NTSB investigations: Hiller UH-12E
415 cases on aircraft the registry lists as Hiller UH-12E. 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, newest first
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.aircraft_model_code IN ('4360122', '4360137'))
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.
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.aircraft_model_code IN ('4360122', '4360137'))
ORDER BY c."eventDate" DESC, c."ntsbNumber" DESCRun it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
NTSB CHI92DCD09Accident · No injuriesFinal reportHiller Hiller UH-12E · Dows, IAContaminated fuel resulting in a loss of engine power.NTSB LAX92LA349Accident · Minor injuriesLimited investigationFinal reportHiller UH12-E, Saloy Conver · Arvin, CAThe failure of the tension torsion bar pin due to fatigue. Contributing to this accident was that it was not possible for the pilot to flare the helicopter on landing.NTSB CHI92DCD04Accident · No injuriesFinal reportHiller UH-12E · Milford, IAA total loss of engine power for an undetermined reason as the helicopter was performing aerial application maneuvers.NTSB LAX92LA152Accident · No injuriesLimited investigationFinal reportHiller UH-12E · Watsonville, CAA failure of the pilot to conduct an adequate pre-flight inspection of the aircraft to ensure that the fuel supply was free of contaminates. Contributing to this accident was fuel contamination.NTSB LAX92LA146Accident · No injuriesLimited investigationFinal reportHiller UH-12E · Huron, CAA separation of the control rotor cuff due to fatigue.NTSB FTW92LA007Accident · No injuriesLimited investigationFinal reportHiller UH-12E · Palacios, TXThe pilot's inadequate preflight.NTSB SEA91TL#02Accident · No injuriesClass 3Final reportHiller-Soloy UH-12E · Vernal, UTNTSB CHI91LA245Accident · Serious injuriesLimited investigationFinal reportHiller 1345 · Michigan City, INFuel exhaustion due the pilot's delay in refueling. Factors related to the accident were pressure induced by others (passenger), and the absence of suitable terrain.NTSB LAX91LA249Accident · No injuriesLimited investigationFinal reportHiller UH-12E · Huron, CAThat unknown pilot(s) impoperly used the throttle control which caused an overspeed condition. Contributing to this accident was the connecting rod bolt fatigue failure.NTSB LAX91LA191Accident · No injuriesLimited investigationFinal reportHiller UH-12E · Delano, CAThat the pilot improperly performed the autorotation by misjudging the flare altitude. Contributing to this accident was the total failure of the freewheeling sprag clutch due to excessive wear and the soft dirt terrain.NTSB LAX90DVA08Accident · Minor injuriesFinal reportHiller UH-12-E · Los Banos, CAThe pilot's failure to maintain a lookout for obstructions along his swath run.NTSB CHI90DTG02Accident · No injuriesFinal reportHiller UH-12-E · Garrison, NDThe failure of the helicopter tail rotor control cable. A factor related to the accident was the chafing of the tail rotor control cable.NTSB SEA90LA025Accident · No injuriesLimited investigationFinal reportHiller UH-12E · Raymond, WALoss of engine power due to fatigue failure of the impeller. The helicopter was substantially damaged as a result of a roll-over on uneven terrain.NTSB 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.NTSB 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.NTSB CHI89DEM09Accident · Minor injuriesFinal reportHiller UH-12E · Hudsonville, MIThe fatigue failure of one of the tension-torsion pins.NTSB LAX89DUJ09Accident · Minor injuriesFinal reportHiller UH-12E · Tolleson, AZAn engine failure due to water contamination in the fuel supply which preceded an autorotation and collision with the ground during night time conditions.NTSB CHI89DEP04Accident · No injuriesFinal reportHiller UH-12E · Waterford, WIThe pilot's inability to maintain control during an autorotational landing attempt following the failure of the main rotor drive train torsional coupling.NTSB DEN89DTM02Accident · Serious injuriesFinal reportHiller UH-12E · Mack, COThe pilot's failure to maintain proper altitude during a swath run.NTSB LAX89DVM02Accident · Minor injuriesFinal reportHiller UH-12E · Salinas, CAThe separation of the torsion coupling in the main rotor drive system.NTSB DEN89LA084Accident · No injuriesLimited investigationFinal reportHiller UH-12E · Golden, COImproper in-flight planning/decision by the CFI which resulted in loss of tail rotor effectiveness and loss of directional control. Contributing factors were high density altitude, tailwind, and rough/uneven terrain.NTSB LAX88DVA16Accident · Minor injuriesFinal reportHiller UH-12E · Helm, CADuring an aerial application flight, the pilot lost control of the helicopter just after liftoff and collided with the terrain. Inspection of the wreckage revealed that the chemical trucks filler hose was still attached to the helicopter when it lifted off.NTSB LAX88DUG06Accident · Minor injuriesFinal reportHiller UH-12E · Thermal, CAShortly after refueling the helicopter & reloading the hopper, the plt took off & was starting to spray a field when the eng suddenly lost power. The plt said the helicopter was dscndg from about 30 ft when the power loss occurred; thus, he barely had time to…NTSB NYC88DGM01Accident · 1 fatalFinal reportHiller UH-12E · Lovely, PAThe undetermined loss of engine power while performing low level aerial application operations.NTSB LAX88DUM06Accident · No injuriesFinal reportHiller UH12E · Bard, CADuring helicopter aerial application, engine power was lost. Plt applied back cyclic and tail rotor contacted terrain, followed by hard landing. Investigation revealed less than useable fuel remaining.NTSB CHI88DER06Accident · No injuriesFinal reportHiller UH-12E · Buffalo Lake, MNWhen the helicopter lifted off, the left tail rotor cable separated. Directional control was lost and the aircraft collided with the terrain. The pilot reported no injuries, however the helicopter sustained substantial damage. An inspection of the left tail…NTSB MIA88LA225Accident · No injuriesLimited investigationFinal reportHiller UH-12E · Clewiston, FLThe plt stated the fuel gages indicated 20 gals when he took off on spraying flt. He had just completed the spray run & started to pull up from about 10 ft & 25 mph. At that time the eng quit '& sounded just like it would if it ran out of gas'. There was not…NTSB NYC88DFJ02Accident · Minor injuriesFinal reportHiller UH-12E · Cherry Creek, NYThe pilot reported that during an aerial application operation, he heard a noise that was followed by a decay in rotor RPM. Subsequently, he was forced to land in an area of tall trees & the helicopter was damaged. An investigationrevealed that a connecting…NTSB 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…NTSB LAX88DVA05Accident · No injuriesFinal reportHiller 12E · Firebaugh, CADuring an aerial application, the helicopter collided with a guy wire and then a field. The pilot knew that the wire was there. He stated that he simply forgot that it was there and did not see it. There were no mechanical problems prior to the accident.NTSB FTW88DRA05Accident · No injuriesFinal reportHiller UH-12E · La Salle, TXAcft was substantially damaged during an emergency autorotation following an engine failure while the acft was completing an aerial application maneuver. Acft touched down tail low and the main rotor blades flexed down and cut off the tail boom. Investigation…NTSB FTW88DRA03Accident · Serious injuriesFinal reportHiller UH-12-D · Bon-Wier, TXGround crewmember's failure to follow established procedures for secureing the aircraft to the transport trailer.NTSB DEN88LA046Accident · No injuriesLimited investigationFinal reportHiller UH-12E · Vernal, UTThe commercial plt and two passengers were surveying a road route in mountainous terrain. At cruise, the pilot noticed a drop in manifold pressure, followed by a loss of oil pressure. The plt reported that the engine quit. An autorotation to a snow covered…NTSB MIA88LA014Accident · Minor injuriesLimited investigationFinal reportHiller UH-12E · Union Church, MSAt an altitude of aprx 75 feet during an agricultural turn, the plt reported that the engine lost power. While executing a forced landing, the rotor blades contacted trees, after which, during the descent, the right skid collided with a stump & the helicopter…NTSB LAX87DUJ11Accident · Minor injuriesFinal reportHiller UH-12E · Scottsdale, AZDuring an aerial application flight, the plt made a turn-around & was starting to make another swath run when he heard a loud 'bang' & then the helicopter collided with terrain. An inspn of the main rotor head & pin revealed the hub had failed from hi cycle…NTSB MKC87LA145Accident · Minor injuriesLimited investigationFinal reportHiller 12E · Ulysess, KSDuring a helicopter aerial application operation, acft suffered a main rotor system hub failure. PIC was unable to control the acft and an uncontrolled descent resulted. Acft struck the terrain and was substantially damaged and the PIC suffered minor…NTSB DEN87LA157Accident · No injuriesLimited investigationFinal reportHiller UH-12E · Ray, NDThe plt reports that he was departing from an aerial app operating area. He said there was a tree line along a road with an opening and the takeoff was made toward the opening. There were wires across the opening and the poles were obscured by the trees on…NTSB DEN87LA146Accident · No injuriesLimited investigationFinal reportHiller UH-12E · Grafton, NDThe plt was positioning the helicopter for an aerial application project. Before taking off, he checked the fuel quantity indicator & estimated there was 30 min of fuel on board. The proposed flt was estimated to take 10 min. During flt, the eng lost power &…NTSB SEA87FA106Accident · 1 fatalField investigationFinal reportHiller UH-12E · Shelton, WAThe pilot was properly certificated for the flight; however, due to operator insurance restrictions, all prior commercial flights had required the owner/operator to accompany this pilot, therefore this was the pilot's first commercial flight as sole pilot.…NTSB LAX87DUJ05Accident · No injuriesFinal reportHiller UH-12E · Tolleson, AZThe plt stated that he landed the acft on a platform on top of a chemical tank truck. The truck was parked on a slight slope with its left side six inches lower than the right. The plt reduced power to idle and the loader began to load the helicopter with…NTSB CHI87DER03Accident · No injuriesFinal reportHiller UH-12ET · Big Lake, MNAircraft was being maneuvered for landing on a ground support trailer when it experienced a power failure. Due to high trees autorotation was made to adjacent field. Aircraft landed on rough/uneven terrain and rolled over. Investigation revealed contaminated…NTSB LAX86FVA14Accident · Minor injuriesFinal reportHiller UH-12E · Lemoore, CAThe plt reptd that while returning to the loading area after spraying a field, he heard a loud pop emanating from the engine compartment. Shortly thereafter he observed a fire in the engine compartment and lost forward and aft control of the helicopter. The…NTSB FTW86LA167Accident · No injuriesLimited investigationFinal reportHiller UH-12E · Norias, TXThe commercial plt was engaged in a livestock round-up and attempted to hover over a wire fence. The acft skid caught on the fence causing a loss of acft control and subsequent impact with the terrain.NTSB LAX86FVM08Accident · No injuriesFinal reportHiller UH 12E · Gonzales, CAA loss of power was expereinced as the acft descended into a field at the beginning of an aerial application spray run. The plt initiated a forced landing into the field. During the landing the right skid dug into the field, tipping the helicopter onto its…NTSB 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…NTSB ATL86FEK03Accident · No injuriesFinal reportHiller UH-12E · Pataskala, OHThe acft autorotated to a forced landing after the eng quit at 600 ft AGL. The landing was made in a corn field. The plt told a FAA inspector at the scene that he had 8 gals of fuel remaining. When the fuel tank was drained it contained aprx 6 oz total. The…NTSB LAX86DVA09Accident · No injuriesFinal reportHiller UH-12E · Delano, CAThe helicopter rotor blade delaminated shortly after departing the operator's north base at Delano, CA. The investigation determined the blade contained extensive voids on the bond line. The blade was rejected by the manufacturer as being unairworthy. The…NTSB LAX86FVM05Accident · Minor injuriesFinal reportHiller UH12E · Castroville, CAThe acft landed hard and rolled over after the lndg skid failed in a forced lndg. The plt said he was crusing at 500 ft AGL over an open field when he heard a loud bang. The helicopter began to vibrate severely and spiral to the right. The plt lost ground…NTSB LAX86LA113Accident · No injuriesLimited investigationFinal reportHiller UH-12E · Lodi, CAWhile on an aerial agricultural spraying flight the acft engine lost total power. The plt executed an immediate autorotation landing. Upon ground contact, the acft skid for about 8 ft until the front skid contacted the ground furrow and nosed over causing the…NTSB SEA86FA039Accident · 1 fatalField investigationFinal reportHiller-Soloy UH-12E · Horton, ORThe fork connecting the rotorcraft's blue blade to the main rotor hub separated after a long term fatigue crack had spread through more than 60% of the fork circumference. The operator failed to carry out the appropriate inspection of the fork unit as…