FLIGHT FINDINGSAVIATION OCCURRENCE MAP
Back to map

ERA19FA066 · Eipper QUICKSILVER MXLII

14 Dec 2018 · Fredericksburg, VA, United States

Eipper QUICKSILVER MXLII · Accident: aerodynamic stall/spin on approach

From Shannon Airport (EZF) to Shannon Airport (EZF)

Report a problem

Event

NTSB case
ERA19FA066
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
1 · all aircraft and ground
Ground fatalities
0
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Eipper QUICKSILVER MXLII

Aircraft type
Eipper QUICKSILVER
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N350FT
Operator
Unknown
Onboard fatalities
Unknown
Route
From Shannon Airport (EZF), Fredericksburg, VATo Shannon Airport (EZF), Fredericksburg, VA
Aircraft age
About 10 years (built 2008)
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Approach · VFR pattern crosswind
Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Aerodynamic stall/spin
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Substantial

Cause areas

  • Aircraft › Aircraft oper/perf/capability
  • Personnel issues › Task performance

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

The commercial pilot was operating an experimental amateur-built airplane on a personal flight in the airport traffic pattern. Video and audio recovered from an airframe-mounted camera, along with track data recorded by two onboard GPS receivers, revealed that, during the initial climb, the throttle was reduced, and then increased back to climb engine power for the upwind and crosswind legs of the traffic pattern. As the airplane turned toward the downwind leg at an altitude of about 300 feet, the throttle was reduced, increased briefly, and then was reduced again to what sounded consistent with an idle setting. The video and GPS track data showed that rather than aligning with the downwind leg of the traffic pattern, the airplane continued in a tightening, steepening, left turn with the engine at idle power. The airplane's last GPS-recorded position was over the accident site. The GPS data also showed that the airplane's groundspeed during the turn was near the airplane's published/placarded stall speeds. Just before ground impact, the video camera recorded a "pop" sound consistent with activation of the airplane's ballistic recovery system parachute. Postaccident examination of the airframe and engine revealed no preimpact mechanical anomalies that would have precluded normal operation.

The pilot had purchased the airplane about 3 months before the accident. At the time of purchase, the airplane had an open-cockpit, tubular-framed configuration. The pilot subsequently enclosed the open cockpit using PVC tubing, sheets of plexiglass, and zip ties. The investigation could not determine whether the cockpit modifications affected the handling and stall characteristics of the airplane. These modifications notwithstanding, the GPS data showed that the airplane was operating at or near its stall speed, had entered a tight left turn, and had likely encountered an aerodynamic stall before it descended to ground impact.

Probable cause

The pilot's exceedance of the airplane's critical angle of attack, which led to an aerodynamic stall while turning in the traffic pattern at low altitude.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ERA19FA066
Event ID
20181214X02810
Case number
ERA19FA066
Dataset
full-current
Source SHA-256
5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: f4ba021bfe925149601bbb38423debe0783c006eabfea36833d3ddda7ae21d19; retrieved 2026-09-15T06:52:00.680Z.