N51CX, cancelled Aug 18, 1997
Service difficulty reports · 17
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 = 'N51CX' AND deregistration_id = 'N51CX-1997-08-18' 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 = 'N51CX' AND deregistration_id = 'N51CX-1997-08-18' 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 IXXA9700036Skin · crackedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT ELEVATOR LOWER SKIN PANEL WAS FOUND TO BE CRACKED AT STATION XE32. REPAIR WAS ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW SKIN PANEL IN ACCORDANCE WITH FAA DER APPROVED DRAWING C0SDR IXXA9700042Actuator · corrodedDURING ROUTINE C-CHECK INSPECTION, THE LEFT MAIN LANDING GEAR RETRACT ACTUATOR PIN BOSS HOLE WAS FOUND TO BE CORRODED. REPAIR WAS ACCOMPLISHED BY OVERSIZING THE BOSS HOLE, FABRICATION AND INSTALLATION OF A OVERSIZE BUSHING IN ACCORDANCE WITH DOUGLAS FAX FILE SDR IXXA9700035Angle · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON THE RIGHT HAND VERTICAL STABILIZER BASE ATTACH ANGLE AT FUSELAGE STATION 1593 TO 1604. REPAIR WAS ACCOMPLISHED BY CORROSION REMOVAL, FABRICATION AND INSTALLATION OF A REPAIR ANGLE IN ACCORDANCE WITHSDR IXXA9700046Web · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION AND A CRACK WERE FOUND ON THE WEB STRUCTURE FOR ACCESS PANEL 603R AT STATION 200. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A FILLER AND A REPAIR DOUBLER IN ACCORDANCE WITH FAA DESDR IXXA9700037Jamb · crackedDURING ROUTINE C-CHECK INSPECTION, THE LOWER AFT, FORWARD CARGO DOOR JAMB WEB WAS FOUND TO BE CRACKED AT FUSELAGE STATION 1160, BETWEEN LONGERONS 30 AND 31 RIGHT. REPAIR WAS ACCOMPLISHED BY STOP DRILLING THE CRACK, FABRICATION AND INSTALLATION OF A REPAIR DOUSDR IXXA9700045Plating · corrodedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT WING, UPPER SURFACE EXTERNAL PLATING WAS FOUND WITH A CORROSION BULGE AT STATION XFS393, STRINGER 7. REPAIR WAS ACCOMPLISHED BY REMOVAL OF CORROSION PER DC-8 SRM 57-2-1 FIG 32, SHEET 2, FABRICATION AND INSTALLATIOSDR IXXA9700039Plating · corrodedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT WING OUTBOARD SLOT UPPER LEADING EDGE PLATING WAS FOUND TO BE CORRODED AT STATION XOLDI 6.224. REPAIR WAS ACCOMPLISHED BY REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF INTERNAL FILLER AND AN EXTERNASDR IXXA9700047Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE EXTERNAL PLATING AT STATION 1573.5, AND LONGERON 28 RIGHT, JUST AFT OF THE EXISTING DRAIN MAST. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A FILLER AND RSDR IXXA9700040Plating · corrodedDURING ROUTINE C-CHECK INSPECTION, THREE SHEARED RIVETS AND CORROSION WERE FOUND ON THE EXTERIOR PLATING AT FUSELAGE STATION 1757 RIGHT. REPAIR WAS ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND EXTERNAL REPAISDR IXXA9700044Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT ELEVATOR TRAILING EDGE EXTERNAL PLATING WAS FOUND TO BE BULGING AT STATION XE122. REPAIR WAS ACCOMPLISHED BY REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW SECTION OF PLATING IN ACCORDANCE WITHSDR IXXA9700043Aileron · corrodedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT OUTBOARD AILERON LOWER EXTERNAL PLATING WAS FOUND TO HAVE SURFACE CORROSION AND BULGING AT STATION XA615 TO XA642. REPAIR WAS ACCOMPLISHED BY REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF NEW SECTIOSDR IXXA9700038Aileron · crackedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT INBOARD AILERON UPPER LEADING EDGE PLATING WAS FOUND TO BE CRACKED AT STATION XA490. REPAIR WAS ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF NEW PLATING SECTION IN ACCORDANCE WITH FAA DSDR IXXA9686Clamp · brokenINVESTIGATION OF THIS EVENT FOUND AN ENGINE ANTI-ICE DUCT CLAMP BOLT HAD FAILED ALLOWING BLEED AIR TO ENTER THE ENGINE COWLING. THE HOT AIR DAMAGED THE ENGINE WIRING HARNESS WHICH CAUSED SEVERAL ENGINE INDICATION SYSTEM MALFUNCTIONS. INSPECTION OF THE REMAINSDR IXXA9682Control Amp · intermittentEN ROUTE BETWEEN ELP AND TOL IN CRUISE FLIGHT AT FL 37, THE MAIN CARGO COMPARTMENT SMOKE DETECTOR LIGHT ILLUMINATED. ATC WAS ADVISED, AND THE AIRCRAFT DIVERTED TO OKC. ON THE GROUND IN OKC, AND AIRCRAFT WAS CHECKED FOR SIGNS OF FIRE, SMOKE, OR ODORS OF COMBUSDR IXXA96114Smoke Detector · malfunctionedEN ROUTE BETWEEN ELP AND TOL IN CRUISE FLT AT FL 37, THE MAIN CARGO SMOKE DETECTOR LIGHT ILLUMINATED, FOLLOWED BY AN ACRID SMELL. THE FE DONNED A PBE AND ENTERED THE MAIN CARGO COMPARTMENT, BUT SAW NO VISIBLE SMOKE. THE A/C DIVERTED TO OKC, DETAILED INSPECTISDR IXXA9638Fuel Pump · leakingON DESCENT INTO SJU, THE NR 4 ENGINE WAS PRECAUTIONARILY SHUT DOWN DUE TO LOW OIL QUANTITY. ON THE GROUND IN SJU, MAINTENANCE DETERMINED THAT THE ENGINE FUEL PUMP GEARBOX DRIVE SEAL WAS LEAKING INTO ITS SPLINE CAVITY. THE DRIVE WAS RESEALED, AND THE ENGINE LSDR IXXA95134Grnd Shift Mech · out of rigON DEPARTURE OUT OF EWR, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE 'RETRACT' POSITION. THE AIRCRAFT APPEARED TO BE STUCK IN THE 'GROUND' MODE. THE AIRCRAFT RETURNED TO EWR FOR MAINTENANCE. THE AIRCRAFT WAS FERRIED TO A MAINTENANCE FACILITY WHERE THE NOS
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