MIA97LA103 · Hughes TH-55
Hughes TH-55 · Accident: loss of engine power while maneuvering
From 3A1 to an unrecorded destination
Event
- NTSB case
- MIA97LA103
- 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 TH-55
- Aircraft type
- Hughes TH-55
- 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
- N818D
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From 3A1To 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
- Maneuvering
- 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
- Loss of engine power
- 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
- Pilot in command(cfi) › Aircraft control, not maintained
- Reason for occurrence undetermined
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The flight instructor and student pilot remained in closed traffic in order to perform practice maneuvers and emergency procedure training to include autorotations. Witnesses saw the helicopter take off to the west and turn immediately to the right, climb to an altitude of 30 feet above ground level (AGL), and attain an estimated forward airspeed of 20 to 30 knots. The helicopter was then observed in a descent and disappear out of view before the witnesses heard the sound of impact with the ground. Several of the witnesses stated that just prior to impact they heard what sounded like the engine overspeed, and then cut off. The helicopter landed near a telephone pole and support lines. There was no evidence found to indicate that the helicopter contacted the pole or the lines. According to the first people to arrive at the crash site, the student pilot did not know what had happened. The CFI said, 'we had been flying for about an hour. We'd finished our training and were heading back with...[the student] on the controls, when the engine quit. I said I've got it and took the controls, but we were too low, with no time to recover, and crashed.' Examination of the wreckage revealed that the main and tail rotor RPM was low at impact,' because the rotor blades showed little damage. In addition, the engine and airframe examinations revealed no discrepancies. Several attempts were made to talk to the CFI at the hospital to get his factual account of the accident, but all attempts to interview him were unsuccessful. The NTSB Form 6120.1/2, was returned without a statement from the CFI.
Probable cause
a loss of engine power for undetermined reasons and the pilot-in-command's failure to maintain control of the helicopter. Factors in this accident were: an improper autorotation as a result of improper collective use and resulting failure to maintain main rotor rpm.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record MIA97LA103
- Event ID
- 20001208X07601
- Case number
- MIA97LA103
- 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: 5deaf2106ec454b56e9038ceba47fc00fa44c5d8f6e7d0ac6695faa4a5e2e72d; retrieved 2026-09-21T12:12:06.780Z.