NTSB CAROL · Event
Event ANC25LA008
Registry · N55PK
FAA Aircraft Registry record.
Make / Model
CUB CRAFTERS INC CC18-180
Year of manufacture
2019 · 5 years old at event
Engine
LYCOMING O-360-C1G (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20200108
ADS-B equipped
Yes — Mode-S A6FE61
Registrant of record
GLASHEEN SEAN T
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The incorrect installation of the rear flight control stick, resulting in the pilot’s inability to control the pitch attitude, coupled with the pilot’s inadequate control system check before departure, all which resulted in an aerodynamic stall during takeoff.
Factual narrative
On November 2, 2024, about 1436 Alaska daylight time, a Cub Crafters CC18-180 airplane, N55PK, sustained substantial damage when it was involved in an accident at the Lake Hood Airport (LHD) Anchorage, Alaska. The pilot was seriously injured. The airplane was operated as a public aircraft flight. The accident airplane was owned by the U.S. Department of the Interior and operated by the National Park Service. The purpose of the flight was to reposition the airplane back to Fairbanks, Alaska, where the pilot and airplane were based. The airplane departed from runway 32 at LHD. The pilot reported that, after the airplane became airborne, he was unable to move the flight control stick forward and the airplane started climbing aggressively. The pilot attempted to use the elevator trim control to lower the nose and level the airplane. However, the airplane stalled and began an uncontrolled, nose-down descent toward the runway. The pilot was able to level the airplane slightly but there was insufficient altitude to recover from the stall. The airplane impacted the runway and came to rest about 78 ft from the initial impact site, resulting in substantial damage to the fuselage and both wing lift struts. A postaccident examination revealed that the rear flight control stick was incorrectly installed. The flight control stick was installed in reverse. The curve of the control stick was curved forward; the control stick would contact the pilot’s seatback, which restricted movement and limited the control stick from moving forward. The pilot’s front seat was found in the full aft and locked position. It was the operator’s practice that pilots could remove the aft control stick when they were flying cargo so that the cargo wouldn’t interfere with the control stick. The accident pilot reported that he had never removed the rear control stick in the airplane, nor had he received training on how to remove or install the rear flight control stick. The pilot was unaware that the rear flight control stick could be installed incorrectly. The pilot had always flown with an instructor pilot in the rear seat. The pilot did not know who installed the rear control stick before his flight, and the subsequent accident investigation was unable to identify who installed it incorrectly. The pilot stated that he performed a preflight inspection and found no discrepancies. The rear control stick was already installed when he arrived. The weight and balance was calculated to be within limits. He then taxied the airplane to Runway 32 for departure. He said, in part: ”I did one last carburetor heat check and one last control check and then got clearance from the tower for takeoff.” A postaccident reenactment of the flight control check and takeoff was conducted in an exemplary CC18 in the Office of Aviation Services hangar. The front seat was positioned in the aft position and the rear control stick was installed backward. The flight control check appeared normal with no binding. After applying backstick pressure to simulate the takeoff, forward pressure was applied, and the control stick became jammed in the forward position and was unmovable in any direction until the pilot leaned forward and the stick released. During the reenactment, the control stick became jammed with the front seatback frame. Cub Crafters’ supplement dated January 13, 2016, which describes the process and requirements for reinstalling the rear control stick, states in part: “Ensure full range of motion (including trim) is met without the rear stick contacting anything.” Additionally, the supplement must be added to the pilot’s operating handbook and the Federal Aviation Administration approved flight manual when the rear control stick is removed and reinstalled. As a result of this investigation, the U.S. Department of the Interior issued a safety alert (DOI SA 25-01) dated November 15, 2024, to address the correct installation of the rear flight control stick. Additionally, the safety alert highlights the preflight and before takeoff checklists requiring flight control checks to verify the maximum range of travel is available. The pilot reported that during takeoff, just after becoming airborne, he was unable to move the flight control stick forward. The airplane started climbing aggressively and the pilot attempted to recover using elevator trim control. The airplane subsequently stalled and began an uncontrolled, nose-down descent toward the runway. During the descent, the pilot was able to level the airplane; however, there was insufficient altitude to recover from the stall. The airplane impacted the runway, resulting in substantial damage to the fuselage and both wing lift struts. The accident pilot reported that just before departure, he did a control system check, which did not reveal any anomalies. A postaccident examination revealed that the rear flight control stick was incorrectly installed. The flight control stick was installed in reverse. The curve of the control stick was curved forward, which resulted in the control stick contacting the pilot’s (front) seatback, which limited movement and prevented the control stick from moving full forward. The investigation did not determine who improperly installed the control stick. However, it was normal practice for the pilots to remove and reinstall the rear seat control stick if they were flying with just cargo in the rear seat area. The pilot reported that he has never removed the control stick and was not trained to do so. Had the pilot been trained on the removal and installation of the control stick, he may have noticed the control stick was installed backwards during his preflight. He also stated that he was not aware that the control stick could be installed incorrectly. The airplane manufacturers’ supplement dated January 13, 2016, which describes the process and requirements for reinstalling the rear control stick, states in part: “Ensure full range of motion (including trim) is met without the rear stick contacting anything.” Additionally, the supplement must be added to the pilot’s operating handbook and the Federal Aviation Administration approved flight manual when the rear control stick is removed and reinstalled. Following the accident, the operator issued an agency safety alert to address the correct installation of the rear flight control stick. Additionally, the safety alert highlights the preflight and before takeoff checklists requiring flight control checks to verify the maximum range of travel. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Personnel issues-Experience/knowledge-Training-Training with equipment-Pilot
- — Personnel issues-Task performance-Inspection-Preflight inspection-Pilot
- — Personnel issues-Experience/knowledge-Knowledge-Knowledge of equipment-Pilot
- — Personnel issues-Experience/knowledge-Knowledge-Knowledge of equipment-Maintenance personnel
- — Personnel issues-Action/decision-Info processing/decision-Identification/recognition-Pilot
- — Organizational issues-Support/oversight/monitoring-Training-Initial training-Operator
- — Organizational issues-Support/oversight/monitoring-Training-Initial training-Manufacturer
- — Organizational issues-Management-Policy/procedure-Adequacy of policy/proc-Manufacturer
- — Organizational issues-Development-Design-Equipment design-Manufacturer
- — Aircraft-Aircraft systems-Flight control system-Control column section-Incorrect service/maintenance
Verbatim from NTSB's published report. Source file
NTSB_2024_ANC25LA008.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 (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.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- 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 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- 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…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
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