N205CA, cancelled Feb 11, 2009
Service difficulty reports · 42
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 = 'N205CA' AND deregistration_id = 'N205CA-2009-02-11' 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 = 'N205CA' AND deregistration_id = 'N205CA-2009-02-11' 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 COMA9810180Battery · dischargedAFT SECTION OF EMERGENCY FLOOR LIGHTING IS INOPERABLE. REPLACED EMERGENCY BATTERY.SDR COMA9810171Door · not latchedSERVICE DOOR WARNING DURING TAKEOFF. FOUND FUEL SERVICE DOOR UNLATCHED. SECURED DOOR CLOSED AND AIRCRAFT RETURNED TO SERVICE.SDR COMA9810150Switch · dirtyAUTOFEATHER SYSTEM INOPERABLE DURING TAKEOFF. CLEANED THE AUTOFEATHER ARMING SWITCHES IN POWER LEVER QUADRANT.SDR COMA9810120Sign · looseEXIT SIGN LOOSE AT ROW 5A. REPLACED EXIT SIGN.SDR COMA9810108T/O Warning · malfunction'TRIM' AURAL WARNING DURING TAKEOFF. REPLACED THE AUDIO WARNING UNIT.SDR COMA9810078Actuator · malfunctuatingOUTBOARD FLAP INDICATION IS FLUCTUATING BETWEEN 2 AND 7 UNITS. COULD NOT DUPLICATE DISCREPANCY. REPLACED RIGHT HAND OUTBOARD FLAP ACTUATOR FOR TROUBLESHOOTING.SDR COMA9810015Crossbeam · corroded2C TASK 532D-147-03I REVEALED RIGHT CROSSBEAM AT FRAME 28 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERVICEABLE PART USING EMB 120 STANDARD PRACTICES.SDR COMA9810014Crossbeam · corroded2C TASK 151-01Z REVEALED LEFT CROSSBEAM TO BE CORRODED AT FRAME 33. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 STANDARD PRACTICES.SDR COMA9810009Crossbeam · corroded2C TASK 5320-147-03I REVEALED LEFT CROSSBEAM AT FRAME 23 TO BE CORRODED TO LIMITS. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 STANDARD PRACTICES.SDR COMA9810008Crossbeam · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT CROSSBEAM AT FRAME 20 TO BE HEAVILY CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810007Crossbeam · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED CROSSBEAM AT FRAME 20 TO BE HEAVILY CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810006Sill · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED NR 1 CABIN SILL RIGHT TO BE HEAVILY CORRODED. REMOVED CORRODED SILL AND INSTALLED SERVICABLE SILL USING EMB 120 STANDARD PRACTICES.SDR COMA9810005Buttstrap · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED NR 1 BUTTSTRAP TO BE HEAVILY CORRODED. REMOVED CORRODED BUTTSTRAP AND INSTALLED SERVICABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810004Buttstrap · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED NR 1 CENTER BUTTSTRAP TO BE HEAVILY CORRODED. REMOVED CORRODED BUTTSTRAP AND INSTALLED SERVICABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810013Crossbeam · corroded2C TASK 532D-147-03I REVEALED RIGHT CENTER CROSSBEAM AT FRAME 28 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERVICEBLE PART USING EMB 120 STANDARD PRACTICES.SDR COMA9810012Crossbeam · corroded2C TASK 5320-147-03I REVEALED LEFT CROSSBEAM AT FRAME 28 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERVICABLE PART USING EMB 120 STANDARD PRACTICES.SDR COMA9810011Crossbeam · corroded2C TASK 5320-147-03I REVEALED CROSSBEAM (RIGHT) AT FRAME 23 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB STANDARD PRACTICES.SDR COMA9810010Crossbeam · corroded2C INSPECTION TASK 5310-131-01I REVEALED THAT THE RIGHT CROSSBEAM AT FRAME 16 WAS CORRODED TO LIMITS. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB STANDARD PRACTICES.SDR COMA9810003Buttstrap · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT NR 1 BUTTSTRAP TO BE HEAVILY CORRODED. REMOVED CORRODED PART AND INSTALLED SERVICEABLE PART USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9810002Frame T-Section · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT MIDDLE T-SECTION AT FRAME 16 TO BE HEAVILY CORRODED. REMOVED CORRODED T-SECTION AND INSTALLED SERVICABLE T-SECTION USING EMB120 SRM STANDARD PRACTICES.SDR COMA9710483Solenoid · shortedON 1C TASK 35-09, THE OXYGEN MASKS AT ROW 9 FAILED TO DEPLOY. INVESTIGATION FOUND THE OXYGEN MASK DOOR SOLENOID TO BE SHORTED. THE SOLENOID WAS REPLACED WITH A NEW PART, OK FOR SERVICE.SDR COMA9710467Relay Box · malfunctionedSMOKE IN COCKPIT AND CABIN AFTER PUSH BACK. FOUND GROUND COOLING FANS NOT OPERATING. REPLACED THE LANDING GEAR RELAY BOX.SDR COMA9710333Pcu · damagedPCU ASSEMBLY REMOVED FROM AIRCRAFT FOR AD 95-22-12 COMPLIANCE. UPON INITIAL RECEIVING INSPECTION SEVERAL OF THE FORWARD PORTION OF THE SPLINES WERE FOUND TO BE GROUND DOWN. PCU WAS REMOVED FROM SERVICE AND RETURNED TO MANUFACTURER FOR FURTHER DISPOSITON.SDR COMA9710315Radar Antenna · failedWEATHER RADAR DOES NOT WORK. REPLACED THE ANTENNA.SDR COMA9710298Actuator · malfunctionFLAP CONTROL FAULT WARNING WITH FLAPS RETRACTED. REPLACED THE LT OUTBOARD FLAP ACTUATOR.SDR COMA9710276Skin · bird strikeBIRD STRIKE ON LOWER FUSELAGE. INSPECTED EXTERIOR OF AIRCRAFT AND FOUND NO EVIDENCE OF BIRD STRIKE.SDR COMA9710262Flap Contl Unit · malfunctionedFLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED THE FLAP CONTROL UNIT.SDR COMA9610338Deice Boots · wornLT AND RT WING DEICE BOOTS AND LT AND RT ENGINE INLET DEICE BOOTS FAILED DURING FLIGHT. REPLACED WING AND ENGINE INLET DEICE BOOTS.SDR COMA9610298Sign · missingEMERGENCY EXIT SIGN AT ROW 5 IS MISSING. REPLACED EMERGENCY EXIT SIGN.SDR COMA9610263Flap Contl Unit · malfunctionFLAP DISAGREE WARNING AFTER TAKEOFF. REPLACED THE FLAP CONTROL UNIT. PART TOTAL CYCLES, 2,052.SDR COMA9610158Propeller · leakingLEFT ENGINE LEAKED A LARGE AMOUNT OF OIL DURING TAXI FROM HANGAR TO GATE. REPLACED THE LT PROPELLER ASSY.SDR COMA9610137Control Valve · failedLEFT INLET BOOT FAILED IN-FLIGHT. REPLACED LEFT INLET DEICE EJECTOR VALVE.SDR COMA9610116Wire · chafedRT HYDRAULIC RESERVOIR LOW PRESSURE INDICATOR ILLUMINATED. REPAIRED CHAFED WIRE AT PRESSURE SWITCH.SDR COMA9610095Control Box · malfunctionLANDING GEAR INTRANSIT LIGHTS REMAINED ON WITH GEAR RETRACTED. REPLACED THE LANDING GEAR CONTROL BOX.SDR COMA9610084Flap Tracks · dirtyFLAP DISAGREEMENT WARNING WHEN FLAPS RETRACTED AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. CLEANED AND INSPECTED FLAP TRACKS AND OPERATIONAL CHECK NORMAL.SDR COMA9610046Annunciator · defectiveTAKEOFF FLAPS AURAL WARNING SOUNDED DURING TAKEOFF ROLL. REPLACED THE FLAP ANNUNCIATOR UNIT.SDR COMA9512035Iva-81a Av · defectiveTHE PILOTS VSI IS COMPLETELY UNUSABLE IN ALL PHASES OF FLIGHT. REPLACED THE PILOTS TCASIVSI.SDR COM11936Tq Sig Cond · defectiveLEFT TORQUE INDICATION ERRATIC. LEFT PROPELLER AUTOFEATHERED. REPLACED THE TORQUE SIGNAL CONDITIONER.SDR COM11924Ahrs · defectivePILOTS ESHI SHOWS RED FLAG. REPLACED THE NR NR 1 AHRS.SDR COM11859Engine · failedLEFT ENGINE FAILED ABRUPTLY IN FLIGHT. REMOVED AND REPLACED LEFT ENGINE.SDR COM11843Skin Support · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I AND 5720-552/652-01I. THE SKIN SUPPORTS WERE REPLACED IAW AERODESIGN REPORT NR 1327-2. P/N: 120-17056-007, 4 EA; 120-17056-019, 1 EA; 120-17056-013, 1 EA; 120-170SDR COM11838Sensor · defectiveNLG A SYSTEM INTRANSIT LIGHT IS ILLUMINATING INTERMITTENTLY. REPLACED THE NLG DOWNLOCK PROXIMITY SENSOR.
Back to N205CA, cancelled Feb 11, 2009