N2251A

Service difficulty reports not matched to an aircraft · 25

They name N2251A, 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 = 'N2251A' 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 HEEA065202Indicator · malfunctionedTORQUEMETER INDICATOR GAUGE BOUNCES IN-FLIGHT.Nov 17, 1999 · N2251A · Bell 206L1 · Engine BMEP/Torque IndicatingSDR HEEA063143Altimeter · incorrectALTIMETER READS INCORRECT.Jul 29, 1999 · N2251A · Bell 206L1 · Altimeter, Barometric/EncoderSDR HEEA060389Actuator · failedACTUATOR INOPERATIVE.Jan 28, 1999 · N2251A · Bell 206L1 · Main Rotor ControlSDR HEEA060387Actuator · malfunctionedUNABLE TO ADJUST STROKE ON ACTUATOR.Jan 28, 1999 · N2251A · Bell 206L1 · Main Rotor ControlSDR HEEA0012907Actuator · failedACTUATOR DOES NOT MOVE.Feb 10, 1998 · N2251A · Bell 206L1 · Main Rotor ControlSDR HEEA0012821Indicator · defectiveINDICATES 5 PSI HIGH AT 100 PSI.Feb 5, 1998 · N2251A · Bell 206L1 · Engine Oil PressureSDR HEEA0012159Transponder · failedTRANSPONDER NO TEST LIGHT AND NO POWER. PERFORMED PRELIMINARY INSPECTION AND FOUND REPLY LIGHT DIM, REPLACED V301 PHOTOCELL. REPAIRED. BENCH CHECK GOOD.Nov 28, 1997 · N2251A · Bell 206L1 · ATC Transponder SystemSDR HEEA0011302Gyro · noisyDIR GYRO ROTOR NOISY PRECESSES AND WILL NOT SLAVE + OR -5 VOLTS.Oct 8, 1997 · N2251A · Bell 206L1 · Directional Gyro and Indicating SystemSDR HEEA0010434Airspeed Ind · reads highAIR SPEED INDICATOR READS 15 KNOTS TOO HIGH.Jul 10, 1997 · N2251A · Bell 206L1 · Airspeed/Mach IndicatorSDR HAI00010003Flexure · wornFLEXURE BEARINGS WORN AND UNSTAKED.Jun 2, 1997 · N2251A · Bell 206L1 · Main Rotor Transmission MountSDR HAIHEEA9924Washer · wornTAIL ROTOR RUBBER BUMPER HAS WORN THROUGH AT ACCELERATED RATE. THESE ARE THE BLACK RUBBER BUMPERS. THIS PARTICULAR ONE HAD BEEN INSTALLED FOR ONLY ONE WEEK. THE PREVIOUS RUBBER BUMPER HAD BEEN INSTALLED FOR ONLY THREE WEEKS AND HAD JUST 81 FLIGHTHOURS. IT May 28, 1997 · N2251A · Bell 206L1 · Tail Rotor SystemSDR HAIHEEA9768Bumper · wornRUBBER BUMPER HAS WORN OUT PREMATURELY. REPLACED WITH SERVICEABLE PART.Apr 30, 1997 · N2251A · Bell 206L1 · Tail Rotor SystemSDR HEEA979080Ml4000 · failedINSTALLED UNIT IN AIRCRAFT AND TURNED ON POWER. THREE OF THE FUNCTION LIGHTS ILLUMINATED THEN WENT OUT AFTER A FEW SECONDS. THE DISPLAY WINDOW NEVER DID LIGHT UP. IT WAS VERIFIED THAT UNIT WAS GETTING POWER. REPLACED 2 EACH REAR TRANSISTORS. REPAIRED PROBLFeb 11, 1997 · N2251A · Bell 206L1 · Long-Range Navigation (LORAN) SystemSDR HEEA968615Washer · wornTAIL ROTOR RUBBER BUMPER HAS WORN THROUGH AT ACCELERATED RATE. THESE ARE THE BLACK RUBBER BUMPERS.Dec 4, 1996 · N2251A · Bell 206L1 · Tail Rotor SystemSDR HEEA968614Washer · wornRUBBER BUMPER HAS WORN OUT PREMATURELY.Dec 4, 1996 · N2251A · Bell 206L1 · Tail Rotor SystemSDR HEEA967188Indicator · sticksINDICATOR STICKS AT ABOUT 530 DEGREES.----MODIFY TO P/N 206-075-680-103.May 9, 1996 · N2251A · Bell 206L1 · Engine EGT/TIT Indicating SystemSDR HEEA966675Blade · paint peelT/R BLADE PAINT PEELING.Feb 8, 1996 · N2251A · Bell 206L1 · Tail Rotor BladesSDR HEEA956249Flexure · wornFLEXURE WORN.Dec 13, 1995 · N2251A · Bell 206L1 · Main Rotor Transmission MountSDR HEEA955524Regulator · malfunctionGENERATOR DELAYED IN COMING ON LINE.Aug 2, 1995 · N2251A · Bell 206L1 · DC RegulatorSDR HEEA955234Altimeter · case leakALTIMETER EXCESSIVE CASE LEAK.Jun 26, 1995 · N2251A · Bell 206L1 · Altimeter, Barometric/EncoderSDR HEEA955126Panel · defectiveFORWARD R/H SIDE OF ROOF PANEL HITTING R/H AIRFRAME PANEL TRANSITION AREA. PANEL NEEDS TO BE MOVED TO THE RIGHT APPROXIMATELY 1/8" FOR INSERT ALIGNMENT. TRANSITION AREAS ON L/H AND R/H SIDES, FORWARD OF THE FORWARD ROLL OVER BEAM BULKHEADS, HITS THE BULKHEADJun 2, 1995 · N2251A · Bell 206L1 · Fuselage Miscellaneous StructureSDR HEEA955092Support · req replacementASB 206L-93-89 REV. B (REPLACEMENT OF -109 SUPPORT WITH -113 SUPPORT)May 25, 1995 · N2251A · Bell 206L1 · Main Rotor Mast/SwashplateSDR HEEA955075Panel · mis mfgSEVERAL AREAS OF PANEL ALONG AFT EDGE HAVE INSUFFICIENT EDGE DISTANCE TO LOCATE RIVETS. PANEL HAS 4 EACH 1/4" INSERTS ON L/H AND 4 EACH 1/4" INSERTS ON R/H WING WALK AREA THAT ARE NOT REQUIRED. INSERTS IN CENTER AREA OF PANEL APPEAR TO BE 3/16" TOO FAR TO THMay 25, 1995 · N2251A · Bell 206L1 · Fuselage Miscellaneous StructureSDR HEEA955002Channel · mis mfgCHANNEL HAS PILOT HOLES DRILLED ON AFT END. THEY DO NOT LINE UP WITH THE HOLES ON THE CHANNEL THAT WAS REMOVED. (NO EDGE DISTANCE)May 15, 1995 · N2251A · Bell 206L1 · Fuselage Miscellaneous StructureSDR HEEA954274Bearing · crackedCRACKED INBOARD AND OUTBOARD BEARING. ALSO REPLACED TWO EACH SLEEVES P/N 206-010-733-003. REMOVED FROM T/R HUB S/N AFS-5896, T.T. 2232:00. SCRAPPED BEARINGS AND SLEEVES LOCALLY.Jan 16, 1995 · N2251A · Bell 206L1 · Tail Rotor Blades
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