# Service difficulty reports: N293CA, cancelled Nov 20, 2012 A list on [N293CA, cancelled Nov 20, 2012](https://openairdocs.org/deregistered/N293CA-2012-11-20.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 · 88 reports - [SDR YTRAN293CA4](https://openairdocs.org/sdr/YTRAN293CA4.md): Float · bent · Oct 15, 2010 · N293CA · Bell 412 · Emergency Flotation Section > THE ACFT WAS IN FOR THE FIRST ROUTINE SCHEDULED 24 MONTH ACTIVATION/ INSP REQUIRED FOR THE OEM EMERGENCY FLOATATION KIT THAT IS INSTALLED IN CONJUNCTION WITH STC’D MID BAG WITH LIFE RAFT FLOAT KIT. THE STC’D FLOAT STEP KIT WAS INSTALLED 24 MONTHS AGO DUE TO T - [SDR YTRAN293CAJZ3](https://openairdocs.org/sdr/YTRAN293CAJZ3.md): Float · malfunctioned · Oct 15, 2010 · N293CA · Bell 412 · Emergency Flotation Section > THE AIRCRAFT WAS IN FOR THE FIRST 24 MONTH ACTIVATION/ INSPECTION. THE KIT WAS INSTALLED NEW 24 MONTHS AGO AND ONE OF THE PREREQUISITES FOR INSTALLATION OF THE STC'D KIT IS REMOVING THE OEM STEPS AND INSTALLING THE STC'D OPTIONAL STEPS. OUR COMPANY ELECTED T - [SDR YTRAN293CAJZ2](https://openairdocs.org/sdr/YTRAN293CAJZ2.md): Float · binding · Oct 15, 2010 · N293CA · Bell 412 · Emergency Flotation Section > THE ACFT WAS IN FOR THE FIRST 24 MONTH ACTIVATION/ INSP. THE KIT WAS INSTALLED NEW 24 MONTHS AGO AND 1 OF THE PREREQUISITES FOR INSTALLATION OF THE STC'D KIT IS REMOVING THE OEM STEPS AND INSTALLING THE STC'D OPTIONAL STEPS. OUR COMPANY ELECTED TO INSTALL TH - [SDR YTRAN293CAJZ1](https://openairdocs.org/sdr/YTRAN293CAJZ1.md): Cable · broken · Oct 15, 2010 · N293CA · Bell 412 · Emergency Flotation Section > THE ACFT IS EQUIPPED WITH STC'D EMERGENCY FLOAT BAGS WITH LIFE RAFT. THE EMERGENCY RAFT PULL CABLE TO ACTIVATE THE RAFT FAILED COMPLETELY DURING THE INITIAL 24 MONTH ROUNTINE INSP. THE CABLE IS MADE FROM INFERIOR NON-AVIATION GRADE MATERIALS AND THIS FAILURE - [SDR YTRR079854](https://openairdocs.org/sdr/YTRR079854.md): Compensator · erratic · Jun 6, 2002 · N293CA · Bell 412 · Engine EGT/TIT Indicating System > GAVE ERRATIC AND ERRONEOUS READINGS DURING GROUND RUN. TRIM COMPENSATOR WAS RECEIVED NEW FROM PRATT AND WHITNEY WITH THE ENGIEN AFTER OVERHAUL. - [SDR YTRR079853](https://openairdocs.org/sdr/YTRR079853.md): Governor · malfunctioned · Jun 6, 2002 · N293CA · Bell 412 · Turbine Governor > GOVERNOR WAS CAUSING A TORQUE SPLIT IN THE NR 2 ENGINE. - [SDR YTRR079852](https://openairdocs.org/sdr/YTRR079852.md): Bearing · worn · Jun 6, 2002 · N293CA · Bell 412 · Main Rotor Head > ROD END BEARING EXCESSIVELY WORN. - [SDR YTRR079851](https://openairdocs.org/sdr/YTRR079851.md): Bearing · worn · Jun 6, 2002 · N293CA · Bell 412 · Main Rotor Head > ROD END BEARING EXCESSIVELY WORN. - [SDR YTRR079850](https://openairdocs.org/sdr/YTRR079850.md): Bearing · worn · Jun 6, 2002 · N293CA · Bell 412 · Main Rotor Head > ROD END BEARING WORN EXCESSIVELY. - [SDR YTRR079849](https://openairdocs.org/sdr/YTRR079849.md): Bearing · worn · Jun 6, 2002 · N293CA · Bell 412 · Main Rotor Head > ROD END BEARING EXCESSIVELY WORN. - [SDR YTRR077529](https://openairdocs.org/sdr/YTRR077529.md): Line · cracked · Jan 2, 2002 · N293CA · Bell 212 · Fuel Control/Reciprocating Engines > P3 FILTER LINE ON NR 1 ENGINE CRACKED, REPLACED P3 FILTER LINE ASSEMBLY WITH NEW SERVICEABLE ASSEMBLY. - [SDR HEEA065146](https://openairdocs.org/sdr/HEEA065146.md): Encoder · failed · Nov 15, 1999 · N293CA · Bell 412 · Altimeter, Barometric/Encoder > GPS CONSTANTLY READS EXY. ALTIMETER IS IN ERROR. - [SDR HEEA063388](https://openairdocs.org/sdr/HEEA063388.md): Gyro · malfunctioned · Aug 13, 1999 · N293CA · Bell 412 · Auto Flight System > FLAG CIRCUIT NOT PULLING HSI. - [SDR HEEA063320](https://openairdocs.org/sdr/HEEA063320.md): Control Unit · failed · Aug 12, 1999 · N293CA · Bell 412 · DC Generating System > CONTROL UNIT WOULD NOT COME ON-LINE. - [SDR HEEA063296](https://openairdocs.org/sdr/HEEA063296.md): Control Unit · failed · Aug 10, 1999 · N293CA · Bell 412 · DC Generating System > NR 1 GENERATOR WILL NOT COME ON-LINE. - [SDR HEEA063228](https://openairdocs.org/sdr/HEEA063228.md): Indicator · damaged · Aug 9, 1999 · N293CA · Bell 412 · Airspeed/Mach Indicator > RED LINES HAVE FADED TO ORANGE ON AIRSPEED INDICATOR. - [SDR HEEA060773](https://openairdocs.org/sdr/HEEA060773.md): Computer · failed · Feb 22, 1999 · N293CA · Bell 412 · Autopilot Computer > AFCS COMPUTER FAILS DATT & PCPL LOGIC 14.1 TEST. - [SDR HEEA060736](https://openairdocs.org/sdr/HEEA060736.md): Computer · malfunctioned · Feb 22, 1999 · N293CA · Bell 412 · Autopilot System > JIA PIN 54 BROKEN. - [SDR HEEA060733](https://openairdocs.org/sdr/HEEA060733.md): Battery · defective · Feb 22, 1999 · N293CA · Bell 412 · Battery/Charger System > BATTERY PACK TRIPS CIRCUIT BREAKER. TIME SINCE REPAIR 522:10 HOURS. - [SDR HEEA060717](https://openairdocs.org/sdr/HEEA060717.md): Actuator · malfunctioned · Feb 22, 1999 · N293CA · Bell 412 · Main Rotor Control > AFCS IN ATT. MODE HAS CONSTANT ROLL MOTORING. - [SDR HEEA060716](https://openairdocs.org/sdr/HEEA060716.md): Actuator · sticks · Feb 22, 1999 · N293CA · Bell 412 · Main Rotor Control > ROTARY ACTUATOR STICKS INTERMITTENTLY. DATE OF MFG 10-29-98. - [SDR HEEA060694](https://openairdocs.org/sdr/HEEA060694.md): Receiver · defective · Feb 22, 1999 · N293CA · Bell 412 · Localizer/VOR System > GLIDE SLOPE DEFECTIVE, OUT OF SPECS. - [SDR HEEA060642](https://openairdocs.org/sdr/HEEA060642.md): Nut · corroded · Feb 16, 1999 · N293CA · Bell 412 · Main Rotor Mast/Swashplate > CORROSION ON THREADS. REPLACED WITH SERVICEABLE PART. - [SDR HEEA060641](https://openairdocs.org/sdr/HEEA060641.md): Liner · corroded · Feb 16, 1999 · N293CA · Bell 412 · Main Rotor Mast/Swashplate > LINER/MAST WORN AND CORRODED. REPLACED WITH SERVICEABLE PART. - [SDR HEEA060632](https://openairdocs.org/sdr/HEEA060632.md): Bearing · corroded · Feb 16, 1999 · N293CA · Bell 412 · Main Rotor Mast/Swashplate > WORN AND CORRODED. REPLACED LINER AND RETURNED TO SERVICE. - [SDR HEEA0016850](https://openairdocs.org/sdr/HEEA0016850.md): Actuator · sticks · Dec 1, 1998 · N293CA · Bell 412 · Main Rotor Control > ROTOR ACTUATOR STICKS INTERMITTENTLY. DATE OF MFG 10-29-98. - [SDR HEEA0016592](https://openairdocs.org/sdr/HEEA0016592.md): Oil Cooler · failed · Oct 28, 1998 · N293CA · Bell 412 · Engine Oil Cooler > TRANS. OIL TEMP HIGH. - [SDR HEEA0016562](https://openairdocs.org/sdr/HEEA0016562.md): Indicator · sticking · Oct 28, 1998 · N293CA · Bell 412 · Engine RPM Indicating System > NEEDLES NR 1 AND NR 2 STUCK AND ERRATIC. - [SDR HEEA0016035](https://openairdocs.org/sdr/HEEA0016035.md): Altimeter · reads high · Sep 11, 1998 · N293CA · Bell 412 · Altimeter, Barometric/Encoder > PILOT REPORTED ALTIMETER UNIT READS 125 FEET HIGH OUT OF TOLERANCE. WHEN RECEIVED UNIT, IT HAD LOOSE PARTS INSIDE. - [SDR HEEA0015888](https://openairdocs.org/sdr/HEEA0015888.md): Actuator · inoperative · Aug 27, 1998 · N293CA · Bell 412 · Entrance Stairs > STEP ACTUATOR INOPERATIVE. - [SDR HEEA0015813](https://openairdocs.org/sdr/HEEA0015813.md): Transponder · out of tolerance · Aug 27, 1998 · N293CA · Bell 412 · Dependent Position Determining System > TRANSPONDER FRAMING OUT OF TOLERANCE. - [SDR HEEA0015761](https://openairdocs.org/sdr/HEEA0015761.md): Indicator · inoperative · Aug 25, 1998 · N293CA · Bell 412 · DME/TACAN System > INDICATOR TOTALLY INOPERATIVE. - [SDR HEEA0015752](https://openairdocs.org/sdr/HEEA0015752.md): Altimeter · damaged · Aug 25, 1998 · N293CA · Bell 412 · Altimeter, Barometric/Encoder > ALTIMETER READS 140 FEET HIGH AND HAS LOOSE PARTS INSIDE. - [SDR HEEA0015664](https://openairdocs.org/sdr/HEEA0015664.md): Indicator · broken · Aug 17, 1998 · N293CA · Bell 412 · Integrated Flight System > CONNECTOR BROKE FREE FROM INDICATOR HOUSING. - [SDR HEEA0015577](https://openairdocs.org/sdr/HEEA0015577.md): Computer · malfunctioned · Aug 14, 1998 · N293CA · Bell 412 · Autopilot Computer > AFCS COMPUTER YAW KICKS. - [SDR HEEA0015535](https://openairdocs.org/sdr/HEEA0015535.md): Indicator · failed · Aug 13, 1998 · N293CA · Bell 412 · Attitude Gyro and Indicating System > GYRO VALID FLAG WILL NOT PULL. REPAIRED BY PHI, CALIBRATED, BENCH CHECK GOOD. - [SDR HEEA0015276](https://openairdocs.org/sdr/HEEA0015276.md): Indicator · malfunctioned · Jul 27, 1998 · N293CA · Bell 412 · Attitude Gyro and Indicating System > ATTITUDE INDICATOR LIGHTS INOPERATIVE. REPLACED 5-VOLT LIGHTS. - [SDR HEEA0014727](https://openairdocs.org/sdr/HEEA0014727.md): Indicator · malfunctioned · Jun 11, 1998 · N293CA · Bell 412 · Attitude Gyro and Indicating System > ATTITUDE INDICATOR PRECESSES 1 DEGREE A MINUTE. REBALANCED STATIC AND DYNAMIC. RECALIBRATED ROLL AND PITCH ERECTIONS. UNIT BENCH CHECKS GOOD. - [SDR HEEA0014714](https://openairdocs.org/sdr/HEEA0014714.md): Actuator · failed · Jun 10, 1998 · N293CA · Bell 412 · Entrance Stairs > STEP ACTUATOR 'S INTERNAL GEAR SEEMS TO BE STRIPPED. - [SDR HEEA0014700](https://openairdocs.org/sdr/HEEA0014700.md): Gyroscope · malfunctioned · Jun 10, 1998 · N293CA · Bell 412 · Directional Gyro and Indicating System > HORIZONTAL GYRO WILL NOT ERECT AND NO CURRENT DRAWN. - [SDR HEEA0014542](https://openairdocs.org/sdr/HEEA0014542.md): Valve · inoperative · Jun 4, 1998 · N293CA · Bell 412 · Fuel Selector/Shut-Off Valve > FUEL SYSTEM VALVE INOPERATIVE. - [SDR HEEA0014118](https://openairdocs.org/sdr/HEEA0014118.md): Attitude Gyro · failed · May 4, 1998 · N293CA · Bell 412 · Attitude Gyro and Indicating System > ATTITUDE GYRO INOPERATIVE. - [SDR HEEA0014084](https://openairdocs.org/sdr/HEEA0014084.md): Probe · failed · Apr 29, 1998 · N293CA · Bell 412 · Fuel Quantity Sensor > FUEL QTY SENSOR CHAFED WIRE AND TROUBLESHOOTING. - [SDR HEEA0014083](https://openairdocs.org/sdr/HEEA0014083.md): Altimeter · error · Apr 29, 1998 · N293CA · Bell 412 · Altimeter, Barometric/Encoder > ENCODING ALT INDICATES 200 FEET LOW OUT OF TOLERANCE. - [SDR HEEA0014082](https://openairdocs.org/sdr/HEEA0014082.md): Altimeter · failed · Apr 29, 1998 · N293CA · Bell 412 · Altimeter, Barometric/Encoder > ENCODER READS OUT OF TOLERANCE AT 10,000 FEET AND ABOVE. - [SDR HEEA0014069](https://openairdocs.org/sdr/HEEA0014069.md): Valve · failed · Apr 29, 1998 · N293CA · Bell 412 · Aircraft Fuel Distribution System > VALVE INOPERATIVE. - [SDR HEEA0013998](https://openairdocs.org/sdr/HEEA0013998.md): Actuator · failed · Apr 21, 1998 · N293CA · Bell 412 · Entrance Stairs > STEP ACTUATOR INOPERATIVE. - [SDR HEEA0013997](https://openairdocs.org/sdr/HEEA0013997.md): Actuator · failed · Apr 21, 1998 · N293CA · Bell 412 · Entrance Stairs > STEP ACTUATOR INOPERATIVE. - [SDR HEEA0013996](https://openairdocs.org/sdr/HEEA0013996.md): Actuator · stripped · Apr 21, 1998 · N293CA · Bell 412 · Entrance Stairs > ACTUATOR INTERNAL GEAR SEEMS TO BE STRIPPED. - [SDR HEEA0013806](https://openairdocs.org/sdr/HEEA0013806.md): Inverter · malfunction · Apr 2, 1998 · N293CA · Bell 412 · AC Inverter > 450VA INVERTER CAUSES FUEL GAUGE TO FLUCTUATE. Next page: https://openairdocs.org/deregistered/N293CA-2012-11-20/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 = 'N293CA' AND deregistration_id = 'N293CA-2012-11-20' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N293CA-2012-11-20/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.