N146US, cancelled Nov 1, 2002

Service difficulty reports · 37

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N146US' AND deregistration_id = 'N146US-2002-11-01'
  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 0101231146Longeron · corrodedDURING M-CHECK, FOUND CORROSION ON VERTICAL LEG OF LONGERON AT NUMBER 3 AIR CONDITIONING EXHAUST DOOR CUTOUT AT BS 515-520 JUST ABOVE THE LOWER EDGE. REPAIRED PER EA 11-180800.Feb 28, 2001 · N146US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 0101221146Doubler · corrodedDURING M-CHECK, FOUND CORROSION ON FORWARD CARGO DOOR JAMB DOUBLER AT BS 910 ABOVE L43R. REPAIRED PER EA 11-180797.Feb 15, 2001 · N146US · Doug DC1040 · Fuselage Main, StructureSDR 0101201146Floorbeam · damagedDURING M-CHECK, MAIN CABIN FLOORBEAM AT BS 1293 WAS FOUND SEVERED AT LBL 106 AND CRACKED AT RBL 106 JUST INSIDE OF NR 3 LT AND NR 3 RT DOORS. REPAIRED PER EA 11-180795.Jan 29, 2001 · N146US · Doug DC1040 · Fuselage Main, Floor BeamSDR 0101431146Beam · corrodedDURING M-CHECK, FOUND CORROSION ON LOWER END OF BEAM AT BS 1521 PRESSURE BULKHEAD. REPAIRED PER EA 11-182647.Jan 26, 2001 · N146US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9722511146Tr Unit · malfunctionedON TAKEOFF ROLL AS POWER WAS APPLIED, THE NR 1 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT APPROXIMATELY 30 KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED THE REVERSER ON MEL 78-1A.Dec 3, 1997 · N146US · Doug DC1040 · Engine Thrust ReverserSDR 9722201146Thrust Reverser · malfunctionedDURING LANDING ROLLOUT, THE NR 1 ENGINE THRUST REVERSER FAILED TO STOW. THE CREW RECYCLED THE REVERSER AND A COMPRESSOR STALL OCCURRED. MAX EGT WAS 650C. THE ENGINE WAS SHUT DOWN. THE OUTBOARD REVERSER SLEEVE DEPARTED THE AIRCRAFT. MAINTENANCE LOCKED OUT Nov 26, 1997 · N146US · Doug DC1040 · Engine Thrust ReverserSDR 9722871146Web · crackedDURING L-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL, LEFT AND RIGHT CORNER WEB AROUND FASTENERS FS 488. REPAIRED PER EA 11-153553.Nov 21, 1997 · N146US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9711421146Tr Unit · locked outDURING TAKEOFF ROLL, NR 2 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT 90 KNOTS. MAINTENANCE VERIFIED THAT THE THRUST REVERSER WAS LOCKED OUT AND CHANGED THE MEL TO 78-2A.Jun 14, 1997 · N146US · Doug DC1040 · Engine Thrust ReverserSDR 9705451146Web · crackedDURING LINE CHECK, MULTIPLE CRACKS WERE FOUND IN THE NCA6246-28 NOSE GEAR SUPPORT WEB AT THE UPPER FORWARD CORNERS OF BOTH LEFT AND RIGHT WEBS. REPAIRED PER EA 11-123544.Mar 1, 1997 · N146US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9703081146Compressor · stalledDURING LANDING, THE NR 3 ENGINE COMPRESSOR STALLED WHILE IN REVERSE. ENGINE WAS SHUT DOWN WHILE STILL IN REVERSE. PERFORMED INSPECTION WITH NO FAULTS FOUND, OPERATIONAL CHECK OK.Feb 12, 1997 · N146US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9702801146Tr System · malfunctionedDURING TAKEOFF, THE NR 3 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED. TAKEOFF WAS ABORTED. RERIGGED REVERSER SYSTEM.Feb 9, 1997 · N146US · Doug DC1040 · Engine Thrust ReverserSDR 9702491146Tt2 Sensor · failedDURING TAKEOFF, THE NR 1 ENGINE FAILED TO ACCELERATE. TAKEOFF WAS ABORTED AT 70 KNOTS. MAINTENANCE REPLACED THE TT2 SENSOR AND RETURNED TO SERVICE.Feb 7, 1997 · N146US · Doug DC1040 · Engine BMEP/Torque IndicatingSDR 9624451146Compressor · stalledDURING POWER REDUCTION AT FL210, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL. AS EGT CLIMBED TO 750 DEGREES, THE ENGINE WAS SHUT DOWN AND RESTARTED. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND CONTINUED FLIGHT TO PHL WITHOUT FURTHER INCIDENT. VISUAL ANNov 14, 1996 · N146US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9621731146Tr Light · illuminatedDURING TAKEOFF ROLLOUT, THE NR 3 THRUST REVERSER LIGHT ILLUMINATED AT 60 KNOTS. CREW ABORTED TAKEOFF AND WHILE TAXING, REALIZED THAT THE REVERSER WAS ON MEL FROM A PREVOUS INCIDENT. FLIGHT DEPARTED AND TO BOS WITHOUT FURTHER INCIDENT.Oct 10, 1996 · N146US · Doug DC1040 · Engine Thrust ReverserSDR 9621741146Rev Unlock Light · illuminatedDURING TAKEOFF ROLLOUT, THE NR 3 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED THE REVERSER AND DEFERRED REPAIR PER MEL 78-1A.Oct 8, 1996 · N146US · Doug DC1040 · Engine Thrust ReverserSDR 9617961146Position Ind · malfunctionedDURING TAKEOFF, THE GEAR RETRACTED BUT THE RED GEAR POSITIONS INDICATORS REMAINED ILLUMINATED. RECYCLED GEAR AND THE LIGHT WENT OUT. MAINTENANCE PERFORMED INSPECTIONS AND BITE TESTS, OPERATIONAL CHECK OK.Aug 15, 1996 · N146US · Doug DC1040 · Landing Gear Position and WarningSDR 9617951146Proximity Box · failedDURING TAKEOFF, ALL RED GEAR POSITION LIGHTS ILLUMINATED AND THE WARNING HORN SOUNDED WITH THE GEAR HANDLE UP. RECYCLED GEAR BUT LIGHT REMAINED ILLUMINATED UNITL PASSING 10,000 FEET. MAINTENANCE REPLACED THE MAIN LANDING GEAR PROXIMITY BOX.Aug 15, 1996 · N146US · Doug DC1040 · Landing Gear Position and WarningSDR 9613101146Apu · firePRIOR TO PUSHBACK, APU TAILPIPE FIRE DEVELOPED. AIRCRAFT APU FIRE BOTTLES WERE DISCHARGED AND FLAMES EXTINGUISHED. THE PASSENGERS WERE DEPLANED THROUGHT THE JETWAY WITHOUT INCIDENT. NO SMOKE WAS PRESENT IN CABIN. MAINTENANCE INSPECTED APU AND SURROUNDING SJun 15, 1996 · N146US · Doug DC1040 · Airborne Auxiliary Power Unit (APU) SystemSDR 9608821146Header · crackedDURING L-CHECK, FOUND A .75 INCH CRACK IN THE FORWARD CARGO DOOR CUTOUT UPPER HEADER FS 938. REPAIRED HEADER (P/N ADA0217) PER EA 11-103925.Apr 17, 1996 · N146US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9608811146Skin · crackedDURING L-CHECK, FOUND A .5 INCH CRACK IN THE UPPER SKIN OF THE RIGHT INBOARD ELEVATOR. REPAIRED SKIN PER EA 11-104237.Apr 17, 1996 · N146US · Doug DC1040 · Elevator, Plate/SkinSDR 9608791146Web · crackedDURING L-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL LEFT AND RIGHT SIDE WEBS AT FS 495, Z= -64. REPAIRED WEBS (P/N NCA6246-25, -27) PER EA 11-102158.Apr 16, 1996 · N146US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9602801146Stall Transducer · malfunctionedDURING TAKEOFF, AUTO SLAT WOULD NOT RETRACT AND STICK SHAKER ACTIVATED. DUMPED 16,000 LBS OF FUEL AND RETURNED TO DTW. REPLACED AT/SC COMPUTER (11-2232-9-0001, SN 10201) AND THE NR 1 STALL TRANSDUCER (11-3418-9-0001, SN 00438).Feb 4, 1996 · N146US · Doug DC1040 · Stall Warning SystemSDR 9519011146Compressor · stalledDURING CRUISE, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL WITH THE EGT GOING TO MAX FOR 30 SECONDS. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO BOS WHERE AN UNEVENTFUL TWO ENGINE LANDING WAS ACCOMPLISHED. NO FUEL WAS DUMPED. THE AIRCRAFT WAS FENov 23, 1995 · N146US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9507371146Epr Indication · malfunctionedDURING TAKEOFF ROLL, THE NR 1 ENGINE EPR INDICATION FAILED AND THE TAKEOFF WAS ABORTED. THE EPR INDICATOR WAS REPLACED AND A GROUND RUNUP CONFIRMED PROPER SYSTEM OPERATION.May 4, 1995 · N146US · Doug DC1040 · Engine Pressure Ratio (EPR)SDR 95005701146Rccb · failedDURING PREFLIGHT CHECK, THE AIRCRAFT EMERGENCY POWER FAILED TO TEST. FOUND REMOTE CONTROL CIRCUIT BREAKER (RCCB) B1-189 STUCK OPEN. REPLACED RCCB, OPERATIONAL CHECK OK.Apr 12, 1995 · N146US · Doug DC1040 · DC Generating SystemSDR 9501791146Intercostal · crackedDURING PERIODIC CHECK, A CRACK WAS FOUND ON THE FUSELAGE BELT FRAME TO INTERCOSTAL STRAP AT FS 445, LBL 25 TO THE ACCESS DOOR 115AZ. REPLACED STRAP.Feb 2, 1995 · N146US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9501781146Floor Beam · crackedDURING PERIODIC CHECK, A CRACK WAS FOUND ON THE FLOOR BEAM AT FS 879, RBL 29 - 37. REMOVED DAMAGE AND REPAIRED PER EA 11-96621.Feb 2, 1995 · N146US · Doug DC1040 · Fuselage Main, Floor BeamSDR 9501531146Doubler · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE INNER SKIN STIFFENER AT FS 1156, STR 50L AND 51L. INSTALLED NEW DOUBLER PER EA 11-96638.Jan 28, 1995 · N146US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9501551146Longeron · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON LONGERON AT STR 44L, FS 1581. INSTALLED REPAIR STRAP PER 11-96601.Jan 27, 1995 · N146US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9501541146Longeron · crackedDURING PERIODIC CHECK, A CRACK WAS FOUND ON THE END FITTING AT LONGERON 18R, FS 1988 AND LONGERON 19R, FS 1990. INSTALLED STRAP DOUBLERS PER EA 11-96271.Jan 27, 1995 · N146US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9503181146Longeron · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE LONGERON 44L, FS 1581. REMOVED CORROSION AND INSTALLED DOUBLER PER EA 11-96601.Jan 25, 1995 · N146US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9501281146Bulkhead Angle · corrodedDURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE SUPPORT ANGLE OF THE FORWARD BULKHEAD IN THE CENTER WHEEL WELL, AT RBL 10-29. INSTALLED REPAIR ANGLE PER EA 11-93766.Jan 23, 1995 · N146US · Doug DC1040 · Fuselage Main, BulkheadSDR 9501271146Skin · corrodedDURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE MOUNTING RINGS UNDER THE FOUR RADIO ALTIMETER ANTENNAS. INSTALLED TITANIUM DOUBLERS PER EA 11-96572.Jan 23, 1995 · N146US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9501261146Bolt · crackedDURING PERIODIC INSPECTION, CRACK INDICATIONS WERE FOUND ON THE WING PYLON TO FRONT SPAR FITTING ATTACH NR 2 LOWER BOLT. REPLACED NR 2 AND NR 4 LOWER BOLTS.Jan 23, 1995 · N146US · Doug DC1040 · Wing, Nacelle/Pylon Attach FittingsSDR 9501141146Bulkhead Support · corrodedDURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE SUPPORT ANGLE OF THE FORWARD BULKHEAD IN THE CENTER WHEEL WELL AT LBL 19-29. INSTALLED REPAIR ANGLE PER EA 11-93766.Jan 19, 1995 · N146US · Doug DC1040 · Fuselage Main, BulkheadSDR 9501301146Longeron · corrodedDURING PERIODIC INSPECTION, CORROSION WAS FOUND IN THE AFT CARGO COMPARTMENT AT FS 1801-1815, STR 44R. REPLACED LONGERON PER EA 11-96636.Jan 12, 1995 · N146US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9500631146Skin · damagedDURING PERIODIC INSPECTION, NON-STANDARD REPAIR WAS FOUND AT FS 515 - 560, STR 24L - 23L. REMOVED DAMAGE AND INSTALLED DOUBLERS PER EA 11-96400.Jan 12, 1995 · N146US · Doug DC1040 · Fuselage Main, Plate/Skin
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