# Service difficulty reports: N5010F, cancelled Jun 19, 2002 A list on [N5010F, cancelled Jun 19, 2002](https://openairdocs.org/deregistered/N5010F-2002-06-19.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR HEEA072706](https://openairdocs.org/sdr/HEEA072706.md): Indicator · failed · Apr 19, 2001 · N5010F · Bell 212 · Weather Radar System > DOES NOT PAINT TARGETS. FOUND UNIT HAS NO NOISE, ADJUSTED AUTOMATIC NOISE CONTROL. TROUBLESHOT VIDEO BOARD AND REPLACED R1450 RESISTOR. REPAIRED. BENCH CHECK GOOD. - [SDR HEEA065226](https://openairdocs.org/sdr/HEEA065226.md): Valve · inoperative · Nov 17, 1999 · N5010F · Bell 212 · Aircraft Fuel Distribution System > VALVE INOPERATIVE. - [SDR HEEA065219](https://openairdocs.org/sdr/HEEA065219.md): Indicator · reads high · Nov 17, 1999 · N5010F · Bell 212 · DC Indicating System > AMMETER READS 50 AMPS HIGHER. - [SDR HEEA065211](https://openairdocs.org/sdr/HEEA065211.md): Indicator · erratic · Nov 17, 1999 · N5010F · Bell 212 · Fuel Control/Reciprocating Engines > FUEL PRESSURE INDICATOR HAD UNRELIABLE ERRATIC READINGS. - [SDR HEEA065210](https://openairdocs.org/sdr/HEEA065210.md): Indicator · intermittent · Nov 17, 1999 · N5010F · Bell 212 · Fuel Control/Reciprocating Engines > FUEL PRESSURE INDICATOR INTERMITTENTLY STICKS AT ZERO. - [SDR HEEA065097](https://openairdocs.org/sdr/HEEA065097.md): Gyro · failed · Nov 11, 1999 · N5010F · Bell 212 · Turn and Bank/Rate of Turn Indicator > NO TURN INDICATIONS DISPLAY ON GYRO. - [SDR HEEA063218](https://openairdocs.org/sdr/HEEA063218.md): Indicator · intermittent · Aug 9, 1999 · N5010F · Bell 212 · Attitude and Direction Data System > INDICATOR OPERATES INTERMITTENTLY. - [SDR HEEA061728](https://openairdocs.org/sdr/HEEA061728.md): Brake Assy · malfunctioned · Apr 6, 1999 · N5010F · Bell 212 · Main Rotor Brake > WHEN ROTOR BRAKE CALIPERS WERE INSTALLED, INBOARD MICROSWITCH CONTACTS ROTOR BRAKE QUILL HOUSING. INBOARD MICROSWITCH WAS INSTALLED DIFFERENT ON THIS CALIPER ASSY THAN THE ONE REMOVED. SCRAPPED SWITCH ASSY ON INBOARD SIDE OF ROTOR BRAKE CALIPER. - [SDR HEEA061681](https://openairdocs.org/sdr/HEEA061681.md): Tarsyn · failed · Apr 5, 1999 · N5010F · Bell 212 · Autopilot System > UNIT DOES NOT SLAVE IN MAGNETIC COMPASS MODE. UNIT FUNCTION GOOD ON SST BENCH. - [SDR HEEA060127](https://openairdocs.org/sdr/HEEA060127.md): Indicator · sticking · Jan 21, 1999 · N5010F · Bell 212 · Engine BMEP/Torque Indicating > TORQUE METER INDICATOR'S NR 1 NEEDLE STICKS. - [SDR HEEA0016487](https://openairdocs.org/sdr/HEEA0016487.md): Gyro · inoperative · Oct 27, 1998 · N5010F · Bell 212 · Integrated Flight System > GYRO INOPERATIVE. - [SDR HEEA0016423](https://openairdocs.org/sdr/HEEA0016423.md): Inverter · failed · Oct 23, 1998 · N5010F · Bell 212 · AC Inverter > INVERTER WOULD NOT COME ON LINE AT INITIAL INSTALLATION FROM STOCK. - [SDR HEEA0016422](https://openairdocs.org/sdr/HEEA0016422.md): Inverter · malfunctioned · Oct 23, 1998 · N5010F · Bell 212 · AC Inverter > INVERTER TRIPS CIRCUIT BREAKER. - [SDR HEEA0016420](https://openairdocs.org/sdr/HEEA0016420.md): Flux Valve · inaccurate · Oct 23, 1998 · N5010F · Bell 212 · Directional Gyro and Indicating System > READING IS OFF 80 DEGREES. - [SDR HEEA0016419](https://openairdocs.org/sdr/HEEA0016419.md): Valve · incorrect · Oct 23, 1998 · N5010F · Bell 212 · Directional Gyro and Indicating System > COMPASS HAS INCORRECT HEADINGS, OUTPUT UNRELIABLE. - [SDR HEEA0016418](https://openairdocs.org/sdr/HEEA0016418.md): Control Unit · failed · Oct 23, 1998 · N5010F · Bell 212 · DC Generating System > CONTROL UNIT WILL NOT COME ON LINE. - [SDR HEEA0016412](https://openairdocs.org/sdr/HEEA0016412.md): Tarsyn · failed · Oct 23, 1998 · N5010F · Bell 212 · Autopilot System > TARSYN - PIN C OF BOTTOM CONNECTOR HAS PINS BACKING OUT OF CONNECTOR. - [SDR HEEA0016411](https://openairdocs.org/sdr/HEEA0016411.md): Tarsyn · failed · Oct 23, 1998 · N5010F · Bell 212 · Autopilot System > TARSYN FAILS TEST 8.5 ON SST. - [SDR HEEA0016409](https://openairdocs.org/sdr/HEEA0016409.md): Gyro · failed · Oct 23, 1998 · N5010F · Bell 212 · Attitude Gyro and Indicating System > RT FLAG ON ADI NOT PULLED. - [SDR HEEA0016408](https://openairdocs.org/sdr/HEEA0016408.md): Indicator · sticking · Oct 23, 1998 · N5010F · Bell 212 · Engine EGT/TIT Indicating System > ITT INDICATOR STICKS AT 580 DEGREES. - [SDR HEEA0016396](https://openairdocs.org/sdr/HEEA0016396.md): Indicator · failed · Oct 23, 1998 · N5010F · Bell 212 · Integrated Flight System > NO ADF POINTER INFO DISPLAYED. - [SDR HEEA0016395](https://openairdocs.org/sdr/HEEA0016395.md): Indicator · failed · Oct 23, 1998 · N5010F · Bell 212 · Hydraulic Pressure Indicator > HYDRAULIC PRESSURE NEEDLE WILL NOT RETURN TO ZERO. - [SDR HEEA0016394](https://openairdocs.org/sdr/HEEA0016394.md): Indicator · failed · Oct 23, 1998 · N5010F · Bell 212 · Attitude and Direction Data System > GS FLAG WILL NOT PULL. - [SDR HEEA0016393](https://openairdocs.org/sdr/HEEA0016393.md): Indicator · sticking · Oct 23, 1998 · N5010F · Bell 212 · Attitude and Direction Data System > HSI INDICATOR'S TO/FROM FLAG STICKS, NR 2 BEARING POINTER RATCHETS. - [SDR HEEA0016391](https://openairdocs.org/sdr/HEEA0016391.md): Transponder · failed · Oct 23, 1998 · N5010F · Bell 212 · ATC Transponder System > NO CODE TRANSMITTER. NO REPLY LIGHT. NO TEST LIGHT. TIME SINCE REPAIR 0:00 HOURS. - [SDR HEEA0016390](https://openairdocs.org/sdr/HEEA0016390.md): Transponder · malfunctioned · Oct 23, 1998 · N5010F · Bell 212 · ATC Transponder System > TRANSPONDER HAS LOW POWER. TIME SINCE REPAIR 0:00 HOURS. - [SDR HEEA0016389](https://openairdocs.org/sdr/HEEA0016389.md): Control · malfunctioned · Oct 23, 1998 · N5010F · Bell 212 · HF Communications System > LEDS LIGHT UP, DISPLAY BAD. - [SDR HEEA0015867](https://openairdocs.org/sdr/HEEA0015867.md): Ejector · cracked · Aug 27, 1998 · N5010F · Bell 212 · Engine Collector/Tailpipe/Nozzle > LEFT EJECTOR ASSEMBLY'S WELDS ARE CRACKED AND HAS LOOSE RIVETS. - [SDR HEEA0015318](https://openairdocs.org/sdr/HEEA0015318.md): Tarsyn · failed · Jul 29, 1998 · N5010F · Bell 212 · Autopilot System > DIRECTIONAL GYRO HAS NO SYNCHRO HEADING OUTPUT. TIME SINCE REPAIR, 7:15 HOURS. - [SDR HEEA0010852](https://openairdocs.org/sdr/HEEA0010852.md): Link Assy · worn · Aug 21, 1997 · N5010F · Bell 212 · Main Rotor Drive System > LINK ASSY HAS EXCESSIVE PLAY. - [SDR HEEA0010771](https://openairdocs.org/sdr/HEEA0010771.md): Indicator · failed · Aug 19, 1997 · N5010F · Bell 212 · Altimeter, Barometric/Encoder > INDICATES 3000 FEET AT FIELD ELEVATION - [SDR HEEA968271](https://openairdocs.org/sdr/HEEA968271.md): Valve · intermittent · Oct 14, 1996 · N5010F · Bell 212 · Fuel Transfer Valve > INOPERATIVE, CYCLES INTERMITTENT. - [SDR HEEA968177](https://openairdocs.org/sdr/HEEA968177.md): Transceiver · malfunction · Oct 10, 1996 · N5010F · Bell 212 · VHF Communications System > FREQUENCY DOES NOT SHOW TILL 20 OR 30 MINUTES. - [SDR HEEA968087](https://openairdocs.org/sdr/HEEA968087.md): Indicator · failed · Oct 3, 1996 · N5010F · Bell 212 · Weather Radar System > INDICATOR CAUSES R/T NOT TO TRANSMIT. - [SDR HEEA968080](https://openairdocs.org/sdr/HEEA968080.md): Transceiver · faulty · Oct 3, 1996 · N5010F · Bell 212 · VHF Communications System > AFTER UNIT HEATS UP, MODULATION BEGINS TO BREAK UP. - [SDR HEEA967996](https://openairdocs.org/sdr/HEEA967996.md): Bearing · failed · Oct 1, 1996 · N5010F · Bell 212 · Tail Rotor Drive System > DUST SHIELD SPINNING. REPLACEMENT PART PURCHASED AS PER ASB212-95-95 REV. B. - [SDR HEEA967995](https://openairdocs.org/sdr/HEEA967995.md): Bearing · failed · Oct 1, 1996 · N5010F · Bell 212 · Tail Rotor Drive System > DUST SHIELD SPINNING. REPLACEMENT PART PURCHASED AS PER ASB212-95-95 REV. B. - [SDR HEEA967994](https://openairdocs.org/sdr/HEEA967994.md): Bearing · failed · Oct 1, 1996 · N5010F · Bell 212 · Tail Rotor Drive System > DUST SHIELD SPINNING. - [SDR HEEA967699](https://openairdocs.org/sdr/HEEA967699.md): Transceiver · malfunction · Aug 29, 1996 · N5010F · Bell 212 · VHF Communications System > TRANSCEIVER WILL NOT TUNE. - [SDR HEEA967148](https://openairdocs.org/sdr/HEEA967148.md): Valve · malfunction · May 8, 1996 · N5010F · Bell 212 · Fuel Transfer Valve > VALVE INOPERATIVE. CYCLES CONSTANTLY. - [SDR HEEA956313](https://openairdocs.org/sdr/HEEA956313.md): Blade · dented · Dec 27, 1995 · N5010F · Bell 212 · Tail Rotor Blades > TR BLADE HAS DENT ON TRAILING EDGE. - [SDR HEEA955660](https://openairdocs.org/sdr/HEEA955660.md): Control Unit · failed · Aug 31, 1995 · N5010F · Bell 212 · DC Generating System > #1 GENERATOR FAILS TO COME ON LINE. RELAY 212-075-199-1 BLOWS IT OUT. REPLACED Q4 TRANSISTOR P/N 05-990044. BENCH CHECK OK. ## 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 = 'N5010F' AND deregistration_id = 'N5010F-2002-06-19' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N5010F-2002-06-19/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.