NTSB CAROL · Event
Event ANC05LA052
Registry · N955DW
FAA Aircraft Registry record.
Make / Model
CUB CRAFTERS PA18-150
Year of manufacture
2004 · 1 years old at event
Engine
LYCOMING O-360-C4P (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20060802
ADS-B equipped
Yes — Mode-S AD479A
Registrant of record
WITHAM DAVID
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The flight instructor's inadequate supervision of the flight, and the dual student's failure to maintain directional control.
Factual narrative
On March 27, 2005, about 1530 Alaska standard time, a wheel-equipped Cub Crafter's PA-18 airplane, N955DW, sustained substantial damage following a loss of control and collision with the runway while landing at the Fairbanks International Airport, Fairbanks, Alaska. The certificated flight instructor and the private pilot/airplane owner were not injured. The local instructional 14 CFR Part 91 flight operated in visual meteorological conditions without a flight plan. The purpose of the flight was for the private pilot to increase his proficiency in operating a tailwheel airplane. During a telephone conversation with the NTSB investigator-in-charge (IIC) on March 28, the flight instructor related that he was providing flight instruction to the private pilot to improve his tailwheel takeoff and landing procedures. The instructor noted that the private pilot had recently been involved in a landing mishap in a tailwheel airplane (the accident airplane, N955DW), and that the FAA had notified the pilot that they wished to re-examine his tailwheel proficiency in a pending flight check. The instructor stated that the accident landing was the third full-stop landing of the day on runway 19L. He said that the two previous landings had been completed satisfactorily. On the accident landing, the airplane began to veer to the left shortly after touch down, and the instructor said he assisted the private pilot by applying the right brake. He noted that when he placed his foot on the rudder pedal to apply the right brake, the rudder pedal had already been fully deflected to the right by the private pilot. The airplane did not respond to the control inputs, and continued to swerve to the left. The right main landing gear subsequently collapsed, and the right wing struck the runway, damaging the wing spars. The flight instructor said he was unaware of any preaccident mechanical problems with the airplane, but thought possibly the left brake may have heated up and expanded, resulting in the left brake dragging. An FAA inspector from the Fairbanks Flight Standards District Office inspected the accident airplane's left brake assembly on March 29, and found no evidence of a mechanical malfunction. The certificated flight instructor was providing tailwheel instruction to the private pilot/airplane owner. While landing on runway 19L, a 6,500 foot long by 100 foot wide hard-surfaced runway, the instructor said that the airplane swerved to the left and the private pilot made a correction to the right by completely deflecting the right rudder. The instructor stated he also applied the right brake in addition to ensuring that the rudder was all the way to the right, but the airplane continued to the left. The right main landing gear subsequently collapsed, and the right wing contacted the runway, sustaining structural damage to the main spar. The instructor stated that he wasn't sure, but thought it possible the left brake had heated up, and was dragging during the accident landing. Postaccident inspection of the airplane by an FAA inspector disclosed no evidence of any mechanical malfunction of the left brake or wheel assembly. Wind at the time of the accident was reported to be from 163 degrees (magnetic) at 5 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_ANC05LA052.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
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Academic papers and agency reports matching this event's aircraft type or causal vocabulary (loss of control). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
- NTSB Aircraft Accident Reports 2022 · Accident report
Loss of Control on Takeoff in Icing Conditions — Citation 560XL
Cessna Citation 560XL fatal takeoff icing accident, March 2018. Investigation of a Citation 560XL loss-of-control takeoff accident in icing conditions.
- Semantic Scholar 2021 · Article (Aviation)
ANALYSIS OF GENERAL AVIATION FIXED-WING AIRCRAFT ACCIDENTS INVOLVING INFLIGHT LOSS OF CONTROL USING A STATE-BASED APPROACH
Inflight loss of control (LOC-I) is a significant cause of General Aviation (GA) fixed-wing aircraft accidents. The United States National Transportation Safety Board’s database provides a rich source…
- NASA NTRS 2021 · Presentation
Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
Abstract—We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.
- NASA NTRS 2021 · Conference Paper
Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.
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