NTSB CAROL · Event
Event MIA05CA039
Registry · N7188N
FAA Aircraft Registry record.
Make / Model
ROBINSON HELICOPTER R22 BETA
Year of manufacture
2000 · 4 years old at event
TCDS
H10WE · ROBINSON HELICOPTER CO
Engine
LYCOMING 0-360-C1F (200 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20000615
ADS-B equipped
Yes — Mode-S A99D42
Registrant of record
TURN AND CLIMB AVIATION CO
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The improper landing flare by an unknown pilot at an unknown time resulting in a hard landing and substantial damage to the helicopters tailcone.
Factual narrative
On November 4, 2004, about 0900 eastern standard time, a Robinson R-22, N7188N, registered to Brentone LTD and operated by Lunsford Air Inc, as a Title 14 CFR Part 91 instructional flight, had substantial damage discovered during a preflight inspection at Spruce Creek Airport, Daytona Beach, Florida. Visual meteorological conditions prevailed and no flight plan was filed. The flight was originating at the time of the accident. During a preflight inspection, damage was discovered to the tailcone assembly of the helicopter. Upon further examination and consulting with the manufacturer of the helicopter by the operator, it was determined that a major repair was required to return the helicopter to airworthiness condition. The forward bulkhead, forward bulkhead skin, and doublers for that area of the tailcone had to be replaced. The questionnaire submitted to the manufacturer by the operator to aid in assessing the type of repair required stated, "damage was sustained during a hovering autorotation." On December 3, 2004, an inspector from the FAA notified the NTSB of the damage. On December 8, 2004 a completed Pilot/Operator Aircraft Accident Report was provided by the instructor pilot, who flew the helicopter the day before the damage was discovered. He stated he had not seen the damage and does not know when or how it occurred. He only assumes the cause was from a hard set down during a practice hovering autorotation. During a preflight inspection damage was discovered to the tailcone assembly of the helicopter. Upon further examination and consulting with the manufacture of the helicopter, by the operator, it was determined that a major repair was required to return the helicopter to airworthiness condition. The forward bulkhead, forward bulkhead skin, and doublers for that area of the tailcone had to be replaced. On the questionnaire submitted to the manufacture by the operator to aid in assessing the type of repair required stated "damage was sustained during a hovering autorotation." On December 3, 2004, an inspector from the FAA notified the NTSB of the damage. On December 8, 2004 a completed Pilot/Operator Aircraft Accident Report was provide by the instructor pilot who flew the helicopter the day before the damage was discovered. He stated he had not seen the damage and does not know when or how it occurred. He only assumes the cause was from a hard set down during a practice hovering autorotation. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_MIA05CA039.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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