# Accident 19890802026729A: Beech A24R, Sarasota - Brad, FL, August 2, 1989

- Type: FAA accident report (Accident/Incident Data System), as reported
- Date: August 2, 1989, 13:50 local time
- Place: Sarasota - Brad, FL
- Airport: Sarasota-Bradenton
- Damage: Destroyed
- Phase of flight: Forced/Precautionary Landing
- Operating rules: General operating rules (Part 91)
- Location: 27.3998° N, 82.5309° W: From the FAA, an estimate near the named town, within about 3 miles
- Nearby events: https://openairdocs.org/map.md?lat=27.3998&lon=-82.5309&mi=10
- Aircraft: N24586, a cancelled registration (https://openairdocs.org/deregistered/N24586-2013-04-15) (OpenAirDocs)
- Registry model: Beech A24R (registry code 1151252, https://openairdocs.org/model/beech-a24r) (OpenAirDocs)
- Registry engine: Lycoming I0360 series (registry code 41515, https://openairdocs.org/engine/lycoming-i0360-series) (OpenAirDocs)
- Reported make and model: BEECH A24R
- Reported engine: LYC IO360A1B
- People aboard: 2
- Fatal injuries: 2
- Pilot flight hours: 3,200 total, 1 in this make and model, 150 in the last 90 days
- NTSB investigation: [NTSB MIA89FA210](https://openairdocs.org/ntsb/MIA89FA210) (OpenAirDocs)
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/19890802026729A

## Narrative

As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^.

PROPELLER HUB AND BLADES SEPARATED FROM ENGINE ON CLIMBOUT. TRIED TO TURN BACK,STALLED,CRASHED IN RESIDENTIAL AREA.

## The NTSB's investigation of this event (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB MIA89FA210](https://openairdocs.org/ntsb/MIA89FA210), Aug 2, 1989: Beech A24R (N24586), Sarasota, FL, destroyed, 2 fatal. Probable cause: FAILURE OF THE PROPELLER HUB DUE TO PREVIOUS DAMAGE, WHICH RESULTED IN SUBSEQUENT FATIGUE FAILURE OF THE HUB; AND FAILURE OF THE PILOT TO MAINTAIN FLYING SPEED, WHICH RESULTED IN A STALL AND…

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. For accidents, the NTSB's own investigation is the fuller record.

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