N618US

Service difficulty reports · 66

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 = 'N618US' AND registry_match = 'registration'
  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 0600676718Control Panel · smokeWHILE AT CRUISE, ACARS SCREEN WENT BLANK, AND THEN STARTED TO SMOKE. FLIGHT CREW PULLED ACARS C/B'S SMOKE STOPPED AND DISSIPATED. FLIGHT CONTINUED ON AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED ACARS CONTROL PANEL. OPS CHECKED GOOD, AIRCRApr 4, 2006 · N618US · Boeing 747251F · Data Transmission Auto CallSDR 0501466718Control Panel · failedDURING CRUISE THE PMS (PERFORMANCE MANAGEMENT SYSTEM) WENT BLANK. SMELLED ELECTRICAL SMOKE, AND SMOKE WAS VISIBLE FROM PEDESTAL AROUND PMS BASE. FLIGHT CREW PUT ON O2 MASKS AND GOGGLES, REFERRED TO RED CHECK LIST AND COM PROCEDURE. FOUND PMS CDU C/B POPPED,Sep 24, 2005 · N618US · Boeing 747251F · Flight Management Computing Hardware SystemSDR 0501576718Frame · corrodedDURING L-CHECK FOUND CORROSION AND CRACK ON FRAME IN LT BLG WHEEL WELL AT BS 1146. REPAIRED IAW EA 67-165244.Sep 16, 2005 · N618US · Boeing 747251F · Fuselage Main, FrameSDR 0501566718Frame · crackedDURING L-CHECK FOUND CRACK IN FRAME AT BS 380 S27R AND S28R. REPAIRED IAW EA 67-165241.Sep 15, 2005 · N618US · Boeing 747251F · Fuselage Main, FrameSDR 0501146718Fuel Cell · leakingDURING TAKE-OFF THERE WAS A STRONG FUEL ODOR IN COCKPIT. SMELL CLEARED ONCE PACKS WERE TURNED ON. AIRCRAFT CONTINUED ON TO DESTINATION AND LANDED WITHOUT INCIDENT. ANC MAINTENANCE FOUND LEAK ON SEAM 15 INCHES AHEAD OF NR 2 SUMP DRAIN, AND SEALED EXTERNAL TAJul 8, 2005 · N618US · Boeing 747251F · Fuel StorageSDR 0501136718Odor · detectedDURING ROTATION AT TAKE-OFF, THERE WAS A STRONG SMELL OF FUEL ODOR. SMELL CLEARED IN 2-3 MINUTES AFTER PACK ACTIVATION. AIRCRAFT CONTINUED ON TO DESTINATION AND LANDED WITHOUT INCIDENT. SIN MAINTENANCE CHECKED FOR FUEL LEAKS, NONE FOUND. AIRCRAFT OK FOR REJul 7, 2005 · N618US · Boeing 747251F · Air Distribution SystemSDR 0500656718Skin · crackedDURING OVERNIGHT LINE CHECK, FOUND CRACK IN FUSELAGE SKIN AT BS 1705 S34L. REFERENCE SB 747-53A2487, AD 2002-23-15 AND AD 2004-07-22. REPAIRED PER EA 67-192649.Apr 28, 2005 · N618US · Boeing 747251F · Fuselage Main, Plate/SkinSDR 0401436718Engine · fireDURING TAXI IN, THE NR 2 ENGINE FIRE WARNING ANNUNCIATED. THE CREW SHUT DOWN THE ENGINE AND DISCHARGED THE LT FIRE BOTTLE FOR NR 2 ENGINE. THE FIRE WARNING CEASED. NO OTHER ABNORMAL ENGINE INDICATIONS WERE OBSERVED. MAINTENANCE INSPECTION FOUND EVIDENCE OF A Aug 24, 2004 · N618US · Boeing 747251F · Engine (Turbine/Turboprop)SDR 0400696718Bulkhead · crackedDURING H-CHECK FOUND CRACK IN BULKHEAD CHORD AT BS 1000 FROM 36L TO 40L. REPAIRED PER EA 67-165121.May 5, 2004 · N618US · Boeing 747251F · Fuselage Main, BulkheadSDR 0400726718Floorbeam · crackedDURING H-CHECK FOUND CRACK IN UPPER DECK FLOORBEAM CHORD AT BS 520. REPAIRED PER EA 67-165122.May 4, 2004 · N618US · Boeing 747251F · Fuselage Main, Floor BeamSDR 0400716718Floorbeam · crackedDURING H-CHECK FOUND CRACK IN UPPER DECK FLOORBEAM CHORD AT BS 420 BETWEEN LBL 8 AND RBL 58. REPAIRED PER EA 67-165119.May 4, 2004 · N618US · Boeing 747251F · Fuselage Main, Floor BeamSDR 0400736718Fitting · crackedDURING H-CHECK FOUND CRACK IN NOSE CARGO DOOR FRAME CLOSURE FITTING. REPAIRED PER EA 67-165115.Apr 30, 2004 · N618US · Boeing 747251F · Fuselage Main, Attach FittingsSDR 0302056718Amplifier · faultyDURING CRUISE, THE NR 5 MAIN DECK CARGO SMOKE DETECTION SYSTEM INDICATED A FIRE. THE OVERHEAD CARGO FIRE LIGHT ILLUMINATED AND THE MASTER FIRE WARNING ACTIVATED. VISUALLY INSPECTED CARGO ON MAIN DECK WITH NO SIGNS OF FIRE OR SMOKE. AIRCRAFT CONTINUED TO DESNov 15, 2003 · N618US · Boeing 747251F · Smoke DetectionSDR 0301696718Computer · inoperativeDURING CLIMB THE LOWER YAW DAMPER LIGHT ILLUMINATED BRIEFLY AND THE AIRCRAFT WAS DIFFICULT TO CONTROL IN HEADING. SLOWED AIRCRAFT TO 270 KNOTS AND TURNED OFF LOWER YAW DAMPER BUT AIRCRAFT WAS STILL DIFFICULT TO CONTROL IN HEADING. AIRCRAFT DECLARED AN EMERGENCSep 4, 2003 · N618US · Boeing 747251F · Autopilot SystemSDR 0300166718Bulkhead · crackedDuring "L" check found crack on #4 pylon rear engine mount bulkhead. Repaired per EA 67-165031.Jan 28, 2003 · N618US · Boeing 747251F · Nacelle/Pylon, Bulkhead/FirewallSDR 0300176718Bulkhead · crackedDuring "L" Check found crack on #2 pylon rear engine mount bulkhead. Repaired per EA 67-165032.Jan 28, 2003 · N618US · Boeing 747251F · Nacelle/Pylon, Bulkhead/FirewallSDR 0300186718Web · crackedDuring "L" check found crack in frame web at BS 360 at S23 and S24. Repaired per EA 67-165034.Jan 28, 2003 · N618US · Boeing 747251F · Fuselage Main, FrameSDR 0300196718Web · crackedDuring "L" check found crack in frame web at BS 380 S23R. Repaired per EA 67-165035.Jan 28, 2003 · N618US · Boeing 747251F · Fuselage Main, FrameSDR 0300136718Web · crackedDuring "L" check found crack in nose wheel wheel top panel frame web at BS 284 LBL 10. Repaired per EA 67-165037.Jan 27, 2003 · N618US · Boeing 747251F · Fuselage Main, FrameSDR 0200176718Battery · overheatedDURING FLIGHT, A STRONG ELECTRICAL FUME EMITTED IN THE COCKPIT. FUME SMELL DID NOT DISSIPATE AFTER COMPLYING WITH THE EMERGENCY PROCEDURES AND THE COM. CREW DIVERTED TO NRT, DECLARED AN EMERGENCY, AND DUMPED 100,000 LBS OF FUEL. DURING LANDING WHILE IN REVERSEJan 22, 2002 · N618US · Boeing 747251F · Battery/Charger SystemSDR 0104206718Wire · burnedDURING FLIGHT, A STRONG ELECTRICAL FUME EMITTED IN THE COCKPIT. REMOVED CAPTAIN'S FLUORESCENT GLARESHIELD LIGHTS AND FUMES DISSIPATED. AIRCRAFT CONTINUED TO DESTINATIONA AND LANDED WITHOUT INCIDENT. REPLACED WIRE AT CAPTAIN'S GLARESHIELD LIGHT. OPERATIONAL Nov 8, 2001 · N618US · Boeing 747251F · Flight Compartment LightingSDR 0002946718Seat Track · crackedDURING M CHECK, FOUND CRACK IN SEAT TRACK CROWN AT BS 1727 RBL 33. REPAIRED PER EA 67-177772.Jul 6, 2000 · N618US · Boeing 747251F · Fuselage, Seat/Cargo Attach FittingsSDR 0002476718Floorbeam · corrodedDURING M CHECK, FOUND CORROSION ON FLOORBEAM AT BS 1840 BL 0. REPAIRED PER EA 67-177822.Jul 1, 2000 · N618US · Boeing 747251F · Fuselage Main, Floor BeamSDR 0002486718Floorbeam · corrodedDURING M CHECK, FOUND CORROSION ON HORIZONTAL FLANGE OF LONGITUDINAL FLOORBEAM AT BS 1140 LBL 50. REPAIRED PER EA 67-177827.Jun 28, 2000 · N618US · Boeing 747251F · Fuselage Main, Floor BeamSDR 0002146718Skin · crackedDURING M-CHECK, FOUND CRACK IN THE NUMBER 4 INBOARD PYLON SKIN, AT SLOT SEAL, NACELLE STATION 180. REPAIRED PER EA 67-175573.Jun 16, 2000 · N618US · Boeing 747251F · Nacelle/Pylon, Plate/SkinSDR 0002256718Flange · corrodedDURING -M- CHECK FOUND CORROSION ON CABIN FLOOR, RT SIDEWALL FLANGE AT BS 1500. REPAIRED PER EA 67-176782.Jun 14, 2000 · N618US · Boeing 747251F · Fuselage Miscellaneous StructureSDR 0002136718Frame · crackedDURING M-CHECK, FOUND CRACK ON FRAME AT BS 1416, STRINGER 23R. REPAIRED PER EA 67-177809.Jun 5, 2000 · N618US · Boeing 747251F · Fuselage Main, FrameSDR 0001536718Skin · crackedDURING LINE MAINTENANCE INSPECTION FOUND CRACK IN NR 4 PYLON INBOARD SKIN, SLOT SEAL CUTOUT, NAS STATION 180. REPAIRED PER EA 67-175573.May 2, 2000 · N618US · Boeing 747251F · Nacelle/Pylon, Plate/SkinSDR 9905236718Fire Loop · malfunctionedDURING CRUISE, THE NR 4 ENGINE NACELLE FIRE DETECTION FAULT LIGHT ILLUMINATED. THE FIRE DETECTION LIGHT ILLUMINATED INTERMITTENTLY AND THE 'A' AND 'B' NACELLE TEMP INDICATORS INTERMITTENTLY INDICATED HIGH. AIRCRAFT DIVERTED TO DTW AND LANDED WITHOUT INCIDENTDec 3, 1999 · N618US · Boeing 747251F · Fire DetectionSDR 9901666718Frame · crackedDURING M CHECK, FOUND CRACK IN C3 CLOSURE FRAME ON THE MAIN DECK FS 281, LBL 45. REPAIRED CLOSURE FRAME PER EA 67-164977.Apr 5, 1999 · N618US · Boeing 747251F · Fuselage Main, FrameSDR 9901556718Frame · crackedDURING PERIODIC CHECK, FOUND CRACKS AT FS 380, STR 25L FRAME WEB AND STR 25R FRAME. REPAIRED PER EA 67-164976.Apr 5, 1999 · N618US · Boeing 747251F · Fuselage Main, FrameSDR 9806976718Tachometer · malfunctionedDURING TAKEOFF ROLL AT APPROXIMATELY 115 KTS, THE NR 4 ENGINE N1 RPM INDICATION MALFUNCTIONED. THE TAKEOFF WAS ABORTED. MAINTENANCE PLACED THE NR 4 ENGINE N1 INDICATION SYSTEM ON MEL AND THE AIRCRAFT RETURNED TO SERVICE.Apr 19, 1998 · N618US · Boeing 747251F · Engine RPM Indicating SystemSDR 9807426718Floorbeam · crackedDURING PERIODIC CHECK, FOUND A CRACK IN A UPPER DECK FLOORBEAM UPPER CHORD FASTENER HOLE AT THE FUSELAGE FRAME FS 360, RIGHT SIDE. REPAIRED PER EA 67-121410.Apr 3, 1998 · N618US · Boeing 747251F · Fuselage Main, Floor BeamSDR 9807416718Floorbeam · crackedDURING PERIODIC CHECK, FOUND A CRACK IN 2 UPPER DECK FLOORBEAM UPPER CHORD FASTENER HOLES AT THE FUSELAGE FRAME FS 340, LEFT SIDE. REPAIRED PER EA 67-121410.Apr 3, 1998 · N618US · Boeing 747251F · Fuselage Main, Floor BeamSDR 9807406718Floorbeam · crackedDURING PERIODIC CHECK, FOUND A CRACK IN A UPPER DECK FLOORBEAM UPPER CHORD FASTENER HOLE AT THE FUSELAGE FRAME FS 380, RIGHT SIDE. REPAIRED PER EA 67-121410.Apr 3, 1998 · N618US · Boeing 747251F · Fuselage Main, Floor BeamSDR 9807396718Floorbeam · crackedDURING PERIODIC CHECK, FOUND A CRACK IN 2 UPPER DECK FLOORBEAM UPPER CHORD FASTENER HOLES AT THE FUSELAGE FRAME FS 500, RIGHT SIDE. REPAIRED PER EA 67-121410.Apr 3, 1998 · N618US · Boeing 747251F · Fuselage Main, Floor BeamSDR 9804876718Compressor · stalledWHILE AT CRUISE FL350, THE NR 1 ENGINE COMPRESSOR STALLED. THE ENGINE WAS SHUT DOWN AFTER REACHING AN EGT OF 1002C FOR 5 SECONDS. NO RESTART WAS ATTEMPTED. THE FLIGHT CONTINUED TO KIX WITHOUT FURTHER DIFFICULTY. THE AIRCRAFT WAS REMOVED FROM SERVICE AND THMar 22, 1998 · N618US · Boeing 747251F · Turbine Engine Compressor SectionSDR 9804836718Breather Tube · crackedWHILE IN CRUISE, THE NR 1 ENGINE OIL QUANTITY WENT TO ZERO WITH THE OIL PRESSURE DROPPING RAPIDLY DOWN TO 8 TO 9 PSI. THE ENGINE WAS SHUT DOWN PER COM PROCEDURE AND THE AIRCRAFT RETURNED TO ANC WITHOUT DIFFICULTY. MAINTENANCE INSPECTED THE ENGINE AND REPLACEMar 20, 1998 · N618US · Boeing 747251F · Turbine Engine Oil SystemSDR 9803856718Spar Web · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON FRONT SPAR WEB AT THE LOWER CHORD FS 1014 TO 1018. REPAIRED PER EA 67-153201.Jan 27, 1998 · N618US · Boeing 747251F · Wing SparSDR 9803846718Spar Web · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON FRONT SPAR WEB AT THE LOWER CHORD FS 997 TO 1001. REPAIRED PER EA 67-153201.Jan 27, 1998 · N618US · Boeing 747251F · Wing SparSDR 9801646718Fitting · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON END FITTINGS FOR STR 38R AND 40R AT FS 2360. REPLACED FITTINGS (P/N 65B04370-46) PER BOEING DRAWING 65B04160.Jan 26, 1998 · N618US · Boeing 747251F · Fuselage Miscellaneous StructureSDR 9801666718Fitting · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON END FITTINGS FOR STR 42L, 44L, 46L, 48L, 49L, 50L, AND 51L AT FS 2360. REPLACED FITTINGS (P/N 65B04370-7) PER BOEING DRAWING 65B04161.Jan 23, 1998 · N618US · Boeing 747251F · Fuselage Miscellaneous StructureSDR 9801656718Fitting · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON END FITTINGS FOR STR 42R, 44R, 46R, 48R, 49R, 50R, AND 51R AT FS 2360. REPLACED FITTINGS (P/N 65B04370-8) PER BOEING DRAWING 65B04161.Jan 23, 1998 · N618US · Boeing 747251F · Fuselage Miscellaneous StructureSDR 9801636718Fitting · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON END FITTINGS FOR STR 38L AND 40L AT FS 2360. REPLACED FITTINGS (P/N 65B04370-45) PER BOEING DRAWING 65B04160.Jan 23, 1998 · N618US · Boeing 747251F · Fuselage Miscellaneous StructureSDR 9801196718Fitting · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON END FITTINGS FOR LONGERONS 38L, 40L, 42L, 44L, 46, 48L, 49L, 50L, AND 51L AT FS 2360. REPLACED FITTINGS PER BOEING DRAWING 65B02699.Jan 17, 1998 · N618US · Boeing 747251F · Fuselage Miscellaneous StructureSDR 9801186718Fitting · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON END FITTINGS FOR LONGERONS 38R, 42R, 44R, 46R, 48R, 49R, 50R, AND 51R AT FS 2360. REPLACED FITTINGS PER BOEING DRAWING 65B02699.Jan 17, 1998 · N618US · Boeing 747251F · Fuselage Miscellaneous StructureSDR 9714556718Oil Filter · dirtyWHILE IN CRUISE, THE NR 3 ENGINE OIL FILTER BYPASS LIGHT BEGAN TO FLICKER, AFTER 2-3 MINUTES THE LIGHT WAS STEADY AND REMAINED STEADY WHEN POWER WAS REDUCED TO IDLE. THE ENGINE WAS SHUT DOWN AND LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE FOUND THE MAJul 28, 1997 · N618US · Boeing 747251B · Turbine Engine Oil SystemSDR 9709046718Spar Web · corrodedDURING ARMAR, FOUND CORROSION ON LEFT WING FRONT SPAR WEB FSS 607. REPAIRED PER \NEA 67-121744.Mar 23, 1997 · N618US · Boeing 747251F · Wing SparSDR 9709056718Doubler · crackedDURING ARMAR, FOUND CRACKED DOUBLER IN NOSE WHEEL WELL BS 400, RBL 26. REPAIRED PER EA 66-121741.Mar 20, 1997 · N618US · Boeing 747251F · Fuselage Miscellaneous StructureSDR 9709066718Frame · crackedDURING ARMAR, FOUND CRACK IN FRAME AT CABLE CUT OUT BELOW STR 26L, FS 434. REPAIRED PER EA 67-121723.Mar 17, 1997 · N618US · Boeing 747251F · Fuselage Main, Frame
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