NTSB investigations, WA

33 cases where the first occurrence was “Loss of engine power(partial) - mech failure/malf”.

Cases per year

19822026
NTSB investigations, WA per year, 1982–2026: 33 cases
19822
19833
19843
19851
19864
19871
19882
19893
19901
19911
19933
19943
19971
20033
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20051

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.\"eventStateOrRegion\" = 'WA' AND c.\"eventCountry\" = 'USA'
    AND c.\"mKey\" IN (SELECT o.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_occurrences.parquet' o WHERE o.\"occurrenceNumber\" = 1 AND o.\"occurrenceCode\" = 352)
  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 SEA05LA138Accident · No injuriesLimited investigationFinal reportBell 47G-2A · Oroville, WAThe failure of the throttle cable housing, which permitted the engine's RPM to decay to the idle position. Contributing factors were the trees and the lack of suitable terrain for a forced landing.Jul 5, 2005 · N38926 · Substantial damageNTSB SEA04LA064Accident · No injuriesLimited investigationFinal reportGrumman G-44 · Belliigham, WAThe failure of the pilot to select the proper touchdown point while conducting a forced landing. Factors included the #1 engine malfunction, the right propeller oil control valve leak, and the shallow subsurface terrain condition.Apr 2, 2004 · N65914 · Substantial damageNTSB SEA03LA156Accident · No injuriesLimited investigationFinal reportHughes 269C · Marblemount, WAThe partial failure of a magneto during hover taxi over water, leading to a forced landing in shallow water near the shoreline. Factors include the aircraft being over a lake at the time that the partial loss of power made it impossible to keep it airborne.Jul 25, 2003 · N500HS · Substantial damageNTSB SEA03LA076Accident · No injuriesLimited investigationFinal reportFokker F27MK 600 · Port Townsend, WAThe failure of the accessory drive shaft due to deterioration of bearing number 1 in the aft fork of the universal joint for undetermined reasons during cruise flight.Apr 17, 2003 · N730FE · Substantial damageNTSB SEA03FA026Accident · No injuriesField investigationFinal reportCessna 172K · Gig Harbor, WAThe loss of engine power in the climb due to the fracture of the number seven engine crankshaft cheek due to the propagation of a fatigue crack initiation point. Factors include a vehicle pulling onto the road that the pilot selected for his forced emergency…Jan 14, 2003 · N1909V · Substantial damageNTSB SEA97LA186Accident · No injuriesLimited investigationFinal reportCessna 172M · Langley, WAA failed exhaust valve. Factors were tailwind and excessive airspeed during the ensuing forced landing. .Aug 5, 1997 · N73158 · Substantial damageNTSB SEA94LA242Accident · Minor injuriesLimited investigationFinal reportCessna P206D · Lopez, WAA worn throttle control lever.Sep 18, 1994 · N8761Z · Substantial damageNTSB SEA94LA143Accident · No injuriesLimited investigationFinal reportWray KR-2 · Puyallup, WAAn improperly functioning fuel boost pump.May 28, 1994 · N786RW · Substantial damageNTSB SEA94LA082Accident · No injuriesLimited investigationFinal reportCessna 185 · Fort Lewis, WAThe fuel shutoff valve seized in a partially open position.Mar 13, 1994 · N4732E · Substantial damageNTSB SEA93LA181Accident · No injuriesLimited investigationFinal reportHiller UH-12E · Auburn, WAFailure of the connecting rod bolt. The high vegetation was a factor.Aug 23, 1993 · N9785C · Substantial damageNTSB SEA93LA092Accident · Minor injuriesLimited investigationFinal reportTaylorcraft BL-65 · Spokane, WAFailure of the number 4 cylinder exhaust valve seat and the inadvertent stalling of the aircraft by the pilot in command. Factors contributing to the accident were buildings and power lines.Apr 10, 1993 · N29553 · Substantial damageNTSB SEA93LA078Accident · No injuriesLimited investigationFinal reportSchweizer G-164B-600 · Quincy, WAUnsuitable terrain encountered during a forced landing after an engine cylinder assembly had separated. Factors include a snowbank.Mar 18, 1993 · N7503L · Substantial damageNTSB SEA91LA249Accident · No injuriesLimited investigationFinal reportCessna 177 · Snohomish, WAThe separation of the mixture control cable (core) resulting from separation of the adel clamp assembly and improper adjustment by maintenance personnel.Sep 23, 1991 · N3314T · Substantial damageNTSB SEA90FA057Accident · 2 fatalField investigationFinal reportCessna 170 · Republic, WAImproper inspection and airworthiness certification of the aircraft on the last annual inspection by an FAA authorized repair station, the inadequate engine performance and low cylinder compression, and the pilots attempt to takeoff with known aircraft…Mar 25, 1990 · N4130V · DestroyedNTSB SEA89LA093Accident · No injuriesLimited investigationFinal reportPiper PA-22-150 · Black Diamond, WAPower loss due to magneto failure. Contributing to the accident were lack of suitable terrain for forced landing and the presence of obstacles.May 28, 1989 · N6121D · Substantial damageNTSB SEA89LA073Accident · No injuriesLimited investigationFinal reportDonner/Parton Avid Flyer · Stanwood, WAAn ignition lead became disconnected from one cylinder, which resulted in a partial power loss. A factor related to the accident was: soft terrain in the touchdown area.Apr 20, 1989 · N4409D · Substantial damageNTSB SEA89LA059Accident · No injuriesLimited investigationFinal reportGrumman-Schweizer G-164A · Rosalia, WAA loss of engine power due to a supercharger failure. Contributing to the accident was the soft terrain on which the forced landing was made.Mar 25, 1989 · N8792H · Substantial damageNTSB SEA88LA148Accident · No injuriesLimited investigationFinal reportWeatherly 620 · Wilbur, WAThe pilot reported that an engine power loss occurred during an aerial application maneuver. The pilot made a forced landing in rough terrain. Examination of the engine revealed deteriorated seals in the engine driven fuel pump. Exam of the electric fuel pump…Aug 8, 1988 · N4603G · Substantial damageNTSB SEA88LA071Accident · No injuriesLimited investigationFinal reportCessna 172XP · Walla Walla, WADuring descent for landing the pilot noted a surge coming from the engine area, accompanied by an increase in rpm's. both the oil temperature and the oil pressure gauges were reading zero. The cylinder head temperature had reached 500 degrees and smoke was…Apr 10, 1988 · N736KG · Substantial damageNTSB SEA87LA111Accident · Minor injuriesLimited investigationFinal reportde Havilland DHC-2 MK.1 · Sedro Woolley, WAShortly after takeoff a loss of power occurred and the aircraft struck trees in flight. Less than 1/2 fuel was available in all three fuel tanks. The fuel selector valve was tested and found that the selections plate was indexed off center for all selections…Jun 8, 1987 · N64384 · DestroyedNTSB SEA86LA237Accident · No injuriesLimited investigationFinal reportCessna 150L · Kent, WADuring an instructional flight a partial loss of power occurred due to the mixture control cable at the carburetor end becoming loose. During forced landing on a field, two railroad ties, on a dirt pile, were struck. It was dusk at the time of the accident.Sep 3, 1986 · N18079 · Substantial damageNTSB SEA86LA226Accident · No injuriesLimited investigationFinal reportHegsted S16B · Kelso, WAThe student pilot was on final when the engine ceased operating. A forced landing was accomplished with touchdown being about 100 yards short of the runway. A hard landing was made with the aircraft coming to rest inverted. The needle valve to the carburetor…Aug 27, 1986 · N10LH · Substantial damageNTSB SEA86LA208Accident · Minor injuriesLimited investigationFinal reportCurtiss JN4-D · Vancouver, WAThe plt reported a normal takeoff was made with 1300 RPM. At liftoff a small amount of black smoke emitted from both exhaust stacks and the RPM dropped to 1250. After clearing the rwy, more black smoke emitted and the RPM dropped to 1200. The plt cleared two…Aug 17, 1986 · N511JN · Substantial damageNTSB SEA86LA187Accident · No injuriesLimited investigationFinal reportBoeing PT13/17 · Vancouver, WAThe plt reported the engine started running rough near woodland, Washington and an approach was set up, but due to many aircraft in the pattern the pilot elected to go to scappose, Washington (about 10 NM south of woodland). At scappose, Washington the pilot…Jul 31, 1986 · N1307N · Substantial damageNTSB SEA85LA076Accident · No injuriesLimited investigationFinal reportWeatherly 201B · Davenport, WAA vibration started in the engine and while the plt was monitoring the engine gauges he noted a loss of all oil pressure. A landing was made on a field and during rollout the left main gear was torn off when it struck a mound of dirt. The acft then struck…Mar 15, 1985 · N1263W · Substantial damageNTSB SEA84IA233Incident · No injuriesIncident investigationFinal reportBoeing 747-200B · Seattle, WADuring climbout, passing thru 4000 ft MSL, the acft experienced a failure of the #2 engine. The crew reported hearing an explosive sound followed by a drop in fuel flow with N1 speed decreasing to 30% RPM on the #2 engine. The acft returned to Seattle for an…Sep 29, 1984 · N613US · Minor damageNTSB SEA84LA153Accident · Minor injuriesLimited investigationFinal reportHughes 269C · Mt. St. Helens, WAThis accident occurred at the 5500 ft level on Mt. St. Helens. Density alt at the time was 7500 ft. at aprx 40-50 ft aglengine and rotor RPM began to decay rapidly. The acft landed hard on a rock ledge with one skid partially off the ledge. As rotor RPM…Jul 2, 1984 · N58397 · DestroyedNTSB SEA84LA130Accident · No injuriesLimited investigationFinal reportAyres S2R-1820 · Pasco, WAThe plt was applying herbicides to a corn field when a power loss to idle RPM occurred. During an emergency landing, the main gear sunk into soft sand & the acft nosed over. An exam revealed that the throttle bracket, p/n 19703-5001, had failed.Jun 12, 1984 · N4025K · Substantial damageNTSB SEA84LA027Accident · No injuriesLimited investigationFinal reportCessna 150F · Prosser, WAAccording to the pilot shortly after departure the engine began running rough for the second time. The pilot elected to make a precautionary landing on a gravel road he was familiar with. During the landing flare, with a gusty crosswind, directional control…Dec 17, 1983 · N6841F · Substantial damageNTSB SEA84LA019Accident · No injuriesLimited investigationFinal reportMorton B8M · Shelton, WAThe acrt collided with fir trees, about 18 feet tall, during an off-arpt forced landing after a power loss. The plt suspected carburetor ice. He said the engine began to run rough and RPM dropped to about 1200/1500 RPM. When he was unable to clear the trees…Nov 9, 1983 · N37860 · Substantial damageNTSB SEA83LA146Accident · No injuriesLimited investigationFinal reportPiper PA-38-112 · Dixie, WAAbout an hour after departure the engine began to run rough. The pilot did a magneto check and noted a drop of 300 RPM. A precautionary landing was made into a field of tall wheat. During landing roll the left main landing gear struck a hole. Examination of…Jul 11, 1983 · N4461E · Substantial damageNTSB SEA82DA139Accident · No injuriesFinal reportEnstrom F280 · Seattle, WAHelicopter made an emergency forced landing after power loss aircraft landed heavily in loose dirt and damaged skids and rotors. Post-accident exam found "throttle activating arm was improperly engaged to throttle stop."Aug 9, 1982 · N267Q · Substantial damageNTSB SEA82DA082Accident · No injuriesFinal reportHughes 269A · 2nm Nnm Redmond, WAThe engine lost power during the climb and the pilot executed an autorotation. Upon landing the aircraft rocked back and the main rotor severed the tail boom.Jun 9, 1982 · N8730F · Substantial damage