WAS STILL WELL ABOVE THE GLIDESLOPE. CONTRIBUTING TO THE STALL AND LOSS OF CONTROL WAS THE ACCUMULATION OF AIRFRAME ICE THAT DEGRADED THE AERODYNAMIC PERFORMANCE OF THE AIRPLANE.

Additional Details

Registration

N410UE

Serial Number

776

Number of Engines

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Number of Seats

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Expiration Date

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Last Action Date

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Last Update Date

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Unique ID

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Data Source

Data provided by the US Federal Aviation Administration. View on FAA.gov

Last updated: 2026-05-15 01:32:20 UTC