# Service difficulty reports: N267CA, cancelled Nov 27, 2007

A list on [N267CA, cancelled Nov 27, 2007](https://openairdocs.org/deregistered/N267CA-2007-11-27.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 99 reports

- [SDR COMA0210023](https://openairdocs.org/sdr/COMA0210023.md): Lamp · May 31, 2002 · N267CA · Emb EMB120RT · Emergency Lighting
  > FLIGHT 5005 ONE EMERGENCY FLOOR LIGHT AT ROW 8 IS INOP.DEFERRED MAINT PER MEL.
- [SDR COMA0210018](https://openairdocs.org/sdr/COMA0210018.md): Sign · broken · May 3, 2002 · N267CA · Emb EMB120RT · Emergency Lighting
  > FLIGHT 5021 EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN.REPLACED EXIT SIGN.
- [SDR COMA0210016](https://openairdocs.org/sdr/COMA0210016.md): Door · Apr 18, 2002 · N267CA · Emb EMB120RT · Service Doors
  > FLIGHT 5061 SERVICE DOOR WARNING DURING T/O.CLOSED AND LATCHED SERVICE DOOR.
- [SDR COMA0210005](https://openairdocs.org/sdr/COMA0210005.md): Servo · binding · Feb 17, 2002 · N267CA · Emb EMB120RT · Autopilot System
  > FLIGHT 5009 PILOT AND COPILOT RUDDER PEDALS BINDING.REPLACED THE RUDDER SERVO.
- [SDR COMA0110152](https://openairdocs.org/sdr/COMA0110152.md): Pin · broken · Oct 23, 2001 · N267CA · Emb EMB120RT · Brake
  > FLIGHT 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 AT
- [SDR COMA0110153](https://openairdocs.org/sdr/COMA0110153.md): Controller · faulty · Oct 22, 2001 · N267CA · Emb EMB120RT · Landing Gear Door Retract Section
  > FLIGHT #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.
- [SDR COMA0110150](https://openairdocs.org/sdr/COMA0110150.md): Sensor · malfunctioned · Oct 1, 2001 · N267CA · Emb EMB120RT · Central Warning
  > FLIGHT 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.
- [SDR COMA0110141](https://openairdocs.org/sdr/COMA0110141.md): Computer · faulty · Sep 4, 2001 · N267CA · Emb EMB120RT · Attitude and Direction Data System
  > FLIGHT #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.
- [SDR COMA0110135](https://openairdocs.org/sdr/COMA0110135.md): Proximity Switch · malfunctioned · Aug 1, 2001 · N267CA · Emb EMB120RT · Central Warning
  > TAKE OFF TRIM AURAL WARNING.REPLACED DEFECTIVE ELEV. TRIM PROXIMITY SENSOR.
- [SDR COMA0110131](https://openairdocs.org/sdr/COMA0110131.md): Proximity Switch · malfunctioned · Aug 1, 2001 · N267CA · Emb EMB120RT · Central Warning
  > TAKE OFF TRIM AURAL WARNING. REPLACED DEFECTIVE ELEV. TRIM PROXIMITY SENSOR.
- [SDR COMA0110022](https://openairdocs.org/sdr/COMA0110022.md): Skin · gouged · Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Main, Plate/Skin
  > THE 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.
- [SDR COMA0110021](https://openairdocs.org/sdr/COMA0110021.md): Support Bracket · cracked · Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > A SKIN SUPPORT FOR FRAME 13A IS CRACKED. THE REPAIR IS TO INSTALL A DOUBLER IN ACCORDANCE WITH AERODESIGN REPORT NR 3653-1.
- [SDR COMA0110020](https://openairdocs.org/sdr/COMA0110020.md): Bracket · cracked · Jan 12, 2001 · N267CA · Emb EMB120RT · Cargo/Baggage Doors
  > THE 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.
- [SDR COMA0110019](https://openairdocs.org/sdr/COMA0110019.md): Frame · nicked · Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Main, Frame
  > THE 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.
- [SDR COMA0110018](https://openairdocs.org/sdr/COMA0110018.md): Strap · corroded · Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Main, Structure
  > THE 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.
- [SDR COMA0110017](https://openairdocs.org/sdr/COMA0110017.md): Strap · corroded · Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Main, Structure
  > THE 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.
- [SDR COMA0110015](https://openairdocs.org/sdr/COMA0110015.md): Skin · cracked · Jan 12, 2001 · N267CA · Emb EMB120RT · Nacelle/Pylon, Plate/Skin
  > THE LEFT HAND NACELLE AFT OUTBOARD SKIN IS CRACKED. A DOUBLER WAS INSTALLED IN ACCORDANCE WITH AERODESIGN REPORT NR 3860-1.
- [SDR COMA0110014](https://openairdocs.org/sdr/COMA0110014.md): Support Bracket · cracked · Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > THE 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.
- [SDR COMA0110013](https://openairdocs.org/sdr/COMA0110013.md): Floor Support · corroded · Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > THE 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.
- [SDR COMA0110012](https://openairdocs.org/sdr/COMA0110012.md): Firewall · cracked · Jan 12, 2001 · N267CA · Emb EMB120RT · Nacelle/Pylon, Bulkhead/Firewall
  > THE AIRCRAFT HAS A CRACK IN THE APU FIREWALL WEB. INSTALLED A DOUBLER IN ACCORDANCE WITH AERODESIGN REPORT NR 2677-3.
- [SDR COMA0110011](https://openairdocs.org/sdr/COMA0110011.md): Floorbeam · corroded · Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Main, Floor Beam
  > THE 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.
- [SDR COMA0110010](https://openairdocs.org/sdr/COMA0110010.md): Floorbeam · corroded · Jan 12, 2001 · N267CA · Emb EMB120RT · Fuselage Main, Floor Beam
  > THE 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.
- [SDR COM0160009](https://openairdocs.org/sdr/COM0160009.md): Attach Angle · cracked · Jan 12, 2001 · N267CA · Cndair CL6002B19 · Fuselage, Wing Attach Fittings
  > THE 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.
- [SDR COMA0110016](https://openairdocs.org/sdr/COMA0110016.md): Floor Support · cracked · Jan 12, 2001 · N267CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE 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.
- [SDR COMA0110009](https://openairdocs.org/sdr/COMA0110009.md): Fairing · cracked · Jan 12, 2001 · N267CA · Cndair CL6002B19 · Aerodynamic Fairings
  > THE 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.
- [SDR COMA0060795](https://openairdocs.org/sdr/COMA0060795.md): Solenoid · shorted · Oct 4, 2000 · N267CA · Cndair CL6002B19 · Engine Controls
  > LEFT HAND FLIGHT IDLE STOP CIRCUIT BREAKER IS TRIPPED. REPLACED FIS SOLENOID.
- [SDR COMA0010365](https://openairdocs.org/sdr/COMA0010365.md): Switch · broken · Sep 15, 2000 · N267CA · Emb EMB120RT · Power Lever
  > AUTOFEATHER WARNING DURING TAKEOFF ROLL, AIRCRAFT RETURNED TO THE GATE. REPLACED BROKEN MICRO-SWITCH ON THE LEFT POWER LEVER.
- [SDR COMA0010319](https://openairdocs.org/sdr/COMA0010319.md): Skin · cracked · Aug 24, 2000 · N267CA · Emb EMB120RT · Fuselage Main, Plate/Skin
  > DURING 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.
- [SDR COMA0010247](https://openairdocs.org/sdr/COMA0010247.md): Solenoid · failed · Jul 3, 2000 · N267CA · Emb EMB120RT · Engine Controls
  > FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER IS TRIPPED.\NREPLACED THE FLIGHT-IDLE STOP SOLENOID.
- [SDR COMA0010244](https://openairdocs.org/sdr/COMA0010244.md): Computer · malfunctioned · Jul 2, 2000 · N267CA · Emb EMB120RT · Attitude and Direction Data System
  > ATTITUDE DISPLAY WARNING ON MAP. REPLACED THE NR 2 AHRS COMPUTER.
- [SDR COMA0010243](https://openairdocs.org/sdr/COMA0010243.md): Warning System · false activation · Jun 30, 2000 · N267CA · Emb EMB120RT · Central Warning
  > TAKE OFF TRIM CONFIG WARNING. COULD NOT DUPLICATE. TRIM AURAL WARNING SYSTEM CHECKS SATISFACTORY.
- [SDR COMA0010162](https://openairdocs.org/sdr/COMA0010162.md): Sensor · malfunctioned · Jun 9, 2000 · N267CA · Emb EMB120RT · Elevator Tab Control System
  > TAKEOFF TRIM WARNING. REPLACED THE LEFT HAND ELEVATOR TRIM PROXIMITY SENSOR.
- [SDR COMA0010054](https://openairdocs.org/sdr/COMA0010054.md): Solenoid · malfunctioned · Apr 16, 2000 · N267CA · Emb EMB120RT · Power Lever
  > FLIGHT IDLE SOLENOID CIRCUIT BREAKER TRIPPED. REPLACED THE LEFT HAND SOLENOID.
- [SDR COMA0010044](https://openairdocs.org/sdr/COMA0010044.md): Warning System · activated · Mar 24, 2000 · N267CA · Emb EMB120RT · Central Warning
  > TRIM FAIL T/O CONFIG WARNING. COULD NOT DUPLICATE. SYSTEM TEST WAS NORMAL.
- [SDR COMA0010006](https://openairdocs.org/sdr/COMA0010006.md): Wire · disconnected · Jan 9, 2000 · N267CA · Emb EMB120RT · Elevator Tab Control System
  > TAKEOFF CONFIG WARNING. REPAIRED ELEVATOR TRIM PROXIMITY SENSOR WIRING CONNECTIONS.
- [SDR COMA9910187](https://openairdocs.org/sdr/COMA9910187.md): Blade · damaged · Dec 16, 1999 · N267CA · Emb EMB120RT · Propeller Blade Section
  > FOUND NR 4 BLADE RIGHT PROP HAD TIP DAMAGE. REMOVED AND REPLACED NR 4 BLADE RIGHT PROP.
- [SDR COMA9910153](https://openairdocs.org/sdr/COMA9910153.md): Bulb · failed · Sep 21, 1999 · N267CA · Emb EMB120RT · Emergency Lighting
  > FLOOR TRACK LIGHT AT SEAT 9A IS INOPERABLE. REMOVED AND REPLACED BULB.
- [SDR COMA9910130](https://openairdocs.org/sdr/COMA9910130.md): Light · missing · Aug 9, 1999 · N267CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY EXIT LIGHT CONVER MISSING ROW 5. REPLACED LIGHT ASSY.
- [SDR COMA9910119](https://openairdocs.org/sdr/COMA9910119.md): Hyd Pump · leaking · Jul 23, 1999 · N267CA · Emb EMB120RT · Hydraulic Pump (Electric/Engine), Main
  > BLUE HYDRAULIC SYSTEM LOW PRESSURE WARNING. REPLACED ENGINE HYDRAULIC PUMP.
- [SDR COMA9910087](https://openairdocs.org/sdr/COMA9910087.md): Light · inoperative · May 28, 1999 · N267CA · Emb EMB120RT · Emergency Lighting
  > GRR - FLT 5024 - EMERGENCY LIGHTS ARE INOPERABLE. COULD NOT DUPLICATE. EMERGENCY LIGHTS OPERATE NORMAL. (M)
- [SDR COMA9910044](https://openairdocs.org/sdr/COMA9910044.md): Pcu · malfunctioned · Mar 21, 1999 · N267CA · Emb EMB120RT · Propeller Controlling System
  > RIGHT HAND PROPELLER OVER SPEED TO 103 DEGREES. REPLACED THE PROPELLER CONTROL UNIT.
- [SDR COMA9910037](https://openairdocs.org/sdr/COMA9910037.md): Fuel Door · missing · Feb 20, 1999 · N267CA · Emb EMB120RT · Fluid Service Doors
  > SINGLE POINT FUEL SERVICE DOOR MISSING. REPAIRED DAMAGE CAUSED BY SEPARATION OF FUEL SERVICE DOOR AND REPLACED DOOR.
- [SDR COMA9810245](https://openairdocs.org/sdr/COMA9810245.md): Sensor · burnt · Oct 29, 1998 · N267CA · Emb EMB120RT · Stall Warning System
  > LAVATORY SMOKE ALARM ACTIVATED SMOKE IN COCKPIT. REPLACED BURNT AOA VANE CURRENT SENSOR.
- [SDR COMA9810136](https://openairdocs.org/sdr/COMA9810136.md): Control Unit · failed · Jun 5, 1998 · N267CA · Emb EMB120RT · Landing Gear Brake System
  > AIRCRAFT HAS NO BRAKES DURING LANDING ROLL. REPLACED THE BRAKE CONTROL UNIT.
- [SDR COMA9810080](https://openairdocs.org/sdr/COMA9810080.md): Sensor · malfunction · Apr 1, 1998 · N267CA · Emb EMB120 · Landing Gear Position and Warning
  > RT MLG, GREEN DOWN INDICATION, CAME ON WITH GEAR RETRACTED. REPLACED THE RT MLG DOWNLOCK SENSOR.
- [SDR COMA9810047](https://openairdocs.org/sdr/COMA9810047.md): Control Box · malfunction · Feb 23, 1998 · N267CA · Emb EMB120RT · Landing Gear Retraction/Extension System
  > LANDING GEAR WILL NOT RETRACT. REPLACED THE LANDING GEAR CONTROL BOX.
- [SDR COMA9810039](https://openairdocs.org/sdr/COMA9810039.md): Sensor · malfunction · Feb 5, 1998 · N267CA · Emb EMB120RT · Elevator Tab Control System
  > TAKEOFF TRIM WARNING SOUNDED. REPLACED THE ELEVATOR TRIM TAB PROXIMITY SENSORS.
- [SDR COMA9810032](https://openairdocs.org/sdr/COMA9810032.md): Bulb · failed · Jan 24, 1998 · N267CA · Emb EMB120RT · Emergency Lighting
  > FLOOR EMERGENCY LIGHT AT GALLEY AREA IS INOP. REPLACED BULB.
- [SDR COMA9710471](https://openairdocs.org/sdr/COMA9710471.md): Battery · discharged · Nov 9, 1997 · N267CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY LIGHTS ARE INOP. REPLACED THE EMERGENCY LIGHTS BATTERIES.
- [SDR COMA9710387](https://openairdocs.org/sdr/COMA9710387.md): Floorbeam · corroded · Aug 20, 1997 · N267CA · Emb EMB120RT · Fuselage Main, Floor Beam
  > DURING 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.

Next page: https://openairdocs.org/deregistered/N267CA-2007-11-27/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N267CA-2007-11-27/reports

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