NTSB investigations, 2000
41 cases where the first occurrence was “Loss of engine power(partial) - mech failure/malf”.
Cases per year
| 1982 | 91 |
|---|---|
| 1983 | 77 |
| 1984 | 88 |
| 1985 | 82 |
| 1986 | 76 |
| 1987 | 58 |
| 1988 | 76 |
| 1989 | 67 |
| 1990 | 74 |
| 1991 | 62 |
| 1992 | 48 |
| 1993 | 53 |
| 1994 | 54 |
| 1995 | 60 |
| 1996 | 42 |
| 1997 | 43 |
| 1998 | 50 |
| 1999 | 35 |
| 2000 | 41 |
| 2001 | 28 |
| 2002 | 36 |
| 2003 | 24 |
| 2004 | 45 |
| 2005 | 33 |
| 2006 | 28 |
| 2007 | 37 |
Where
Open the mapLatest 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 year(c.\"eventDate\") = 2000
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.
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 year(c."eventDate") = 2000 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
Run 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 LAX01LA050Accident · Serious injuriesLimited investigationFinal reportCessna 182J · Paradise, CAFuel exhaustion during a descent due to an inadequate fuel supply. Contributing factors were the pilot's improper preflight planning, his misjudged altitude while performing the emergency landing, and his lack of certificate qualification and recent flight…NTSB NYC01LA012Accident · Serious injuriesLimited investigationFinal reportPiper PA-60-601P · S. Burlington, VTThe pilot's improper in-flight decision to perform a precautionary landing, and his failure to maintain airspeed after he experienced a partial loss of power on one engine. A factor was the partial loss of power on one engine due to an induction air leak.NTSB CHI01LA013Accident · No injuriesLimited investigationFinal reportRepublic RC-3 · Baraboo, WIthe failure of the number five intake valve spring during initial climbout and that there was no suitable terrain during the forced landing. A factor was the corn crop.NTSB LAX00FA347Accident · Minor injuriesField investigationFinal reportCessna 207A · Valle, AZImproper maintenance and adjustment of the engine magnetos resulting in a loss of optimum performance during a critical takeoff that required peak engine performance.NTSB ATL00LA096Accident · No injuriesLimited investigationFinal reportPiper PA-28-140 · Deland, FLA partial loss of engine power during initial climb following takeoff, due to the restricted movement of the number two cylinder's exhaust valve.NTSB MIA00LA263Accident · Minor injuriesLimited investigationFinal reportGrumman AA-5 · Zephyrhills, FLthe intentional stall/mush by the pilot-in-command due to obstructions ahead resulting in a hard landing. Contributing to the accident was the partial loss of engine power due to fuel starvation caused by wear, fatigue, then overstress separation of the…NTSB CHI00LA274Accident · Minor injuriesLimited investigationFinal reportWidner Pietenpol Aircamper · Andover, MNThe trees and the unsuitable terrain for landing encountered during the forced landing. Factors were the side slip to avoid the trees initiated by the pilot, the fractured piston, and the cracked cylinder.NTSB LAX00FA310Accident · 1 fatalField investigationFinal reportPiper PA-31-350 · Hilo, HIDeterioration and failure of the oil filter converter plate gasket, which resulted in a loss of engine power and a subsequent in-flight fire.NTSB IAD00LA070Accident · Minor injuriesLimited investigationFinal reportJordan Kitfox Model 1 · Waynesville, OHA broken carburetor jet needle, which blocked fuel from entering the carburetor's mixing tube and resulted in a partial loss of engine power.NTSB FTW00LA239Accident · No injuriesLimited investigationFinal reportGrumman-Schweizer G-164B · Kaplan, LAthe failure of the supercharger during takeoff. A contributing factor was the lack of suitable terrain for the forced landing.NTSB NYC00LA234Accident · No injuriesLimited investigationFinal reportCessna 152 · Culpeper, VAThe partial loss of power due to an inadequate annual inspection, which resulted in the throttle linkage becoming disconnected from the throttle.NTSB LAX00GA297Accident · 1 fatalFinal reportBell 412 · Cold Springs, NVfailure of the compressor turbine disc due to cyclic fatigue brought about by repeated operation near or above the engines' temperature/power limits by company personnel over an extended period of time. Factors in the accident were: 1) the high density…NTSB CHI00LA253Accident · No injuriesLimited investigationFinal reportPiper PA-38-112 · Coopersville, MIfuel starvation due to the blocked carburetor. Factors relating to the accident were the foreign object (tab), the improper maintenance performed on the carburetor, and the corn crop.NTSB IAD00LA071Accident · No injuriesLimited investigationFinal reportShowalter Rotorway 152 · Ravenna, OHThe pilot/owner's inadequate installation of an ignition lead that resulted in a partial loss of engine power and forced landing to unsuitable terrain. A factor in the accident was the soybean crop in the forced landing site.NTSB NYC00LA214Accident · No injuriesLimited investigationFinal reportPiper PA-25 · Wildwood, NJThe partial loss of power caused by detonation of the #3 piston.NTSB IAD00LA066Accident · No injuriesLimited investigationFinal reportWaco UPF7 · Warrenton, VAthe loss of engine power over unsuitable terrain due to an inoperative magneto.NTSB CHI00LA220Accident · Serious injuriesLimited investigationFinal reportFloroski Anderson Kingfisher · Deerwood, MNthe open carburetor heat air box resulting in a loss of engine power, the diminished climb rate and the altitude/clearance not possible by the pilot. Factors were the trees and the bent carburetor heat push-pull rod.NTSB DEN00LA134Accident · Serious injuriesLimited investigationFinal reportCessna 310D · Pagosa Springs, COThe pilot inadvertently stalling the airplane. Factors were the pilot's failure to use the entire available runway, the high density altitude weather condition, and a partial loss of power on one engine due to a burned exhaust valve.NTSB NYC00LA198Accident · Serious injuriesLimited investigationFinal reportWarrington Surrel Guppy · Churchville, MDThe pilot's failure to maintain airspeed which resulted in an inadvertent stall. Factors in this accident were an open canopy and a decrease in engine power.NTSB DEN00LA130Accident · No injuriesLimited investigationFinal reportCessna 150L · Reserve, NMSeizure of the starter clutch assembly needle bearing, which caused the engine to develop less than full rated power and the airplane to achieve less than expected climb performance. Factors were noncompliance of a service bulletin, unsuitable terrain on…NTSB LAX00LA271Accident · No injuriesLimited investigationFinal reportAir Tractor AT-401 · Ripley, CAA loss of engine power due to the separation of a connecting rod from the crankshaft.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 MIA00LA207Accident · Serious injuriesLimited investigationFinal reportCessna P210N · Boone, NCThe failure of the inter-cooler duct connecting the inter-cooler to the engine due to inadequate attachment of the inter-cooler to the aircraft which resulted in loss of turbocharger air overboard and loss of engine power and damage to the aircraft during a…NTSB FTW00LA190Accident · Minor injuriesLimited investigationFinal reportMooney M20C · Whitney, TXThe partial loss of engine power, which resulted from the worn carburetor.NTSB LAX00LA260Accident · No injuriesLimited investigationFinal reportCessna 172N · Santa Ana, CAThe loss of engine power during the initial takeoff climb, at too low an altitude to afford remedial action, because of an ingested valve, and the airplane's subsequent collision with the ground adjacent to the runway.NTSB FTW00LA175Accident · Serious injuriesLimited investigationFinal reportCessna 177 · Nacogdoches, TXthe loss of engine power during a go-around resulting from the failure of the worn carburetor heat control cable. A contributing factor was the lack of suitable terrain for the forced landing.NTSB FTW00LA160Accident · Minor injuriesLimited investigationFinal reportCessna 195 · Kaufman, TXThe failure of the left magneto, which resulted in a partial loss of engine power. Factors were the fouled number 3, 4, and 5 rear spark plugs and the lack of suitable terrain for the precautionary landing.NTSB NYC00LA141Accident · 1 fatalLimited investigationFinal reportCarlson Criquet · East Palestine, OHThe failure of the powerplant to produce adequate power for undetermined reasons, and the pilot's continued operation of the airplane with known deficiencies.NTSB NYC00LA129Accident · No injuriesLimited investigationFinal reportCessna 120 · Beaumont, PAA crack in the crankcase which resulted in a partial power loss.NTSB FTW00LA138Accident · Minor injuriesLimited investigationFinal reportNoteman RV6-A · Kanab, UTThe partial loss of engine power as result of the failure of an exhaust valve. A factor was the lack of suitable terrain for the forced landing.NTSB NYC00FA122Accident · No injuriesField investigationFinal reportMcDonnell Douglas DC-10-30 · Newark, NJStress rupture of the 2nd-stage low pressure turbine anti-rotation nozzle locks, resulting from inadequate nozzle lock design.NTSB ATL00LA046Accident · No injuriesLimited investigationFinal reportAir Tractor AT-401-B · Lawrenceburg, TNThe loss of engine power due to a stuck exhaust valve that resulted in the collision with a tree while maneuvering for the forced landing.NTSB LAX00LA157Accident · Minor injuriesLimited investigationFinal reportCessna 207 · Yreka, CAthe total loss of engine power while in cruise flight due to the fatigue failure of the engine's anti-ice bleed air line, which resulted in the pilot's inability to utilize the engine anti-ice system. Contributing factors were the icing conditions and the…NTSB FTW00TA116Accident · Minor injuriesFinal reportHughes OH-6A · El Paso, TXThe failure of the pilot to maintain rotor rpm during an autorotation, which resulted in a hard landing. A factor was the partial loss of engine power resulting from the separation of the power control line due to fatigue, as a consequence of improper…NTSB FTW00LA108Accident · Minor injuriesLimited investigationFinal reportNorth American T-28B · Bridgeport, TXThe partial loss of engine power for an undetermined reason.NTSB FTW00LA107Accident · No injuriesLimited investigationFinal reportCessna 172N · Maud, OKthe loss of engine power while maneuvering as a result of the separation of the exhaust rocker arm retaining stud due to fatigue, which resulted in a precautionary landing.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 FTW00LA097Accident · No injuriesLimited investigationFinal reportGrumman-Schweizer G-164A · Gillett, ARThe cracked #8 cylinder resulting in failure of the cylinder. A factor was the plowed/furrowed terrain.NTSB ATL00LA030Accident · Minor injuriesLimited investigationFinal reportBurak Stanley A XF4 · Brooksville, FLThe owner/builder's failure to build the airplane within the design stress limits of the drive shaft assembly, that resulted in the failure of the Flex Coupling Retention Bolts.NTSB FTW00LA058Accident · No injuriesLimited investigationFinal reportCessna A185F · Houston, TXthe loss of engine power during climb as a result of fatigue cracking of the #4 cylinder head and its subsequent separation from its barrel.NTSB LAX00LA062Accident · Minor injuriesLimited investigationFinal reportCessna 172A · Dos Palos, CAA partial loss of engine power due to the failure of maintenance personnel to properly install and safety the throttle arm to the carburetor throttle shaft.