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CEN25LA029 · Cub Crafters CARBON CUB EX3

27 Oct 2024 · Ogallala, NE, United States

Cub Crafters CARBON CUB EX3 · Accident: flight control system malfunction/failure during initial climb

From an unrecorded airport to Centennial Airport (KAPA)

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Event

NTSB case
CEN25LA029
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
0 · 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

Cub Crafters CARBON CUB EX3

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
N257ST
Operator
Unknown
Onboard fatalities
Unknown
Route
From not recordedTo Centennial Airport (KAPA), Englewood, CO
Aircraft age
About 3 years (built 2021)
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
Initial climb
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
Destroyed

Cause areas

  • Aircraft › Aircraft systems
  • Personnel issues › Task performance

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

NTSB narrative

The pilot reported that he performed a flight control check before departing in his experimental, amateur-built airplane, and that the flight controls operated normally. During the initial climb, about 30 to 50 ft above ground level, the elevator control went slack. He could not regain elevator control and adjusted engine power in an attempt to regain control of the airplane’s pitch; however, the airplane descended and impacted the runway surface. The airplane skidded off the runway, the pilot egressed, and the airplane was destroyed by postimpact fire. A postaccident examination of the airplane found that the top elevator control cable was not attached to the elevator horn. The securing bolt, nut, and cotter pin were not located. The lower elevator control cable remained attached via its bolt, but the securing nut and cotter pin were not located. A review of maintenance information about the airplane revealed that the airplane was originally assembled about three years before the accident, and had undergone several condition inspections, including one by a mechanic who was different than the owner/builder. The most recent condition inspection was performed by the owner/builder about nine months before the accident, and would have included inspection of all flight control surfaces. There was no logbook record of any recent maintenance to the elevator, nor did the pilot recall any. Based on the available information, it is likely that the elevator control cable was improperly secured during maintenance; however, when the maintenance occurred could not be determined.

Probable cause

The improper installation of the elevator control cable hardware, which resulted in the separation of the elevator control cable and a loss of pitch control in flight.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record CEN25LA029
Event ID
20241028195380
Case number
CEN25LA029
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: 7f731f6d585b83f6b715000c1b89e030c86f3182c8e80e1f6a973d79b3c15930; retrieved 2026-09-16T19:24:54.241Z.