N8950E, cancelled Aug 13, 2008

Service difficulty reports · 35

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 = 'N8950E' AND deregistration_id = 'N8950E-2008-08-13'
  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 0001709990Wire · failedSMOKE AND ELECTRICAL SMELL IN COCKPIT. CAPTAIN''S DECLARED AN EMERGENCY AND PROCEEDED TO BUF. SMOKE CLEARED IN 5 MINUTES. CFR WAS CALLED OUT AND LANDING WAS UNEVENTFUL. MAINTENANCE FOUND BURNT WIRE TO MAP LIGHT AND PLACED ON MEL. AIRCRAFT RETURNED TO SERVMay 1, 2000 · N8950E · Doug DC931 · Light System WiringSDR 9901529990Engine · failedDURING DESCENT, THE LEFT ENGINE OIL PRESSURE BEGAN FLUCTUATING, OIL QUANTITY DROPPED TO ZERO AND THE LOW OIL PRESSURE LIGHT ILLUMINATED. CREW SHUT DOWN THE LEFT ENGINE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE. AIRCRAFT RETURApr 14, 1999 · N8950E · Doug DC931 · Engine (Turbine/Turboprop)SDR 9810039990Web · corrodedDURING H-CHECK, FOUND CORROSION ON FLOOR WEB AT FS 149, RBL 4.5 INCHES UNDER FLOOR PANEL NR 13. REPAIRED PER EA 99-159693.Aug 28, 1998 · N8950E · Doug DC931 · Fuselage Miscellaneous StructureSDR 9809989990Frame · crackedDURING H-CHECK, FOUND FINGER DOUBLER CRACKED FROM EDGE OF LAP TO FASTENER AT FS 261, LONGERON 1. REPAIRED PER EA 99-160260.Aug 25, 1998 · N8950E · Doug DC931 · Fuselage Main, FrameSDR 9807919990Window Seal · blownDURING CLIMB AT 13,000 FEET AND 5 PSI, THE CAPTAIN'S SLIDING WINDOW SEAL BLEW OUT AND CAUSED A LOUD NOISE AND SOME LOSS OF CABIN PRESSURE. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE RESEALED WINDOW.May 1, 1998 · N8950E · Doug DC931 · Flight Compartment WindowsSDR 9807189990Batteries · dischargedDURING LINE CHECK, FOUND EMERGENCY OVERHEAD LIGHTING IN FIRST CLASS SECTION DIM. MAINTNANCE REPLACED BATTERIES AND POWER SUPPLY.Apr 22, 1998 · N8950E · Doug DC931 · Emergency LightingSDR 9806109990Prox Sensor · brokenDURING APPROACH, NOSE LANDING GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW VERIFIED VISUALLY THROUGH PEEP HOLE THAT GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR PROXIMITY SENSOR BROKEN. Apr 6, 1998 · N8950E · Doug DC931 · Landing Gear Position and WarningSDR 9723009990Batteries · dischargedDURING PERIODIC CHECK, FOUND AFT END OF FORWARD OVERHEAD EMERGENCY LIGHTS AND FORWARD TWO OVERHEAD OVAL FIXTURES INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.Dec 8, 1997 · N8950E · Doug DC931 · Emergency LightingSDR 9717649990Duct · crackedDURING CLIMB, THE LEFT ENGINE EXPERIENCED A FIRE WARNING INDICAITON. CREW REDUCED LEFT ENGINE POWER SETTING AND FIRE WARNING CEASED. AIRCRAFT RETURNED TO LGA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE 13TH STAGE MANIFOLD ON THE LEFT ENGINSep 14, 1997 · N8950E · Doug DC931 · Pneumatic Distribution SystemSDR 9715859990Windshield · crackedDURING CLIMB AT FL280, THE FIRST OFFICER'S WINDSHIELD OUTER PANE CRACKED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. REPLACED THE WINDSHIELD AND THE WINDSHIELD TEMPERATURE CONTROLLER (P/N 961-5059-002, S/N 03001).Aug 20, 1997 · N8950E · Doug DC931 · Flight Compartment WindowsSDR 9713009990Power Supply · malfunctionedDURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS DIM. REPLACED POWER SUPPLIES AND BATTERIES, OPERATIONAL CHECK NORMAL.Jul 2, 1997 · N8950E · Doug DC931 · Emergency LightingSDR 9712339990Unsafe Light · illuminatedDURING APPROACH, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. CREW ACCOMPLISHED GO-AROUND PROCEDURES AND RECYCLED GEAR. NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TESTED SYSTEM AND NO PROBLEMS WERE FJun 19, 1997 · N8950E · Doug DC931 · Landing Gear Position and WarningSDR 9704349990Wire · cutDURING PERIODIC CHECK, FOUND LEFT EMERGENCY EVACUATION SLIDE LIGHT WITH WIRE CUT. INSTALLED SPLICE, OPERATIONAL CHECK NORMAL.Feb 26, 1997 · N8950E · Doug DC931 · Light System WiringSDR 9704329990Battery Pack · dischargedDURING PERIODIC CHECK, BOTH NACELLE EMERGENCY LIGHTS FAILED TEN MINUTE TEST. REPLACED BOTH BATTERY PACK, OPERATIONAL CHECK NORMAL.Feb 26, 1997 · N8950E · Doug DC931 · Emergency LightingSDR 9703259990Controller · malfunctionedCABIN PRESSURE WARNING LIGHT ILLUMINATED EN ROUTE. CREW EXECUTED EMERGENCY DESCENT TO 23,000 FEET AND CABIN PRESSURE WAS REGAINED. FLIGHT CONTINUED TO DESTINATION AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CABIN PRESSURE CONTROLLER, AMPLIFIEFeb 14, 1997 · N8950E · Doug DC931 · Cabin Pressure ControllerSDR 9700279990Power Supply · malfunctionedDURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL.Jan 7, 1997 · N8950E · Doug DC931 · Emergency LightingSDR 9626799990Epr Lines · frozenAS THROTTLES WERE ADVANCED FOR TAKEOFF, THE RIGHT ENGINE EPR INDICATION WAS INOPERATIVE. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE APPLIED HEAT TO ASSOCIATED EPR LINES AND RAN ENGINE. INDICATIONS WERE OK, SUSPECT ICING OF EPR RELATED LINES.Dec 22, 1996 · N8950E · Doug DC931 · Engine Pressure Ratio (EPR)SDR 9626189990Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES.Dec 8, 1996 · N8950E · Doug DC931 · Emergency LightingSDR 9621459990Terminal Block · shortedDURING LANDING, FLIGHT ATTENDANT OBSERVED SPARKS COMING FROM OVEN TIMER AREA. COCKPIT CREW SMELLED AN ELECTRICAL BURNING SMELL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND TERMINAL STUD SHORTED AT S3-25 TERMINAL BLOCK IN OVERHEAD COMPANIONWAY. REPLOct 6, 1996 · N8950E · Doug DC931 · DC Power Distribution SystemSDR 9611869990Unsafe Light · illuminatedNOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED SEVERAL GEAR SWINGS. DISCREPANCY COULD NOT BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE.May 28, 1996 · N8950E · Doug DC931 · Landing Gear Position and WarningSDR 9611429990Shutoff Valve · leakingLOSS OF NOSE WHEEL STEERING ACCOMPANIED BY SMOKE IN CABIN OCCURRED DURING TAXI OUT. RIGHT HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE FOUND RUDDER POWER SHUTOFF VALVE LEAKING. REPLACED VALVE, OPERATIONAL CHECK NORMAL.May 23, 1996 · N8950E · Doug DC931 · Hydraulic System, MainSDR 9606229990Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN BATTERY PACK, OPERATIONAL CHECK NORMAL.Mar 15, 1996 · N8950E · Doug DC931 · Emergency LightingSDR 9602669990Epr Indicator · failedTHE NR 2 ENGINE EPR INDICATION UNRELIABLE ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR INDICATOR WITH A SERVICEABLE UNIT.Jan 28, 1996 · N8950E · Doug DC931 · Engine Pressure Ratio (EPR)SDR 9519469990Battery Pack · dischargedDURING LINE CHECK, FOUND FORWARD EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY. OPERATIONAL CHECK GOOD.Nov 30, 1995 · N8950E · Doug DC931 · Emergency LightingSDR 9514829990Angle · crackedDURING LINE CHECK, FOUND A CRACK IN THE LEFT PYLON UPPER SKATE ANGLE FS 1104. REPAIRED ANGLE PER EA 99-99246.Sep 5, 1995 · N8950E · Doug DC931 · Nacelle/Pylon StructureSDR 9508969990Gear Light · malfunctionedNOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE ON APPROACH INTO MSP. RECYCLED GEAR AND NORMAL INDICATION WAS ACHIEVED. FLIGHT LANDED WITHOUT INCIDENT. LUBED NOSE LANDING GEAR. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE.Jun 4, 1995 · N8950E · Doug DC931 · Landing Gear Position and WarningSDR 9507549990Angle · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND 3 CRACKS IN THE RIGHT SIDE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT THE AFT END. REPAIRED PER XEA X9-53-83.May 5, 1995 · N8950E · Doug DC931 · Fuselage, Stabilizer Attach FittingsSDR 9507539990Frame · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A 2 INCH CRACK IN THE FS 1143 CANTED FRAME FORWARD OF THE INTERIOR TAILCONE RELEASE HANDLE. REPAIRED PER XEA X9-53-88.May 4, 1995 · N8950E · Doug DC931 · Fuselage Main, FrameSDR 9507289990Hinge · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LEFT WING FLAP, FORWARD HINGE NR 3 FASTENER BORES. REPAIRED PER OHM 27-50-5 AND EA X9-27-16.May 1, 1995 · N8950E · Doug DC931 · Trailing Edge FlapsSDR 9506869990Hinge · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN RIGHT WING FLAP NR 2 FORWARD HINGE FASTENER BORES. REPLACED HINGE PER X9-27-15 AND OHM 27-50-5.Apr 19, 1995 · N8950E · Doug DC931 · Trailing Edge FlapsSDR 9506069990Hinge · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN FLAP HINGE FITTING BORES, RIGHT WING FORWARD HINGE NR 3 AND LEFT WING FORWARD HINGE NR 2. REPLACED RIGHT WING FITTING AND REPAIRED LEFT WING FITTING PER OHM 27-50-5.Apr 11, 1995 · N8950E · Doug DC931 · Wing, Control Surface Attach FittingsSDR 9505289990Bracket · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND TWO INCH CRACK IN A PANEL ATTACH ANGLE RIGHT WING LEADING EDGE LOWER SURFACE WS 118. REPAIRED PER XEA X9-57-18.Mar 30, 1995 · N8950E · Doug DC931 · Wing Miscellaneous StructureSDR 9503569990Splice Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 22L SPLICE FITTING AT FS 851 - 870. REPLACED FITTING PER SRM 51-30-5.Mar 4, 1995 · N8950E · Doug DC931 · Fuselage Miscellaneous StructureSDR 9503259990Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN THE FORWARD CARGO DOOR HORIZONTAL ANGLE BRACE FITTING. REPLACED FITTING PER SRM 51-10-2 AND 51-30-3.Feb 28, 1995 · N8950E · Doug DC931 · Cargo/Baggage DoorsSDR 9501469990Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN SEAT TRACK SUPPORT FITTING FS 680, LBL 44. REPLACED FITTING PER SRM 51-30-5.Jan 21, 1995 · N8950E · Doug DC931 · Fuselage Miscellaneous Structure
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