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Atlas / NTSB / MIA05CA039

NTSB CAROL · Event

Event MIA05CA039

2004-11-04 Daytona Beach, Florida, United States Airport · 7FL6 None 1 aircraft Status: Completed

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 ↗.