N241CA, cancelled Nov 16, 2006
Service difficulty reports · 35
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 = 'N241CA' AND deregistration_id = 'N241CA-2006-11-16' 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 = 'N241CA' AND deregistration_id = 'N241CA-2006-11-16' 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 COMA9810251Torque Ind · failedRIGHT HAND ENGINE TORQUE INDICATOR FAILED. REPLACED TORQUE INDICATOR.SDR COMA9810240Line · leakingWHILE RUNNING NR 2 ENGINE, IT STARTED LEAKING FUEL. REPLACED RIGHT VENT VALVE MOTIVE FLOW LINE.SDR COMA9810121Solenoid · shortedFLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER TRIPPED. REPLACED SOLENOID.SDR COMA9810112Wheel · crackedMAIN WHEEL ASSEMBLY WAS REMOVED FROM AIRCRAFT BY MECHANIC DUE TO LOW PRESSURE. TIRE SHOP FOUND INBOARD (P/N 300-604-1) WAS MISSING A SECTION OF WHEEL FLANGE APPROXIMATELY 12 INCHES LONG. WHEEL ASSEMBLY HAS GONE THRU 45 TIRE CHANGES SINCE NEW. WHEEL ASSEMBLYSDR COMA9810107Wheel · crackedMAIN WHEEL ASSEMBLY WAS REMOVED FROM AIRCRAFT BY MECHANIC DUE TO LOW PRESSURE. TIRE SHOP FOUND INBOARD (P/N 300-604-1) WAS MISSING A SECTION OF WHEEL FLANGE APPROXIMATELY 12 INCHES LONG. WHEEL ASSEMBLY (P/N 3-1446-1) WHEEL ASSEMBLY HAS GONE THROUGH 45 TIRE CSDR COMA9810075Connector · looseEMERGENCY LIGHT AT ROW 2 INOPERABLE. REPAIRED LOOSE CONNECTION AT BULB.SDR COMA9810063Eec · malfunctionedTORQUE INDICATION FLUCTUATED +- 20 PERCENT DURING TAKEOFF ROLL. DEFERRED THE ELECTRONIC ENGINE CONTROL SYSTEM.SDR COMA9810062Buttstrap · corrosionDURING 2C INSPECTION, TASK 5310-131-01I REVEALED CENTER BUTTSTRAP TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMBRAER 120 SRM STANDARD PRACTICES.SDR COMA9810061Buttstrap · corrosionDURING 2C INSPECTION, TASK 5310-131-01I REVEALED BUTTSTRAP TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMBRAER 120 SRM STANDARD PRACTICES.SDR COMA9810060Buttstrap · corrosionDURING 2C INSPECTION, TASK 5310-131-01I REVEALED BUTTSTRAP THAT WAS CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMBRAER 120 SRM STANDARD PRACTICES.SDR COMA9810059Crossbeam · corrosionDURING 2C INSPECTION, TASK 5310-131-01I REVEALED CROSSBEAM AT FRAME 20 TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMBRAER 120 SRM STANDARD PRACTICES.SDR COMA9810058Crossbeam · corrosionDURING 2C INSPECTION, TASK 5310-131-01I REVEALED THE CROSSBEAM AT FRAME 16 TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMBRAER SRM STANDARD PRACTICES.SDR COMA9810057Sill · corrosionDURING 2C INSPECTION, TASK 5310-131-01I REVEALED CABIN SILL TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMBRAER SRM STANDARD PRACTICES.SDR COMA9810056Sill · corrodedDURING 2C INSPECTION, TASK 5310-131-01I, REVEALED CABIN SILL TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMBRAER SRM STANDARD PRACTICES.SDR COMA9810055Tcas Tray · corrodedDURING 2C INSPECTION ZONE 100 TASK 5310-132-01I, FOUND TCAS SUPPORT TRAY CORRODED BEYOND LIMITS. REMOVED CORRODED TRAY AND BUILT UP NEW SERV TRAY IAW STC ST00075W1-D.SDR COMA9810043Connector · looseLANDING GEAR CONTROL COULD NOT BE SELECTED UP. GROUND SAFETY LOCK ENGAGED. SECURED LOOSE QUICK DISCONNECT COUPLING AT RIGHT HAND MLG WEIGHT ON WHEELS PROXIMITY SENSOR WIRING HARNESS.SDR COMA9810037Lamp · failedOVERHEAD EMERGENCY LIGHT AT ROW 2B IS INOP. REPLACED THE LIGHT BULB.SDR COMA9810022Lamp · failedEMERGENCY LIGHTS AT ROW SIX ARE INOPERATIVE. REPLACED LAMP FOR ROW SIX FLOOR EMERGENCY LIGHT TRACK.SDR COMA9710493Wire · failedLANDING GEAR CANNOT BE SELECTED TO RETRACT. CONTROL SELECTOR CANNOT BE MOVED. REPAIRED WARN WIRING IN RIGHT HAND MLG FOR THE AIR/GROUND WEIGHT ON WHEELS SYTEM.SDR COMA9710373Skin · corrodedDURING COMPLIANCE OF E-6 INSPECTION, THE FUSELAGE LOWER SKIN WAS FOUND CORRODED AT FRAMES NR 21, 22 AND 23. THREE SEPARATE REPAIRS WERE PERFORMED. THE DAMAGE AT FRAMES 21 AND 22 WERE REPAIRED PER SRM 53-00-01, FIGURE 202. THE DAMAGE AT FRAME 23 WAS REPAIREDSDR COMA9710336Fire Control · failedLEFT ENGINE WHEEL WELL FIRE WARNING DURING FLIGHT. ENGINE SECURED AND BOTH FIRE BOTTLES DISCHARGED. FIRE WARNING PERSISTED. FALSE WARNING, REPLACED THE FIRE DETECTOR CONTROL.SDR COMA9710313Safety Pin · not removedNLG DID NOT RETRACT. REMOVED DOWN LOCK SAFETY PIN FROM NLG. AIRCRAFT RETURNED TO SERVICE.SDR COMA9710310Skin · crackedWHILE AIRCRAFT WAS IN THE HANGAR FOR SCHEDULED MAINTENANCE, MECHANIC NOTICED A CRACK IN THE LEFT NACELLE OUTBOARD AFT SKIN, JUST BELOW THE ROLLER SUPPORT FOR THE OUTBOARD FLAP. THE SKIN WAS REPAIRED PER AERODESIGN REPORT NR 2331-1 REV IR, 6-12-97.SDR COMA9710304Connector · looseTAKEOFF TRIM AURAL WARNING SOUNDED DURING TAKEOFF. REPLACED IMPROPER WIRING CONNECTIONS AT THE ELEVATOR TRIM PROXIMITY SENSORS.SDR COMA9710302Aural Warning · sounded'TAKEOFF TRIM' AURAL WARNING SOUNDED DURING TAKE OFF. RESET AURAL WARNING COMPUTER. DISCREPANCY WOULD NOT DUPLICATE.SDR COMA9710093Prox Sensor · inoperativeGEAR HANDLE WOULD NOT MOVE AFTER TAKEOFF. REPLACED RT MLG PROX. SENSOR.SDR COMA9610281Solenoid · malfunctionFLIGHT IDLE STOP SOLENOID CHECK DOES NOT FUNCTION. REPLACED SOLENOID.SDR COMA9610160Hydraulic Pump · failedGREEN HYDRAULIC SYSTEM ELECTRIC PUMP, FAILED. REPLACED THE GREEN SYSTEM ELECTRIC HYDRAULIC PUMP.SDR COMA9512026Dnlock Sensor · defectiveLANDING GEAR WOULD NOT EXTEND NORMALLY. EMERGENCY EXTENTION SYSTEM USED. REPLACED DEFECTIVE DOWNLOCK PROXIMITY SENSOR.SDR COMA9512013Roller · wornFLAP DISAGREEMENT WARNING CLIMB. OUTBOARD FLAPS DID NOT RETRACT FULLY. REPLACED THE LT OUTBOARD FLAP ASSY ROLLERS.SDR COM11944Sensor · damagedDURING LANDING, LEFT MLG INDICATED UNSAFE ON A-SYSTEM AND SAFE ON B-SYSTEM. REPLACED DAMAGED PROXIMITY SENSOR FOR A SYSTEM DOWNLOCK.SDR COM11919Skin Support · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I. THE SKIN SUPPORTS WERE REPAIRED IAW AERO-DESIGN REPORT NR 1327-2. P/N; 120-17056-005, 1 EA; 120-17056-007, 4 EA; 120-17056-019, 1 EA; 120-17056-017, 1 EA; 120-SDR COM11897Pcu · out of adjustDURING TAKEOFF LT NP INDICATED 99.3 PERCENT. ADJUSTED PCU FOR 100 PERCENT PROPELLER RPM.SDR COM11850Contl Valve · defectiveANTI-SKID SYSTEM DOES NOT TEST. REPLACED BRAKE ANTI-SKID CONTROL VALVE.SDR COM11789Control Cable · brokenGO AROUND BUTTON ON LEFT POWER LEVER IS INOPERATIVE. REPAIRED BROKEN WIRE IN POWER LEVER QUADRANT.
Back to N241CA, cancelled Nov 16, 2006