Extra Flugzeugbau EA 300/L
Service difficulty reports · 19
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'EA300L' ORDER BY difficulty_date 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 sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'EA300L' ORDER BY difficulty_date 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.
SDR 2022FA0000050Brake Pads · looseTHE EXTRA 300L UTILIZES A CLEVELAND BRAKE ASSY PN# 30-164 AND CLEVELAND WHEEL ASSEMBLY 40-151. WE FOUND THAT WHEN WE REPLACE THE BRAKE PADS WITH PMA RAPCO BRAKE PADS RA066-06200 THAT THEY CAN FALL OFF THE PRESSURE PLATE PN# 063-01200 AND BACKING PLATE PN# 064SDR CA151214007Blade · loose(CAN) BLADES WERE FOUND LOOSE DURING PRE-FLIGHT INSPECTION IN HUB. PROP TOTAL TIME SINCE NEW 75.8. PROPELLER WAS REMOVED AND SENT FOR TEAR DOWN INSPECTION. PROPELLER RETURNED SERVICEABLE (SHIMS ADDED) ON BLADE NR 1 AND INSTALLED. MANUFACTURER HAS SERVICE BSDR 2008FA0000495Fuel Sys · malfunctionedAPPROX 9 GALLONS OF FUEL IN CENTER TANK BECAME INACCESSIBLE DURING FLT, PRECAUTIONARY LANDING. AFTER DEPARTING USING CENTER TANK FUEL FOR A 120 MILE FERRY FLIGHT, SWITCHED TO THE WING TANKS FOR THE PREPONDERANCE OF THE TRIP. NEARING THE DESTINATION WITH TSDR 2007FA0001042Fuel Control · malfunctionedTHE AIRCRAFT EXPERIENCED AN INFLIGHT ENGINE SHUTDOWN RESULTING IN A FORCED LANDING ON THE BEACH. THE CAUSE OF THE INFLIGHT ENGINE SHUTDOWN WAS THE INTERNAL FAILURE OF THE FUEL SERVO. THE FUEL SERVO WAS EVALUATED . THE FAILED UNIT WAS SENT TO THE MANUFACTURER SDR 2005FA0001579Longeron · crackedDURING ROUTINE 1,000 HR INSPECTION CRACKS WERE FOUND IN THE UPPER LONGERON AT THE HORIZONTAL STABILIZER ATTACHMENT, THESE WERE VERIFIED USING A FLUORESCENT DYE CHECK PENETRANT METHOD, CRACKS WERE ALSO FOUND IN THE VERTICAL TUBE SUPPORTING FORCES FROM THE TAIL SDR 2002FA0001224Setscrew · backed outPROPELLER GOVERNOR SET SCREW INSIDE CASE HALVES, BACKED OUT CAUSING A CHAIN REACTION OF ENGINE DAMAGE. ALL MAJOR ENGINE COMPONENTS BROKEN (NON-REPAIRABLE), RESULTING IN AN ENGINE FAILURE AND A FORCED LANDING.SDR 2002FA0000575Skin · delaminatedWING SKIN DELAMINATION OCCURRED IN FLIGHT. CRACKS IN PAINT AND FUEL SEEPAGE FROM AREA WAS REASON FOR DISCOVERY. DELAMINATION AREA IS 72 INCHES OUTBOARD ON TOP SIDE OF RIGHT WING AND EXTENDS APPROXIMATELY 30 INCHES FURTHER OUTBOARD. DELAMINATION AREA STARTS SDR 2001FA0000353Control Cable · looseROUTINE ANNUAL INSPECTION REVEALED AFT RUDDER CABLE THIMBLE EYES WERE LOOSE IN THE LOOP AT THE ATTACHMENT TO THE RUDDER. THE THIMBLE COULD BE REMOVED FROM THE LOOP. THE NICROPRESS CRIMP WAS MADE TOO FAR FROM THE THIMBLE. REPLACED THE RUDDER CABLES WITH NEW ONESDR 20001012SH027Grip · dislodgedELEVATOR TRIM BALL GRIP CAME OFF IN-FLIGHT. OWNER COMMENTED HE NOTICED RED MARKS ON HIS RIGHT PANTS LEG JUST ABOVE THE KNEE ON SEVERAL OCCASIONS. SUBMITTER SUGGESTED ALL EXTRA OWNERS CHECK THEIR TRIM KNOBS FOR LOOSENESS AS THIS IS A POTENTIALLY LIFE THREATENSDR 20001012SH026Heat Shield · failedEXHAUST HEAT SHIELD FAILED ITS CLAMP ATTACH TABS. SUBMITTER STATED THIS CONDITION COULD BE CONSIDERED SERIOUS IN THE EVENT A PART FAILS AND BECOMES LOOSE IN THE ENGINE COMPARTMENT. (X)SDR 20001016SH004Heat Shield · looseEXHAUST HEAT SHIELD FAILED ITS CLAMP ATTACH TABS. THIS CONDITION COULD BE CONSIDERED SERIOUS IN THE EVENT A PART FAILS AND BECOMES LOOSE IN THE ENGINE COMPARTMENT. (X)SDR CA000801023Cowling · elongated(CAN) SAME PROBLEM AS WITH C-GAKN. COWLING IS FALLING OFF DUE TO STRUCTURALLY INADEQUATE FIREWALL.SDR CA000801022Firewall · loose(CAN) FIRE WALL NEEDS TO BE STIFFENED.SDR CA000614046Fuel Tank · cracked(CAN) FUEL TANK CRACKED ALONG SIDE WHERE WELDED. AUTOMATIC FUEL CATCH SHIELD DID NOT WORK AND GAS DRIPPED INTO CABIN NOT OVERBOARD AS SUPPOSED TO.SDR CA000801021Blade · loose(CAN) LOOSE PROPELLER BLADES.SDR 99ZZZX2475Hose · leakingFUEL HOSE CONNECTS FUSELAGE FILLER NECK WITH MAIN FUSELAGE TANK. HOSE SEPARATED FROM TOP OF TANK AT RANGE AND ALLOWED FUEL TO ENTER COCKPIT. HOSE WAS FOUND CUT TOO SHORT FROM FACTORY ALLOWING ENOUGH CLEARANCE AT TOP FOR IT TO BACK OFF OF TANK FLANGE. FLEXINSDR CA000801020Propeller · loose(CAN) LOOSE PROPELLER BLADES.SDR CA000801019Propeller · loose(CAN) LOOSE PROPELLER BLADES.SDR 97ZZZX4468Screen · brokenTHE AIRCRAFT'S COWLING MOUNTED ALUMINUM AIR INTAKE SCREEN FOUND BROKEN ALONG THE UPPER AND LOWER EDGES. THE SCREEN WAS ONLY SECURED ON THE EDGES. FAILURE WOULD RESULT IN PIECES ENTERING THE FUEL INJECTION BODY, WHICH IS UNFILTERED, ON THIS AIRCRAFT. A NEW S
Back to Extra Flugzeugbau EA 300/L