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MIA82DA028 · Smith WCS-222 (BELL 47G) WCS-222 (B

2 Jan 1982 · Miami, FL, United States

Smith WCS-222 (BELL 47G) WCS-222 (B · Accident: total loss of engine power (mechanical failure) en route

From Miami, FL to Miami, FL

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Event

NTSB case
MIA82DA028
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

Smith WCS-222 (BELL 47G) WCS-222 (B

Aircraft type
Smith WCS-222
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
N23BS
Onboard fatalities
Unknown
Route
From Miami, FLTo Miami, 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 · 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
Total loss of engine power (mechanical 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

  • Engine assembly, connecting rod › Failure, total

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

DURING FLIGHT, THE ENGINE LOST POWER AND FIRE ERUPTED ON THE ENGINE COMPARTMENT. SUBSEQUENTLY, THE ENGINE DRIVEN HYDRAULIC BOOST FOR THE FLIGHT CONTROL SYSTEM BECAME INOPERATIVE. THE PILOT WAS FLYING OVER A POPULATED AREA. DURING HIS FORCED LANDING, HE WAS FORCED TO DIVERT TO A SECOND LANDING SITE WITH A CROSSWIND TO AVOID PERSONNEL AND OBSTRUCTIONS. THE WIND WAS GUSTING TO 12 KNOTS. DURING TOUCHDOWN, THE MAIN ROTOR BLADES FLEXED DOWNWARD AND SEVERED THE TAIL BOOM. THE ENGINE COMPARTMENT FIRE WAS STILL BURNING IN THE VICINITY OF THE AIR CLEANER, BUT WAS EXTINGUISHED WITHOUT FURTHER DAMAGE TO THE AIRCRAFT. AN INVESTIGATION REVEALED THAT A CONNECTING ROD ASSEMBLY HAD FAILED.

Verbatim NTSB analysis from the NTSB dataset

Sources

NTSB record MIA82DA028
Event ID
20020917X02339
Case number
MIA82DA028
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: e42b5b76a6d5e2464074079af41086661bbeb8b541a1abdd0adf1541c62520d4; retrieved 2026-09-24T03:49:19.572Z.