Grumman G-164A
NTSB investigations · 434
Matched to the registry by N-number and event date, 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_aircrafts.parquet' a JOIN 'https://openairdocs.org/data/latest/ntsb_case_detail.parquet' c ON c.\"mKey\" = a.case_mkey
WHERE a.aircraft_model_code IN ('3952704')
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_aircrafts.parquet' a JOIN 'https://openairdocs.org/data/latest/ntsb_case_detail.parquet' c ON c."mKey" = a.case_mkey
WHERE a.aircraft_model_code IN ('3952704')
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 CEN25LA160Accident · No injuriesClass 4 · LimitedFinal reportGrumman G164 · Louise, TXThe reported loss of engine power for undetermined reasons.NTSB CEN24LA364Accident · No injuriesClass 4 · LimitedFinal reportGrumman G-164A · LaPlace, LATotal loss of engine power during the agricultural application flight for reasons that could not be determined.NTSB CEN24LA313Accident · No injuriesClass 3 · LimitedFinal reportGrumman G164 · Dyess, ARThe improper overhaul of the carburetor and the malfunction of left magneto which resulted in a partial loss of engine power.NTSB ERA24LA286Accident · No injuriesClass 3 · LimitedFinal reportGrumman G-164A · Toccoa, GAThe pilot’s failure to set the engine speed control fully forward during takeoff, resulting in an engine surge and subsequent loss of control during landing.NTSB CEN23LA317Accident · No injuriesClass 3 · LimitedFinal reportGrumman G-164A · Patoka, ILA partial loss of engine power due to the failure of two compressor turbine blades as a result of the engine operating near or above the engine’s operating limits for an undetermined amount of time beyond the recommended engine’s TBO limit, which led to…NTSB CEN18LA357Accident · No injuriesLimited investigationFinal reportGrumman G164 · Opelousas, LAThe loss of two securing bolts that allowed the left magneto to move around, which disrupted the spark timing and resulted in the engine losing total power.NTSB CEN18LA152Accident · No injuriesLimited investigationFinal reportGrumman G 164A · Garwood, TXA partial loss of engine power for reasons that could not be determined because postaccident examination of the engine did not reveal any anomalies that would have precluded normal operation.NTSB ERA15LA314Accident · No injuriesLimited investigationFinal reportGrumman G164 · Trenton, NCThe pilot's decision to land the airplane with a tailwind and his subsequent application of excessive braking, which resulted in a nose-over.NTSB CEN15LA330Accident · Minor injuriesLimited investigationFinal reportGrumman G-164A · Emmett, KSThe engine failure due to several loose, damaged cylinder stud nuts and hold-down bolts. Contributing to the accident was maintenance personnel’s failure to detect that the cylinder nuts and hold-down bolts were not properly secured during the engine’s most…NTSB CEN15LA204Accident · Minor injuriesLimited investigationFinal reportGrumman G 164A · Maysville, OKThe loss of engine power for reasons that could not be determined because a postaccident examination of the airframe and engine did not reveal any anomalies that would have precluded normal operation.NTSB WPR14LA130Accident · No injuriesLimited investigationFinal reportGrumman G164 - A · Caruthers, CAAn undetected fatigue crack in the landing gear leg, which initiated at an electrical arc-induced damage site of undetermined origin and resulted in landing gear failure. Contributing to the severity of damage to the airplane was the close proximity of an…NTSB CEN13LA533Accident · Minor injuriesLimited investigationFinal reportGrumman G-164A · Atlantic, IAThe pilot’s delay in releasing product to reduce the airplane’s weight and improve its climb performance, which was reduced because of the high density altitude.NTSB CEN13LA443Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Monte Vista, COThe partial loss of engine power due to a fatigue failure of the engine cylinder exhaust rocker housing as a result of an excessively torqued rocker assembly.NTSB CEN12LA491Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Fergus Falls, MNA total loss of engine power due to a cracked No. 2 cylinder head.NTSB CEN12LA458Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Egeland, NDThe partial loss of engine power for reasons that could not be determined during postaccident examinations.NTSB WPR12CA242Accident · No injuriesData collectionFinal reportGrumman G-164A · Riverton, WYThe pilot's loss of directional control during the landing roll and his deliberate application of excessive braking pressure, which resulted in a noseover.NTSB CEN11LA556Accident · No injuriesLimited investigationFinal reportGrumman G-164A · El Campo, TXSeparation of the No. 3 cylinder exhaust valve rocker arm, which resulted in a loss of engine power.NTSB WPR11LA260Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Buttonwillow, CAThe pilot's misjudgment of the landing approach and subsequent long landing and overrun of the runway resulting in a collision with ground obstacles. Contributing to the accident was the pilot's likely fatigue and dehydration.NTSB ERA11LA290Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Albion, NYA bearing failure in the engine’s supercharger section, which resulted in a total loss of engine power during flight. Contributing to the accident was the soft soil of the forced landing site.NTSB WPR09LA373Accident · Minor injuriesLimited investigationFinal reportGrumman G164 · Riverdale, CAThe partial loss of engine power due to the failure of the engine's supercharger-blower.NTSB CHI08CA242Accident · No injuriesData collectionFinal reportSchweizer G-164A · Jefferson, IAThe loss of engine power for an undetermined reason and the unsuitable terrain encountered during the forced landing. The corn crop was a factor.NTSB CHI08CA217Accident · No injuriesData collectionFinal reportGrumman G-164A · Veedersburg, INThe oil filler cap not reinstalled by the pilot prior to the aerial application flight and the total loss of engine oil during an aerial application. Additional causes were the low altitude of the operation and the unsuitable terrain encountered by the pilot…NTSB DFW08CA192Accident · No injuriesData collectionFinal reportGrumman G-164A · Bovina, TXLoss of engine power for undetermined reasons.NTSB NYC08LA245Accident · 1 fatalLimited investigationFinal reportGrumman G-164A · Pelham, GAA partial loss of engine power for undetermined reasons which led to a forced landing in unsuitable terrain.NTSB NYC07LA207Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Goshen, NYA loss of engine power during cruise flight for undetermined reasons.NTSB DFW07CA129Accident · No injuriesData collectionFinal reportGrumman G-164A · Sayre, OKThe partial loss of engine power on takeoff-initial climb for an undetermined reason. A factor associated with the accident was the lack of suitable terrain for a forced landing.NTSB CHI06LA147Accident · Minor injuriesLimited investigationFinal reportAllied Ag Cat Productions G-164A · Gonvick, MNThe aborted takeoff not performed by the pilot. A contributing factor is the reported loss of takeoff performance.NTSB DFW06LA130Accident · 1 fatalLimited investigationFinal reportGrumman G-164A · DeWitt, ARThe failure by both pilots to maintain adequate visual lookout and the Grumman G-164A pilot's impairment caused by the recent use of marijuana.NTSB LAX06CA168Accident · No injuriesData collectionFinal reportGrumman G-164A · Yuba City, CAthe pilot's failure to attain and maintain an adequate airspeed during the takeoff initial climb.NTSB NYC05LA126Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Felton, DEThe mechanic's inadequate annual inspection, and failure to comply with an airworthiness directive, which resulted in a total failure of the second stage turbine rotor.NTSB LAX05LA152Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Yuba City, CAa partial loss of engine power due to multiple cracks in the number 7 cylinder. The reasons for the cracks were not determinedNTSB DFW05CA084Accident · No injuriesData collectionFinal reportGrumman G-164A · Gilbert, LAThe pilot's failure to maintain control of the airplane during landing. A contributing factor was a deflated right main tire.NTSB IAD04LA027Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Chatsworth, NJA blocked internal oil passage, which resulted in inadequate lubrication of the blower impeller shaft, and the subsequent partial loss of engine power.NTSB CHI04CA163Accident · No injuriesData collectionFinal reportGrumman G-164A · Hutchinson, MNThe pilot's failure to maintain airspeed during the low altitude turn after takeoff. A factor to the accident was the low altitude and the swampy terrain condition.NTSB FTW04LA164Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Garwood, TXThe separation of the right main landing gear wheel and axle during take-off. Contributing factors were the fatigue of the bolts on the right main landing gear and the rough and uneven terrain.NTSB CHI03LA132Accident · No injuriesLimited investigationFinal reportGrumman G-164A · North Platte, NEThe pilot's failure to maintain directional control and the collapse of the main landing gear. A factor to the accident was the quartering tailwind.NTSB CHI02LA212Accident · No injuriesLimited investigationFinal reportGrumman G-164 · Central City, NEThe pilot was not able to maintain clearance with the trees when the airplane encountered a downdraft at a low altitude. An additional cause was the pilot's inadequate evaluation of the approaching weather conditions. Factors associated with the accident were…NTSB DEN02LA081Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Two Buttes, COthe failure of the right main landing wheel master brake cylinder and the subsequent inadvertent ground loop during the landing roll by the pilot.NTSB CHI02LA152Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Langdon, NDThe pilot did not maintain directional control while taxiing. A contributing factor was the wind gust condition present at the time of the accident.NTSB FTW01LA209Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Eagle Lake, TXthe partial loss of engine power for an undetermined reason, which resulted in an in flight collision with trees and terrain.NTSB CHI01LA134Accident · No injuriesLimited investigationFinal reportAir Tractor G-164A · Casselton, NDThe pilot's failure to maintain directional control of the airplane while recovering from a bounced landing. A factor was the collapse of the right main landing gear.NTSB ATL00LA087Accident · No injuriesLimited investigationFinal reportGrumman G164A · Dillon, SCA total loss of engine power due to a cracked cylinder head. A factor was the emergency landing into unsuitable terrain, and the subsequent nose over.NTSB LAX00LA261Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Gridley, CAA partial loss of engine power due to the failure of an exhaust valve during an aerial application flight.NTSB NYC00LA144Accident · No injuriesLimited investigationFinal reportGrumman G-164-A · Toms River, NJThe failure of the number 9 cylinder connecting rod, due to a primer leak initiation of a partial hydraulic lock. A factor in the accident was the unsuitable terrain, to which the forced landing had to be made.NTSB LAX00LA199Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Biggs, CAThe broken exhaust valve rocker arm of the number 3 cylinder that resulted in a total loss of engine power during an aerial application flight.NTSB FTW00LA098Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Garwood, TXThe failure of the left magneto, which resulted in the partial loss of engine power during takeoff.NTSB NYC00LA009Accident · Minor injuriesLimited investigationFinal reportGrumman G164 · Burkittsville, MDThe vehicle drivers inadequate lookout.NTSB FTW99LA157Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Monaville, TXThe pilot's failure to touch down on the dry area of the landing strip. A factor was the soft terrain condition on the sides of the grass strip.NTSB FTW98LA410Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Mart, TXThe loss of engine power for an undetermined reason. A factor was the lack of suitable terrain for the forced landing.NTSB SEA98LA140Accident · No injuriesLimited investigationFinal reportGrumman-Schweizer G-164A · Caldwell, IDThe pilot-in-command's misjudgment of clearance with a power line, resulting in a collision with the line. Factors included a power line and dark night light conditions in the spray area.
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