N810ME, cancelled Mar 31, 2010

Service difficulty reports · 170

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 = 'N810ME' AND deregistration_id = 'N810ME-2010-03-31'
  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 MWEA080071Control Valve · faultyLEFT AIRCRAFT SYSTEM UNABLE TO HOLD CABIN PRESSURE AT 24,000 FEET, FLOW LIGHT WAS ON WITH OUTFLOW VALVE CLOSED. REMOVED AND REPLACED LEFT PACK FLOW CONTROL VALVE.May 17, 2008 · N810ME · Doug DC982 · Cabin Pressure Control SystemSDR MWEA080016Support · corrodedCORROSION AROUND BOLT HOLE ALONG ENTIRE LENGTH OF AFT CARGO DOOR THRESHOLD PLATE SUPPORT STRUCTURE. FABRICATED AND INSTALLED SPACERS.Jan 28, 2008 · N810ME · Doug DC982 · Fuselage Miscellaneous StructureSDR MWEA080014Skin · corrodedAFT LAVATORY SERVICE PANEL, BOX AND FUSELAGE SKIN SEPARATED AND CORROSION LEVEL 1 FOUND IN BETWEEN AT FORWARD LOWER CORNER. CUT OUT DAMAGE AND FABRICATED AND INSTALLED DOUBLER.Jan 23, 2008 · N810ME · Doug DC982 · Fuselage Main, Plate/SkinSDR MWEA080011Cusp Web · corrodedAFT CARGO COMPARTMENT HAS CORROSION ON BOTTOM OF CUSP MEMBRANE AT DOME NUT JUST AFT OF FRAME STATION 1174L. FABRICATED AND INSTALLED DOUBLER.Jan 18, 2008 · N810ME · Doug DC982 · Fuselage Miscellaneous StructureSDR MWEA070310Smoke Detector · false indicationWHILE EN ROUTE, LEFT AFT LAVATORY SMOKE ALARM ACTIVATED. FLIGHT ATTENDANT REPORTED, NO SIGN OF SMOKE, NO SMELL OF SMOKE AND NO SIGNS OF TAMPERING. REMOVED AND REPLACED SMOKE DETECTOR.Dec 26, 2007 · N810ME · Doug DC982 · Smoke DetectionSDR MWEA070263Wire · brokenFLOOR TRACK EMERGENCY LIGHT INOPERATIVE FROM ROW 27 AFT. FOUND SPLICE BROKEN REPLACED SPLICE.Oct 28, 2007 · N810ME · Doug DC982 · Light System WiringSDR MWEA070259Smoke Detector · faultyLEFT REAR LAV SMOKE ALARM SOUNDED. REMOVED AND REPLACED AFT LEFT LAVATORY SMOKE DETECTOR.Oct 17, 2007 · N810ME · Doug DC982 · Smoke DetectionSDR MWEA070095Lanyard · brokenAFT GALLEY GIRT BAR CABLE BROKEN. REMOVED AND REPLACED AFT GALLEY GIRT LANYARD.Apr 13, 2007 · N810ME · Doug DC982 · Emergency EquipmentSDR MWEA070094Girt Bar · stuckFLIGHT ATTENDANT UNABLE TO DISARM GIRT BAR AT AFT GALLEY DOOR. DISARMED AFT GALLEY SLIDE.Apr 13, 2007 · N810ME · Doug DC982 · Emergency EquipmentSDR MWEA070078Shear Tie · damagedSHEAR CLIP DAMAGE FROM DRILL MARK. FABRICATED AND INSTALLED SHEAR TIE.Apr 5, 2007 · N810ME · Doug DC982 · Fuselage Internal Mounting StructureSDR MWEA070077Skin · dentedEVIDENCE OF SKIN DENTED AT STATION 541 BETWEEN LONGERERON 26 AND LONGERON 27. FABRICATED AND INSTALLED FILLER.Apr 4, 2007 · N810ME · Doug DC982 · Fuselage Main, Plate/SkinSDR MWEA070076Skin · dentedLONGERON 27 AT STATION 636 EVIDENCE OF SKIN DENTED. FABRICATED AND INSTALLED DOUBLER.Apr 4, 2007 · N810ME · Doug DC982 · Fuselage Main, Plate/SkinSDR MWEA070041Latch · brokenAFT TAIL CONE DOOR ARMING, DISARMING GUARD WILL NOT REMAIN DOWN AND LOCKED ON PLACE. REMOVED AND REPLACED LATCH.Mar 5, 2007 · N810ME · Doug DC982 · Aerodynamic FairingsSDR MWEA070026Slide · low pressureAFT EVACUATION SLIDE PRESSURE IS LOW AT 1500 PSI. REMOVED AND REPLACED AFT SLIDE.Feb 2, 2007 · N810ME · Doug DC982 · Escape SlideSDR MWEA060295Skin · damagedLIGHTNING STRIKE ON 2 EACH RIVET HEADS, STATION 484, 3 INCH OB OF LONGERON 3 LT. FABRICATED AND INSTALLED DOUBLER.Nov 12, 2006 · N810ME · Doug DC982 · Fuselage Main, Plate/SkinSDR MWEA060286Flashlight · inoperativeEMERGENCY LIGHT BESIDE ENTRANCE DOOR INOPERATIVE. REMOVED AND REPLACED FLASH LIGHT.Sep 2, 2006 · N810ME · Doug DC982 · Emergency EquipmentSDR MWEA060141Seal · crackedCARGO DOOR SEAL DRESSER HAS APPROXIMATELY .250 INCH CRACK, LOCATED AT BOTTOM EDGE OF DOOR CUTOUT AT STATION 674. FABRICATED AND INSTALLED SEAL DEPRESSOR.Jul 5, 2006 · N810ME · Doug DC982 · Cargo/Baggage DoorsSDR MWEA060140Support · corrodedCORROSION ON MID CARGO DOOR THRESHOLD PLATE SUPPORT STRUCTURE, LOCATED AT FORWARD, LOWER CORNER OF DOOR CUTOUT. FABRICATED AND INSTALLED STRAP.Jul 5, 2006 · N810ME · Doug DC982 · Fuselage Miscellaneous StructureSDR MWEA060139Threshold · corrodedCORROSION ALONG ENTIRE LENGTH OF AFT CARGO DOOR THRESHOLD, PLATE SUPPORT STRUCTURE. FABRICATED AND INSTALLED SHEAR FASTENER.Jul 5, 2006 · N810ME · Doug DC982 · Fuselage Miscellaneous StructureSDR MWEA060138Doubler · delaminatedSIX RUDDER TRIM TAB TRAILING EDGE IS DELAMINATED, NEAR THE CENTER OF THE TAB. FABRICATED AND INSTALLED DOUBLER.Jul 5, 2006 · N810ME · Doug DC982 · Rudder, Spar/RibSDR MWEA060052Crank Assy · defectiveTAIL CONE FAILED THE PULL TEST AND THE TAIL CONE DID NOT DEPLOY WHEN USING THE VENTRAL STAIR DOOR. REMOVED AND REPLACED CRANK ASSEMBLY.May 27, 2006 · N810ME · Doug DC982 · Aerodynamic FairingsSDR MWEA060041Skin · damagedFOUND FORWARD PASSENGER DOOR DAMAGED. FABRICATED AND INSTALLED DOUBLER.Apr 11, 2006 · N810ME · Doug DC982 · Passenger/Crew DoorsSDR MWEA060018Engine · frozenRIGHT ENGINE PRESSURE RATIO DID NOT ADVANCE PAST 1.02, ALL OTHER INDICATIONS NORMAL. DISCONNECTED PT7 LINES AT CROSSBRIDAL AND DETERMINTED THAT THE LINES WERE OBSTRUCTED WITH ICE BETWEEN BRIDAL AND PT7 TRAP, RAN ENGINES, OPERATIONS CHECKED GOOD.Feb 18, 2006 · N810ME · Doug DC982 · Engine (Turbine/Turboprop)SDR MWEA070015Splice · faultyFORWARD SECTION CABIN FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. FOUND BAD SPLICE, REPLACED SPLICE.Feb 14, 2006 · N810ME · Doug DC982 · Light System WiringSDR MWEA060007Seat Track · out of alignmentFIRST OFFICERS INBOARD AFT SEAT TRACK NOT IN ALIGNMENT WITH THE OTHER SEAT TRACK. FABRICATED AND INSTALLED TEE FITTING.Jan 19, 2006 · N810ME · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA060001O-Ring · leakingRT HYDRAULIC QUANTITY LOW ONE QUART ON FINAL APPROACH. REMOVED AND REPLACED RT PRESSURE REDUCER O-RING.Jan 4, 2006 · N810ME · Doug DC982 · Hydraulic System, MainSDR MWEA050115Engine · malfunctionedNUMBER TWO ENGINE PRESSURE RATIO DECREASED AT 0.2 AND ENGINE PRESSURE RATIO AND 10 PERCENT N1 BOTH PACKS ALSO SHUTDOWN. SERVICED FUEL CONTROL BELLOWS. INSPECTED PT2 MOISTURE TRAP AND PT7 MOISTURE TRAP, PS4 STRAINER, CHECKED PT2 AND PT7 LINE AND FITTING AND BOct 12, 2005 · N810ME · Doug DC982 · Engine (Turbine/Turboprop)SDR MWEA050107Pump · inoperativeRT ENGINE HYDRAULIC PUMP INOPERATIVE. REMOVED AND REPLACED RT ENGINE HYDRAULIC PUMP.Sep 28, 2005 · N810ME · Doug DC982 · Hydraulic Pump (Electric/Engine), MainSDR MWEA050106Overheat Sensor · inoperativeTAIL COMPARTMENT HIGH TEMPERATURE LIGHT CAME ON. REMOVED AND REPLACED OVERHEAT SENSOR AND TIGHTENED RIGHT CLAMP.Sep 16, 2005 · N810ME · Doug DC982 · Overheat DetectionSDR MWEA050100Apu · overtempTAIL COMPARTMENT HIGH LIGHT CAME ON. FOUND AUXILIARY POWER UNIT CONTROL VALVE LEAKING AND HOIST ACCESS PANEL OFF AND HOT AIR BLOWING OUT. REINSTALLED HOIST PANEL, VERIFIED LEAK AT V BAND CLAMP ON LOAD CONTROL OUTLET DUCT. REMOVED AND INSPECTED CLAMP, NO DEFSep 2, 2005 · N810ME · Doug DC982 · Airborne Auxiliary Power Unit (APU) SystemSDR MWEA050074Odor · detectedPILOT SMELLED AN ODOR LIKE ELECTRICAL WIRING COMING FROM COCKPIT (NO SMOKE OR FUMES). INSPECTED THE ELETRICAL ELETRONICS COMPARTMENT AND FORWARD ACCESSORY COMPARTMENT, LOWERED CENTER OVERHEAD COCKPIT COMPARMENT PANELS AND INSPECTED WIRING, NO FAULTS NOTED. VJul 30, 2005 · N810ME · Doug DC982 · Air Distribution SystemSDR MWEA050067Seat Track · wornFIRST OFFICERS UPPER AND LOWER SEAT TRACK IS WORN AND ADJUSTMENT HOLES ELONGATED. REMOVED AND REPLACED SEAT TRACK.Jul 5, 2005 · N810ME · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA050066Seat Track · wornCAPTAIN'S UPPER AND LOWER SEAT TRACK IS WORN AND ADJUSTMENT HOLES ELONGATED. FABRICATED AND INSTALLED UPPER AND LOWER SEAT TRACK.Jul 5, 2005 · N810ME · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA050065Door · inoperativeDURING INVESTIGATION OF LOOSE EXIT SIGN, COULD NOT REMOVE LEFT AFT OVERWING EXIT DOOR. REMOVED LEFT AFT DOOR BY DISPLACING FORWARD AND AFT ADJACENT SIDE WALL TRIM STRIPES, ADJUSTED SAME SIDE WALL PANELS AND REINSTALLED DOOR, OPERATIONAL CHECKED NORMAL.Jul 3, 2005 · N810ME · Doug DC982 · Emergency ExitsSDR MWEA050064Wire · misroutedFLOOR TRACK LIGHTING IN FORWARD CABIN G2 AISLE AREA, WIRES ARE MISROUTED AND IS MISSING PROTECTIVE TRACK PIECE FROM CENTER TO RIGHT WALL. SECURED EMERGENCY FLOOR TRACK LIGHTING WIRES AT FORWARD CABIN INTO THE NEW WIRE PROTECTION TRACKS, OPERATIONS CHECKED GOOJun 30, 2005 · N810ME · Doug DC982 · Light System WiringSDR MWEA050046Drain · obstructedLOUD SQUEAL WAS AUDIBLE THROUGHOUT CABIN AND COCKPIT SEEMED TO BE IN FORWARD GALLEY. FOUND GALLEY DRAIN PLUGGED POSSIBLE CAUSE OF SQUEAL. CLEANED DRAIN, CLEANED GALLEY PASSENGER DOOR SEALS, PRESSURIZED CABIN TO 7.5 PSI, LEAK DOORS AND SEALS NO AUDIBLE SQEALSJun 5, 2005 · N810ME · Doug DC982 · Buffet/GalleysSDR MWEA050028Wire · exposedEMERGENCY TRACK LIGHTING WIRES EXPOSED. REPAIRED WIRES AND SECURED END CAP IAW 20-50-00 AND 33-50-00. OPERATION CHECK GOOD.Feb 25, 2005 · N810ME · Doug DC982 · Light System WiringSDR MWEA040209Strap · damagedAFT PRESSURE BULKHEAD TEE HAS FOUR HOLES WITH TOO SHORT OF EDGE DISTANCE IN FORWARD UPPER FLANGE OF TEE BETWEEN LONGERON 18 RIGHT AND 17 RIGHT. SUBMITTED TO BOEING FOR DISPOSITION. FABRICATED AND INSTALLED NEW STRAPS AND FASTENERS.Nov 17, 2004 · N810ME · Doug DC982 · Fuselage Main, BulkheadSDR MWEA040207Longeron · damagedFORWARD CARGO BAY FRAME STATION 309 LONGERON 28 RIGHT NEEDS TO BE CUT AND SPLICED. FABRICATED AND INSTALLED NEW SPLICE.Nov 16, 2004 · N810ME · Doug DC981 · Fuselage Main, Longeron/StringerSDR MWEA040203Bulkhead · damagedAFT PRESSURE BULKHEAD REQUIRES REPLACEMENT DUE TO BLENDING BETWEEN LONGERONS 19 AND 20 RIGHT. FABRICATED AND INSTALLED NEW SECTION.Nov 12, 2004 · N810ME · Doug DC982 · Fuselage Main, BulkheadSDR MWEA040206Skin · dentedSKIN DENT AT STATION 294 LONGERON 24 RIGHT. FOUND TO BE OUT OF LIMITS. REMOVED DOUBLER, COLD WORK SKIN AND INSTALLED DOUBLER.Nov 1, 2004 · N810ME · Doug DC982 · Fuselage Main, Plate/SkinSDR MWEA040166Warning Light · false indicationTAIL CONE ANNUCIATOR ILLUMINATED. INSPECTED TAIL CONE LOCK/LATCH INSTALLATION, RESET CABLE LOCKBALL. OK FOR CONTINUED SERVICE.Sep 15, 2004 · N810ME · Doug DC982 · Central WarningSDR MWEA040115Structure · oversizedDURING TAILCONE DROP TEST, AFT CABIN DOOR ARMING PIN WOULD NOT ENGAGE DUE TO PIN HITTING COVER ABOVE DOOR. TRIMMED SLOT LONGER.Jul 6, 2004 · N810ME · Doug DC982 · Aerodynamic FairingsSDR MWEA040119Doubler · crackedAT STATION 370 ON THE FORWARD CARGO DOOR WEB THERE IS A CRACK ON THE WEB UNDER THE FLOOR RAIL. FABRICATED AND INSTALLED DOUBLER.Jul 6, 2004 · N810ME · Doug DC982 · Fuselage Main, StructureSDR MWEA040118Frame · wornFRAME STATION 579 FRAME FORMER FROM LONGERON 22 LEFT THROUGH 23 LEFT REQUIRES FLANGE REPAIR. FABRICATED AND INSTALLED REPAIR FORMER.Jul 6, 2004 · N810ME · Doug DC982 · Fuselage Main, FrameSDR MWEA040117Angle · out of toleranceFORWARD CARGO DOOR JAMB PAN REPAIR AFT END HAS TWO FASTENERS WITH EDGE DISTANCE BELOW TOLERANCE AND GAP IS EXCESSIVE BETWEEN REPAIR PAN AND WHERE ORIGINAL PAN WAS CUT. FABRICATED AND INSTALLED 2 EACH REPAIR ANGLES.Jul 6, 2004 · N810ME · Doug DC982 · Fuselage Main, FrameSDR MWEA040113Finger Doubler · out of toleranceRIGHT PRIMARY STATIC PORT AREA FUSELAGE SKIN HAS A CONTOUR CHANGE OUT OF TOLERANCE WHERE REPAIR IS INSTALLED, STATION 607 IN BETWEEN LONGERON 22 RIGHT AND 23 RIGHT. FABRICATED AND INSTALLED FINGER DOUBLER AND FILLER.Jul 6, 2004 · N810ME · Doug DC982 · Fuselage Main, Plate/SkinSDR MWEA040114Torque Tube · corrodedCENTER CARGO DOOR AFT TORQUE TUBE IS CORRODED. REMOVED AND REPLACED AFT TORQUE TUBE.Jul 6, 2004 · N810ME · Doug DC982 · Cargo/Baggage DoorsSDR MWEA040116Longeron · out of toleranceRIGHT PRIMARY STATIC PORT AREA FUSELAGE SKIN BUTT JOINT SKIN TO SKIN FLUSHNESS IS OUT OF TOLERANCE LOCATED AT STATION 589 LONGERON 26 RIGHT, UPPER SKINS ARE OUT AT .022, LOWER SKINS ARE OUT AT .015. FABRICATED AND INSTALLED LONGERON.Jul 6, 2004 · N810ME · Doug DC982 · Fuselage Main, Plate/SkinSDR MWEA040112Door Frame · corrodedFORWARD CARGO DOOR JAMB PAN, LOWER EDGE HAS AREAS OF SEVERE CORROSION. FABRICATED AND INSTALLED REPAIR PARTS.Jul 2, 2004 · N810ME · Doug DC982 · Fuselage Main, Structure
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