MIA05CA072
2005-03-06 · Opa Locka, Florida, United States · None · 1 aircraft · Status: Completed
Airport OPF
N21427 has since been reassigned. It is now registered to a different aircraft (AIR CREATION TRIKE TWIN, built 1998), which was not involved in this event.
Aircraft involved
Probable cause & findings
The dual student's improper descent rate during a simulated engine failure and simulated forced landing and the CFI's inadequate remedial action which resulted in a hard landing.
Factual narrative
On March 6, 2005, about 1730 eastern standard time, a Piper PA-44-180, N21427, registered to and operated by Delta Connection Academy Inc., as a Title 14 CFR Part 91 instructional flight, had a hard landing at the Opa Locka Airport, Opa Locka, Florida. Visual meteorological conditions prevailed and no flight plan was filed. The commercial-rated pilot-in-command/certified flight instructor (CFI) and the commercial-rated dual student reported no injuries, and the airplane incurred substantial damage. The flight originated from North Perry Airport, Pembroke Pines, Florida, earlier that day, about 1600. The CFI stated they were conducting instrument approaches and landings at Opa Locka Airport. During a takeoff, he gave his student the indication of a simulated engine failure, the student then retarded the throttles and initiated a descent to land. While on descent, the CFI and dual student noticed a higher than normal descent rate and both corrected by adding back pressure on the control column and adding engine power. After touchdown the instructor heard an abnormal noise and decided to taxi to the ramp. Once the airplane was secure, the CFI conducted an inspection and found damage to the fuselage and terminated the flight. The pilots stated there were no mechanical failures or malfunctions to the airplane or any of its systems prior to the accident. The CFI stated they were conducting instrument approaches and landings at Opa Locka Airport. During a takeoff, he gave his student the indication of a simulated engine failure, the student then retarded the throttles and initiated a descent to land. While on descent, the CFI and dual student noticed a higher than normal descent rate and both corrected by adding back pressure on the control column and adding engine power. After touchdown the instructor heard an abnormal noise and decided to taxi to the ramp. Once the airplane was secure, the CFI conducted an inspection and found damage to the fuselage and terminated the flight. The pilots stated there were no mechanical failures or malfunctions to the airplane or any of its systems prior to the accident. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_MIA05CA072.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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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…