N610NW, cancelled Nov 24, 2008
Service difficulty reports · 48
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 = 'N610NW' AND deregistration_id = 'N610NW-2008-11-24' 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.
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 = 'N610NW' AND deregistration_id = 'N610NW-2008-11-24' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 0700439610Clamp · brokenWHILE CLIMBING PASS FL280, THE CABIN ALTITUDE BEGAN TO CLIMB UNCONTROLLABLY AT 1000 FPM. FLIGHT CREW INITIATED AN EMERGENCY DESCENT TO 8000 FEET AND RETURNED TO DEPARTURE. COM PROCEDURES WERE COMPLIED WITH, THE OUTFLOW VALVE WAS CONFIRMED CLOSED BUT THE CABISDR 0500219610Coupling · separatedDURING CRUISE FLIGHT, THE CABIN CONTINUED TO CLIMB. WHEN CABIN PRESSURE REACHED 9500 FEET, THE CREW SWITCHED TO MANUAL PRESSURE CONTROL AND STILL UNABLE TO STOP THE LOSS OF PRESSURE. BOTH PACKS WERE AT FULL COLD WITH 18-20 PSI, ALL ANTI-ICE OFF, AND OUTFLOW SDR 0500259610Stiffener · crackedDURING H-CHECK FOUND CRACK IN AFT CARGO COMPARTMENT FORWARD BULKHEAD VERTICAL STIFFENER AT BS 756 L26L. REPAIRED PER EA 99-201836.SDR 0500239610Bulkhead · corrodedDURING H-CHECK FOUND CORROSION ON AFT PRESSURE BULKHEAD WEB AND DOUBLER BETWEEN L22 TO L23R. REPAIRED PER EA 96-202500.SDR 0300899610Valve · inoperativeON DESCENT BUT LEVEL AT FL240 THE CABIN ALTITUDE AND MASTER WARNING LIGHTS ILLUMINATED. CABIN CLIMBED AT 1500 FPM AND EMERGENCY DESCENT WAS INITIATED. CABIN MASKS DEPLOYED DURING THE RAPID DESCENT TO 11,000 FEET YET CABIN ALTITUDE NEVER INDICATED OVER 12,000SDR 0200939610Skin · crackedDuring Hck in DHN, crack damage was found at the fwd service door skin at the lower left corner area. Repaired per EA 96-189244,SDR 0100439610Apu · overservicedDURING CLIMB, FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN. FORWARD LAV DETECTOR SOUNDED. FLIGHT CREW RETURNED TO DEPARTURE AIRPORT. SMOKE BEGAN TO DISSIPATE DURING RETURN TO DEPARTURE AIRPORT. AN UNEVENTFUL LANDING WAS PERFORMED. MAINTENANCE FOUND APU OIL OSDR 0002389610Duct · blownDURING DESCENT AT 23,000 FEET, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. FLIGHT CREW DECLARED YELLOW EMERGENCY AND CONTINUED TO DESTINATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DUCT ASSEMBLY BLOWN ON RIGHT SIDE NEAR WATER SEPARATOSDR 0000489610Fire Detector · malfunctionedAFTER TAKEOFF, CARGO FIRE DETECTION SYSTEM A INDICATED A FIRE IN THE FORWARD CARGO HOLD. THE AIRCRAFT HAD CARGO FIRE DETECTION SYSTEM B ON MEL, SO THE CREW DID NOT HAVE SECONDARY VERIFICATION CAPABILITY. THE CREW DISCHARGED THE FORWARD CARGO AREA FIRE EXTINGSDR 9902989610Temp Light · illuminatedTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. CREW DECLARED AN EMERGENCY AND THE FLIGHT WAS RETURNED TO BNA. AIRCRAFT LANDED WITHOUT INCIDENT. PROBLEM COULD NOT BE DUPLICATED ON GROUND. NO LEAKS WERE FOUND IN TAIL AREA. AIRCRAFT RETURSDR 9902399610Fuel Control · out of adjustDURING TAKEOFF ROLL AT 100 KNOTS, THE RIGHT ENGINE WOULD NOT REACH TARGET EPR INDICATION. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TRIMMED THE FUEL CONTROLS FOR THE LEFT AND RIGHT ENGINES. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.SDR 9900949610Frame · crackedDURING PERIODIC CHECK, FOUND FRAME UNDER AIRSTAIR TORQUE TUBE CRACKED IN AFT ACCESSORY COMPARTMENT. BRACKET TO FRAME WAS ALSO BROKEN. INSTALLED REPAIR PER EA 96-165737.SDR 9900939610Frame · crackedDURING PERIODIC CHECK, FOUND FRAME CRACKED IN RADIUS; BOTTOM OF CANTED FRAME AT FS 1143. INSTALLED REPAIR PER EA 96-165739.SDR 9809669610Clamps · looseTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CLAMPS AT LEFT AUGMENTATION VALVE, OPERATIONAL CHECK NORMAL.SDR 9809089610Computer · inoperativeEN ROUTE TO IAD, ALL STALL WARNING INDICATIONS SOUNDED OFF. FLIGHT CREW FOLLOWED COM PROCEDURES, CONTACTED DISPATCH CONTROL, DIVERTED FLIGHT TO DTW, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE STALL WARNING COMPUTER. OPRATIONAL CHECK NORMAL.SDR 9806369610Battery · dischargedDURING LINE CHECK, FOUND AFT EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.SDR 9724219610Battery Pack · dischargedFLIGHT ATTENDANT REPORTED AFT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.SDR 9724739610Bulkhead Skin · crackedDURING PERIODIC CHECK, FOUND CRACK IN AFT PRESSURE BULKHEAD SKIN AT LOWER RIGHT CORNER. REPAIRED PER EA 96-154147.SDR 9718959610Slide · low batteryDURING PERIODIC CHECK, SERVICE DOOR EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE.SDR 9719709610Skin · corrodedDURING L CHECK, FOUND CORROSION ON WINDOW CUTOUT FLANGE AT WINDOW 15R. REPAIRED PER EA 96-151737.SDR 9717879610Temp Controller · malfunctionedAFTER TAKEOFF, FLIGHT ATTENDANTS REPORTED CABIN AS BEING VERY WARM WITH SMOKE PRESENT. ALARM IN RIGHT LAVATORY ACTIVATED. CREW TURNED OFF BOTH PACKS AND SMOKE BEGAN TO DISSIPATE. FLIGHT WAS RETURNED TO GRB AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED SDR 9715669610Switch · out of adjustDURING TAKEOFF, THE AFT CABIN DOOR WARNING LIGHT ILLUMINATED. ABORTED TAKEOFF. ADJUSTED DOOR WARNING SWITCH, FUNCTIONAL CHECK OK.SDR 9714299610Clip · corrodedDURING M CHECK, FOUND CORROSION ON STRINGER CLIP FITTING AT LEFT WING XRS 111.5 BETWEEN STR 12 AND 13. REPLACED FITTING PER SRM 51-30-5.SDR 9714289610Clip · corrodedDURING M CHECK, FOUND CORROSION ON STRINGER CLIP FITTING AT RIGHT WS 1137 BETWEEN STR 11 AND 12. REPLACED FITTING PER SRM 51-30-5.SDR 9708529610Bulbs · failedDURING APPROACH, NOSE LANDING GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW REPLACED INDICATION LIGHT BULBS AND RECYCLED GEAR. NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH NOSE GEARSDR 9706359610Battery · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 7 THROUGH 10 INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.SDR 9703669610Retract Mech · out of adjustRIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT CONTINUED TO DTW AT REDUCED SPEED. ON GEAR EXTENSION, GEAR DOOR OPEN LIGHT REMAINED ON. CREW DECLARED AN EMERGENCY AND UTILIZED EMERGENCY GEAR EXTENSION PROCEDURES ON LANDING. AIRCRAFT SDR 9700529610Strut · reqd serviceLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. FLIGHT RETURNED TO IND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NOSE GEAR STRUT LOW. SERVICED STRUT TO PROPER LEVELS, OPERAITONAL CHECK NORMAL.SDR 9619969610Battery Pack · looseDURING LINE MAINTENANCE INSPECTION, EXTERIOR EMERGENCY LIGHTS ILLUMINATED WITH SWITCH IN ARMED POSITION. TIGHTENED TERMINAL 7 ON BATTERY PACK, OPERATIONAL CHECK NORMAL.SDR 9617319610Fuse · blownDURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED FUSE IN BATTERY PACK, OPERATIONAL CHECK NORMAL.SDR 9617329610Fuse · blownDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE IN EMERGENCY POWER PACK, OPERATIONAL CHECK NORMAL.SDR 9616649610Fuse · blownDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE, OPERATIONAL CHECK NORMAL.SDR 9610559610Door Switch · malfunctionedDURING CLIMBOUT, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT DIVERTED TO LGA AND LANDED WITHOUT INCIDENT. LIGHT REMAINED ON AFTER GEAR EXTENSION, GEAR WAS VISUALLY CONFIRMED THROUGH PERISCOPE TO BE DOWN AND LOCKED. MAINTENANCE SDR 9607829612Evac Slide · low pressureDURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE EMERGENCY EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE.SDR 9605989610Relay · malfunctionedDURING LINE MAINTENANCE INSPECTION, FOUND LEFT AND RIGHT NACELLE EMERGENCY LIGHTS INOPERATIVE. REPLACED RELAY R2-213, OPERATIONAL CHECK NORMAL.SDR 9607669610Control Panel · malfunctionLOSS OF B-PHASE ITEMS ON NR 2 GENERATOR OCCURRED EN ROUTE. FLIGHT DIVERTED TO DFW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 2 GENERATOR CONTROL PANEL, OPERATIONAL CHECK NORMAL.SDR 9605279610Epr Transmitter · malfunctionedNR 2 ENGINE EPR INDICATION DID NOT REACH TARGET ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE FLIGHT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMITTER WITH A SERVICEABLE UNIT.SDR 9603669610Epr Transmitter · malfunctionedNR 2 ENGINE EPR INDICATION FAILED IN CRUISE FLIGHT. THE AIRCRAFT DIVERTED TO DCA AND LANDED WITHOUT INCIDENT. MAINTENANCE PURGED THE SYSTEM OF MOISTURE AND REPLACED THE EPR TRANSMITTER. SYSTEM OPERATION RETURNED TO NORMAL.SDR 9603369610Slide · low pressureDURING PERIODIC CHECK, FOUND AFT TAIL SECTION EMERGENCY EVACUATION SLIDE WITH LOW PRESSURE. REPLACED SLIDE.SDR 9606689610Doubler · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE WING CENTER SECTION LOWER DOUBLER AT STR 21, FS 617 AT LBL 10. REPAIRED DOUBLER PER EA 12-5730-9-C0732.SDR 9606659610Longeron · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING STRINGERS 11, 16, 17 AND ON RIGHT WING STRINGERS 11, 12, 17, 18 APPROXIMATELY WS 58 TO 69. REPAIRED STRINGER PER EA 12-5713-9-C0660.SDR 9600359610Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE CENTER WING END FITTING (SECOND STRINGER FROM THE FORWARD END). REPLACED END FITTING (P/N 3920326-501N) PER SRM 51-30-2.SDR 9521859610Fittings · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FS 908 LOWER FRAME FITTINGS AT LONGERON 18R. REPLACED FITTINGS (P/N 49129-501, 4912817-501, 4912817-504) PER SRM 51-30-5.SDR 9521769610Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT MAIN LANDING GEAR RETRACT FITTING PIN. REPLACED FITTING PER OHM 57-40-1.SDR 9522259610Doubler · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING LANDING GEAR SUPPORT UPPER DOUBLER. REPAIRED DOUBLER (P/N 5912438) PER EA 12-5730-9-C0654.SDR 9521619610Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND RUST ON THE CENTER FLAP HINGE FITTING UPPER BUSHINGS. REPLACED FITTING PER MM 57-40-1.SDR 9517709610Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL LEFT TIE FITTING FS 37. REPLACED FITTING PER SRM 51-30-2.SDR 9522249610Skin · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING TRAILING EDGE FLAP OUTBOARD AFT LOWER SPAR CAP STA 335. REPAIRED CAP (P/N 5912125-1) PER EA 12-5750-9-C0618.
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