N804ME, cancelled May 7, 2013

Service difficulty reports · 119

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 = 'N804ME' AND deregistration_id = 'N804ME-2013-05-07'
  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 MWEA080132Inverter · faultyBAS A/C EMERGENCY BUS COMES ON WHEN EMERGENCY POWER IS SELECTED ON. REPLACED EMERGENCY INVERTER. (K)Nov 16, 2008 · N804ME · Doug DC981 · AC InverterSDR MEW2008F00000Battery Pack · inoperativeEMERGENCY LIGHTS ABOVE, ON COCKPIT CEILING ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. (K)Aug 6, 2008 · N804ME · Doug DC981 · Emergency LightingSDR MWE2008F00007Slide · unwanted deployDURING CLIMB, THE PITCH AUTHORITY (ELEVATOR) FELT STIFF ALTHOUGH CONTROLLABLE, PRIMARY PITCH TRIM WORK OK, ALT LONG TRIM AND AUTO PILOT WORKED NORMAL INSP OF AFT ACCESSORY COMPARTMENT FOR ELEVATOR AUTHORITY ISSUE FOUND THE TAIL CONE SLIDE HAD DEPLOYED IN THE Jul 7, 2008 · N804ME · Doug DC981 · Escape SlideSDR MWEA080044Pan · crackedCENTER CARGO DOOR OUTER PAN HAS A .75 INCH CRACK IN PAN RADIUS AT THE FORWARD END OF DOOR, INLINE WITH BEAM NR 1. FABRICATED AND INSTALLED DOUBLER.Mar 22, 2008 · N804ME · Doug DC981 · Cargo/Baggage DoorsSDR MWE2008F00008Slide · inoperativeTAILCONE SLIDE PRESSURE AT (0). REMOVED AND REPLACED TAILCONE SLIDE. (K) Dec 10, 2007 · N804ME · Doug DC981 · Escape SlideSDR MWEA070116Bottle · low pressureTAIL CONE EVACUATION SLIDE BOTTLE PRESSURE GAUGE NOT IN THE GREEN BAND. REMOVED AND REPLACED TAIL CONE SLIDE ASSEMBLY.May 11, 2007 · N804ME · Doug DC981 · Escape SlideSDR MWEA060285Battery · inoperativeCEILING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERYSep 15, 2006 · N804ME · Doug DC981 · Emergency LightingSDR MWEA060217Wire · brokenEXIT ROW WON'T EXTINGUISH WHEN POWER IS REMOVED FROM AIRCRAFT. REPLACED BROKEN WIRE.Aug 22, 2006 · N804ME · Doug DC981 · Light System WiringSDR MWEA060178Seat Track · corrodedFOUND CORROSION ON INBOARD FLANGE OF SEAT TRACK AT FRAME STATION 1136 TO 1146, X +44. Z 0, AROUND BOARD FASTENER HOLES. FABRICATED AND INSTALLED SEAT TRACK.Aug 22, 2006 · N804ME · Doug DC981 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA060177Floorbeam · corrodedSUPPORT ON FLOORBEAM UPPER FLANGE AT FRAME STATION 1169, X-29, Z 0. FABRICATED AND INSTALLED FLOORBEAM.Aug 22, 2006 · N804ME · Doug DC981 · Fuselage Main, Floor BeamSDR MWEA060176Web · crackedFOUND WEB CRACKED AT FRAME STATION Y 1300 X+48. FABRICATED AND INSTALLED WEB.Aug 22, 2006 · N804ME · Doug DC981 · Fuselage Miscellaneous StructureSDR MWEA060174Fitting · corrodedGALLEY 1 INBOARD FUSE MOUNTED FOOT, FRAME STATION 152 X-45 Z 0. FABRICATED AND INSTALLED FITTINGS.Aug 22, 2006 · N804ME · Doug DC981 · Fuselage Main, Attach FittingsSDR MWEA060173Fitting · corrodedGALLEY 1 OUTBOARD FUSE MOUNTED FOOT FRAME STATION 152 X-51 Z0 IS CORRODED. FABRICATED AND INSTALLED FITTINGS.Aug 22, 2006 · N804ME · Doug DC981 · Fuselage Miscellaneous StructureSDR MWEA060172Strap · corrodedFOUND SURFACE CORROSION ON THRESHOLD STRAP Z-46, X-18 AND FRAME STATION Y 636-693. FABRICATED AND INSTALLED STRAP.Aug 22, 2006 · N804ME · Doug DC981 · Fuselage Miscellaneous StructureSDR MWEA060171Strap · corrodedFOUND SURFACE CORROSION ON THRESHOLD STRAP Z-46, X-18 AND FRAME STATION Y 1155 TO 1219. FABRICATED AND INSTALLED NEW STRAP.Aug 22, 2006 · N804ME · Doug DC981 · Fuselage Miscellaneous StructureSDR MWEA060170Seat Track · corrodedFOUND SEAT TRACK IS CORRODED AT NUTPLATE AS VIEWED FROM AFT CARGO BAY Y 1267 AND X +24, Z 0. FABRICATED AND INSTALLED SEAT TRACK.Aug 22, 2006 · N804ME · Doug DC981 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA060175Panel · corrodedFOUND FORWARD GALLEY SERVICE DOOR THRESHOLD FLOOR PANEL CORRODED. FABRICATED AND INSTALLED PANEL.Aug 22, 2006 · N804ME · Doug DC981 · Fuselage Miscellaneous StructureSDR MWEA060145Controller · inoperativeMASTER WARNING (CABIN ALERT) ILLUMINATED. REMOVED AND REPLACED CABIN PRESSURE CONTROL.Jul 13, 2006 · N804ME · Doug DC981 · Cabin Pressure ControllerSDR MWEA060012Blades · bentLEFT ENGINE COMPRESSOR STALL/SURGE. REMOVED BENT TIPS AS NECESSARY ON VARIOUS ENGINE BLADES AND BLENDED AS REQUIRED PER IAW BOEING MM 72-33-22.Feb 7, 2006 · N804ME · Doug DC981 · Turbine Engine Compressor SectionSDR MWEA060011Tab · obstructedNO CONTROL INPUT EVEN WHEN CONTROL COLUMN WAS MOVED AFT. REMOVED SCREW THAT WAS WEDGED BETWEEN ELEVATOR CONTROL TAB STOP AND INBOARD ATTACHED FITTING.Feb 3, 2006 · N804ME · Doug DC981 · Elevator Control SystemSDR MWEA060009Indicator · inoperativeRIGHT ENGINE OIL TEMERATURE PEGGED OVER 165, ALL OTHER INDICATIONS NORMAL. REMOVED AND REPLACED RIGHT ENGINE OIL TEMERATURE INDICATOR.Feb 1, 2006 · N804ME · Doug DC981 · Engine Oil TemperatureSDR MWEA050104Skin · corrodedLEADING EDGE AT STATION 375 HAS CORROSION. FABRICATED AND INSTALLED DOUBLER AND FILLER.Sep 7, 2005 · N804ME · Doug DC981 · Leading Edge DevicesSDR MWEA050060Structure · vibrationDURING CRUISE PILOT REPORTED A LOUD HUMMING SOUND AND VIBRATION. VISUALLY INSPECTED ALL LANDING GEARS AND WHEEL WELLS, INSPECTED AIRCRAFT FUSELAGE, DOORS,WINGS AND PANELS. PERFORMED ENGINE VIBRATION TEST. NO DEFECTS FOUND.Jun 27, 2005 · N804ME · Doug DC981 · Fuselage Main, StructureSDR MWEA040194Slide · dischargedAFT GALLEY SLIDE PRESSURE INDICATOR IS INDICATING IN THE RED (READS 2000 PSI). REMOVED AND REPLACED AFT GALLEY DOOR SLIDE.Oct 22, 2004 · N804ME · Doug DC981 · Escape SlideSDR MWEA040154Seat Track · wornCAPTAIN'S AFT INBOARD SEAT TRACK IS WORN. FABRICATED AND INSTALLED CHANNEL.Aug 25, 2004 · N804ME · Doug DC981 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA040151Seat Track · wornFIRST OFFICER'S AFT INBOARD SEAT TRACK IS WORN. FABRICATED AND INSTALLED SEAT TRACK TEE.Aug 24, 2004 · N804ME · Doug DC981 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA040150Intercostal · corrodedCORROSION ON INTERCOSTAL AT FRAME STATION 775 BETWEEN LONGERON 27 AND 28 LEFT. FABRICATED AND INSTALLED INTERCOSTAL.Aug 24, 2004 · N804ME · Doug DC981 · Fuselage Miscellaneous StructureSDR MWEA040149Seat Track · corrodedAFT BAGGAGE PIT, RIGHT SEAT TRACK BETWEEN STATION 1212 AND 1325 HAS SEVERAL AREAS OF CORROSION. FABRICATED AND INSTALLED TRACK.Aug 23, 2004 · N804ME · Doug DC981 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA040148Fitting · corrodedFLOOR SUPPORT FITTINGS AT FRAME STATION 430 BETWEEN NUMBER 30 AND 29 RIGHT LONGERON HAS MODERATE CORROSION ON THE UPPER SURFACE, ALSO NUT PLATES ARE CORRODED. FABRICATED AND INSTALLED FITTING AND INSTALLED TWO EACH NUT PLATES.Aug 23, 2004 · N804ME · Doug DC981 · Fuselage Main, Attach FittingsSDR MWEA040110Generator · inoperativeLEFT GENERATOR FAILED. REMOVED AND REPLACED LEFT GENERATOR.Jun 24, 2004 · N804ME · Doug DC981 · AC Generation SystemSDR MWEA040097Generator · inoperativeAIRCRAFT CROSSTIE LOCKOUT ILLUMINATED WITH LEFT GENERATOR OFF LIGHT. REMOVED AND REPLACED LEFT ENGINE GENERATOR.Jun 13, 2004 · N804ME · Doug DC981 · AC Generation SystemSDR MWEA040086Window Frame · lightning strikeLIGHTNING STRIKE ON LEFT SIDE CABIN WINDOW FRAME NR 34 ON AFT UPPER SIDE. BLENDED OUT DAMAGE, ACCEPTABLE FOR STRENGTH AS IS.Jun 7, 2004 · N804ME · Doug DC981 · Fuselage Main, StructureSDR MWEA040085Window Frame · lightning strikeLIGHTNING STRIKE ON CABIN WINDOW FRAME 29 AFT LOWER SIDE. BLENDED OUT DAMAGE, ACCEPTABLE AS TEMPORARY REPAIR TO BE PERMANENTLY REPAIRED ON OR BEFORE 7,000 CYCLES.Jun 7, 2004 · N804ME · Doug DC981 · Fuselage Main, StructureSDR MWEA040084Window Frame · lightning strikeLIGHTNING STRIKE ON LEFT SIDE CABIN WINDOW NR 29 FRAME ON LOWER FORWARD CORNER. BLENDED OUT DAMAGE, ACCEPTABLE AS TEMPORARY REPAIR TO BE PERMANENTLY REPAIRED ON OR BEFORE 7,000 CYCLES.Jun 7, 2004 · N804ME · Doug DC981 · Fuselage Main, StructureSDR MWEA040075Separator · inoperativeSTRONG FUMES IN CABIN. REMOVED AND REPLACED WATER SEPARATOR.May 12, 2004 · N804ME · Doug DC981 · Humidity Control SystemSDR MWEA040069Generator · inoperativeLEFT GENERATOR LIGHT CAME ON, WAS ABLE TO RESET LEFT GENERATOR, THEN FOURTY-FIVE MINUTES LATER LEFT GENERATOR LIGHT CAME ON AGAIN, STARTED AUXILIARY POWER UNIT, BUT UNABLE TO POWER LEFT SIDE OF ELECTRICAL POWER SYSTEM. REMOVED AND REPLACED GENERATOR CONTROL May 9, 2004 · N804ME · Doug DC981 · AC Generation SystemSDR MWEA040013Bolt · misinstalledDURING GEAR RETRACTION A LOUD NOISE COMING FROM THE NOSE GEAR AREA. LT FORWARD NOSE GEAR DOOR RETRACT LINK NOT LATCHED COMPLETELY, FOUND RELEASE HANDLE BOLT INSTALLED IMPROPERLY. REPOSITIONED BOLT CLOSED AND LOCKED FORWARD NOSE GEAR DOOR.Jan 28, 2004 · N804ME · Doug DC981 · FastenersSDR MWEA030475Pitot Line · leakingCAPTAIN'S MACH INDICATOR HAS .14 MACH SPLIT AND EIGHT KNOTS SPLIT BETWEEN FIRST OFFICER'S AIRSPEED. SELECTING CENTRAL AIR DATA COMPUTER TO BOTH ON ONE AND TWO CORRECTED THE SPLIT. FOUND MASSIVE LEAK IN PITOT ON NUMBER ONE PITOT SYSTEM, TIGHTENED FITTINGS, LEDec 6, 2003 · N804ME · Doug DC981 · Pitot/Static SystemSDR MWEA030394Skin · crackedFUSELAGE EXTERNAL SKIN IS CRACKED APPROXIMATELY 1.25 INCH AT STATION 1437 BETWEEN LONGERON 3 AND 4 RT. FABRICATED AND INSTALLED DOUBLER.Sep 25, 2003 · N804ME · Doug DC981 · Fuselage Main, Plate/SkinSDR MWEA030389Seat Track · wornFIRST OFFICERS SEAT TRACK (FORWARD INBOARD) HAS WORN AREAS. FABRICATED AND INSTALLED NEW SEAT TRACK.Sep 22, 2003 · N804ME · Doug DC981 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA030376Spacer · corrodedAFT CARGO DOOR LOWER JAMB HAS LIGHT CORROSION ALONG THE ENTIRE LENGTH AROUND AND INSIDE SCREW HOLES. FABRICATED AND INSTALLED JAMB SPACER.Sep 16, 2003 · N804ME · Doug DC981 · Fuselage Main, StructureSDR MWEA030375Skin · crackedFUSELAGE EXTERNAL SKIN IS CRACKED APPROXIMATELY .25 INCH OUT OF RIVER HOLE AT STATION 1437 BETWEEN LONGERON 2 AND 3 LEFT. REMOVED CRACK IN SKIN, FABRICATED AND INSTALLED DOUBLER AND FILLER.Sep 16, 2003 · N804ME · Doug DC981 · Fuselage Main, Plate/SkinSDR MWEA030374Doubler · crackedFUSELAGE EXTERNAL SKIN IS CRACKED APPROXIMATELY 1 INCH AT STATION 1437 BETWEEN LONGERON 3 AND 4 LEFT. FABRICATED AND INSTALLED EXTERNAL DOUBLER AND FILLER.Sep 16, 2003 · N804ME · Doug DC981 · Fuselage Main, Plate/SkinSDR MWEA030373Doubler · dentedDENT LOCATED BETWEEN LONGERON 26 LEFT AND 25 LEFT AT STATION 694. FABRICATED AND INSTALLED REPAIR DOUBLER.Sep 16, 2003 · N804ME · Doug DC981 · Fuselage Main, Plate/SkinSDR MWEA030372Doubler · dentedDENT LOCATED AT 1 INCH BELOW LONGERON 4 LEFT AND SEVERAL VERY SMALL DENTS LOCATED AROUND THIS DENT AT STATION 219. FABRICATED AND INSTALLED REPAIR DOUBLER.Sep 16, 2003 · N804ME · Doug DC981 · Fuselage Main, Plate/SkinSDR MWEA030243Contactor · inoperativePRIMARY TRIM INOPERATIVE. REMOVED AND REPLACED NOSE DOWN PRIMARY LONGITUDINAL TRIM CONTACTOR.Jun 9, 2003 · N804ME · Doug DC981 · Stabilizer Control SystemSDR MWEA030241Retainer · corrodedRIGHT UPPER COCKPIT WINDOW RETAINER IS CORRODED IN LOWER FORWARD CORNER. REMOVED DAMAGE AND INSTALLED FILLER AND EXTERNAL DOUBLER.Jun 3, 2003 · N804ME · Doug DC981 · Flight Compartment WindowsSDR MWEA030228Motor · defectivePRIMARY TRIM PROBLEM. REMOVED AND REPLACED PRIMARY LONGITUDINAL TRIM ACTUATOR MOTOR AND FIRST OFFICERS YOKE TRIM SWITCH AND REPLACED CONNECTORS.May 21, 2003 · N804ME · Doug DC981 · Stabilizer Control SystemSDR MWEA030128Bolt · shearedNR 1 MAIN WHEEL ASSY THROUGH BOLT SHEARED OFF. REPLACED NR 1 WHEEL AND TIRE ASSEMBLY.Feb 23, 2003 · N804ME · Doug DC981 · TireSDR MWEA030036Line · disconnectedON LEFT THROTTLE, SPLIT INCREASED WITH ALTITUDE TO ABOUT 1 1/2 KNOBS. -- RECONNECTED PRESSURE TOTAL 2 LINE.Jan 18, 2003 · N804ME · Doug DC981 · Engine Controls
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