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.

SDR COMA9810251Torque Ind · failedRIGHT HAND ENGINE TORQUE INDICATOR FAILED. REPLACED TORQUE INDICATOR.Nov 5, 1998 · N241CA · Emb EMB120RT · Engine BMEP/Torque IndicatingSDR COMA9810240Line · leakingWHILE RUNNING NR 2 ENGINE, IT STARTED LEAKING FUEL. REPLACED RIGHT VENT VALVE MOTIVE FLOW LINE.Oct 20, 1998 · N241CA · Emb EMB120RT · Aircraft Fuel Distribution SystemSDR COMA9810121Solenoid · shortedFLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER TRIPPED. REPLACED SOLENOID.May 14, 1998 · N241CA · Emb EMB120RT · Power LeverSDR 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 ASSEMBLYApr 20, 1998 · N241CA · Emb EMB120RT · Wheel/Ski/FloatSDR 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 CApr 20, 1998 · N241CA · Emb EMB120RT · Wheel/Ski/FloatSDR COMA9810075Connector · looseEMERGENCY LIGHT AT ROW 2 INOPERABLE. REPAIRED LOOSE CONNECTION AT BULB.Mar 24, 1998 · N241CA · Emb EMB120RT · Emergency LightingSDR COMA9810063Eec · malfunctionedTORQUE INDICATION FLUCTUATED +- 20 PERCENT DURING TAKEOFF ROLL. DEFERRED THE ELECTRONIC ENGINE CONTROL SYSTEM.Mar 6, 1998 · N241CA · Emb EMB120RT · Fuel Control/Turbine EnginesSDR 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.Mar 4, 1998 · N241CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Mar 4, 1998 · N241CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Mar 4, 1998 · N241CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Mar 4, 1998 · N241CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Mar 4, 1998 · N241CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Mar 4, 1998 · N241CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Mar 4, 1998 · N241CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Mar 4, 1998 · N241CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Feb 10, 1998 · N241CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9810037Lamp · failedOVERHEAD EMERGENCY LIGHT AT ROW 2B IS INOP. REPLACED THE LIGHT BULB.Feb 8, 1998 · N241CA · Emb EMB120RT · Emergency LightingSDR COMA9810022Lamp · failedEMERGENCY LIGHTS AT ROW SIX ARE INOPERATIVE. REPLACED LAMP FOR ROW SIX FLOOR EMERGENCY LIGHT TRACK.Jan 12, 1998 · N241CA · Emb EMB120RT · Emergency LightingSDR 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.Dec 10, 1997 · N241CA · Emb EMB120RT · Landing Gear System WiringSDR 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 REPAIREDAug 20, 1997 · N241CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR 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.Jul 27, 1997 · N241CA · Emb EMB120RT · Fire DetectionSDR COMA9710313Safety Pin · not removedNLG DID NOT RETRACT. REMOVED DOWN LOCK SAFETY PIN FROM NLG. AIRCRAFT RETURNED TO SERVICE.Jun 14, 1997 · N241CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR 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.Jun 12, 1997 · N241CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR COMA9710304Connector · looseTAKEOFF TRIM AURAL WARNING SOUNDED DURING TAKEOFF. REPLACED IMPROPER WIRING CONNECTIONS AT THE ELEVATOR TRIM PROXIMITY SENSORS.May 30, 1997 · N241CA · Emb EMB120RT · Central WarningSDR COMA9710302Aural Warning · sounded'TAKEOFF TRIM' AURAL WARNING SOUNDED DURING TAKE OFF. RESET AURAL WARNING COMPUTER. DISCREPANCY WOULD NOT DUPLICATE.May 29, 1997 · N241CA · Emb EMB120RT · Central WarningSDR COMA9710093Prox Sensor · inoperativeGEAR HANDLE WOULD NOT MOVE AFTER TAKEOFF. REPLACED RT MLG PROX. SENSOR.Jan 27, 1997 · N241CA · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9610281Solenoid · malfunctionFLIGHT IDLE STOP SOLENOID CHECK DOES NOT FUNCTION. REPLACED SOLENOID.Sep 18, 1996 · N241CA · Emb EMB120RT · Power LeverSDR COMA9610160Hydraulic Pump · failedGREEN HYDRAULIC SYSTEM ELECTRIC PUMP, FAILED. REPLACED THE GREEN SYSTEM ELECTRIC HYDRAULIC PUMP.May 31, 1996 · N241CA · Emb EMB120RT · Hydraulic Pump (Electric/Engine), MainSDR COMA9512026Dnlock Sensor · defectiveLANDING GEAR WOULD NOT EXTEND NORMALLY. EMERGENCY EXTENTION SYSTEM USED. REPLACED DEFECTIVE DOWNLOCK PROXIMITY SENSOR.Dec 14, 1995 · N241CA · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9512013Roller · wornFLAP DISAGREEMENT WARNING CLIMB. OUTBOARD FLAPS DID NOT RETRACT FULLY. REPLACED THE LT OUTBOARD FLAP ASSY ROLLERS.Nov 27, 1995 · N241CA · Emb EMB120RT · Trailing Edge FlapsSDR COM11944Sensor · damagedDURING LANDING, LEFT MLG INDICATED UNSAFE ON A-SYSTEM AND SAFE ON B-SYSTEM. REPLACED DAMAGED PROXIMITY SENSOR FOR A SYSTEM DOWNLOCK.Aug 4, 1995 · N241CA · Emb EMB120RT · Landing Gear Position and WarningSDR 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-Jun 17, 1995 · N241CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COM11897Pcu · out of adjustDURING TAKEOFF LT NP INDICATED 99.3 PERCENT. ADJUSTED PCU FOR 100 PERCENT PROPELLER RPM.May 21, 1995 · N241CA · Emb EMB120RT · Propeller Controlling SystemSDR COM11850Contl Valve · defectiveANTI-SKID SYSTEM DOES NOT TEST. REPLACED BRAKE ANTI-SKID CONTROL VALVE.Mar 31, 1995 · N241CA · Emb EMB120RT · Landing Gear Brake SystemSDR COM11789Control Cable · brokenGO AROUND BUTTON ON LEFT POWER LEVER IS INOPERATIVE. REPAIRED BROKEN WIRE IN POWER LEVER QUADRANT.Feb 16, 1995 · N241CA · Emb EMB120RT · Power Lever
Back to N241CA, cancelled Nov 16, 2006