N269CA, cancelled Sep 19, 2022
Service difficulty reports · 72
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 = 'N269CA' AND deregistration_id = 'N269CA-2022-09-19' 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 = 'N269CA' AND deregistration_id = 'N269CA-2022-09-19' 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 COMA0210028WireFLIGHT 5080 TAKE OFF TRIM CONFIG WARNING DURING T/O.REPAIRED BROKEN WIRE AT ELEVATOR TAB PROX SENSOR.SDR COMA0210020Eec · defectiveFLIGHT 5023 DURING CLIMB OUT OF MCO THE #2 ENGINE POWER LEVER INPUT WAS IN EXCESS OF ONE INCH BEFORE IT TOOK EFFECT.REPLACED THE #2 EEC.SDR COMA0210004Latch · brokenFLIGHT 5021 L/H MLG, INBD GEAR DOOR, DOES NOT CLOSE AFTER GEAR RETRACTION.REPLACED THE DOOR LATCH.SDR COMA0210002Handle · defectiveFLIGHT 5021 L/H MLG INDICATED INTRANSIT AFTER GEAR RETRACTION.REPLACED THE L/H INBD GEAR DOOR LATCH.SDR COMA0210001Door LatchFLIGHT 5070 L/H MLG DID NOT RETRACT WHEN GEAR SELECTED UP.FOUND L/H MLG DOOR UNLATCH - SECURED DOOR LATCH, NO OTHER DEFECTS FOUND.SDR COMA0110164Switch · out of adjFLIGHT 5028 - SERVICE DOOR WARNING LIGHT AFTER T/O.ADJUSTED THE FUEL SERVICE DOOR MICRO SWITCH.SDR COMA0110160Power LeverFLIGHT #5056. POWER LEVER SPLIT DURING T/O.POWER LEVER SPLIT WITHIN LIMITS. AIRCRAFT RETURNED TO SERVICE.SDR COMA0110158Rib · crackedDURING A SERVICE CHECK, MECHANIC NOTICED A CRACK LOCATED AT THE COCKPIT OVERHEAD CREW ASSIST HANDLE MOUNT ON LEFT SIDE.DAMAGE WAS REMOVED FROM THE RIB. A FILLER AND A DOUBLER WAS FABRICATED AND INSTALLED. WORK WAS ACCOMPLISHED IN ACCORDANCE WITH AERODESIGN RESDR COMA0110157Sensor · malfunctionedFLIGHT 5049 - THREE KNOB POWER LEVER SPLIT DURING T/O. REPLACED THE RT ENGINE T2 SENSOR.SDR COMA0110134Computer · malfunctionedDURING LANDING APPROACH INTO MCO WHEN FLAPS WERE SELECTED FROM 25 TO 45 DEGREES AUDIBLE FLAP CAUTION ACTIVATED, CREW DECLARED AN EMERGENCY AND LANDED SAFELY. INTERROGATED THE FLAP COMPUTER AND FOUND NUMEROUS FAULT CODES. CLEARED FAULT CODES, PERFORMED OPERATSDR COMA0110133Flap TrackDURING LANDING APPROACH INTO EYW WHEN FLAPS WERE SELECTED FROM 25 TO 45 DEGREES, FLAP DISAGREE CAUTION ACTIVATED.REPLACED THE FLAP ROLLERS FOR THE LEFT INBOARD FLAP AND THE RIGHT OUTBOARD FLAP.SDR COMA0110043Fan · failedLAVATORY SMOKE DETECTOR ACTIVATED, SMOKE SMELL IN COCKPIT. REPLACED THE LEFT HAND GROUND COOLING FAN.SDR COMA0110038Landing Gear · malfunctionedLANDING GEAR SLOW TO EXTEND, AND INDICATED UNSAFE. RECYCLED GEAR WITH SAME RESULTS. COULD NOT DUPLICATE. LANDING GEAR RETRACTION CHECKS WERE NORMAL.SDR COMA0110037Shear Tie · crackedDURING A 400 FLIGHT CYCLE CHECK, A CRACKED RIVET HEAD WAS DISCOVERED ON THE RIGHT SIDE OF AIRCRAFT FUSELAGE ALONG FRAME 9. UPON FURTHER INVESTIGATION, THE SKIN SUPPORT BRACKET IN WHICH SAID RIVET PASSES THROUGH WAS FOUND TO BE CRACKED. THE SUPPORT BRACKET WASDR COMA0110036Shear Tie · crackedDURING A 400 FLIGHT CYCLE CHECK, A CRACKED RIVET HEAD WAS DISCOVERED ON THE RIGHT SIDE OF AIRCRAFT FUSELAGE ALONG FRAME 9. UPON FURTHER INVESTIGATION, THE SKIN SUPPORT BRACKET IN WHICH SAID RIVET PASSES THROUGH WAS FOUND TO BE CRACKED. THE SUPPORT BRACKET WASDR COMA0110035Spring · brokenON POST-FLIGHT INSPECTION, CREW NOTICED OIL LEAKING FROM LEFT PROPELLER. MAINTENANCE DETERMINED SOURCE TO BE THE NR 1 PROP BLADE. THE BLADE WAS REMOVED, AND THE BLADE SEAL COIL SPRING WAS FOUND TO BE BROKEN. THE BLADE SEAL ASSEMBLY WAS REPLACED, THE BLADE RSDR COMA0110034Spring · brokenON POST-FLIGHT INSPECTION CREW NOTICED OIL LEAKING FROM LEFT PROPELLER. MAINTENANCE DETERMINED SOURCE TO BE THE NR 1 PROP BLADE. THE BLADE WAS REMOVED, AND THE BLADE SEAL COIL SPRING WAS FOUND TO BE BROKEN. THE BLADE SEAL ASSEMBLY WAS REPLACED, THE BLADE RESDR COMA0010366Smoke Detector · malfunctionedTHE LAVATORY SMOKE DETECTOR ACTIVATED DURING TAXI, AIRCRAFT RETURNED TO THE GATE. DEFERRED THE LAVATORY SMOKE DETECTOR.SDR COMA0010161Battery · dischargedOVERHEAD EMERGENCY LIGHT AT ROW 6 IS INOPERABLE. REPLACED BATTERY PACK.SDR COMA0010065Pcu · out of rigRIGHT PROPELLER NP INDICATED 97 PERCENT MAX. FOUND TRANSFER TUBE TO PCU RIGGING DISCREPANCY. ADJUSTED RIGGING AND ACFT. RETURNED TO SERVICE.SDR COMA0010035Sensor · malfunctionedNLG INTRANSIT LIGHT REMAINED ON AFTER GEAR RETRACTED. REPLACED THE NLG DOWNLOCK SENSOR.SDR COMA0010027Sign · inoperativeCABIN DOOR EMERGENCY LIGHT WAS INOPERABLE. REPLACED LIGHT ASSY.SDR COMA0010021Sign · brokenEXIT SIGN AT ROW 8 WAS BROKEN. REPLACED EXIT SIGN.SDR COMA0010015Indicator · malfunctionedRIGHT HAND HYDRAULIC RESERVOIR, LOW LEVEL, WARNING. REPLACED THE QUANTITY GAUGE.SDR COMA0010009Battery · dischargedAFT SECTION CABIN EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY.SDR COMA9910191Indicator · erraticRT ENGINE T6 INDICATOR FLUCTUATED FULL SCALE. REPLACED T6 INDICATOR GAUGE.SDR COMA9910183Sensor · out of adjustTRIM WARNING DURING TAKEOFF. ADJUSTED THE ELEVATOR TRIM PROXIMITY SENSORS.SDR COMA9910178Wire · damagedTAKEOFF TRIM AURAL WARNING. REPAIRED DAMAGED WIRE SPLICE AT THE ELEVATOR TRIM PROXIMITY SENSORS.SDR COMA9910152Sensor · faieldAFTER TAKEOFF AND GEAR RETRACTION, NOSE GEAR INDICATION WAS RED B, LIGHTS REMAINED ON AFTER CYCLING GEAR. REMOVED AND REPLACED NOSE LANDING GEAR PROX SENSOR FOR B SYSTEM.SDR COMA9910136Fuel Heater · leakingFUEL LEAKING FROM LEFT ENGINE. REPLACED THE FUEL HEATER.SDR COMA9910075Check Valve · failedSMOKE FLOWED HEAVILY FROM COCKPIT GASPERS DURING DESCENT THRU 14,000 FT. TORQUE REDUCED TO 20 PERCENT. REMOVED AND REPLACED LEFT ENGINE OIL PRESSURE CHECK VALVE. GROUND RAN A/C, NO SMOKE OR SMELL NOTED.SDR COMA9910074Outflow Valve · failedAUTO PRESSURIZATION INOPERATIVE. REMOVED AND REPLACED PRESS OUTFLOW VALVE.SDR COMA9910070Valve · malfunctionedSMOKE IN COCKPIT COMING FROM AIRCRAFT VENTS. REPLACED THE LEFT ENGINE 2.5 SWITCHING VALVE.SDR COMA991066Air Dist · odorSMOKE IN COCKPIT AND CABIN, FOR APPROXIMATELY 20 SECONDS DURING LANDING APPROACH. INSPECTED AIRCRAFT COOLING AND RECIRCULATION SYSTEM. NO DEFECTS FOUND.SDR COMA9910023Actuator · failedWHEN SELECTING FLAPS TO 45 DEGREES, THE FLAP DISAGREE CAUTION ACTIVATED. REPLACED THE EIGHT OUTBOARD FLAP ACTUATOR.SDR COMA9810271Warning · activatedFUEL WARNING ON MAP DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE.SDR COMA9810216Socket · shortedNAVIGATION LIGHTS CIRCUIT BREAKER TRIPPED TWICE. REPLACED DEFECTIVE LIGHT SOCKET.SDR COMA9810129Ahrs · failedPILOTS AHRS FAILED. REPLACED NR 1 AHRS.SDR COMA9810116Box Control · malfunctionedWHEN LANDING GEAR EXTENDED BOTH GREEN AND RED INDICATOR LIGHTS ILLUMINATED, AND ANTI-SKID FAIL INDICATION. COULD NOT DUPLICATE DISCREPANCY. REPLACED LANDING GEAR CONTROL ASSEMBLY FOR TROUBLESHOOTING.SDR COMA9810067Relay Box · failedTAKEOFF AURAL WARNING SOUNDED AFTER TAKEOFF. REPLACED THE LANDING GEAR RELAY BOX.SDR COMA9810064Light Assy · overheatedSMOKE IN CABIN DURING TAXI OPERATIONS. REPLACED OVERHEATED FLUORESCENT LIGHT ASSY AT SEAT 4B.SDR COMA9810048Relay Box · malfunctionUNABLE TO RAISE LANDING GEAR AFTER TAKEOFF. BOTH INTRANSIT RED AND GREEN SAFE INDICATORS WERE ON. REPLACED THE LANDING GEAR RELAY BOX.SDR COMA081341Battery · dischargedNUMEROUS EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY BATTERY.SDR COMA9710321Indication · malfunctionedWHEN LANDING GEAR RETRACTED, THE B-SYSTEM INTRANSIT LIGHTS REMAINED ON. COULD NOT DUPLICATE DISCREPANCY. LANDING GEAR EXTENSION AND RETRACTION CHECKS NORMAL.SDR COMA9710260Skin · dentedFUSELAGE RT SKIN WAS PREVIOUSLY FOUND TO HAVE A LARGE DENT BETWEEN FRAMES 14 AND 15, AND STRINGERS 12R AND 13R. THE DENT WAS DEFERRED PER SRM LIMITATIONS. AT THIS TIME THE DENT WAS REPAIRED EMBRAER FAX NR SST-387/97. ALSO, STRINGER 13R WAS SLIGHTLY DAMAGED.SDR COMA9710259Omega Beam · corrodedON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT FWD CENTER OMEGA BEAM WAS FOUND TO HAVE A SMALL AREA OF CORROSION THROUGH THE PART. THE OMEGA BEAM WAS REPAIRED PER AERODESIGN REPORT NR 2181-4, REV IR, DATED 5-6-97.SDR COMA9710258Angle · corrodedON 4C TASK 5320-152-01I, THE SUPPORT ANGLE FOR THE AFT EMERGENCY EXIT LOWER GUIDE PIN RECEPTACLES, WAS FOUND CORRODED. REPLACED PER SRM STANDARD PRACTICES.SDR COMA9710257Angle · corrodedON 2C TASK 5310-131-01I, THE FWD FLOOR SUPPORT ANGLE UNDER THE PAX DOOR ENTRANCE THRESHOLD WAS FOUND CORRODED. REPLACED PER SRM STANDARD PRACTICES.SDR COMA9710256Sill · corrodedON 4C TASK 5330-162-01I, THE RT FWD FLOOR SUPPORT SILL IN THE CARGO COMPARTMENT WAS FOUND CORRODED. REPLACED PER SRM STANDARD PRACTICES.SDR COMA9710255Crossbeam · corrodedON 4C TASK 5320-142-01I, THE RT CABIN FLOORBEAM CROSSBEAM AT FRAME 36 WAS FOUND CORRODED. REPLACED PER SRM STANDARD PRACTICES.
Back to N269CA, cancelled Sep 19, 2022