N1082G

Service difficulty reports not matched to an aircraft · 30

They name N1082G, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N1082G' AND registry_match IS NULL
  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 HEEA076269Blade · corrodedCOMPRESSOR BLADE CORRODED.Oct 9, 2001 · N1082G · Bell 212 · Engine (Turbine/Turboprop)SDR HEEA065207Receiver · failedRECEIVER FAILED 2 YEAR INSPECTION.Nov 17, 1999 · N1082G · Bell 212 · Glide Slope SystemSDR HEEA063390Indicator · reads lowTRIPLE TACHOMETER INDICATOR READS 3 PERCENT LOW.Aug 13, 1999 · N1082G · Bell 212 · Main Rotor Indicating SystemSDR HEEA063372Indicator · inoperativeROTOR PORTION OF TACHOMETER INOPERATIVE.Aug 13, 1999 · N1082G · Bell 212 · Main Rotor Indicating SystemSDR HEEA061687Transceiver · failedVHF TRANSCEIVER INOPERATIVE WHEN INSTALLED.Apr 5, 1999 · N1082G · Bell 212 · VHF Communications SystemSDR HEEA061686Transceiver · failedVHF TRANSCEIVER WILL NOT TRANSMIT OR RECEIVE ON 119.70 THROUGH 131.57.Apr 5, 1999 · N1082G · Bell 212 · VHF Communications SystemSDR HEEA060703Indicator · erraticINDICATOR SPHERE IS ERRATIC IN PITCH.Feb 22, 1999 · N1082G · Bell 212 · Attitude and Direction Data SystemSDR HEEA060081Engine · overtempITT ABOVE 900 DEGREES FOR OVER 40 SECONDS.Jan 21, 1999 · N1082G · Bell 212 · Engine (Turbine/Turboprop)SDR 98ZZZX4746Engine · failedON 10-28-98 DURING RECONNAISSANCE OF OGLNY, CA, FIRE NOTICED, RPM LOW 97 PERCENT, THEN NOTICED LARGE TORQUE SPLIT. WITH N1 ON NR 2 ENGINE AT IDLE AND ITT 900 DEGREES CELSIUS, PILOT WENT TO MANUAL THROTTLE, BUT NO RESPONSE BY ENGINE.Oct 28, 1998 · N1082G · Bell 212 · Engine (Turbine/Turboprop)SDR HEEA0016421Receiver · failedGPS RECEIVER WILL NOT HOLD SATELLITES.Oct 23, 1998 · N1082G · Bell 212 · Global Positioning SystemSDR HEEA0016417Transceiver · malfunctionedVHF TRANSCEIVER HAS STATIC, HARD TO RECEIVE.Oct 23, 1998 · N1082G · Bell 212 · VHF Communications SystemSDR HEEA0016414Compressor · failedNOISE COMING FROM COMPRESSOR.Oct 23, 1998 · N1082G · Bell 212 · Turbine Engine Compressor SectionSDR HEEA0016403Caution Panel · failedPANEL ASSY LIGHTS FLICKER INTERMITTENTLY.Oct 23, 1998 · N1082G · Bell 212 · Central WarningSDR 99ZZZX684Window · brokenDURING CRUISE FLIGHT, TOP THIRD OF WINDOW BROKE OUT AND DEPARTED AIRCRAFT. NO OTHER DAMAGE OCCURRED. CAUSE UNKNOWN. MAINTENANCE REPLACED WINDOW. REF: 212 IPC, CHAPTER 52-99-00, PAGE 46, ITEM 20, FIGURE 52-11.Sep 13, 1998 · N1082G · Bell 212 · Flight Compartment WindowsSDR HEEA0015362Control Unit · failedNR 2 GENERATOR INOPERATIVE.Jul 29, 1998 · N1082G · Bell 212 · DC Generator-AlternatorSDR HEEA0015279Control Unit · leakingNR 2 SIDE HAS INTERNAL AIR LEAK THAT PREVENTS NR 2 ENGINE FROM TOPPING. (BOTH SERVO VALVES LEAK).Jul 27, 1998 · N1082G · Bell 212 · Fuel Control/Turbine EnginesSDR HEEA0014912Gearbox · making metalCOMBINING GEARBOX HAS METAL CONTAMINATION ON NR 2 SIDE.Jun 22, 1998 · N1082G · Bell 212 · Turbine Engine Reduction GearSDR HEEA0013630Damper Assy · defectiveDAMPER ASSY SIGHT GLASS CLOUDY AND LEAKING. SERIAL NUMBERS REMOVED ARE A1187 AND R19-11869.Mar 26, 1998 · N1082G · Bell 212 · Main Rotor HeadSDR HEEA0012220Indicator · failedN1 INDICATOR NEEDLE HAS STICKY OPERATION THROUGHOUT SCALE.Dec 3, 1997 · N1082G · Bell 212 · Engine RPM Indicating SystemSDR HEEA0012211Altimeter · failedALTIMETER INDICATES LOW OUT OF TOLERANCE ABOVE 3000 FEET.Dec 3, 1997 · N1082G · Bell 212 · Altimeter, Barometric/EncoderSDR HEEA0011691Indicator · stickingTEMPERATURE NEEDLE STICKING.Oct 22, 1997 · N1082G · Bell 212 · Hydraulic Indicating SystemSDR HEEA0011361Trim Compensator · intermittentINTERMITTENT ITT FUNCTION.Oct 9, 1997 · N1082G · Bell 212 · Engine EGT/TIT Indicating SystemSDR HEEA0011355Inverter · malfunctionINVERTER VOLTAGE OUTPUT HIGH CAUSING INTERMITTENT INVERTER WARNING.Oct 9, 1997 · N1082G · Bell 212 · AC Generator-AlternatorSDR HEEA0010406Indicator · sticksRADAR ALTIMETER WHEN POINTER IS SET AT ZERO AND POWER IS SHUT OFF,UNIT POINTS INTERMITTENTLY AND STICKS BELOW ZERO.Jul 9, 1997 · N1082G · Bell 212 · Ground Proximity SystemSDR HEEA0010171Rate Gyro · malfunctionGYRO CAUSES RATE OF TURN NEEDLE ON ADI TO PEG OFF.Jun 19, 1997 · N1082G · Bell 212 · Turn and Bank/Rate of Turn IndicatorSDR HAIHEEA9819Indicator · failedDME DOES NOT TURN ON. REPLACED HEADER DUE TO BURNT SPOT ON 192V CONTACT. APPLIED HUMISEAL. UNIT FIRES UP, BUT DOES NOT CHANNEL. FOUND BURNT R801. REPLACED R801. ALSO REPLACED 2 EACH SCREWS P/N 047-4808-01 ON COVER. UNIT HAS BAD DISPLAY SEGMENTS AND NO CHMay 7, 1997 · N1082G · Bell 212 · DME/TACAN SystemSDR HEEA968179Control · defectiveDOESN'T COME ONE. CLEANED ON/OFF SWITCH AND RESOLDERED COLD SOLDER JOINT ON SWITCH. REPAIRED. ALSO FOUND "IDENT" AND "TEST" SWITCHES INTERMITTENT. REPLACED "IDENT" (S106) P/N 031-0061-00 AND "TEST" (S108) P/N031-0061-00. REPAIRED. ALSO REPLACED MISSING BOOct 10, 1996 · N1082G · Bell 212 · VHF Communications SystemSDR HEEA967708Transceiver · inoperativeTRANSCEIVER INOPERATIVE. REPLACED BURNT F1 FUSE, SHORTED Q123 TRANSISTOR, SHORTED Q105 TRANSISTOR AND BURNT R114 RESISTOR. INSTALLED TRANSMITTER SHIELD. INSPECTED AND BENCH CHECK GOOD.Aug 29, 1996 · N1082G · Bell 212 · VHF Communications SystemSDR HEEA967634Grip · damagedTHREADS ON PITCH HORN BORE ARE TO DAMAGED TO ACCEPT NEW THREAD INSERT. ALSO REPLACE BLADE BOLT BUSHING AND DRAG BRACES BUSHING AND INSTALL BUSHING IN PITCH HORN BORE.Aug 8, 1996 · N1082G · Bell 212 · Main Rotor ControlSDR LCFR950515Rod End · sheared barrelTAIL ROTOR PITCH LINK ASSEMBLY SEPARATED IN-FLIGHT. AIRCRAFT LANDED SAFELY. ROD END BARREL SHEARED. NO SIGNS OF CORROSION NOTED. SUSPECT EXCESSIVE ROD END BEARING WEAR PREVENTED BEARING ROTATION. (X)May 15, 1995 · N1082G · Bell 212 · Tail Rotor Control System
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