N156US, cancelled Apr 30, 2002

Service difficulty reports · 28

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 = 'N156US' AND deregistration_id = 'N156US-2002-04-30'
  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 0103161156Duct · brokenON CLIMBOUT AT MSP, NR 1 AND NR 2 MANIFOLD FAIL LIGHTS ILLUMINATED, ACCOMPANIED BY A LOUD BANG AFT OF NR 2 DOOR. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PNEUMATIC DUCT BROKEN AT FLANGE. REPLACED DUCT, OPERATIONAL CHECK OK.Sep 3, 2001 · N156US · Doug DC1040 · Pneumatic Distribution SystemSDR 0002831156Frame · crackedDURING L CHECK FOUND CRACK IN RIGHT HAND MAIN LANDING GEAR WHEEL WELL FRAME AT BS 1505. REPAIRED PER EA 178315.Aug 3, 2000 · N156US · Doug DC1040 · Fuselage Main, FrameSDR 9905091156Engine · malfunctionedDURING DESCENT AT 12,000 FEET WHILE IN TURBULENCE, THE NR 2 ENGINE FLAMED OUT. THE RESTART ATTEMPT WAS SUCCESSFUL WITH ENGINE OPERATION NORMAL FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE INSPECTED THE ENGINE PER THE TAFI MANUAL WITH NO DEFECTS NOTED. ADDITINov 26, 1999 · N156US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9901211156Floorbeam · crackedDURING M-CHECK, FOUND CRACKS ON THE FLOORBEAM UPPER CHORD AT FS 791, LBL 6 TO RBL 2. REPAIRED PER EA 11-162058.Jan 14, 1999 · N156US · Doug DC1040 · Fuselage Main, Floor BeamSDR 9901251156Longeron · crackedDURING M-CHECK, FOUND CORROSION ON HORIZONTAL SECTION OF LONGERON 30R AT FS 1450, 1470 AND 1503. ALSO, FOUND TWO INCH CRACK ON HORIZONTAL SECTION OF LONGERON 30R AT FS 1431. REPAIRED PER EA 11-162065.Jan 13, 1999 · N156US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9901281156Longeron · corrodedDURING M-CHECK, FOUND CORROSION ON LONGERON 32L BETWEEN FS 1501 AND 1521. REPAIRED PER EA 11-162062.Jan 12, 1999 · N156US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9901231156Longeron · crackedDURING M-CHECK, FOUND CORROSION ON HORIZONTAL SECTION OF LONGERON 31R AT FS 1471 AND 1491. CRACKS WERE ALSO FOUND ON HORIZONTAL SECTION OF LONGERON 31R AT FS 1501 AND 1531. REPAIRED PER EA 11-162069.Jan 12, 1999 · N156US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9901271156Longeron · corrodedDURING M-CHECK, FOUND CORROSION ON LONGERON 34R AT FS 1521 AND 1531. REPAIRED PER EA 11-162072.Jan 10, 1999 · N156US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9901241156Longeron · corrodedDURING M-CHECK, FOUND CORROSION ON LONGERON 30L BETWEEN FS 1501 TO 1521. REPAIRED PER EA 11-162061.Jan 10, 1999 · N156US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9901261156Longeron · corrodedDURING M-CHECK, FOUND CORROSION BEYOND SRM LIMITS ON LONGERON 44R AT FS 1601. REPAIRED PER EA 11-162068.Jan 8, 1999 · N156US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9901221156Floorbeam · crackedDURING M-CHECK, FOUND CRACK ON THE FLOORBEAM UPPER CHORD AT FS 879 LBL 7. REPAIRED PER EA 11-162057.Jan 3, 1999 · N156US · Doug DC1040 · Fuselage Main, Floor BeamSDR 9807601156Rccb · inoperativeDURING CRUISE, LOST GROUND SERVICE BUS, VIDEO SYSTEM BECAME INOPERATIVE AND ALSO TOILETS. WATER QUANTITY INDICATED ZERO AND WATER PRESSURE INDICATED LOW. FLIGHT DIVERTED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RCCB BI-339, OPERATIONAL CHECKApr 26, 1998 · N156US · Doug DC1040 · AC Power Distribution SystemSDR 9801791156Actuator · out of adjustON TAKEOFF ROLL AT APPROXIMATELY 60 KNOTS, THE NR 3 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE THRUST REVERSER AND ADJUSTED A LOCK ACTUATOR. THE OPERATIONAL CHECKJan 26, 1998 · N156US · Doug DC1040 · Engine Thrust ReverserSDR 9715881156Wire · brokenDURING LINE INSPECITON, FOUND 'B' ZONE LEFT AISLE FLOOR EMERGENCY LIGHTS INOPERATIVE FROM ROWS 10AB TO 20AB. MAINTENANCE REPAIRED BROKEN WIRE TO THE EMERGENCY PATH LIGHTING AT DOOR 2L.Aug 18, 1997 · N156US · Doug DC1040 · Light System WiringSDR 9710721156Compressor · stalledDURING TAKEOFF ROLL, PASSENGERS REPORTED A FLASH AND FLAME BALL FROM LEFT WING. ALSO, TOWER REPORTED HEARING A LOUD NOISE. TAKEOFF WAS ABORTED AT 80 KNOTS. CREW SUSPECTED NR 1 ENGINE COMPRESSOR STALL BUT REPORTED NO ABNORMAL INDICAITONS. MAINTENANCE INSPECJun 4, 1997 · N156US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9710511156Disagree Light · illuminatedDURING TAKEOFF, THE SLAT DISAGREEMENT LIGHT ILLUMINATED. ABORTED TAKEOFF. MAINTENANCE REPLACED THE FLAP POSITION INDICATOR AND INSTALLED THE DC10 SLAT DISAGREE TEST PANEL PER MM 27-84-00. GROUND AND FLIGHT OPERATIONAL CHECK OK.May 28, 1997 · N156US · Doug DC1040 · Leading Edge Slat Position Indicating SystemSDR 9710481156Prox Contl Box · failedDURING TAKEOFF, THE SLAT DISAGREEMENT LIGHT ILLUMINATED WITH THE TAKEOFF WARNING HORN. ABORTED TAKEOFF. MAINTENANCE REPLACED THE MAIN LANDING GEAR PROXIMITY CONTROL BOX AND THE FLAP POSITION INDICATOR.May 26, 1997 · N156US · Doug DC1040 · Leading Edge Slat Position Indicating SystemSDR 9700461156Switch · failedDURING TAKEOFF, FOUR UNSAFE GEAR UP INDICATION ILLUMINATED. RECYCLED GEAR AND RECEIVED THE SAME INDICATION. FLIGHT RETURNED TO MSP. MAINTENANCE REPLACED THE NR 2 ENGINE THROTTLE SWITCH S1-341.Jan 11, 1997 · N156US · Doug DC1040 · Landing Gear Position and WarningSDR 9603121156Bleed Converter · malfunctionedAT TOP OF DESCENT, THE NR 3 ENGINE EXPERIENCED COMPRESSOR STALL. THE NR 3 ENGINE WAS SHUTDOWN AND RESTARTED. FLIGHT CONTINUED TO LGW WITHOUT FURTHER INCIDENT. REPLACED BLEED CONVERTER AND PS4 RESTRICTOR. PERFORMED ENGINE RUNUP AND ALL PARAMETERS WERE NORMAFeb 10, 1996 · N156US · Doug DC1040 · Compressor Bleed ControlSDR 9520251156Compressor · stalledDURING LANDING WHILE IN REVERSE THRUST, THE NR 1 AND NR 3 ENGINES COMPRESSOR STALLED WITH THE EGTS GOING TO 980 DEGREES FOR 5 SECONDS BEFORE THE ENGINES WERE SHUTDOWN. THE ENGNE WAS INSPECTED, BORESCOPED AND A GROUND RUNUP CONFIRMED PROPER OPERATION OF THE ENDec 13, 1995 · N156US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9514191156Compressor · stalledTOP OF DESCENT, NR 3 ENGINE COMPRESSOR STALLED AND WAS SHUTDOWN. ENGINE WAS RESTARTED AND LANDED WITHOUT FURTHER INCIDENT. THE ENGINE WAS INSPECTED, BORESCOPED AND AN INFLIGHT BLEED CHECK IS SCHEDULED. THE PRBD, EVC REMOVAL AND PRECISION TRIM IS ON DEFERRALSep 11, 1995 · N156US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9513591156Tr Drive Cable · brokenDURING TAKEOFF, THE NR 2 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED. REMOVED BROKEN DRIVE CABLE, INSTALLED LOCKOUT PLATES AND DEFERRED PER MEL 78-1A.Sep 3, 1995 · N156US · Doug DC1040 · Engine Thrust ReverserSDR 9510131156Skin · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE FUSELAGE SKIN, FS 1509 TO 1515, LONGERON 50L AND 50R. REPAIRED SKIN (P/N AYB 7065-1,-2) PER EA 11-98643.Jun 19, 1995 · N156US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9509891156Skin · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN THE FUSELAGE SKIN DOUBLER FS 1975 TO 1986, LONGERON 50L AND 50R. REPAIRED DOUBLER (AGA 7053-1) PER EA 11-98627.Jun 19, 1995 · N156US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9510511156Mounting Rings · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE NR 1 AND NR 2 RADIO ALTIMETER ANTENNA MOUNTING RINGS. REPAIRED PER EA 11-98574.Jun 14, 1995 · N156US · Doug DC1040 · Ground Proximity SystemSDR 9506451156Compressor · stalledDURING DESCENT WITH THE POWER LEVERS RETARDED, THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL WITH A RISE IN EGT FOLLOWED BY A FLAMEOUT. A RELIGHT WAS SUCCESSFUL AND ENGINE OPERATION WAS NORMAL THE REMAINDER OF THE FLIGHT. THE ENGINE WAS INSPECTED AND FUEL PApr 24, 1995 · N156US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9506231156Skin · damagedDURING OVERNIGHT INSPECTION, FOUND FUSELAGE SKIN WAS TORN JUST FORWARD OF DOOR 2L. REMOVED DAMAGE AND REPAIRED PER EA 11-96714.Apr 12, 1995 · N156US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9501151156Compressor · stalledDURING TAKEOFF (CDG), THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL AT 48 KNOTS AND THE TAKEOFF WAS ABORTED. THE ENGINE WAS INSPECTED AND A GROUND RUN-UP CONFIRMED PROPER ENGINE OPERATION. A BORESCOPE HAS BEEN SCHEDULED.Jan 19, 1995 · N156US · Doug DC1040 · Turbine Engine Compressor Section
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