N158US, cancelled Jun 20, 2002

Service difficulty reports · 32

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 = 'N158US' AND deregistration_id = 'N158US-2002-06-20'
  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 0100571158Engine · leakingDURING CLIMB AFTER TAKEOFF, THE CREW REPORTED SMOKE ENTERING THE CABIN FROM A PNEUMATIC SOURCE. THE FLIGHT RETURNED TO LAX AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THE NR 1 ENGINE TO BE LEAKING OIL AND CONTAMINATING THE Feb 16, 2001 · N158US · Doug DC1040 · Turbine Engine Oil SystemSDR 0004391158Service difficultyAFTER TAKEOFF, FOUR GEAR UNSAFE LIGHTS ILLUMINATED WHEN GEAR SELECTED UP. FOLLOWED COM PROCEDURE. VERIFIED GEAR UP VISUALLY. RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND GEAR HANDLE INTERLOCK RELAY INOPERATIVE. REPLACED RELAY. OPERATIONAL CHECK OK.Dec 1, 2000 · N158US · Doug DC1040 · Landing Gear Position and WarningSDR 9903391158Power Lever · out of adjustAFTER TOUCHDOWN WHEN REVERSE THRUST WAS APPLIED, THE NR 3 ENGINE DID NOT ACCELERATE. THE NR 2 ENGINE DEVELOPED MAXIMUM REVERSE THRUST WHILE THE NR 1 THRUST REVERSER WAS INOPERATIVE ON MEL. MAXIMUM BRAKING WAS APPLIED BUT THE AIRCRAFT DID NOT STOP UNTIL APPROAug 9, 1999 · N158US · Doug DC1040 · Power LeverSDR 9900131158Light · smokingDURING APPROACH INTO BOS, FLIGHT ATTENDANT NOTICED SMOKE FROM CABIN LIGHT ABOVE SEAT 2H AND 2J. NOTIFIED COCKPIT AND SHUT LIGHTS OFF. SMOKE DISSIPATED. CAPTAIN DECLARED A PRECAUTIONARY EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED BALLAST ON LIGHTJan 11, 1999 · N158US · Doug DC1040 · Passenger Compartment LightingSDR 9710501158Prox Box · malfunctionedDURING TAKEOFF, GEAR VIBRATION WAS FELT UPON RETRACTION AND ALL UNSAFE GEAR LIGHTS REMAINED RED. RECYCLED GEAR AND OPERATION WAS NORMAL. MAINTENANCE REPLACED BOTH NOSE GEAR TIRES. RESET MAIN LANDING GEAR PROXIMITY BOX AND NO FAULTS WERE FOUND WITH GEAR INDIMay 25, 1997 · N158US · Doug DC1040 · Landing Gear Position and WarningSDR 9710111158Compressor · stalledAT 1,400 FEET DURING TAKEOFF, THE NR 2 ENGINE COMPRESSOR STALLED TWICE WITH EGT MOMENTARILY REACHING 900C ON BOTH OCCASIONS. NO OTHER ABNORMAL INDICATIONS. MAINTENANCE CONTROL RECOMMENDED DIVERSION TO BOS FOR MAINTENANCE. INSPECTION FOUND COMPRESSOR BLADE PMay 21, 1997 · N158US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9702791158Apu · failedDURING BOARDING, THE APU FAILED, FIRE BOTTLES WERE FIRED AND CABIN FILLED WITH SMOKE. REPLACED APU, WATER SEPARATOR BAGS AND PURGED PACKS.Feb 9, 1997 · N158US · Doug DC1040 · APU Core EngineSDR 9701501158Pressure Switch · failedDURING TAKEOFF, THE NR 3 MANIFOLD FAIL LIGHT ILLUMINATED. DUMPED 76,500 LBS OF FUEL AND RETURNED TO IAD. REPLACED THE MANIFOLD PRESSURE SWITCH.Jan 27, 1997 · N158US · Doug DC1040 · Pneumatic Indicating SystemSDR 9624011158Compressor · stalledAT FL310 WHEN POWER WAS REDUCTED FOR DESCENT, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. THERE WAS A SUBSEQUENT VIBRATION UNTIL THE ENGINE WAS SHUT DOWN. NO ABNORMAL EGT OR FUEL FLOW INDICATION AT THE TIME OF INCIDENT. FLIGHT CONTINUED TO DTW WITHOUT FNov 10, 1996 · N158US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9617151158Engine · overtempDURING LANDING ROLLOUT, THE NR 1 ENGINE EGT WENT ABOVE RED LIMIT LINE FOR ABOUT THREE SECONDS. THE ENGINE WAS THEN SHUTDOWN WHILE STILL IN REVERSE AND A/C TAXIED TO GATE WITHOUT FURTHER INCIDENT. PERFORMED ENGINE OVER TEMPERATURE INSPECTION AND NO DISCREPANCAug 7, 1996 · N158US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9615891158Skin · crackedDURING L-CHECK, FOUND A CRACK IN THE RIGHT WING FIXED LEADING EDGE SKIN AT XOS 610. REPAIRED SKIN (P/N ARB2887-502) PER EA 11-105354.Jul 11, 1996 · N158US · Doug DC1040 · Wing, Plate/SkinSDR 9615881158Skin · crackedDURING L-CHECK, FOUND A CRACK IN THE LEFT WING FIXED LEADING EDGE SKIN AT XOS 610. REPAIRED SKIN (P/N ARB2887-501) PER EA 11-105353.Jul 11, 1996 · N158US · Doug DC1040 · Wing, Plate/SkinSDR 9609471158Fuel Control · malfunctionedWHILE WAITING FOR TAKEOFF, THE NR 1 ENGINE COMPRESSOR STALL OCCURRED AT ENGINE IDLE POWER. EGT TEMPERATURE REACHED 700 CELSIUS AND THE NR 1 ENGINE WAS SHUTDOWN. AIRCRAFT RETURNED TO THE GATE. GROUND MAINTENANCE REPLACED THE ENGINE VANE CONTROL, PERFORMED ENApr 30, 1996 · N158US · Doug DC1040 · Fuel Control/Turbine EnginesSDR 9600451158Power Supply · failedDURING LINE CHECK, FOUND THE AFT EMERGENCY LIGHT POWER SUPPLY FAILED BITE TEST. REPLACED THE AFT POWER SUPPLY AND BATTERY PACK.Jan 2, 1996 · N158US · Doug DC1040 · Emergency LightingSDR 9520631158Pneu Manifold · failedDURING CLIMB, THE NR 2 PNEUMATIC MANIFOLD FAIL LIGHT ILLUMINATED INTERMITTENTLY. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. ITEM ENTERED IN MINIMUM EQUIPMENT LIST AND AIRCRAFT APPROVED FOR SERVICE.Dec 18, 1995 · N158US · Doug DC1040 · Pneumatic Distribution SystemSDR 9519761158Pt2 Probe · crackedDURING START OF DESCENT, THE NR 2 ENGINE EGT WENT TO 1010 DEGREES FOR 90 SECONDS. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT CONTINUED TO AN UNEVENTFUL TWO-ENGINE LANDING AT MSP. THE PRBC AND EVC WERE REPLACED AND A PT2 PROBE WAS FOUND CRACKED AND REPLACED. Dec 2, 1995 · N158US · Doug DC1040 · Fuel Controlling SystemSDR 9507661158Pan · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE AFT LAV SERVICE PAN INNER SURFACE FS 1980. REPAIRED PAN PER EA 11-98056. MFG PART NUMBER AGA3098-501.May 7, 1995 · N158US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9508241158Bulkhead · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE CENTER ACCESS PRESSURE BULKHEAD FS 1156 AT LONGERON 43R. REPAIRED PER EA 11-98042.May 4, 1995 · N158US · Doug DC1040 · Fuselage Main, BulkheadSDR 9507741158Skin · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE AFT LAV SERVICE PAN AND SKIN DOUBLER AT FS 1980 - 1986, L50L TO L50R. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER EA 11-98047 AND 11-98056. MFG PART NUMBER: AGA3098-501.May 4, 1995 · N158US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9507641158Web · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON FLOOR WEB AND DOUBLER FS 1900 TO 1928, LBL 107. REPAIRED PER EA 11-98053. MFG PART NUMBER AGA3807-5.May 2, 1995 · N158US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9507621158Frame · crackedDURING PERIODIC CHECK, FOUND CRACK IN THE FORWARD CARGO FLOOR FRAME FLANGE FS 879, LBL 38. REPAIRED PER EA 11-98027. MFG PART NUMBER ADA7034-3.May 1, 1995 · N158US · Doug DC1040 · Fuselage Main, FrameSDR 9507611158Seat Track · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON SEAT TRACK LBL 107, FS 1521. REPAIRED PER EA 11-98049.Apr 28, 1995 · N158US · Doug DC1040 · Fuselage, Seat/Cargo Attach FittingsSDR 9506731158Support · corrodedDURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE FLOOR SUPPORT AT FS 459, LBL 6 TO RBL 56. REPLACED FLOOR SUPPORT.Apr 27, 1995 · N158US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9506721158Seat Track · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 1311 - 1399, LBL 107. REMOVED CORROSION AND REPAIRED SEAT TRACK.Apr 27, 1995 · N158US · Doug DC1040 · Fuselage, Seat/Cargo Attach FittingsSDR 9506711158Support · corrodedDURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE FLOOR SUPPORT AT FS 440, RBL 2 - 6. REPLACED THE FLOOR SUPPORT.Apr 27, 1995 · N158US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9507761158Fasteners · brokenDURING PERIODIC CHECK, FOUND BROKEN FASTENERS COMMON TO THE NR 4 BANJO FITTING AFT FLANGE AND THE PYLON CARRY THROUGH CAP. INSTALLED BUSHINGS AND REPAIRED CHANNELS PER EA 11-098170. MFG PART NUMBER AJC7054-1.Apr 26, 1995 · N158US · Doug DC1040 · Nacelle/Pylon StructureSDR 9506671158Seat Track · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 1476 - 1510, LBL 107. REMOVED CORROSION AND INSTALLED REPAIR.Apr 26, 1995 · N158US · Doug DC1040 · Fuselage, Seat/Cargo Attach FittingsSDR 9506441158Seat Track · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 440 - 485, RBL 9. REPLACED SEAT TRACK.Apr 24, 1995 · N158US · Doug DC1040 · Fuselage, Seat/Cargo Attach FittingsSDR 9506431158R3 Door · crackedDURING PERIODIC CHECK, CRACKS WERE FOUND IN THE FORWARD AND AFT LOWER DOOR 3R STRUCTURE AT FS 1260 AND 1305. STOP DRILLED AND INSTALLED DOUBLER.Apr 24, 1995 · N158US · Doug DC1040 · Emergency ExitsSDR 9506391158L3 Door · crackedDURING PERIODIC CHECK, A CRACK WAS FOUND ON THE DOOR 3L AFT LOWER LIGHTENING HOLE AT FS 1305. STOP DRILLED CRACK AND INSTALLED DOUBLER.Apr 21, 1995 · N158US · Doug DC1040 · Emergency ExitsSDR 9506291158Skin · damagedDURING PERIODIC CHECK, FUSELAGE SKIN WAS FOUND DENTED AND GOUGED AT FS 1801, STR 2L TO 4L. REMOVED DAMAGED AREA AND INSTALLED DOUBLERS.Apr 20, 1995 · N158US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9507751158Frame · crackedDURING PERIODIC CHECK, FOUND A CRACK IN THE FORWARD CARGO FLOOR FRAME AT FS 879, LBL 38. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER EA 11-98027. MFG PART NUMBER: ADA7034-3.Apr 4, 1995 · N158US · Doug DC1040 · Fuselage Main, Frame
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