NTSB CAROL · Event
Event ATL04CA145
Aircraft involved
Probable cause & findings
The pilot's failure to follow the checklist and lower the landing gear prior to landing.
Factual narrative
On July 8th, 2004, at 1045 eastern daylight time, a Cessna 172 RG, N6321R, registered to and operated by Delta Flight Connection, landed wheels-up at Fernandina Beach Municipal Airport, Fernandina Beach, Florida. The airplane was being flown by the pilot during a Commercial Single Engine check ride under the provisions of Title 14, CFR Part 91, when the accident occurred. The private pilot and check-airman were not injured. Visual meteorological conditions prevailed and no flight plan was filed for the local flight. The airplane sustained substantial damage. The flight originated from Fernandina Beach, Florida at 0930. According to the check airman, he initiated single engine failure by pulling the carburator heat out and reducing the throttle to idle. The applicant performed the emergency items and called "gear down", "flaps down" and "something like 1st landing configuration complete". On short final, the check airman stated that he called out certain final items as a safety reminder such as gear down, mixture rich, props forward, cleared to land. " I can not recall if he acknowledged/double-checked these items." According to the Pilot in Command, "while I was plotting my course to make sure that was going to make the runway I was calling out the items on the checklist. I was trying to take the first half of the runway and I was high on the approach. I was trying to concentrate on getting down before the point that he (check airman) pointed out. I finally was getting done and I had my point made until we heard a horrendous noise which was the prop hitting the pavement." Examination of the airplane revealed engine and propeller damage, firewall damage, underbelly of fuselage damage as well as front doors and skin being cracked and buckled. The landing gear, all three wheels, was still in the wheel well. The subsequent functional test of the landing gear system failed to disclose a mechanical problem. The functional test also determined that the landing gear warning horn was properly working. According to the pilot, "while I was plotting my course to make sure that [I] was going to make the runway I was calling out the items on the checklist. I was trying to take the first half of the runway and I was high on the approach. I was trying to concentrate on getting down before the point that he (check airman) pointed out. I finally was getting [down] and I had my point made until we heard a horrendous noise which was the prop hitting the pavement." Examination of the airplane revealed engine and propeller damage, firewall damage, underbelly fuselage damage as well as front doors and skin being cracked and buckled. The landing gear system, all three wheels, were still in the wheel wells. The subsequent functional test of the landing gear system failed to disclose a mechanical problem. The functional test also determined that the landing gear warning horn was operational. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_ATL04CA145.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 (engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- 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…
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