N789EP
Service difficulty reports · 18
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 = 'N789EP' 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 = 'N789EP' 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 2003FA0000236Spinner · crackedDURING PHASE 3 INSPECTION FOUND PROPELLER SPINNER CRACKED AT BLADE CUT OUT ON ONE SIDE. THE PROBLEM IS REOCCURRING, THIS IS THE 5TH SPINNER REPLACEMENT ON THIS AIRCRAFT IN 1928.0 HOURS AND IS A COMMON PROBLEM ON OTHER C-172S AIRCRAFT. CESSNA SERVICE BULLETINSDR 2002FA0001199Transmitter · failedRT FUEL QUANTITY WENT TO "0" IN FLIGHT, AIRCRAFT RETURNED TO HOME STATION. MAINTENANCE FOUND FUEL QUANTITY TRANSMITTER FLOAT SEPERATED FROM THE TRANSMITTER. THE FLOAT ATTACH ARM BROKE OUTBOARD OF THE FLOAT WHERE IT WAS CRIMPED AND THE END PIECE, WASHER AND FSDR 2002FA0001240Bulkhead · crackedFOUND AFT PROPELLER SPINNER BULKHEAD, CRACKED AT ONE FLANGE AT PROPELLER BLADE CUT OUT. EDGE WITH NUTPLATE AND SCREW STILL ATTACHED TO PROPELLER SPINNER. AFT SPINNER BULKHEAD REPLACED AT 82.2 HOURS .SDR 2002FA0001183Bulkhead · crackedFOUND AFT PROPELLER SPINNER BULKHEAD CRACKED AT ONE FLANGE AT PROPELLER BLADE CUT OUT. EDGE WITH NUTPLATE AND SCREW STILL ATTACHED TO PROPELLER SPINNER. CESSNA SERVICE BULLETIN SB02-61-01 WAS ACCOMPLISHED 34.0 HOURS PREVIOUSLY AND THE AFT SPINNER BULKHEAD REPSDR 2002FA0001029Bulkhead · crackedAIRCRAFT UNDERGOING PHASE 1 INSPECTION, MAINTENANCE FOUND AFT PROPELLER SPINNER BULKHEAD CRACKED. A ONE INCH PIECE OF THE BULKHEAD WAS BROKEN OFF CONTAINING 1 NUTPLATE. REPLACED SPINNER BULKHEAD, REINSTALLED PROPELLER, OPERATIONAL CHECK SAT.SDR 2002FA0000758Switch · failedTAXI LIGHT SWITCH FAILED WITH THE LIGHT IN THE OFF POSITION. THIS IS A CIRCUIT BREAKER SWITCH. THIS OPERATOR HAS HAD THREE PREVIOUS FAILURES, THE FAILURES WERE WITH THE SWITCH IN THE ON POSITION.SDR 2002FA0000757Switch · failedTAXI LIGHT SWITCH FAILED WITH THE LIGHT IN THE OFF POSITION. THIS IS A CIRCUIT BREAKER SWITCH AND THIS OPERATOR HAS HAD THREE PREVIOUS FAILURES THE OTHER FAILURES WERE WITH THE SWITCH IN THE ON POSITION.SDR 2002FA0000756Switch · failedLANDING LIGHT SWITCH FAILED IN THE ON POSITION. THE SWITCH WAS TURNED OFF AFTER LANDING AND WHILE TAXI TO PARKING NOTED THE LIGHT WAS STILL ON AND THE SWITCH WAS IN THE OFF POSITION. THE LANDING LIGHT WOULD ONLY TURN OFF WITH THE BATTERY SWITCH. THIS IS A CSDR 20010410AP012Seat Back · bentDURING PHASE 1 MAINTENANCE INSPECTION, CO-PILOTS SEAT BACK WAS RECLINED APPROXIMATELY 4 INCHES FROM FULL UPRIGHT POSITION. FOUND SEAT BACK FRAME P/N 0514215-15 WAS BENT AT THE TOP OF THE RIGHT ATTACH FORGING.SDR 20010418CW010Seat Back · bentMAINTENANCE FOUND RIGHT FROMT SEAT BACK RECLINED APPROXIMATELY 4 INCHES FROM NORMAL UPRIGHT POSITION. THE SEAT WAS REMOVED AND INSPECTED, FINDING THE SEAT BACK FRAME BENT. THE FRAME WAS BENT ON THE LEFT SIDE JUST ABOVE THE ATTACH FORGING PN 05142158. REPLACSDR 20010418CW009Switch · inoperativePILOT REPORTED AVIONICS MASTER SWITCH INOPERATIVE, WHEN BATTERY SWITCH IS TURNED ON, ALL AVIONICS LEFT IN ON POSITION POWER UP REGARDLESS OF AVIONICS MASTER SWITCH POSITION. MAINTENANCE FOUND ONE SIDE OF AVIONICS MASTER SWITCH INOPERATIVE. REPLACED AVIONICSSDR 20010322CW002Buss Tie · arcedPILOT REPORTED TRANSPONDER INOP, NR1 COMM/NAV INTERMIT. MAINT REPLCD NR1 COMM/NAV AND REMOVED TRANSPONDER FOR REPAIRS. NEXT FLIGHT, PILOT REPORTED NR2 COMM/NAV INTERMIT LOSS OF POWER & THE INTERCOMM INOP. MAINT TROUBLESHOOTING FOUND AUDIO PANEL COMM SELSDR 20000814SH002Transmitter · defectiveLEFT FUEL QUANTITY WENT TO EMPTY AND LT LOW FUEL ANNUNCIATOR LIGHT ILLUMINATED IN-FLIGHT. MAINT FOUND THE FUEL QUANTITY TRANSMITTER INOPERATIVE. WHEN THE XMITTER WAS REMOVED FROM FUEL CELL, THE FLOAT WAS MISSING ALONG WITH THE RETAINER WASHER ON THE OTBD ENDSDR 20000809SH026Transmitter · defectiveLEFT FUEL QTY WENT TO EMPTY, LT LOW FUEL ANNUNCIATOR LIGHT ILLUMINATED IN-FLIGHT. MAINT FOUND THE FUEL QTY TRANSMITTER INOP. WHEN XMITTER REMOVED FROM FUEL CELL, THE FLOAT AND RETAINER WASHER ON OTBD END OF THE FLOAT ARM WERE MISSING. FUEL CELL OPENED AND THSDR 20000720SH011Plug · wornPERFORMED LYC SI 1492B. DURING THE PHASE 2 INSPECTION, OIL FILTER REMOVED AND CUT OPEN FOR INSPECTION. AN EXCESSIVE AMOUNT OF ALUMINUM FLAKES WERE DISCOVERED. ALL 4 CYLINDERS REMOVED ENOUGH TO INSPECT AND REPLACED 8 WORN PISTON PIN PLUGS WITH P/N 60828 PLUGSDR 20000623SH002Plug · wornPERFORMED LYC SI 1492B. DURING PHASE 2 INSPECTION, OIL FILTER WAS REMOVED AND CUT OPEN FOR INSPECTION. AN EXCESSIVE AMOUNT OF ALUMINUM FLAKES WERE DISCOVERED. ALL 4 CYLINDERS REMOVED ENOUGH TO INSPECT AND REPLACED 8 WORN PISTON PIN PLUGS WITH PN 60828 PLUGSSDR 99ZZZX3579Nozzle · looseDURING PHASE INSPECTION, FOUND ALL FOUR FUEL INJECTION NOZZLES PN LW 18265 HAD SCREENS AND SHIELDS LOOSE AROUND NOZZLE BODY. REPLACED WITH 4 EACH SERVICEABLE NEW NOZZLES.SDR 99ZZZX2731Skin · crackedNEW CESSNA DURING 1ST PHASE 2 INSPECTION, FOUND LEFT FLAP TRAILING EDGE, LOWER SKIN CRACKED AT 8 EACH RIVETS STARTING FROM INBOARD END TO OUTBOARD, 2 FEET. REPLACED FLAP WITH NEW ASSY FURNISHED BY CESSNA.
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