MIA00TA200 · Hughes 369D
Hughes 369D · Accident: airframe, component or system failure en route
From PFN · Panama City, FL to an unrecorded destination
Event
- NTSB case
- MIA00TA200
- 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
- 0
- 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
Hughes 369D
- Aircraft type
- Hughes 369
- 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
- N88MP
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From PFN · Panama City, FLTo not recorded
- 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 · cruise
- 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
- Other maintenance personnel › Maintenance, inspection, improper
- Pilot in command › Aircraft preflight, improper
Approximate · Estimated position: the centre of Destin, FL, the place the record names. Not the accident site.
NTSB narrative
The pilot said he had been flying the helicopter at an altitude of about 500 feet, 100 knots indicated airspeed, and 65 to 70 pounds per square inch torque, when he felt a high frequency vibration through the antitorque pedals. He said the vibration dissipated but soon began again, and became excessive with 'strong' forces in the pedals. The forces were soon followed by a loud 'bang' and the aircraft yawed violently to the right, and the nose pitched down. He said the antitorque pedals had no effect, so he lowered the collective control and applied aft cyclic control input to the stop the yaw, and level the aircraft. He said the yaw rate slowed, but did not stop, and at about 70 to 80 degrees of right yaw, he reduced the throttle in an attempt to further reduce/control the yaw condition, and the aircraft yaw stopped. He was then able to execute an autorotative landing to an open field. The on scene examination of the aircraft showed that the stabilizer, as well as an 18-inch section of the hollow portion of the tail had separated from the aircraft in flight. The 90-degree gearbox also partially separated from the aircraft, and was only held by one remaining bolt, and there were contact marks and paint transfer signatures, consistent with those from multiple tail rotor blade strikes at the fracture point. The aft 6 inches of the tailboom with attach points, tail rotor gearbox, and tail rotor assembly were retained for metallurgical examination. The examination revealed that the fractured tail rotor gearbox studs were fatigue failures. In addition, both elastomer bearings in the tail rotor drive fork were examined, and were found to have failed due to fatigue.
Probable cause
improper maintenance inspection of the tail rotor by maintenance personnel and improper preflight inspection of the tail rotor by the pilot, which resulted in worn elastomeric bearings being continued in service, resulting in failure of the tail rotor assembly, and damage to the helicopter during a hard landing.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record MIA00TA200
- Event ID
- 20001212X21557
- Case number
- MIA00TA200
- 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: 2e6ef9f29c5b7d39dfef4cd4b20805f2384d88b508fdde839dc1bf577759badb; retrieved 2026-09-22T12:44:46.880Z.