N267CA, cancelled Nov 27, 2007

Service difficulty reports · 99

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 = 'N267CA' AND deregistration_id = 'N267CA-2007-11-27'
  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 COMA0210023LampFLIGHT 5005 ONE EMERGENCY FLOOR LIGHT AT ROW 8 IS INOP.DEFERRED MAINT PER MEL.May 31, 2002 · N267CA · Emb EMB120RT · Emergency LightingSDR COMA0210018Sign · brokenFLIGHT 5021 EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN.REPLACED EXIT SIGN.May 3, 2002 · N267CA · Emb EMB120RT · Emergency LightingSDR COMA0210016DoorFLIGHT 5061 SERVICE DOOR WARNING DURING T/O.CLOSED AND LATCHED SERVICE DOOR.Apr 18, 2002 · N267CA · Emb EMB120RT · Service DoorsSDR COMA0210005Servo · bindingFLIGHT 5009 PILOT AND COPILOT RUDDER PEDALS BINDING.REPLACED THE RUDDER SERVO.Feb 17, 2002 · N267CA · Emb EMB120RT · Autopilot SystemSDR COMA0110152Pin · brokenFLIGHT MECHANICS TAXIED A/C TO HANGAR FROM GATE AND FELT A BRAKE DRAGGING. A/C WAS JACKED AND THE LEFT INBD BRAKE WAS FOUND TO BE DRAGGING. AFTER THE BRAKE WAS REMOVED, IT WAS DISCOVERED THAT ONE OF THE RETURN SPRING ASSEMBLIES "PIN" WAS BROKEN AT END THAT ATOct 23, 2001 · N267CA · Emb EMB120RT · BrakeSDR COMA0110153Controller · faultyFLIGHT #5009. DURING CLIMB OUT OF MCO A LOUD AIR NOISE EMANATING FROM THE NOSE AREA, AIRCRAFT RETURNED TO THE FIELD.REPLACED THE LANDING GEAR RELAY BOX.Oct 22, 2001 · N267CA · Emb EMB120RT · Landing Gear Door Retract SectionSDR COMA0110150Sensor · malfunctionedFLIGHT 5038. T/O TRIM AURAL WARNING WHEN POWER LEVERS ADVANCED. COULD NOT DUPLICATE DISCREPANCY AND A/C RETURNED TO SERVICE. DURING CALLBACK MAINTENANCE THE LEFT ELEVATOR TRIM PROXIMITY SENSOR WAS DETERMINED TO BE DEFECTIVE AND WAS REPLACED.Oct 1, 2001 · N267CA · Emb EMB120RT · Central WarningSDR COMA0110141Computer · faultyFLIGHT #5027. DURING CLIMB-OUT OF MCO RECEIVED HEADING AND PITCH CAPTIONS, RE-SETTING THE HEADING MONITOR CLEARED THE PITCH CAPTION, BUT HEADING CAPTION REMAINED.REPLACED THE AHC-85.Sep 4, 2001 · N267CA · Emb EMB120RT · Attitude and Direction Data SystemSDR COMA0110135Proximity Switch · malfunctionedTAKE OFF TRIM AURAL WARNING.REPLACED DEFECTIVE ELEV. TRIM PROXIMITY SENSOR.Aug 1, 2001 · N267CA · Emb EMB120RT · Central WarningSDR COMA0110131Proximity Switch · malfunctionedTAKE OFF TRIM AURAL WARNING. REPLACED DEFECTIVE ELEV. TRIM PROXIMITY SENSOR.Aug 1, 2001 · N267CA · Emb EMB120RT · Central WarningSDR COMA0110022Skin · gougedTHE AIRCRAFT SKIN BELOW THE LAVATORY DUMP VALVE DOUBLER IS GOUGED. THE DAMAGE WAS REPAIRED BY INSTALLING AN INTERNAL PATCH (DOUBLER) IN ACCORDANCE WITH EMBRAER FAX SST-1403/003.Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA0110021Support Bracket · crackedA SKIN SUPPORT FOR FRAME 13A IS CRACKED. THE REPAIR IS TO INSTALL A DOUBLER IN ACCORDANCE WITH AERODESIGN REPORT NR 3653-1.Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110020Bracket · crackedTHE AIRCRAFT''S CARGO DOOR TRACK BRACKET IS CRACKED. THE CARGO DOOR AFT TRACK BRACKET WAS REPLACED USING ALTERNATE RIVETS IN ACCORDANCE WITH AERODESING REPORT NR 1657-3.Jan 12, 2001 · N267CA · Emb EMB120RT · Cargo/Baggage DoorsSDR COMA0110019Frame · nickedTHE AIRCRAFT''S FRAME 46A HAS A NICK IN THE UPPER FRAME FLANGE AT A PREVIOUSLY INSTALLED ANGLE. THE FRAME WAS REPAIRED BY REMOVING THE OLD ANGLE, DRESSING AND BLENDING THE NICK AND INSTALLING A SERVICEABLE ANGLE IN ACCORDANCE WITH AERODESIGN REPORT NR 2400-4.Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA0110018Strap · corrodedTHE AIRCRAFT HAS CORROSION PAST THE LIMIT ON THE FLOORBEAM BUTT STRAP UNDER THE FLOOR PANEL, LOCATED AT FRAME 13A. THE FLOORBEAM BUTT STRAP WAS REPLACED IN ACCORDANCE WITH AERODESIGN REPORT NR 1671-2.Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0110017Strap · corrodedTHE AIRCRAFT HAS CORROSION PAST THE LIMIT ON THE FLOORBEAM BUTT STRAP UNDER THE FLOOR PANEL, LOCATED AT FRAME 13A. THE FLOORBEAM BUTT STRAP WAS REPLACED IN ACCORDANCE WITH AERODESIGN REPORT NR 1671-2.Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0110015Skin · crackedTHE LEFT HAND NACELLE AFT OUTBOARD SKIN IS CRACKED. A DOUBLER WAS INSTALLED IN ACCORDANCE WITH AERODESIGN REPORT NR 3860-1.Jan 12, 2001 · N267CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR COMA0110014Support Bracket · crackedTHE AIRCRAFT''S SKIN SUPPORT FOR FRAME 40 IS CRACKED. SKIN SUPPORT WAS REPLACED WITH A SERVICEABLE UNIT IN ACCORDANCE WITH AERODESIGN REPORT NR 3859-1.Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110013Floor Support · corrodedTHE AIRCRAFT''S TWO FLOOR SUPPORT ANGLES UNDER THE PAX DOOR ENTRYWAY THRESHOLD ARE CORRODED. THE PARTS WERE REPLACED IN ACCORDANCE WITH AERODESIGN REPORT NR 3711-1.Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110012Firewall · crackedTHE AIRCRAFT HAS A CRACK IN THE APU FIREWALL WEB. INSTALLED A DOUBLER IN ACCORDANCE WITH AERODESIGN REPORT NR 2677-3.Jan 12, 2001 · N267CA · Emb EMB120RT · Nacelle/Pylon, Bulkhead/FirewallSDR COMA0110011Floorbeam · corrodedTHE AIRCRAFT SUSTAINED DAMAGE IN THE FORM OF CORROSION TO THE UPPER SURFACE OF THE CENTER OMEGA FLOORBEAM. THE OMEGA FLOORBEAM WAS REPAIRED IN ACCORDANCE WITH AERODESIGN REPORT NR 2181-11.Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0110010Floorbeam · corrodedTHE AIRCRAFT OMEGA BEAMS (P/N 120-46158-001) QTY 2, AND 120-46258-002 QTY 1, HAVE EXCESSIVE CORROSION. THE OMEGA BEAMS WERE REPLACED IN ACCORDANCE WITH AERODESIGN REPORT NR 2174-1.Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COM0160009Attach Angle · crackedTHE AIRCRAFT LEFT AND RIGHT WING ATTACH ANGLES ARE CRACKED. THE ANGLES WERE REPAIRED IN ACCORDANCE WITH SRM CHAPTER 53-20-13 PAGES 205 AND 206 AND AERODESIGN REPORT 1226-21.Jan 12, 2001 · N267CA · Cndair CL6002B19 · Fuselage, Wing Attach FittingsSDR COMA0110016Floor Support · crackedTHE AIRCRAFT FLOOR PROPS IN THE COCKPIT ARE CRACKED. THE REPAIR CONSISTS OF CUTTING OUT THE DAMAGED AREA AND SPLICING IN A NEW PIECE IN ACCORDANCE WITH AERODESIGN REPORT 3647-1.Jan 12, 2001 · N267CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0110009Fairing · crackedTHE AIRCRAFT LEFT AND RIGHT WING ATTACH ANGLES ARE CRACKED. THE ANGLES WERE REPAIRED IN ACCORDANCE WITH SRM CHAPTER 53-20-13 PAGES 205 AND 206 AND AERODESIGN REPORT 1226-21.Jan 12, 2001 · N267CA · Cndair CL6002B19 · Aerodynamic FairingsSDR COMA0060795Solenoid · shortedLEFT HAND FLIGHT IDLE STOP CIRCUIT BREAKER IS TRIPPED. REPLACED FIS SOLENOID.Oct 4, 2000 · N267CA · Cndair CL6002B19 · Engine ControlsSDR COMA0010365Switch · brokenAUTOFEATHER WARNING DURING TAKEOFF ROLL, AIRCRAFT RETURNED TO THE GATE. REPLACED BROKEN MICRO-SWITCH ON THE LEFT POWER LEVER.Sep 15, 2000 · N267CA · Emb EMB120RT · Power LeverSDR COMA0010319Skin · crackedDURING A 1C INSPECTION FOUND A CRACK APPROXIMATELY .125 INCH LONG EXTENDING FROM A RIVET ON THE RIGHT SIDE POST SKIN BETWEEN THE RIGHT DV WINDOW AND THE RIGHT WINDSHIELD. STOP DRILLED CRACK AND INSTALLED A DOUBLER IAW EMBRAER REPAIR EST - 474/95.Aug 24, 2000 · N267CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA0010247Solenoid · failedFLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER IS TRIPPED.\NREPLACED THE FLIGHT-IDLE STOP SOLENOID.Jul 3, 2000 · N267CA · Emb EMB120RT · Engine ControlsSDR COMA0010244Computer · malfunctionedATTITUDE DISPLAY WARNING ON MAP. REPLACED THE NR 2 AHRS COMPUTER.Jul 2, 2000 · N267CA · Emb EMB120RT · Attitude and Direction Data SystemSDR COMA0010243Warning System · false activationTAKE OFF TRIM CONFIG WARNING. COULD NOT DUPLICATE. TRIM AURAL WARNING SYSTEM CHECKS SATISFACTORY.Jun 30, 2000 · N267CA · Emb EMB120RT · Central WarningSDR COMA0010162Sensor · malfunctionedTAKEOFF TRIM WARNING. REPLACED THE LEFT HAND ELEVATOR TRIM PROXIMITY SENSOR.Jun 9, 2000 · N267CA · Emb EMB120RT · Elevator Tab Control SystemSDR COMA0010054Solenoid · malfunctionedFLIGHT IDLE SOLENOID CIRCUIT BREAKER TRIPPED. REPLACED THE LEFT HAND SOLENOID.Apr 16, 2000 · N267CA · Emb EMB120RT · Power LeverSDR COMA0010044Warning System · activatedTRIM FAIL T/O CONFIG WARNING. COULD NOT DUPLICATE. SYSTEM TEST WAS NORMAL.Mar 24, 2000 · N267CA · Emb EMB120RT · Central WarningSDR COMA0010006Wire · disconnectedTAKEOFF CONFIG WARNING. REPAIRED ELEVATOR TRIM PROXIMITY SENSOR WIRING CONNECTIONS.Jan 9, 2000 · N267CA · Emb EMB120RT · Elevator Tab Control SystemSDR COMA9910187Blade · damagedFOUND NR 4 BLADE RIGHT PROP HAD TIP DAMAGE. REMOVED AND REPLACED NR 4 BLADE RIGHT PROP.Dec 16, 1999 · N267CA · Emb EMB120RT · Propeller Blade SectionSDR COMA9910153Bulb · failedFLOOR TRACK LIGHT AT SEAT 9A IS INOPERABLE. REMOVED AND REPLACED BULB.Sep 21, 1999 · N267CA · Emb EMB120RT · Emergency LightingSDR COMA9910130Light · missingEMERGENCY EXIT LIGHT CONVER MISSING ROW 5. REPLACED LIGHT ASSY.Aug 9, 1999 · N267CA · Emb EMB120RT · Emergency LightingSDR COMA9910119Hyd Pump · leakingBLUE HYDRAULIC SYSTEM LOW PRESSURE WARNING. REPLACED ENGINE HYDRAULIC PUMP.Jul 23, 1999 · N267CA · Emb EMB120RT · Hydraulic Pump (Electric/Engine), MainSDR COMA9910087Light · inoperativeGRR - FLT 5024 - EMERGENCY LIGHTS ARE INOPERABLE. COULD NOT DUPLICATE. EMERGENCY LIGHTS OPERATE NORMAL. (M)May 28, 1999 · N267CA · Emb EMB120RT · Emergency LightingSDR COMA9910044Pcu · malfunctionedRIGHT HAND PROPELLER OVER SPEED TO 103 DEGREES. REPLACED THE PROPELLER CONTROL UNIT.Mar 21, 1999 · N267CA · Emb EMB120RT · Propeller Controlling SystemSDR COMA9910037Fuel Door · missingSINGLE POINT FUEL SERVICE DOOR MISSING. REPAIRED DAMAGE CAUSED BY SEPARATION OF FUEL SERVICE DOOR AND REPLACED DOOR.Feb 20, 1999 · N267CA · Emb EMB120RT · Fluid Service DoorsSDR COMA9810245Sensor · burntLAVATORY SMOKE ALARM ACTIVATED SMOKE IN COCKPIT. REPLACED BURNT AOA VANE CURRENT SENSOR.Oct 29, 1998 · N267CA · Emb EMB120RT · Stall Warning SystemSDR COMA9810136Control Unit · failedAIRCRAFT HAS NO BRAKES DURING LANDING ROLL. REPLACED THE BRAKE CONTROL UNIT.Jun 5, 1998 · N267CA · Emb EMB120RT · Landing Gear Brake SystemSDR COMA9810080Sensor · malfunctionRT MLG, GREEN DOWN INDICATION, CAME ON WITH GEAR RETRACTED. REPLACED THE RT MLG DOWNLOCK SENSOR.Apr 1, 1998 · N267CA · Emb EMB120 · Landing Gear Position and WarningSDR COMA9810047Control Box · malfunctionLANDING GEAR WILL NOT RETRACT. REPLACED THE LANDING GEAR CONTROL BOX.Feb 23, 1998 · N267CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9810039Sensor · malfunctionTAKEOFF TRIM WARNING SOUNDED. REPLACED THE ELEVATOR TRIM TAB PROXIMITY SENSORS.Feb 5, 1998 · N267CA · Emb EMB120RT · Elevator Tab Control SystemSDR COMA9810032Bulb · failedFLOOR EMERGENCY LIGHT AT GALLEY AREA IS INOP. REPLACED BULB.Jan 24, 1998 · N267CA · Emb EMB120RT · Emergency LightingSDR COMA9710471Battery · dischargedEMERGENCY LIGHTS ARE INOP. REPLACED THE EMERGENCY LIGHTS BATTERIES.Nov 9, 1997 · N267CA · Emb EMB120RT · Emergency LightingSDR COMA9710387Floorbeam · corrodedDURING 4C INSEPCTION TASK 5320-151/152-01I, FOUND RIGHT HAND FLOORBEAM AT FRAME 33 TO BE CORRODED. REMOVED CORRODED FLOORBEAM AND INSTALLED SERV PART IAW EMB 120 SRM CHAPTER 51.Aug 20, 1997 · N267CA · Emb EMB120RT · Fuselage Main, Floor Beam
Back to N267CA, cancelled Nov 27, 2007