ATL04IA132
2004-06-30 · LaGrange, Georgia, United States · None · 1 aircraft · Status: Completed
Airport LGC
Aircraft involved
Probable cause & findings
The pilot's failure to maintain aircraft control during the landing flare.
Factual narrative
On June 30, 2004, at 1615 eastern daylight time, a Pilatus PC-12-45, N718JP, registered to Pezold Air Charters LLC and operated by Total Flight Systems Inc. wing tip collided with runway 31 during a landing at LaGrange-Callaway Airport, LaGrange, Georgia. The Part 135 flight-check was conducted under the provisions of Title 14 Part 91 with no flight plan filed. Visual meteorological conditions prevailed at the time of the accident. The commercial rated pilot-in-command (PIC) , the Federal Aviation Administration (FAA) check-Airman, and the two passengers were not injured. The flight departed Newnan-Coweta County Airport in Newnan, Georgia, on June 30, 2004 at 1600. According to the FAA check-airman, a simulated engine failure was given to the PIC by retarding the throttle. When the PIC stated that they could not reach the airport, the FAA check-airman returned the engine RPM to the green power range. The PIC continued the approach, and during the landing flare to touchdown on runway 31, the left wheel touched down firmly on the runway followed by the right wheel. As the airplane went through a series of lateral gyrations, the left wing tip collided with the runway. No flight control or mechanical anomalies were reported by the pilot. Examination of the right wing tip revealed scraping on the wing tip skin. According to the FAA check-airman, a simulated engine failure was given to the pilot by retarding the throttle. When the pilot stated that they could not reach the airport, the FAA check-airman returned the engine RPM to the green power range. The pilot continued the approach, and during the landing flare to touchdown on runway 31, the left wing tip collided with the runway. No flight control or mechanical anomalies were reported by the pilot. Examination of the right wing tip revealed scraping on the wing tip skin. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_ATL04IA132.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (engine failure). All research papers
- arXiv 2022 · arXiv preprint Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM) A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum) Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…