N212ME, cancelled Dec 17, 2003

Service difficulty reports · 267

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 = 'N212ME' AND deregistration_id = 'N212ME-2003-12-17'
  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 MWEA020699Csd · malfunctionedCREW NOTICED RIGHT CSD LOW OIL PRESSURE LIGHT CAME ON. REMOVED AND REPLACED RIGHT CONSTANT SPEED DRIVE UNIT.Nov 15, 2002 · N212ME · Doug DC932 · Alternator-Generator DriveSDR MWEA020463Skin · dentedFUSELAGE SKIN DENTED AT STATION 999 AFT OF LONGERON 27 RIGHT. -- CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER.Jul 17, 2002 · N212ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA020462Frame · crackedLOWER FRAME ASSY STATION 1000 IS CRACKED, INLINE WITH LONGERON 28 RIGHT. -- INSTALLED REPAIR ANGLE.Jul 17, 2002 · N212ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020458Tee Fitting · dentedAFT PRESSURE BULKHEAD TEE WAS DENTED BETWEEN LONGERONS 29 RIGHT AND 28 RIGHT. REMOVED TEE SECTION FROM LONGERON AND INSTALLED NEW TEE SECTION AND REPAIR SPLICES.Jul 16, 2002 · N212ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA020443Controller · out of adjustAT 31,000 FEET THE AIRCRAFT LOST PRESSURE AND COULD NOT CONTROL IN AUTO OR MANUAL. MASKS AUTOMATICALLY DEPLOYED. PERFORMED ADJUSTMENT / TEST CABIN PRESSURE CONTROL REFERENCE 21-32-0-201. NO DISCREPANCY NOTED.Jul 6, 2002 · N212ME · Doug DC932 · Cabin Pressure ControllerSDR MWEA020031Bracket · crackedAFT CARGO DOOR BEAM #3 END FITTING CRACKED, AFT SIDE OF DOOR. -- REMOVED FITTING AND ANGLE SUPPORT BRACKET. LOCATED AND DEBURRED NEW FITTING AND ANGLE SUPPORT BRACKET.INSTALLED END FITTING AND ANGLE SUPPORT BRACKET.Jan 7, 2002 · N212ME · Doug DC932 · Cargo/Baggage DoorsSDR MWEA020030Pan · crackedAFT CARGO DOOR INNER PAN IS CRACKED UNDER NUMBER 2 AFT. WORKING CORROSION NRI 12570. -- FABRICATED REPAIR ANGLE AND INSTALLED REPAIR ANGLE AND FITTING.Jan 7, 2002 · N212ME · Doug DC932 · Cargo/Baggage DoorsSDR MWEA020029Fitting · crackedAFT CARGO DOOR BEAM NR 4 END FITTING CRACKED, AFT SIDE OF DOOR. REMOVED AND REPLACED NEW FITTING.Jan 7, 2002 · N212ME · Doug DC932 · Cargo/Baggage DoorsSDR MWEA020028Doubler · crackedRIGHT AFT PYLON WEB DOUBLER P/N 9912246 AT STATION 1038 HAS CRACKS EMINATING FROM THE UPPER STRAP ATTACHMENT HOLES. -- FABRICATED AND INSTALLED DOUBLER.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020027WebTHE AFT PYLON BULKHEAD HAS OVERSIZED HOLE WHERE THE UPPER PYLON STRAP ATTACHES TO IT. -- FABRICATED AND INSTALLED WEB AND DOUBLERS.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020026Web · oversizedRIGHT AFT PYLON SPAR WEB (P/N 9958154-21) UPPER HOLES ARE OVERSIZED. -- FABRICATED AND INSTALLED WEB.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020025Spar · damagedREMOVE PYLON SPAR WEB (P/N 9958154-29). THE WEB HAS OVERSIZED HOLES. REMOVED DOUBLER. FABRICATED NEW DOUBLER. INSTALLED WEB.Jan 7, 2002 · N212ME · Doug DC932 · Nacelle/Pylon, Frame/Spar/RibSDR MWEA020024Channel · corrodedCORROSION AROUND AND ON NUT PLATES LOCATED AT STATION 351 ON U-CHANNEL THAT'S RIVETED TO FLOORBEAM APPROXIMATELY 28 INCHES AND 33 INCHES TO THE LEFT OF CENTER. REMOVED CHANNEL, LOCATED HOLES, INSTALLED NUT PLATES ON CHANNEL, AND INSTALLED CHANNEL.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020023Channel · corrodedCORROSION AROUND AND ON NUT PLATES LOCATED ON U-CHANNEL THAT'S ATTACHED TO FLOORBEAM 427 ABOVE FORWARD AT CARGO DOOR OPENING. FABRICATED AND INSTALLED U-CHANNEL.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020022Frame · damagedSTATION 1038 RIGHT FRAME CAP (P/N 9912246-103) HAS TWO OVERSIZED HOLES WHERE THE AFT UPPER ENGINE PYLON ATTACHES. REPAIRED PER TELEX MWX-ORD-01-00570H 19 DEC 2001.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020021Frame · damagedSTATION 1038 RIGHT FRAME CAP (P/N 9912246-105) HAS TWO OVERSIZED HOLES WHERE THE AFT UPPER ENGINE PYLON STRAP ATTACHES. FABRICATED AND INSTALLED DOUBLER.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020020Frame · crackedKEEL AREA FRAME AT STATION 637 IS CRACKED AT OUTBOARD END ON LEFT SIDE. FABRICATED AND INSTALLED REPAIR ANGLE.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020019Web · corrodedWEB AT GALLEY SERVICE DOOR, FROM STATION 150 TO STATION 200, IS CORRODED AT FORWARD SIDE OF SERVICE DOOR OPENING AND AFT SIDE OF SERVICE DOOR OPENING. FABRICATED AND INSTALLED WEB.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020018Longeron · chafedLONGERON 22 RIGHT HAS CHAFE DAMAGE ON UPPER LEG (VIEW THROUGH RIGHT THRUST REVERSER BY PASS DOOR). FABRICATED AND INSTALLED LONGERON SECTION, LONGERON SPLICE AND NEW STRAPS. REMOVED CORROSION FROM SHOVEL CLIP AND REINSTALLED.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA020017Frame · crackedFUSELAGE FORMER CRACKED BELOW LONGERON 15 RIGHT VIEW FROM FORWARD SIDE OF FUSELAGE FRAME 1038. REMOVED AND REPLACED FORMER.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020014Floor Support · corrodedFLOORBOARD SUPPORT AT STATION 200 HAS CORROSION BEYOND LIMITS LOCATED BETWEEN NR 3 SEAT TRACK AND NR 4 SEAT TRACK. REMOVED AND REPLACED FLOOR SUPPORT.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020013Floor Support · corrodedFLOORBOARD SUPPORT AT STATION 200 HAS CORROSION BEYOND LIMITS LOCATED BETWEEN CENTER FLOOR SUPPORT AND NR 3 SEAT TRACK. REMOVED AND REPLACED FLOOR SUPPORT.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020012Floor Support · corrodedFLOORBOARD SUPPORT LOCATED JUST FORWARD OF NUMBER 4 SEAT TRACK FROM STATION 160 TO 200 HAS TWO AREAS OF CORROSION ON TOP SIDE AND SEVERAL AREAS OF CORROSION ON LOWER SURFACE OF FLANGE AROUND THE HOLES. REMOVED, LOCATED, DRILLED AND INSTALLED FLOORBOARD SUPPORJan 4, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020010Frame · chafedFUSELAGE FRAME 1059 HAS CHAFE DAMAGE ON UPPER LEG AT LONGERON 21 RIGHT. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED, FIT, DRILLED AND INSTALLED REPAIR.Jan 4, 2002 · N212ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020009Web · damagedSUBFLOOR HAS SEVERAL AREAS OF BARE METAL AND RIVET HEAD WEAR MARKS FROM STATION 200 TO 218 BETWEEN NUMBER 2 SEAT TRACK AND CENTER FLOOR SUPPORT. FABRICATED AND INSTALLED REPAIR DOUBLER.Jan 4, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020008Seat Track · corrodedNUMBER 3 SET TRACK HAS HEAVY CORROSION FROM STATION 218 TO 248. CUT AND REMOVED SEAT TRACK. LOCATED, DRILLED AND INSTALLED SEAT TRACK.Jan 4, 2002 · N212ME · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA020007Floor Support · corrodedCENTER FLOOR SUPPORT HAS LIGHT CORROSION AROUND SEVERAL FASTENER HOLES FROM STATION 192 TO 200. REMOVED CENTER FLOOR SUPPORT. DRILLED, TRIMMED AND INSTALLED NEW CENTER FLOOR SUPPORT.Jan 4, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020006Skin · crackedSTATION 1010, RIGHT HAND SIDE FUSELAGE SKIN HAS A SMALL CRACK ORIGINATING FROM RIVET BETWEEN LONGERON 14 RIGHT AND 16 RIGHT. CUT OUT CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER.Jan 4, 2002 · N212ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA020002Panel · delaminatedRIGHT WING OUTBOARD TRAILING EDGE PANEL HAS APPROXIMATELY 80 SQUARE INCHES OF DELAMINATION ON THE TOP AREA, INCLUDES MOST OF THE TRAILING EDGE. REMOVED, LOCATED, DRILLED AND INSTALLED NEW TRAILING EDGE PANEL.Jan 4, 2002 · N212ME · Doug DC932 · Wing, Plate/SkinSDR MWEA011487Longeron · chafedKEEL AREA LONGERON 27 LEFT HAS A CHAFE AT STATION 655 AB5. REMOVED, DRILLED AND INSTALLED LONGERON.Dec 17, 2001 · N212ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA011490Longeron · crackedCABIN LONGERON 4 LEFT IS CRACKED AT FRAME STATION 200. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SECTION OF LONGERON.Dec 6, 2001 · N212ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA011489Longeron · crackedCABIN LONGERON 4 LEFT IS CRACKED AT FRAME STATION 160. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SECTION OF LONGERON.Dec 6, 2001 · N212ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA011352Control Box · faultyIN CRUISE NOSE GEAR UNSAFE LIGHT CAME ON, RIGHT GEAR HANDLE UP, RED LIGHT ON IN CRUISE AND APPROACH, LOWERED GEARS, NOSE GEAR RED STAYED ON. QRH PERFORMED, CONFIRMED VISUALLY NOSE GEAR DOWN AND LOCKED. INSPECTED NOSE GEAR SYSTEM, REMOVED AND REPLACED PROXIMITSep 24, 2001 · N212ME · Doug DC932 · Landing Gear Position and WarningSDR MWEA011272Web · chafedFOUND MINOR CHAFE ON WEB IN NOSE WELL. -- BLENDED CHAFE AND REPAIRED WITH DOUBLER REPAIR.Sep 15, 2001 · N212ME · Doug DC932 · Fuselage Main, StructureSDR MWEA011240Light · departedAFTER TAKEOFF, PAX REPORTED RIGHT LOGO LIGHT BULB AND LOVER ASSY DEPARTED AIRCRAFT. CREW VERIFIED STRAY WIRES VISIBLE FROM CABIN AT WING TIP. REPLACED LOGO LIGHT BULB AND LOVER ASSY. REPLACED BROKEN RIGHT AFT NAV LIGHT LENS.Sep 1, 2001 · N212ME · Doug DC932 · Exterior LightingSDR MWEA011001Pressure Switch · failedON APPROACH TO MILWAUKEE, RIGHT ENGINE OIL PRESSURE LOW LIGHT CAME ON, OIL PRESSURE WAS 42 PSI, OIL TEMP 110 DEGREES CELCIUS. SHUT OFF ENGINE, ENGINE WINDMILLED FOR TEN MINUTES WITH OIL PRESSURE AT 42-43 PSI. REMOVED AND REPLACED RIGHT ENGINE LOW OIL PRESSURE Jun 26, 2001 · N212ME · Doug DC932 · Engine Oil PressureSDR MWEA010580Switch · inoperativeTAKE OFF WARNING HORN CAME ON AT 105 KNOTS DURING TAKE OFF ROLL. ABORTED TAKE OFF. MAINTENANCE FOUND PARKING BRAKE SWITCH INOPERATIVE AND REPLACED SWITCH.Apr 13, 2001 · N212ME · Doug DC932 · Landing Gear Brake SystemSDR MWEA010512Transducer · inoperativeSTALL INDICATOR FAILURE ANNUNCIATOR CAME ON AT CLIMBOUT WITH INTERMEDIATE WINDSHEAR INOP LIGHT. REPLACED LEFT ANGLE OF ATTACH VANE.Apr 1, 2001 · N212ME · Doug DC932 · Stall Warning SystemSDR MWEA010161Clip · brokenTAIL CONE AFT INTERIOR HANDLE HAS A BROKEN CLIP AND FAILS PULL CHECK (25 - 35 LBS). REMOVED AND REPLACED CLIP.Feb 19, 2001 · N212ME · Doug DC932 · Aerodynamic FairingsSDR MWEA010166Skin · dentedRUDDER LEFT SKIN HAS .75 INCH BY .75 INCH DENT .010 INCH DEEP AT ZR 28.936. REMOVED AND REPLACED DOUBLER.Feb 19, 2001 · N212ME · Doug DC932 · Rudder, Plate/SkinSDR MWEA010165Skin · damagedAFT CARGO BAG FUSELAGE SKIN HAS MECHANICAL DAMAGE FROM STATION 876 - STATION 890 BETWEEN LONGERON 23 THRU LONGERON 22 LEFT. FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS.Feb 19, 2001 · N212ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA010164Belt · corrodedNR 20 LEFT WINDOW FRAME CORRODED IN BOTH LOWER, INNER CORNERS. REMOVED AND REPLACED WINDOW BELT.Feb 19, 2001 · N212ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010162Panel · dentedLEFT WING UPPER TRAILING EDGE PANEL IS DENTED, STATION 419, 4 INCHES AFT OF REAR SPAR. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER.Feb 19, 2001 · N212ME · Doug DC932 · Wing, Plate/SkinSDR MWEA010160Ring · crackedLEFT WINDOW RING CRACKED, STATION 639 - 658. REMOVED AND REPLACED WINDOW RING.Feb 19, 2001 · N212ME · Doug DC932 · Passenger Compartment WindowsSDR MWEA010159Skin · dentedFUSELAGE SKIN DENTED STATION 980, 2 INCHES BELOW LONGERON 2 RIGHT. FABRICATED AND INSTALLED DOUBLER.Feb 19, 2001 · N212ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA010154Web · crackedVERTICAL WEB CRACKED IN RIGHT PYLON OUTBOARD OF 13TH STRINGER. BLEED NUT ACCESSIBLE THROUGH PANEL 8204A. FABRICATED AND INSTALLED REPAIR DOUBLERS.Feb 13, 2001 · N212ME · Doug DC932 · Nacelle/Pylon, Main FrameSDR MWEA010153Longeron · corrodedCORROSION ON LONGERON 12 LEFT AT STATION 1104. FABRICATED AND INSTALLED LONGERON AND ANGLE.Feb 13, 2001 · N212ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA010152Floor Panel · crackedFLOOR PANEL E-6 IS CRACKED ON AFT OUTBOARD CORNER. FABRICATED AND INSTALLED DOUBLER.Feb 13, 2001 · N212ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010151Angle · crackedCRACK AT STATION 1121 AT LONGERON 17 RIGHT. DRILLED AND INSTALLED REPAIR ANGLES.Feb 13, 2001 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA010148Fitting · crackedFITTING CRACKED AT VERTICAL WEB AT LEFT ENGINE PYLON STRUCTURE, VIEWED THROUGH PANEL 8105A. REMOVED AND REPLACED FITTING.Feb 9, 2001 · N212ME · Doug DC932 · Nacelle/Pylon, Attach Fittings
Back to N212ME, cancelled Dec 17, 2003