N209ME, cancelled Jul 28, 2006

Service difficulty reports · 335

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 = 'N209ME' AND deregistration_id = 'N209ME-2006-07-28'
  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 MWEA040015Indicator · inoperativeFORWARD ENTRANCE DOOR SLIDE PRESSURE GAUGE IS INOPERATIVE. REMOVED AND REPLACED FORWARD EVACUATION SLIDE.Feb 3, 2004 · N209ME · Doug DC932 · Escape SlideSDR MWEA030437Light · looseEMERGENCY EXIT LIGHT FOR SERVICE DOOR AFT SIDE HAS COME LOOSE FROM TOP SIDE. REMOVED AND REPLACED EEPLS EXIT LIGHT FOR SERVICE DOOR.Oct 31, 2003 · N209ME · Doug DC932 · Emergency LightingSDR MWEA030421Control Panel · inoperativeON START OF RT ENGINE, AC CROSS-TIE LOCK OUT CAME ON, UNABLE TO RESET. REMOVED AND REPLACED AC BUSS CONTROL PANEL.Oct 13, 2003 · N209ME · Doug DC932 · AC Generation SystemSDR MWEA030400Thrust Reverser · corrodedLIGHT CORROSION ON OUTER FACE OF LEFT DRIVE ARM, TOP BUCKET IN FLANGE RADIUS. REMOVED AND REPLACED THRUST REVERSER.Oct 1, 2003 · N209ME · Doug DC932 · Engine Thrust ReverserSDR MWEA030395Skin · dentedFUSELAGE SKIN HAS A DENT AT STATION 967, 2 INCHES ABOVE LONGERON 27 LEFT. FABRICATED AND INSTALLED DOUBLER AND FILLERS.Sep 25, 2003 · N209ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA030393Longeron · crackedWHILE REPLACING DOME NUTS FOR FUSELAGE FILET PANEL, FOUND SUSPECT CRACK ON AFT END OF LONGERON 26 RT FRAME STATION 604. FABRICATED AND INSTALLED FITTING.Sep 25, 2003 · N209ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA030392Skin · dentedFUSELAGE SKIN HAS A DENT AT STATION 388 AT LONGERON 5 RIGHT. FABRICATED AND INSTALLED FILLER AND DOUBLER.Sep 25, 2003 · N209ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA030391Skin · gougedLEFT SIDE OF VERTICAL STABILIZER SKIN UNDER VERTICAL TO HORIZONTAL STABILIZER, FAIRING HAS A GOUGE FROM TOP SKIN RADIUS EXTENDING DOWN AT 1.5 INCHES. FABRICATED AND INSTALLED REPAIR DOUBLER.Sep 25, 2003 · N209ME · Doug DC932 · Vertical Stabilizer, Plate/SkinSDR MWEA030272Connector · faultyLEFT ENGINE LOOP A FIRE INDICATION CAME ON. REMOVED AND REPLACED BOTH FIRE EXTINGUISHER BOTTLE,1 EACH SQUIBS,LEFT ENGINE B AND REPLACED FAULTY CONNECTORS,Jul 8, 2003 · N209ME · Doug DC932 · Fire DetectionSDR MWEA030179Switch · dirtyAFTER THROTTLE ADVANCEMENT, TAKEOFF WARNING HORN SOUNDED. ALL INDICATIONS NORMAL. HORIZONTAL STABILIZER SWITCH FOUND STICKING. CLEANED SWITCH.Apr 21, 2003 · N209ME · Doug DC932 · Stabilizer Position IndicatingSDR MWEA030132Control Box · inoperativeWHILE ARMING ANTI-SKID RIGHT OUTBOARD AND INBOARD LIGHTS REMAINED ON. REMOVED AND REPLACED ANTI-SKID CONTROL BOX.Mar 13, 2003 · N209ME · Doug DC932 · Brake Anti-Skid SectionSDR MWEA030105Receiver · inoperativeFIRST OFFICER NR 2 NAV FAILED, VOR, GS, AND LOC FLAGS SHOWING. REMOVED AND REPLACED VOR/ILS RECEIVER.Feb 15, 2003 · N209ME · Doug DC932 · Localizer/VOR SystemSDR MWEA030072Drive Shaft · shearedWHEN ATTEMPTING TO START #2 ENGINE THE N2 WENT TO 10% THEN DROPPED OFF TO ZERO. -- REMOVED AND REPLACED STARTER DRIVE SHAFT.Feb 12, 2003 · N209ME · Doug DC932 · Engine StarterSDR MWEA020727Starter · inoperativeLEFT ENGINE STARTER INOPERATIVE -- REMOVED AND REPLACED ENGINE STARTER.Dec 6, 2002 · N209ME · Doug DC932 · Engine CrankingSDR MWEA020576Altimeter · fluctuatesCAPTAIN'S STANDBY ALTIMETER FLUCTUATING. -- REMOVED AND REPLACED CAPTAIN'S STATIC SELECTOR VALVE.Sep 18, 2002 · N209ME · Doug DC932 · Altimeter, Barometric/EncoderSDR MWEA020521Wing · damagedLEFT OUTBOARD FLAP TRAILING EDGE DAMAGED AND AFT TRAILING EDGE CHANNEL. -- REMOVED AND REPLACED TRAILING EDGE.Aug 29, 2002 · N209ME · Doug DC932 · Trailing Edge FlapsSDR MWEA020459Bracket · crackedCRACKED ANGLE BRACKET FORWARD END UNDER #1 BEAM OF GALLEY DOOR (DOT JH 36). -- FABRICATED AND INSTALLED BRACKET.Jul 25, 2002 · N209ME · Doug DC932 · Galley DoorsSDR MWEA020070Angle · oversizedPYLON WEB ANGLE HAS AN OVERSIZED HOLE. -- FABRICATED AND INSTALLED ANGLE.Feb 6, 2002 · N209ME · Doug DC932 · Nacelle/Pylon, Main FrameSDR MWEA020069Doubler · damagedRIGHT PYLON AFT SPAR WEB DOUBLER HAS OVERSIZED FASTENER HOLES. FABRICATED AND INSTALLED NEW DOUBLER.Feb 6, 2002 · N209ME · Doug DC932 · Nacelle/Pylon, Frame/Spar/RibSDR MWEA020068Angle · oversizedREMOVED RIGHT PYLON AFT SPAR WEB ANGLE TO FACILITATE OTHER MAINTENANCE. (UPPER FASTENER HOLE OVERSIZED.) -- FABRICATED AND INSTALLED "L" ANGLE ON NEW WEB.Feb 6, 2002 · N209ME · Doug DC932 · Nacelle/Pylon, Main FrameSDR MWEA020124Web · oversizedWEB AT 15 RIGHT BETWEEN STATION 1038 AND 1059 HAS OVERSIZED HOLES. -- FABRICATED AND INSTALLED SPLICE ANGLE.Feb 6, 2002 · N209ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020123Web · oversizedREMOVED SECTION OF WEB AT STATION 1038 BETWEEN LONGERON 14 RIGHT AND 17 RIGHT. SPAR STRAP HOLES OVERSIZED. -- FABRICATED AND INSTALLED WEB SECTION AND WEB SPLICES.Feb 6, 2002 · N209ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020121Frame · damagedAT STATION 1038, LONGERON 15 RIGHT INNER, OUTER FRAME CAP AND SHEAR TIE HAS 5 OVERSIZED HOLES. FABRICATED AND INSTALLED REPAIR BUSHINGS AND BUSHING RETAINING STRAPS.Feb 6, 2002 · N209ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020120Angle · oversizedRIGHT PYLON AFT SPAR ANGLE HAS OVERSIZED FASTENER H0LE. -- FABRICATED AND INSTALLED ANGLE.Feb 6, 2002 · N209ME · Doug DC932 · Nacelle/Pylon, Main FrameSDR MWEA020119Fitting · oversizedRIGHT PYLON FITTING HAS OVERSIZE HOLE. -- FABRICATED AND INSTALLED FITTING AND RADIUS BLOCKS.Feb 6, 2002 · N209ME · Doug DC932 · Nacelle/Pylon, Main FrameSDR MWEA020118Angle · oversizedRIGHT SPAR AFT UPPER ANGLE HAS OVERSIZED HOLES. -- FABRICATED AND INSTALLED ANGLE.Feb 6, 2002 · N209ME · Doug DC932 · Nacelle/Pylon, Main FrameSDR MWEA020117Fitting · oversizedREMOVED FITTING THAT ATTACHES TO UPPER WEB AT FUSELAGE STATION 1038 LONGERON 15 RIGHT DUE TO OVERSIZED HOLES. -- FABRICATED AND INSTALLED FITTING.Feb 6, 2002 · N209ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020116Spar · damagedRIGHT PYLON AFT SPAR WEB UPPER HOLES OVERSIZED. FABRICATED AND INSTALLED SPAR WEB.Feb 6, 2002 · N209ME · Doug DC932 · Nacelle/Pylon, Frame/Spar/RibSDR MWEA020115Angle · oversizedRIGHT PYLON AFT SPAR UPPER ANGLE HAS OVERSIZE HOLES. -- FABRICATED AND INSTALLED ANGLE.Feb 6, 2002 · N209ME · Doug DC932 · Nacelle/Pylon, Main FrameSDR MWEA020114Angle · oversizedRIGHT PYLON AFT SPAR ANGLE HAS OVERSIZE HOLE. -- FABRICATED AND INSTALLED ANGLE.Feb 6, 2002 · N209ME · Doug DC932 · Nacelle/Pylon, Main FrameSDR MWEA011251Skin · crackedFUSELAGE SKIN WAS CRACKED AT STATION 718 BELOW LONGERON 10 RIGHT. -- REMOVED DAMAGE, INSTALLED DOUBLERS.Sep 8, 2001 · N209ME · Doug DC932 · Fuselage Main, StructureSDR MWEA011144Engine · overtempON TAKE OFF LEFT ENGINE REACHED 605-610 DEGREES CELSIUS AFTER V1, ABOUT 40 SECONDS AFTER TAKE OFF POWER WAS REDUCED TO BRING TEMP BACK TO 590 DEGREES CELSIUS AT A NORMAL CLIMB, POWER SETTING ENGINE TEMP WAS 545 DEGREES CELSIUS MCI TEMP 37 DEGREES CELSIUS EPR 1Aug 22, 2001 · N209ME · Doug DC932 · Engine (Turbine/Turboprop)SDR MWEA010982Solenoid Valve · inoperativeRIGHT HYDRAULIC TEMP HI ANNUNCIATOR CAME ON DURING TAXI OUT. -- REFERENCE DMI #6-50 "ALTERNATE PUMP WILL NOT OPERATE WHEN SWITCH IS TURNED ON," REMOVED AND REPLACED ALTERNATE PUMP SOLENOID VALVE, OPERATIONAL CHECK GOOD.Jun 13, 2001 · N209ME · Doug DC932 · Hydraulic System, AuxiliarySDR MWEA010981Servo · inoperativeWHEN AUTOPILOT WAS ENGAGED THE AIRCRAFT ROLLED VIOLENTLY TO THE LEFT. AP WAS IMMEDIATELY DISENGAGED AND WE NOTICED A WHINING/HUMMING SOUND WHICH CONTINUED FOR REMAINDER OF THE FLIGHT. -- DEFERRED AUTOPILOT CONTROLLER PER MEL 22-05 PULLED AND COLLERED C/B'S DJun 12, 2001 · N209ME · Doug DC932 · Autopilot SystemSDR MWEA010605Floorboard · corrodedFLOORBOARD A-6 HAS SEVERAL AREAS OF CORROSION ON TOP SURFACE AND CORROSION AROUND SOME OF THE FASTENER HOLES AND BOTTOM HAT CHANNELS HAVE MINOR CHAFES AND CORROSION. FABRICATED AND INSTALLED FLOORBOARD SKIN AND HAT CHANNELS.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010604Floorboard · corrodedFLOORBOARD A-4 HAS SEVERAL AREAS OF CORROSION ON TOP SURFACE AND CORROSION AROUND SOME OF THE FASTENER HOLES AND BOTTOM HAT CHANNELS HAVE MINOR CHAFES AND CORROSION. REMOVED CORROSION AND CHAFING. REPAIRED FLOOR PANEL IAW DC9 SRM 51-30-2 AND DRW 9915597 & SRApr 17, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010603Intercostal · damagedINTERCOSTAL AT STATION 390 LONGERON 27 RIGHT - 29 RIGHT HAS ELONGATED HOLES AND IS BENT. FABRICATED AND INSTALLED INTERCOSTAL AND INBOARD AND OUTBOARD TEE CLIPS.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA010602Intercostal · corrodedINTERCOSTAL AT STATION 1018 AND RBL 15 TO 25 CORRODED AND CRACKED. REMOVED AND REPLACED INTERCOSTAL.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA010601Spar · corrodedRIGHT WING INTERNAL AFT LOWER SPAR TEE HAD HEAVY CORROSION. FABRICATED REPAIR FILLERS, INSTALLED IAW BOEING TELEX MWX-ORD-01-00272H, DATED 03 APRIL 2001. PLACED ON WATCH ITEM 5720 FOR FINAL DISPOSITION.Apr 17, 2001 · N209ME · Doug DC932 · Wing SparSDR MWEA010600Intercostal · crackedINTERCOSTAL BETWEEN STATION 945 - 965 AT CENTERLINE OF AIRCRAFT BELOW SUPPORT IS CRACKED. REMOVED INTERCOSTAL, FABRICATED, DRILLED, AND INSTALLED NEW PART.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA010599Longeron · corrodedLONGERON 28 RIGHT IS CORRODED FROM STATION 323 - 360. REMOVED DAMAGED SECTION, FABRICATED SECTION, REPAIR SPLICE, DRILLED AND INSTALLED.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA010598Floorboard · damagedFLOORBOARD A-1 HAD SEVERAL FASTENERS PULLED THRU AND CORROSION; CHAFES AROUND HAT CHANNELS. REMOVED FLOORBOARD, FABRICATED NEW FLOORBOARD, REMOVED CORROSION FROM HAT CHANNELS, FABRICATED ONE NEW HAT CHANNEL AND INSTALLED ALL.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010597Floorboard · corrodedFLOORBOARD E-9 HAD SEVERAL AREAS OF CORROSION AROUND FASTENER HOLES AND ON HAT CHANNELS. REMOVED FLOORBOARD, FABRICATED SKIN, REMOVED CORROSION FROM HAT CHANNELS, ASSEMBLED NEW SKIN AND CHANNELS.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010596Floorboard · corrodedFLOORBOARD A-5 HAD AREAS OF CORROSION AROUND HOLES AND ON HAT CHANNELS. REMOVED FLOORBOARD, FABRICATED PANEL, HAT CHANNELS, ASSEMBLED AND INSTALLED TOGETHER.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010595Shear Tie · corrodedFOUND CORROSION ON SKIN SPLICE DOUBLER AND FORWARD SIDE OF RIGHT LAV FLOORBEAM AT STATION 996. REMOVED SHEAR TIE, LOCATED, DRILLED, AND INSTALLED NEW SHEAR TIE.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010594Spar · gougedREMOVED LEFT WING SPAR WEB AT TRUNNION AND FOUND GOUGES OUT OF LIMITS. FABRICATED, DRILLED AND INSTALLED NEW WEB SECTION.Apr 17, 2001 · N209ME · Doug DC932 · Wing SparSDR MWEA010592Fitting · gougedFOUND DEEP GOUGES ON FITTING AT STATION XRS 353 BETWEEN STRINGER 11 AND AFT SPAR RIGHT WING. REMOVED FITTING, FABRICATED, DRILLED AND INSTALLED NEW FITTING.Apr 17, 2001 · N209ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA010591Clip · corrodedCORROSION FOUND ON OUTBOARD OF XCW 58 LOWER TEE CAP, HORIZONTAL LEG BETWEEN STRINGER 23. REMOVED 2 CLIPS FOR OUT OF LIMITS CORROSION. FABRICATED DRILLED AND INSTALLED NEW CLIPS.Apr 17, 2001 · N209ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA010590Structure · corrodedAT LEFT WING FOUND CORROSION ON LOWER TEE CAP HORIZONTAL LEG BETWEEN STRINGER 13 AND 14. REMOVED CORROSION, SUBMITTED BLENDOUTS TO BOEING AND ARE ACCEPTABLE PER TELEX MWX-ORD-01-00146H DATED 21, FEB, 2001. PLACED ON WATCH ITEM 5616 FOR REPETITIVE INSPECTION.Apr 17, 2001 · N209ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA010589Clip · damagedSEVERAL CLIPS (6) REQUIRED REPLACEMENT BETWEEN STATION 370 - 427. REMOVED CLIPS, FABRICATED AND INSTALLED NEW CLIPS.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous Structure
Back to N209ME, cancelled Jul 28, 2006