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ERA23LA132 · Stilp Tanner E SAVANNAH S

28 Feb 2023 · Trenton, SC, United States

Stilp Tanner E SAVANNAH S · Accident: flight control system malfunction/failure on approach

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Event

NTSB case
ERA23LA132
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
Event fatalities
Unknown
Ground fatalities
Unknown
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

Stilp Tanner E SAVANNAH S

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
N945HS
Operator
Unknown
Onboard fatalities
Unknown
Route
From not recordedTo not recorded
Aircraft age
About 1 year (built 2022)
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 final
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
Flight control system malfunction/failure
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
  • Aircraft › Aircraft systems

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

NTSB narrative

The pilot/builder in the right seat was on the fifth test flight in his amateur-built airplane with another pilot on board who was assisting. While turning from left base to the final leg of the traffic pattern for landing, with the left-seat pilot at the controls, the Y-stick that controlled both pitch and roll jammed. Both pilots attempted to free the Y-stick with force, but it remained jammed with no control of the flaperons and elevator. The airplane remained in a left, descending turn until it collided with trees and terrain about one mile short of the runway. The airplane sustained substantial damage; the right-seat pilot was seriously injured and the left-seat pilot had minor injuries.

An examination of the wreckage, including the flight control system, was conducted after the accident. Flight control continuity was confirmed from the flaperons, elevator, and rudder to the cockpit controls, except for the impact-related overload fractures. No areas of flight control binding or improper installation were found that would have prevented normal operation. An examination of the Y-stick revealed that the lower portion of the stick had minimal clearance with the cockpit floor and surrounding structure by design. The stick-to-floor clearance was smallest when the stick was near neutral (straight up). The clearance increased as bank was increased left or right. According to the kit manufacturer, the smallest Y-stick-to-structure clearance was 4.83mm (roll input neutral with full forward stick).

The actual Y-stick pre-accident clearance dimensions of the accident airplane could not be determined because of cockpit floor deformation from impact damage. There was no device installed on the floor that would have prevented a foreign object, such as a note pad, mobile phone, logbook, etc., from rolling or sliding under the Y-stick. Both pilots believed that a note pad used by the right-seat pilot to record flight test data fell to the floor during flight and jammed the control. Examination of photos of the 8.5 inch by 11-inch note pad revealed damage consistent with lower Y-stick impingement. It is likely that the note pad fell to the floor during flight and slid under the Y-stick during to the turn to final; when the stick was moved toward neutral, the jam occurred.

The kit manufacturer offered, as an option, a soft boot to cover the lower portion of the Y-stick; however, it is not known if this boot would have prevented the accident scenario.

Probable cause

The loss of control during the base turn to final due to the impingement of the Y-stick control by a notepad.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ERA23LA132
Event ID
20230301106801
Case number
ERA23LA132
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, cause areas. 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: 280018f627b03eda2e9de64e3e1a997c39c615e424ce4c4943175349353f4422; retrieved 2026-09-16T17:22:48.671Z.