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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 ↗.

Related research

Matched on aircraft type or causal vocabulary (engine failure). All research papers