N625US, cancelled Sep 27, 2007

Service difficulty reports · 37

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 = 'N625US' AND deregistration_id = 'N625US-2007-09-27'
  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 0301786625Power Supply · inoperativeDURING LINE CHECK, FOUND ZONE-E FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD.Sep 24, 2003 · N625US · Boeing 747251B · Emergency LightingSDR 0101696625Unknown · odorDURING CRUISE, A SMOKE ODOR WAS NOTICED AROUND DOOR 5L. THE ODOR DISSIPATED AFTER A FEW MINUTES AND THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. CHECKED LIGHTS, CABIN ENTERTAINMENT SYSTEM, LAVATORIES, AND ELECTRONIC EQUIPMENT COMPARTMENMay 5, 2001 · N625US · Boeing 747251B · Air Distribution SystemSDR 0101676625Wire · shortedDURING FLIGHT, THE NR 2 HOT PLATE SPARKED AND EMITTED SMOKE RESULTING IN TRIPPING OF THE CIRCUIT BREAKER. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPAIRED CHAFED WIRE. OPERATIONAL CHECK GOOD.May 5, 2001 · N625US · Boeing 747251B · Buffet/GalleysSDR 0100226625Controller · failedDURING CLIMB AT 24,000 FEET, THE PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED ACCOMPANIED WITH THE NR 2 PACK TRIPPING AND THE PRESSURE RELIEF LIGHT ILLUMINATING. PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET AND CABIN WAS CONTROLLED MANUALLY AT 14,000 FEET. AIJan 18, 2001 · N625US · Boeing 747251B · Cabin Pressure ControllerSDR 0004656625Service difficultyDURING CRUISE, NOTICED FAINT BURNING SMELL. SHUYT DOWN WEATHER RADAR AND SMELL DISAPPEARED. MAINTENANCE FOUND ELECTRICAL CONNECTOR DIRTY. CLEANED CONNECTORS AND REPLACED THE RADAR INDICATORS PRECAUTIONARY. RADAR SYSTEM TESTED OK.Dec 28, 2000 · N625US · Boeing 747251B · Weather Radar SystemSDR 0002966625Acm · failedDURING APPROACH, A SMOKE SMELL WAS NOTICED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE NR 1 AIR CYCLE MACHINE. OPERATIONAL CHECK GOOD.Aug 15, 2000 · N625US · Boeing 747251B · Cabin Cooling SystemSDR 0002976625Acm · failedDURING APPROACH, AN ELECTRICAL SMOKE SMELL WAS NOTICED IN THE CABIN COMPARTMENT. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE NR 3 AIR CYCLE MACHINE. OPERATIONAL CHECK GOOD.Aug 13, 2000 · N625US · Boeing 747251B · Cabin Cooling SystemSDR 0002156625Circuit Board · defectiveDURING FLIGHT, THE NR 4 ENGINE NACELLE TEMPERATURE INDICATED ''A'' FLUCTUATED INTO RED WITH ASSOCIATED FAULT LIGHT AND FIRE DETECTOR LIGHT ILLUMINATING ON ANNUNCIATOR PANEL. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE NR 4 ENGJun 11, 2000 · N625US · Boeing 747251B · Fire DetectionSDR 0002046625Frame · crackedDURING M-CHECK, FOUND CRACK ON FRAME, LOCATED AT BS 500, STRINGER 11R. REPAIRED PER EA 66-176689.May 24, 2000 · N625US · Boeing 747251B · Fuselage Main, FrameSDR 0002026625Shear Tie · crackedDURING M-CHECK, FOUND CRACK ON FRAME SHEAR TIE, LOCATED AT BS 520, STRINGER 11R. REPAIRED PER EA 66-176687 REV A.May 24, 2000 · N625US · Boeing 747251B · Fuselage Main, StructureSDR 0002266625Angle · corrodedDURING -M- INSPECTION, FOUND CORROSION ON CABIN FLOOR RT SIDEWALL FLANGE. REPAIRED PER EA 66-176776.May 22, 2000 · N625US · Boeing 747251B · Fuselage Miscellaneous StructureSDR 0001976625Frame · crackedDURING M-CHECK, FOUND CRACK ON FRAME WEB LOCATED AT STATION 1265. REPAIRED PER EA66-175568.May 22, 2000 · N625US · Boeing 747251B · Fuselage Main, FrameSDR 0002006625Frame · crackedDURING M-CHECK, FOUND CRACKED FRAME WEB AT STRINGER CUTOUT UPPER INBOARD CORNER AT BS 360, STRINGER 10L. REPAIRED PER EA66-176684.May 19, 2000 · N625US · Boeing 747251B · Fuselage Main, FrameSDR 0001996625Frame · crackedDURING M-CHECK, FOUND CRACK ON FRAME WEB AT STRINGER CUTOUT UPPER INBOARD CORNER, AT BS 380, STRINGER 10R. REPAIRED PER EA 66-176683 REV A.May 19, 2000 · N625US · Boeing 747251B · Fuselage Main, FrameSDR 0002036625Frame · crackedDURING M-CHECK, FOUND CRACK ON FRAME, LOCATED AT BS 420, STRINGER 14R. REPAIRED PER EA66-176688.May 18, 2000 · N625US · Boeing 747251B · Fuselage Main, FrameSDR 0002016625Frame · crackedDURING M-CHECK, FOUND CRACK ON INBOARD EDGE OF FRAME WEB, LOCATED AT STATION 360, STRINGER 2R. REPAIRED PER EA 66-176686 REV A.May 18, 2000 · N625US · Boeing 747251B · Fuselage Main, FrameSDR 0001986625Frame · crackedDURING M-CHECK, FOUND CRACK AT CANTED BULKHEAD FRAME LOCATED AT STATION 260, STRINGER 32L. REPAIRED PER EA66-176190.May 18, 2000 · N625US · Boeing 747251B · Fuselage Main, FrameSDR 0002056625Frame · crackedDURING M-CHECK, FOUND CRACK ON FRAME, LOCATED AT BS 460, STRINGER 11 TO 12R. REPAIRED PER EA 66-176727.May 13, 2000 · N625US · Boeing 747251B · Fuselage Main, FrameSDR 9902096625Actuator · failedDURING APPROACH, THE NOSE LANDING GEAR WOULD NOT EXTEND. RECYCLED THE LANDING GEAR AND GEAR EXTENDED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE NOSE LANDING GEAR DOOR ACTUATOR, OPERATIONAL CHECK GOOD.Jun 16, 1999 · N625US · Boeing 747251B · Landing Gear Door ActuatorSDR 9900466625Actuator · leakingDURING CRUISE (TPE), NR 1 HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. TURNED NR 1 HYDRAULIC PUMP OFF AND AIRCRAFT CONTINUED TO NRT AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS TOWED OFF THE RUNWAY TO THE GATE. REPLACED THE NOSE LANDING GEAR DOOR ACTUATOR. OPERATIFeb 9, 1999 · N625US · Boeing 747251B · Landing Gear Door ActuatorSDR 9811166625Battery · dischargedDURING LINE CHECK, FOUND B ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY, OPERATIONAL CHECK GOOD.Sep 26, 1998 · N625US · Boeing 747251B · Emergency LightingSDR 9723526625Spar Web · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE LEFT WING FORWARD SPAR WEB (P/N 65B225851-2) BETWEEN FSS 950-980. REPAIRED PER EA 66-152345.Nov 25, 1997 · N625US · Boeing 747251B · Wing SparSDR 9722826625Spar Web · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON LEFT WING FORWARD SPAR WEB BETWEEN FSSI 1050 TO 1078. REPAIRED PER EA 66-153654.Nov 25, 1997 · N625US · Boeing 747251B · Wing SparSDR 9721396625Power Supply · inoperativeDURING LINE CHECK, FOUND 7 EMERGENCY EXIT SIGNS THROUGHOUT THE AIRCRAFT THAT FAILED THE 10 MINUTE CAPACITY CHECK. REPLACED THE POWER SUPPLIES, OPERATIONAL CHECK GOOD.Nov 13, 1997 · N625US · Boeing 747251B · Emergency LightingSDR 9721426625Press Deck · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON CEILING PRESSURE DECK I BEAM IN THE RIGHT WHEEL WELL FS 1265, RBL 105 TO 117. REPAIRED PER EA 66-152533.Nov 11, 1997 · N625US · Boeing 747251B · Fuselage Miscellaneous StructureSDR 9716656625Pump · leakingDURING CRUISE, THE NR 4 HYDRAULIC SYSTEM INDICATED A LOSS OF FLUID AND PRESSURE. AIRCRAFT DIVERTED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE NR 4 ENGINE DRIVEN PUMP, OPERATIONAL CHECK GOOD.Sep 2, 1997 · N625US · Boeing 747251B · Hydraulic Pump (Electric/Engine), MainSDR 9701866625Engine · bird strikeDURING CLIMB AFTER DEPARTURE, CREW REPORTED POSSIBLE BIRD STRIKE ON RIGHT WING. DURING CRUISE FLIGHT, NR 3 ENGINE HAD A LOW FREQUENCY VIBRATION AT LOWER POWER SETTINGS. NR 3 ENGINE OIL QUANTITY BEGAN TO DECREASE, NR 3 ENGINE WAS SHUT DOWN AND LATER RESTARTEDJan 27, 1997 · N625US · Boeing 747251B · Engine (Turbine/Turboprop)SDR 9701406625Aural Warn · malfunctionedDURING TAKEOFF, THE AURAL WARNING HORN SOUNDED. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE COULD NOT DUPLICATE FAULT, OPERATIONAL CHECK OF AURAL WARNING SYSTEM AND FLAP SYSTEM CHECKED GOOD.Jan 18, 1997 · N625US · Boeing 747251B · Central WarningSDR 9700826625Seat Track · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON SEAT TRACK FLANGE. REPAIRED PER EA 66-121308.Jan 3, 1997 · N625US · Boeing 747251B · Fuselage, Seat/Cargo Attach FittingsSDR 9623076635Compressor · stalledDURING TAKEOFF ROTATION, THE NR 3 ENGINE EXPERIENCED TWO COMPRESSOR STALLS. AT THE TIME OF STALL, EGT ROSE TO 850 DEGREES CELSIUS FOR APPROXIMATELY FIVE MINUTES. EPR WAS 1.60 AND N1 AND N2 FLUCTUATED THEN DROPPED TO THE BOTTOM OF THE SCALE. CREW SHUT DOWN TOct 26, 1996 · N625US · Boeing 747227B · Turbine Engine Compressor SectionSDR 9618976625Control Handle · lack of lubeDURING APPROACH THE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR EXTENSION. RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. LUBRICATED LANDING GEAR CONTROL HANDLE, OPERATIONAL CHECK GOOD.Aug 30, 1996 · N625US · Boeing 747251B · Landing Gear SelectorSDR 9601056625Pack · malfunctionedAFTER TAKEOFF AND SUBSEQUENTLY TURNING OFF PACKS, SMOKE FILLED THE ENTIRE AIRCRAFT. WITH ALL PACKS SHOWING NORMAL OPERATING TEMPERATURE, THE SMOKE DISSIPATED WITHIN A MINUTE. CREW FOLLOWED COCKPIT OPERATING PROCEDURE, DUMPED 177,000 POUNDS OF FUEL, AND RETURJan 17, 1996 · N625US · Boeing 747251B · Cabin Cooling SystemSDR 9600436625Power Supply · inoperativeDURING LINE CHECK, FOUND THE STATE ROOM EMERGENCY TRACK LIGHT INOPERATIVE. REPLACED THE POWER SUPPLY AND BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL.Jan 10, 1996 · N625US · Boeing 747251B · Emergency LightingSDR 9508226625Retract Mech · reqd serviceDURING CLIMB, THE RIGHT BODY GEAR TILT LIGHT ILLUMINATED AND GEAR WOULD NOT RETRACT IN BOTH PRIMARY AND ALTERNATE. CREW FOLLOWED COCKPIT OPERATING MANUAL AND PROCEEDED FOR LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE BLED THE SYSTEM AND RECYCLED CIRCUIT BREMay 20, 1995 · N625US · Boeing 747251B · Landing Gear Retraction/Extension SystemSDR 9508216625Line · chafedDURING CLIMB, THE RIGHT BODY GEAR TILT LIGHT ILLUMINATED AND BOTH PRIMARY AND ALTERNATE GEAR WOULD NOT RETRACT. CREW FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE AND MADE AN UNEVENTFUL LANDING IN MNL. MAINTENANCE FOUND RIGHT TILT ACTUATOR HYDRAULIC LINE CHAFEMay 20, 1995 · N625US · Boeing 747251B · Landing Gear Retraction/Extension SystemSDR 9506156625Bleed Valve · malfunctionedDURING TAKEOFF, THE NR 4 ENGINE EXPERIENCED EGT RISE AND POWER WAS REDUCED TO KEEP WITHIN LIMITS. DURING CLIMB THE FAULT LIGHT CAME ON INDICATING IN THE 8 TO 10 RANGE. THE NACELLE DETECTOR WAS SWITCHED TO 'B' AND THE BELL AND LIGHT CAME ON. THE ENGINE WAS SApr 18, 1995 · N625US · Boeing 747251B · Compressor Bleed ValveSDR 9505466625Control Cable · disconnectedDURING TAKEOFF ROLL, THE NR 4 ENGINE WOULD NOT RESPOND TO POWER LEVER MOVEMENT AND THE TAKEOFF WAS ABORTED. THE CONTROL CABLE IN THE PYLON WAS FOUND TO HAVE DISCONNECTED AT THE PYLON DRUM. THE CABLE BOX IN THE PYLON WAS REPLACED AND THE SYSTEM OPERATION CHECApr 9, 1995 · N625US · Boeing 747251B · Power Lever
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