N543EA
Service difficulty reports · 71
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N543EA' AND registry_match = 'registration' 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 n_number = 'N543EA' AND registry_match = 'registration' 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 SIMA20150108011Web · crackedFORWARD EQUIP COMPARTMENT LT FLOOR WEB HAS A 1/8 INCH CRACK. REPAIRED FWD EQUIP COMPARTMENT LT FLOOR WEB IAW ETN-CR-53-099 & ERS-CR5300-1035.SDR SIMA20150108010Web · crackedFORWARD EQUIP COMPARTMENT RT FLOOR WEB HAS A 1/2 INCH CRACK. REPAIR COMPLIED WITH IAW ETN-CR-53-099.SDR SIMA20150108014Frame · corrodedMAIN AVIONICS COMPARTMENT UNDERFLOOR FRAME AT FS 319.70, BETWEEN STRINGERS 26LT - 26RT IS CORRODED. REPAIRED UNDERFLOOR FRAME IAW SRM 53-21-06. COMPLIED WITH DT CHECKLIST 15-27.SDR SIMA20150108008Drag Angle · crackedRIGHT VERTICAL STAB TO FUSELAGE FWD ANGLE HAS EVIDENCE OF A CRACK ON THE AFT END. APPROX 1/2 INCHES LONG. REPAIRED RT VERTICAL STAB TO FUSELAGE FWD ANGLE AFT END IAW EO CR-55MR-038 & ERS CR-5500-230.SDR SIMA20150108013Frame · corrodedMAIN AVIONICS COMPARTMENT UNDERFLOOR FRAME AT FS 295.00, BETWEEN STRINGERS 25LT - 26RT IS CORRODED. REPAIRED UNDERFLOOR FRAME IAW SRM 53-21-06. COMPLIED WITH DT CHECKLIST 15-27.SDR SIMA20150108009Drag Angle · crackedRIGHT VERTICAL STAB TO FUSELAGE AFT ANGLE HAS EVIDENCE OF A CRACK ON THE FWD END APPROX 3/4 INCHES LONG. REPAIRED IAW ERS-CR-55MR-229.SDR SIMA20150108015Frame · corrodedMAIN AVIONICS COMPARTMENT UNDERFLOOR FRAME AT FS 310.00, BETWEEN STRINGERS 25LT - 26RT IS CORRODED. REPAIRED UNDERFLOOR FRAME IAW SRM 53-21-06. COMPLIED WITH DT CHECKLIST 15-27.SDR SIMA20141231005Access Door · openHOWLING NOISE FROM NOSE AFTER TAKEOFF. FOUND ACCESS DOOR ON GPU CONNECTION TO BE OPEN. GVI OF ACCESS DOOR FOUND TO BE GOOD. CLOSED DOOR, SAW DOOR OPEN WHILE ACFT WAS TAXIING.SDR SIMA20140926002Flashlight · inoperativeFIRST OFFICER`S FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW MM 33-50-16. OPERATIONS CHECKED GOOD.SDR SIMA20140915005Holder · malfunctionedDURING TAXI OUT AN ELEC SMOKE SMELL WAS DETECTED. AFTER RETURN TO GATE FIRST OFFICER`S CHART HOLDER HAD SAME HOT SMELL REMAINING. R & R FIRST OFFICER`S CHART HOLDER IAW AMM 25-18-13. OPERATIONS CHECKED GOOD.SDR SIMA20140821002Pcu · malfunctionedINBOARD FLIGHT SPOILERS & INBD SPOILERONS FAIL CAUTION MSG IN FLIGHT WHEN SPOILER LEVER WAS PULLED. ON MDC FOUND LT INBD MFS PCU JAM. DEFERRED IAW ETN-CR-27-093. REMOVED AND REPLACED LEFT INB MFS PCU IAW CRJ700 AMM 27-61-02. OPS CK OK. TDMI RESTOREDSDR SIMA20140123003Light · inoperativeSEVEN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. INSPECTED & FOUND AS PER COMPONENT LOCATION MANUAL 33-51-00 NORMAL OPERATION.SDR SIMA20131218002Relay · faultyRIGHT ENG WILL NOT START, STRONG FUEL SMELL. R & R START RELAY CHANNEL A K24 & START RELAY CHANNEL B K 26, IAW CRJ 700 AMM CHAPT 20-42-00 & CHAPT 24-05-09. OPERATIONS CHECKED GOOD.SDR SIMA20130427005Flashlight · inoperativeON FLIGHT 3656 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS INOPERABLE. REMOVED AND REPLACED FIRST OFFICER’S SIDE FLASHLIGHT IAW CRJ700 AMM 25-61-02. THE OPERATIONAL CHECK WAS GOOD. MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130318004Flashlight · inoperativeON FLIGHT 3635 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT ASSEMBLY IAW CRJ 700 AMM CHAPT 25-61-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNESDR SIMA20130128009Cable · brokenON FLIGHT 3708 THE CREW REPORTED THE PASSENGER DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ICE BREAK CABLE ASSEMBLY BROKEN. REMOVED AND REPLACED THE CABLE IAW AMM 52-11-02. AIRCRAFT OK FOR SERVICE.SDR SIMA20130125007Holder · brokenDURING MAINTENANCE INSEPCTION FOUND THE PASSENGER DOOR FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PASSENGER DOOR FLASHLIGHT HOLDER AS REQUIRED IAW STANDARD MAINT PRACTICES. THE OPERATIONAL CHECK WAS GOOD. THE SDR SIMA20121129001Coffeemaker · faultyON FLIGHT 3661 EN ROUTE TO LAX FA REPORTED AN ODD ODOR IN THE CABIN. CAPT NOTICED THE ODOR. INSTRUCTED FA TO ADVISE HIM IF THE ODOR CHANGED OR INTENSIFIED. FA CALLED BACK AND ADVISE THAT THE ODOR WAS STRONGER AROUND ROW 10. FA QUESTIONED SOME PAX AND CHECKSDR SIMA20121028005Indicator · trippedON FLIGHT 3782 THE CREW REPORTED THEY RECEIVE SLAT FAIL EICAS CAUTION MESSAGE. THE SLATS FAILED AT 0 DEGREES. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOLLOWED FIM 27-81-09-810-802. EXAMINED ALL 12 SLAT ACTUATOR INDICATORS AND FOUND THE RIGHT SLAT 3 NR 1 ANDSDR SIMA20121028004Slat · unknownON FLIGHT 3791 THE CREW REPORTED THE SLATS FAILED ON APPROACH. THE SLATS FAILED AT 0. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT MDC MDG SLAT ACT MECHNICAL JAM B MESSAGE DISPLAYED ON MDC PERFORMED SFECU 1 AND 2 IAW CRJ 700 AMM 27-51-05-740-801. TESSDR SIMA20120607006Tire · failedFLIGHT 3716, CREW REPORTED RIGHT MAIN LANDING GEAR INBOARD TIRE LOST TREAD ON TAKEOFF. DAMAGE TO FLAP AND RIGHT ENGINE COWLING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 AND NR 4 MAIN LANDING GEAR WHEEL AND TIRE ASSEMBLY. COMPLIED
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