NTSB investigations: Lycoming VO-540 series

11 cases on aircraft whose registry engine model is Lycoming VO-540 series, where the first occurrence was “Loss of engine power(total) - mech failure/malf”. Aircraft are matched to the registry by N-number and event date, checked against the reported serial number, make and model, so older matches can be wrong.

Cases per year

19822026
NTSB investigations: Lycoming VO-540 series per year, 1982–2026: 11 cases
19821
19831
19851
19861
19871
19881
19892
19901
19941
20021

Latest cases

Query with SQL
duckdb -csv -c "SELECT c.\"ntsbNumber\", c.\"eventDate\", c.\"eventType\", c.\"eventCity\", c.\"eventStateOrRegion\", a.n_number, a.\"aircraftMake\", a.\"aircraftModel\", c.\"highestInjuryLevel\", c.\"totalFatal\", c.\"completionStatus\", c.report_url
  FROM 'https://openairdocs.org/data/latest/ntsb_case_detail.parquet' c LEFT JOIN 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' a ON a.case_mkey = c.\"mKey\" AND a.position = 1
  WHERE c.\"mKey\" IN (SELECT x.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' x WHERE x.engine_model_code IN ('41534', '41582')
      AND EXISTS (SELECT 1 FROM 'https://openairdocs.org/data/latest/ntsb_occurrences.parquet' o WHERE o.case_mkey = x.case_mkey AND o.aircrafts_position = x.position AND o.\"occurrenceNumber\" = 1 AND o.\"occurrenceCode\" = 351))
  ORDER BY c.\"eventDate\" DESC, c.\"ntsbNumber\" DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

NTSB SEA02LA073Accident · No injuriesLimited investigationFinal reportHiller UH-12E · Goshen, ORThe failure of company maintenance personnel to identify and replace/repair the degraded exhaust stack. Contributing factors were the mis-rigged carburetor heat control and the pilot's failure to maintain appropriate rotor RPM. Additional contributing factors…Apr 22, 2002 · N3004T · Substantial damageNTSB FTW94LA210Accident · No injuriesLimited investigationFinal reportHiller UH-12L4 · West Helena, ARA total loss of power due to a leak in the main fuel line which occurred as a result of an electrical short which burned a hole in the fuel line. Factors were a failure by the pilot to perform recommended maintenance and the lack of suitable terrain for a…Jun 22, 1994 · N90453 · DestroyedNTSB ATL90LA138Accident · Minor injuriesLimited investigationFinal reportBell BH-47G · Seagrove, NCFailure of a number four connecting rod bolt for an undetermined reason.Jun 28, 1990 · N3081G · Substantial damageNTSB LAX90DVA01Accident · Serious injuriesFinal reportHiller 12E · Huron, CAThe pilot failed to properly preflight the airplane before departing on the accident flight and misjudged the flare during the ensuing autorotation. Factors relating to this accident were oil starvation and total failure of the connecting rod.Oct 16, 1989 · N4026G · Substantial damageNTSB LAX90DUJ03Accident · Serious injuriesFinal reportHiller UH-12E · Yuma, AZThe pilot misjudged the flare altitude. Contributing to this accident was the failure of the engine torsional coupling which ultimately caused the total loss of power.Oct 11, 1989 · N689SB · Substantial damageNTSB MIA88LA183Accident · No injuriesLimited investigationFinal reportHiller UH-12E · Gretna, FLWhile on an aerial application flt, the plt stated he maneuvered the helicopter to release the remaining chemical. He then heard a loud 'screeching' noise followed by silence as the eng quit. The helicopter landed hard breaking the skids. It came to rest on…Jun 1, 1988 · N4029R · Substantial damageNTSB LAX87DVD01Accident · Serious injuriesFinal reportBell 47G4A · Stockton, CAJust after takeoff, the engine experienced a power loss while transporting agricultural equipment. A fractographic examination of the failed fuel disconnect fitting by anamet laboratories, concluded that approximately 70% of the retaining ring on the fuel…Feb 2, 1987 · N28938 · Substantial damageNTSB LAX86FVM06Accident · No injuriesFinal reportHiller UH21E · Salinas, CAThe plt experienced a 'ratcheting' to the right and a decrease in rotor RPM during cruise flt at 75-100 ft AGL. The plt made an autorotation but could not cushion the landing due to the low alt and lack of rotor RPM. The helicopter impacted hard and…Aug 12, 1986 · N169HA · Substantial damageNTSB LAX85FA132Accident · Minor injuriesField investigationFinal reportHiller UH12E · Five Points, CAWhile performing an ag flight the helicopter's engin suddenly lost power. At the time the aircraft was near its max allowable gross weight and it was between 3-5FT AGL. As the aircraft yawed left and descended. The pilot in command attempted to land on a…Feb 3, 1985 · N5323V · Substantial damageNTSB ATL83LA160Accident · No injuriesLimited investigationFinal reportBell 47G-4A · Charleston, WVDuring an approach to land, the engine lost power at aprx 500 ft AGL. The plt reported that during an autorotative landing, he had to maneuver to avoid trees & a ridge in order to land in a suitable area. During this time, rotor RPM dropped & a crash landing…Apr 13, 1983 · N4749R · Substantial damageNTSB LAX82FA245Accident · No injuriesField investigationFinal reportHiller UH-12L3 · Stockton, CAThe pilot reported that the engine lost power at about 5 ft AGL as he was taking off from a trailer. He turned to avoid a gas and water tank near the poll truck. The helicopter came to rest, right-side-up, but was damaged. A fuel leak was found in a line that…Jul 1, 1982 · N86689 · Substantial damage