N153US, cancelled Nov 26, 2002

Service difficulty reports · 27

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 = 'N153US' AND deregistration_id = 'N153US-2002-11-26'
  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 0101951153Transmitter · malfunctionedAT APPROXIMATELY 80 KTS ON TAKEOFF ROLL, THE NR 3 ENGINE FAIL LIGHT ILLUMINATED. THE CREW OBSERVED THE NR 3 N1 AND N2 INDICATIONS DECREASING AND ABORTED TAKEOFF AT 100 KTS. THE EPR INDICATION WAS REPORTED AS NORMAL. MAINTENANCE REPLACED THE N1 TRANSMITTER AMay 23, 2001 · N153US · Doug DC1040 · Engine RPM Indicating SystemSDR 0102391153Stiffener · corrodedIn L check, found corrosion on lower end of stiffener outboard of panel 143CZ of wing center section. Repaired per EA11-182723.May 18, 2001 · N153US · Doug DC1040 · Wing Miscellaneous StructureSDR 0102381153Skin · crackedDuring L check, found crack in upper corners of cutout on wing leading edge. Repaired per EA11-183471.May 18, 2001 · N153US · Doug DC1040 · Wing Miscellaneous StructureSDR 0003351153Connector · looseON FINAL WHEN GEAR HANDLE WAS PLACED IN THE DOWN POSITION, GREEN LIGHTS DID NOT ILLUMINATE. RECYCLED GEAR AND ALL GREEN LIGHTS ILLUMINATED. FLIGHT CONTINUED TO NORMAL LANDING. MAINTENANCE RESEATED PROXIMITY SENSOR BOX. LEFT TEST CHECKED OK. AIRCRAFT RETURSep 8, 2000 · N153US · Doug DC1040 · Landing Gear Position and WarningSDR 9905631153Stiffener · crackedDURING M CHECK, FOUND CRACK ON HORIZONTAL T STIFFENER AT FS1521 BULKHEAD AT X=40, Z=97.350. REPAIRED PER EA 12-171336.Nov 9, 1999 · N153US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9809551153Engine · failedDURING CLIMB-OUT, THE NR 2 ENGINE LOW OIL PRESSURE WARNING LIGHT ILLUMINATED AND THE INDICATED OIL TEMPERATURE WAS INCREASING. THE ENGINE WAS SHUT DOWN. 50,000 LBS OF FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO LAX WITHOUT FURTHER DIFFICULTY. THE AIRCRAFT Jun 12, 1998 · N153US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9707031153Engine · malfunctionedAFTER LANDING WHILE COMING OUT OF ENGINE REVERSER, THE NR 1 ENGINE EGT EXCEEDED LIMITS. THE NR 1 ENGINE WAS SHUT DOWN. MAINTENANCE BORESCOPE INSPECTED ENGINE AND PERFORMED RAB'S SYSTEM CHECK IN ACCORDANCE WITH MM 75-30-00, PG 201-203. NO DISCREPANCIES WERE Apr 2, 1997 · N153US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9707051153Engine · malfunctionedAFTER LANDING WHILE COMING OUT OF ENGINE REVERSE THRUST, THE NR 3 ENGINE EGT BEGAN TO EXCEED LIMITS. ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED ENGINE PER MM 72-00-00, PG 227. NO DISCREPANCIES WERE NOTED.Mar 24, 1997 · N153US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9627201153Reverser System · malfunctionedDURING TAKEOFF ROLL, ENGINE NR 2 AMBER REVERSE UNLOCK LIGHT ANNUNCIATED. TAKEOFF ABORTED AT 120 KNOTS. MAINTENANCE PERFORMED REJECTED TAKEOFF INSPECTION, NO DAMAGE FOUND. REVERSER ON MEL.Dec 28, 1996 · N153US · Doug DC1040 · Engine Thrust ReverserSDR 9627631153Skin · corrodedDURING TRANSITION CHECK, CORROSION WAS FOUND ON THE UNDERWING BARREL SKIN AT FS 1509 TO 1531, LBL 49 TO RBL 49. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLERS PER EA 11-120126 (P/N AYB7065-1).Dec 23, 1996 · N153US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9627621153Skin · delaminatedDURING PERIODIC CHECK, DELAMINATION OF THE VERTICAL STABILIZER SKIN AT STR 375 TO 405 RIGHT SIDE. REPAIRED PER EA 11-120122 (P/N ANC7047-2).Dec 23, 1996 · N153US · Doug DC1040 · Vertical Stabilizer, Plate/SkinSDR 9627641153Support · crackedDURING PERIODIC CHECK, A CRACK WAS FOUND ON THE LEFT HORIZONTAL STABILIZER SECONDARY PIVOT SUPPORT. REMOVED AND REPLACED PIVOT SUPPORT PER EA 11-120135 (P/N AJC7230-1).Dec 20, 1996 · N153US · Doug DC1040 · Horizontal Stabilizer StructureSDR 9627551153Doubler · gougedDURING PERIODIC CHECK, GOUGES WERE FOUND ON THE FORWARD CARGO LOWER JAMB SKIN DOUBLER AT FS 911.97. BLENDED OUT GOUGES AND INSTALLED REPAIR DOUBLER PER EA 11-120623.Dec 19, 1996 · N153US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9627561153Angle · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE FORWARD CARGO JAMB ANGLE AT FS 1002, LONGERON 43R. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER EA 11-120622 (P/N ADA0233-7).Dec 18, 1996 · N153US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9627611153Longeron · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE FUSELAGE OVERWING EXTERNAL LONGERONS AT FS 1404 TO 1515. BLENDED OUT CORROSION AND INSTALLED DOUBLERS PER EA 11-120121.Dec 16, 1996 · N153US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9627571153Doorframe · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE CENTER CARGO DOOR JAMB FRAME AT FS 1787, LONGERON 43R. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS AND SHIMS PER EA 11-120612(PN AFA3876-3).Dec 16, 1996 · N153US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9627581153Mounting Rings · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE RADIO ALTIMETER ANTENNA MOUNTING RINGS. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER EA 11-120609 (P/N AYB7053-1).Dec 12, 1996 · N153US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9627601153Support · crackedDURING PERIODIC CHECK, THE FLOOR PANEL ATTACH TAB WAS FOUND CRACKED AT FS 475, LBL 36 FLOOR SUPPORT RAIL. REMOVED DAMAGED AREA AND INSTALLED REPAIR CHANNEL AND FILLERS PER EA 11-105163 (P/N NCA6042-33).Dec 4, 1996 · N153US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9619781153Fire Wire · chafedDURING INITIAL CLIMB, THE NR 3 ENGINE B-LOOP LIGHT ILLUMINATED. CREW FOLLOWED COM PROCEDURE AND CONTINUED FLIGHT AS SCHEDULED. ON FINAL APPROACH, THE NR 3 ENGINE FIRE WARNING INDICATION ILLUMINATED AGAIN. CREW SHUT THE ENGINE DOWN AND MADE A TWO ENGINE LANDSep 12, 1996 · N153US · Doug DC1040 · Fire DetectionSDR 9609281153Wire · failedDURING LINE INSPECTION, FOUND THE FLOOR TRACK LIGHT INOPERATIVE ON THE RIGHT SIDE OF THE FIRST CLASS CABIN. REPAIRED TRACK WIRING AT DOOR 2R.Apr 25, 1996 · N153US · Doug DC1040 · Light System WiringSDR 9514971153Pneu Ind Loop · failedDURING CRUISE, THE NR 2 PNEUMATIC MANIFOLD FAIL LIGHT ILLUMINATED. FLIGHT RETURNED TO HNL. FOUND THE NR 2 LOOP BAD, DEFERRED PER MEL 36-10A.Oct 1, 1995 · N153US · Doug DC1040 · Pneumatic Indicating SystemSDR 9505871153Nr 3 Bearing · failedDURING CLIMB AT ABOUT 7000 FEET, SMOKE AND FUMES APPEARED IN THE CABIN AND THE AIRCRAFT RETURNED TO MSP WHERE AN UNEVENTFUL LANDING WAS MADE. NO FUEL WAS DUMPED. THE NR 3 ENGINE NR 3 BEARING COMPARTMENT SHOWED EVIDENCE OF DISTRESS AND BLACK OIL WAS FOUND. TApr 16, 1995 · N153US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9505731153Bracket · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE SHEAR TIE AT FS 1761 TO 1782, STR 45R AND 46R. REMOVED CORROSION AND INSTALLED REPAIR STRAP PER EA 11-97995.Apr 13, 1995 · N153US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9505721153Angle · crackedDURING PERIODIC INSPECTION, A CRACK WAS FOUND ON THE 'TEE' ANGLE AT FS 1162, RBL 47 ABOVE ACCESS 142AZ. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER EA 11-97997.Apr 13, 1995 · N153US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9504961153Engine · flame outDURING TAXI OUT, THE NR 2 ENGINE EXPERIENCED A SURGE AND FLAMED OUT WITH THE EGT GOING TO MAX FOR THREE SECONDS. TAIL WIND GUSTS TO 25 KTS WERE BEING EXPERIENCED. THE ENGINE WAS INSPECTED AND BOROSCOPE WAS ACCOMPLISHED. AN ENGINE CHANGE HAS BEEN SCHEDULED.Mar 26, 1995 · N153US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9503551153Compressor · stalledDURING TAKEOFF, THE NR 2 ENGINE COMPRESSOR STALLED AND SHUT DOWN. DUMPED 43,000 LBS OF FUEL AND RETURNED TO LAX. FERRIED AIRCRAFT TO MSP AND REPLACED THE NR 2 ENGINE.Mar 6, 1995 · N153US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9500571153Compressor · stalledDURING LANDING ROLLOUT IN REVERSE THRUST, THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL WITH RISING EGT AND WAS SHUT DOWN. THE ENGINE WAS INSPECTED AND THE RABS SOLENOID WAS REPLACED. A GROUND RUN-UP CONFIRMED PROPER ENGINE OPERATION. A BOROSCOPE IS SCHEDUJan 11, 1995 · N153US · Doug DC1040 · Turbine Engine Compressor Section
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