N1837U, cancelled Jun 10, 2002

Service difficulty reports · 23

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 = 'N1837U' AND deregistration_id = 'N1837U-2002-06-10'
  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 2000UALA00433Battery Pack · failedMID FWD EMERGENCY LIGHT BATTERY PACK FAILED PWR SUPPLY TEST. REPLACED POWER SUPPLY AND BATTERY PACK. CHECKS OK.Jul 20, 2000 · N1837U · Doug DC1010 · Emergency LightingSDR 2000UALA00496Skin · damagedFUSELAGE SKIN AND FRAME DAMAGE DUE TO JETWAY IMPACT WHEN AIRCRAFT ARRIVED AT GATE . IMPACT FORWARD OF 2L DOOR JUST ABOVE FLOORLINE. SKIN DENTED AND TORN OPEN FROM BS 735 TO 760 BETWEEN L27 AND L26. THE FRAME SHEAR TIE IS DAMAGED AT BS 735. FUSELAGE SKIN REJul 2, 2000 · N1837U · Doug DC1010 · Fuselage Main, Plate/SkinSDR 2000UALA00141Fire Loop · damagedNR 3 ENG FIRE DET B-LOOP LIGHT ON. INTERMITTENT FIRE WARN B-LOOP JUST PRIOR LANDING. OPERATIONS WAS NOTIFIED BY FLIGHT CREW THAT ENGINE WAS SHUT DOWN AND EMERGENCY DECLARED. LANDING WAS UNEVENTFUL. *S/D* NR 3 ENGINE ''A'' LOOP WAS PREVIOUSLY DEFERRED FOR Mar 17, 2000 · N1837U · Doug DC1010 · Fire DetectionSDR 99UAL900478Indicator · malfunctioned3L DOOR SLIDE LIGHT WILL NOT TEST. *S/D* REPLACED SLIDE REMOTE PRESSURE INDICATOR.Sep 16, 1999 · N1837U · Doug DC1010 · Emergency EquipmentSDR 98UAL900480Wire · failedEEL LIGHT STRIP OUT AT 1EF THROUGH DOOR 2R, 9AB THROUGH 16AB AND 30HJ THROUGH 38HJ. SPLICED NEW RIBBON BY BULKHEAD 1R, 2L AND REPLACED LEADER CABLE ASSY, CHECKS OK.Sep 28, 1998 · N1837U · Doug DC1010 · Light System WiringSDR 98UAL900262Lights · malfunctionedRED WARNING LIGHTS ILLUMINATED WHEN GEAR HANDLE SELECTED TO GEAR DOWN POSITION. CYCLED GEAR ONCE RED LIGHTS STILL ON. JIGGLED GEAR HANDLE GREEN LIGHTS CAME ON. LANDING NORMAL.Jun 13, 1998 · N1837U · Doug DC1010 · Landing Gear Position and WarningSDR 98UAL900229Fuel Pump · failedSHORTLY AFTER TAKEOFF, NR 1 ENGINE THRUST WENT TO 85 PERCENT N1, THEN UNABLE TO INCREASE OR DECREASE THRUST. OPENED FUEL CROSS FEED VALVE AND THEN ABLE TO CONTROL ENGINE POWER. RETURNED TO SFO. REPLACED THE MAIN FUEL PUMP AND THE MEC. RAN ENGINE AT HIGH POJun 1, 1998 · N1837U · Doug DC1010 · Engine Fuel PumpSDR 98UAL900044Nozzle · crackedNR 2 ENGINE HAS VIBRATION AND HUM THAT FOLLOWED THE THROTTLE. ENGINE REDUCED TO IDLE POWER AND DIVERTED TO LAS. *S/D* PRIMARY CAUSE OF ENGINE FAILURE WAS THE CRACKING OF THE HIGH PRESSURE TURBINE STAGE 1 NOZZLE. ON SEVERAL ADJACENT NOZZLES, THE CRACKS WRAPJan 30, 1998 · N1837U · Doug DC1010 · Fuel Injector NozzleSDR 98UAL900004Rib · crackedA CRACK WAS FOUND ON THE CENTER WING SECTION RIBS LOCATED AT RBL 29.0. THE CRACK RUNS FWD AND AFT DIAGONALLY AND MEASURES APPROXIMATELY 4.00 INCHES IN LENGTH. A DOUBLER WAS INSTALLED IN THE AREA.Jan 5, 1998 · N1837U · Doug DC1010 · Wing, Rib/BulkheadSDR 97UAL900892Duct · rupturedON CLIMBOUT, NR 3 ENGINE FIRE INDICATION. INDICATION STOPPED WHEN ENGINE WAS SHUT DOWN. ENGINE EGT WENT TO 953C MOMENTARILY. *S/D* THE 16TH STAGE PNEUMATIC SUPPLY DUCT FAILED AND RUPTURED AT ONE OF THE ATTACHMENT LUGS. ABNORMAL VIBRATION CONDITION WAS CONDec 24, 1997 · N1837U · Doug DC1010 · Pneumatic Distribution SystemSDR 97UAL900848Bulkhead Web · crackedTHE CENTER WING BOX BULKHEAD WEB AT STATION XCW=46.5 IS CRACKED. THE CRACK IS LOCATED BETWEEN APB7038-52 STIFFENERS AND APB7038-68 ANGLE AND APB 7038-60 TEE. THE CRACK LENGTH IS APPROXIMATELY 8 INCHES LONG. THE CRACK WAS TRIM-OUT AND A PREMANENT REPAIR WAS Nov 26, 1997 · N1837U · Doug DC1010 · Wing, Rib/BulkheadSDR 97UAL900651Wire · failedEMERGENCY LIGHT STRIP AT DOOR 1R STICKING UP. REPLACED LEADER FOR EEL STRIP AT RIGHT-HAND SIDE OF FIRST CLASS.Sep 1, 1997 · N1837U · Doug DC1010 · Light System WiringSDR 97UAL900636Battery Pack · dischargedFIRST CLASS LEFT SIDE EEL LIGHTS INOP. REPLACED BATTERY PACK, CHECKS GOOD.Aug 27, 1997 · N1837U · Doug DC1010 · Emergency LightingSDR 97UAL900531Tube · rupturedDURING THE SLIDE RAFT RETENTION TEST, THE BOTTOM CENTER SUPPORT TUBE SEAM SEPARATED. THE SLIDE RAFT WAS DISCARDED.Jul 1, 1997 · N1837U · Doug DC1010 · Life RaftSDR 97UAL900526Hyd Hose · leakingRETURN TO BLOCKS ACCOUNT OF HYDRAULIC FLUID LEAKING FROM RIGHT MAIN WHEEL WELL. *S/D* NR 1 AUXILARY PUMP PRESSURE HOSE LEAKING. REPLACED HOSE ASSEMBLY.Jul 1, 1997 · N1837U · Doug DC1010 · Hydraulic System, AuxiliarySDR 97UAL900349Engine · malfunctionedCREW REPORTED, SMOKE IN COCKPIT FROM NR 1 PACK AFTER TAKEOFF. SMOKE STOPPED AS SOON AS NR 1 PACK TURNED OFF. SUPPLEMENTAL DATA UPDATE, NO CONFIRMED SOURCE OF THE SMOKE WAS FOUND. THE ENGINE IN THE NR 1 POSITION WAS REPLACED TWO DAYS LATER FOR DETERIORATION May 4, 1997 · N1837U · Doug DC1010 · Engine (Turbine/Turboprop)SDR 97ZZZX1742Aileron · debondedDURING ROUTINE C-CHECK, FOUND RT OTBD AILERON DISBONDED FROM INTERNAL DOUBLER. REPLACED BOTH LOWER SKINS.Mar 31, 1997 · N1837U · Doug DC1010 · AileronsSDR 97ZZZX1269Skin · corrodedDURING MPV MAINTENANCE CHECK, FOUND CENTER W/W TUNNEL SKIN CORRODED OTBD SIDE OF LONGERON 49R, STA 1519. SUSPECT CAUSE WAS MOISTURE. PROPER APPLICATION OF CORROSION PREVENTIVE COULD PREVENT RECURRENCE.Dec 15, 1996 · N1837U · Doug DC1010 · Fuselage Main, Plate/SkinSDR 97ZZZX1268Longeron · corrodedDURING MPV MAINTENANCE CHECK, FOUND CENTER W/W TUNNEL, 48L END FITTING AT STA 1521 BADLY PITTED ALONG OTBD FLANGE. SUSPECT CAUSE WAS MOISTURE. PROPER APPLICATION OF CORROSION PREVENTIVE COULD PREVENT RECURRENCE.Dec 15, 1996 · N1837U · Doug DC1010 · Fuselage Main, Longeron/StringerSDR 97ZZZX1267Longeron · corrodedDURING MPV MAINTENANCE CHECK, FOUND CENTER W/W TUNNEL, LONGERON 50L END FITTINGS CORRODED ALONG OTBD FLANGE, STA 1521. SUSPECT CAUSE WAS MOISTURE. PROPER APPLICATION OF CORROSION PREVENTIVE COULD PREVENT RECURRENCE.Dec 15, 1996 · N1837U · Doug DC1010 · Fuselage Main, Longeron/StringerSDR 97ZZZX1266Longeron · corrodedDURING MPV MAINTENANCE CHECK, FOUND CENTER W/W TUNNEL LONGERON 48L LOWER FLANGE BADLY CORRODED, STA 1506. SUSPECT CAUSE WAS MOISTURE. PROPER APPLICATION OF CORROSION PREVENTIVE COULD PREVENT RECURRENCE.Dec 15, 1996 · N1837U · Doug DC1010 · Fuselage Main, Longeron/StringerSDR 97ZZZX1265T Angle · corrodedDURING MPV MAINTENANCE CHECK, FOUND CENTER CARGO DOOR FRAME LOWER T-ANGLE EXFOLIATED, STA 1681, STR 44R. SUSPECT CAUSE WAS STRESS RELATED. APPLICATION OF CORROSION PREVENTIVE COULD PREVENT RECURRENCE.Dec 15, 1996 · N1837U · Doug DC1010 · Fuselage Miscellaneous StructureSDR 96UAL900048Spring · failedSPOILERS FAILED TO RETRACT AFTER LANDING. HELICAL RETURN SPRING ON SPEEDBRAKE DRUM FOUND BROKEN. REPLACED SPRING.Jan 19, 1996 · N1837U · Doug DC1010 · Drag Control System
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