MIA07LA148 · Bell 206B3
Tiger Aviation Sales Bell 206B3 · Accident: airframe, component or system failure en route
From Oldsmar, FL to Lakeland Linder International Airport (KLAL)
Event
- NTSB case
- MIA07LA148
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Completed
- API-reported fatalities
- 0 · all aircraft and ground
- Ground fatalities
- Unknown
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- General aviation
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Visual Meteorological Cond
Bell 206B3
- Aircraft type
- Bell 206
- Category
- Helicopter
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- N267MW
- Operator
- Tiger Aviation Sales
- Onboard fatalities
- Unknown
- Route
- From Oldsmar, FLTo Lakeland Linder International Airport (KLAL), Lakeland, FL
- Aircraft age
- Not recorded
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 91: General Aviation
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- En route · descent
- First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Airframe, component or system failure
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Substantial
Cause areas
- Company maintenance personnel › Maintenance, replacement, not performed
- Other institution › Maintenance, overhaul, improper
- Other maintenance personnel › Maintenance, replacement, not performed
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
At the start of applying up collective for landing in the Bell 206B3 helicopter, the helicopter began an uncommanded yaw to the right due to failure of the No. 5 tail rotor driveshaft. The helicopter landed hard causing substantial damage to the fuselage structure near the left aft cross tube attach point. The forward fitting of the No.5 tail rotor drive shaft exhibited bond area separation between the splined adapter and the shaft, with subsequent rotation. Cream and green colored adhesives were noted at the seam at the aft edge of the splined adapter, and red colored compound similar to torque paint was noted in the area of the green colored adhesive. Disturbed adhesive and remnants of old clear coat was noted at the seam of the fixed coupling adapter on the aft end of the drive shaft. Disassembly inspection of the No. 5 tail rotor drive shaft driveshaft revealed rotational scoring on the outer surface of the shaft tube and inner surface of the splined adapter at the forward end of driveshaft assembly. In May 1999, the helicopter was involved in a tail rotor sudden stoppage which resulted in damage to at least one tail rotor blade, and tail rotor hub and blades being "…scrapped due to [tail rotor] sudden stoppage." The tail rotor driveshafts were not replaced at that time as required by the maintenance manual, and remained installed until 2004, when they were removed for inspection due to the occurrence in May 1999. The tail rotor drive shafts were inspected and approved for return to service in 2004, by the same facility that had scrapped the tail rotor blades in 1999, which is contrary to the maintenance manual. The driveshafts were reinstalled, and at the time of the accident, the No. 5 tail rotor driveshaft had accumulated 245.8 hours since inspection, and 4,087.4 hours since new. NTSB review of photographs of the tail rotor blades installed in May 1999, revealed evidence of buckling of the skin near the tip of both blades.
Probable cause
The failure of company maintenance personnel to replace the tail rotor drive shafts following tail rotor blade damage in 1999, the failure of maintenance personnel to replace the tail rotor drive shafts in 2004, following their knowledge that the tail rotor blades and hub were scrapped due to tail rotor blade damage, and improper inspection and return to service by an FAA approved repair station for their failure to condemn the tail rotor drive shafts in 2004, all of which resulted in failure of the No. 5 tail rotor drive shaft during approach for landing.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record MIA07LA148
- Event ID
- 20070920X01422
- Case number
- MIA07LA148
- Dataset
- historical-pre2008
- Source SHA-256
- 89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
- The date is the local date, which is the same as the UTC date the NTSB stores.
- API snapshot SHA-256: 11dc155bc942a1abb536a066b73a0bc84d5280d5b1b247d2867698df7bef0dc5; retrieved 2026-09-22T03:27:14.775Z.