# Service difficulty reports: N212ME, cancelled Dec 17, 2003 A list on [N212ME, cancelled Dec 17, 2003](https://openairdocs.org/deregistered/N212ME-2003-12-17.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 6 · 267 reports - [SDR MWEA020699](https://openairdocs.org/sdr/MWEA020699.md): Csd · malfunctioned · Nov 15, 2002 · N212ME · Doug DC932 · Alternator-Generator Drive > CREW NOTICED RIGHT CSD LOW OIL PRESSURE LIGHT CAME ON. REMOVED AND REPLACED RIGHT CONSTANT SPEED DRIVE UNIT. - [SDR MWEA020463](https://openairdocs.org/sdr/MWEA020463.md): Skin · dented · Jul 17, 2002 · N212ME · Doug DC932 · Fuselage Main, Plate/Skin > FUSELAGE SKIN DENTED AT STATION 999 AFT OF LONGERON 27 RIGHT. -- CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER. - [SDR MWEA020462](https://openairdocs.org/sdr/MWEA020462.md): Frame · cracked · Jul 17, 2002 · N212ME · Doug DC932 · Fuselage Main, Frame > LOWER FRAME ASSY STATION 1000 IS CRACKED, INLINE WITH LONGERON 28 RIGHT. -- INSTALLED REPAIR ANGLE. - [SDR MWEA020458](https://openairdocs.org/sdr/MWEA020458.md): Tee Fitting · dented · Jul 16, 2002 · N212ME · Doug DC932 · Fuselage Main, Bulkhead > AFT 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. - [SDR MWEA020443](https://openairdocs.org/sdr/MWEA020443.md): Controller · out of adjust · Jul 6, 2002 · N212ME · Doug DC932 · Cabin Pressure Controller > AT 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. - [SDR MWEA020031](https://openairdocs.org/sdr/MWEA020031.md): Bracket · cracked · Jan 7, 2002 · N212ME · Doug DC932 · Cargo/Baggage Doors > AFT 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. - [SDR MWEA020030](https://openairdocs.org/sdr/MWEA020030.md): Pan · cracked · Jan 7, 2002 · N212ME · Doug DC932 · Cargo/Baggage Doors > AFT CARGO DOOR INNER PAN IS CRACKED UNDER NUMBER 2 AFT. WORKING CORROSION NRI 12570. -- FABRICATED REPAIR ANGLE AND INSTALLED REPAIR ANGLE AND FITTING. - [SDR MWEA020029](https://openairdocs.org/sdr/MWEA020029.md): Fitting · cracked · Jan 7, 2002 · N212ME · Doug DC932 · Cargo/Baggage Doors > AFT CARGO DOOR BEAM NR 4 END FITTING CRACKED, AFT SIDE OF DOOR. REMOVED AND REPLACED NEW FITTING. - [SDR MWEA020028](https://openairdocs.org/sdr/MWEA020028.md): Doubler · cracked · Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, Structure > RIGHT AFT PYLON WEB DOUBLER P/N 9912246 AT STATION 1038 HAS CRACKS EMINATING FROM THE UPPER STRAP ATTACHMENT HOLES. -- FABRICATED AND INSTALLED DOUBLER. - [SDR MWEA020027](https://openairdocs.org/sdr/MWEA020027.md): Web · Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, Structure > THE AFT PYLON BULKHEAD HAS OVERSIZED HOLE WHERE THE UPPER PYLON STRAP ATTACHES TO IT. -- FABRICATED AND INSTALLED WEB AND DOUBLERS. - [SDR MWEA020026](https://openairdocs.org/sdr/MWEA020026.md): Web · oversized · Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, Structure > RIGHT AFT PYLON SPAR WEB (P/N 9958154-21) UPPER HOLES ARE OVERSIZED. -- FABRICATED AND INSTALLED WEB. - [SDR MWEA020025](https://openairdocs.org/sdr/MWEA020025.md): Spar · damaged · Jan 7, 2002 · N212ME · Doug DC932 · Nacelle/Pylon, Frame/Spar/Rib > REMOVE PYLON SPAR WEB (P/N 9958154-29). THE WEB HAS OVERSIZED HOLES. REMOVED DOUBLER. FABRICATED NEW DOUBLER. INSTALLED WEB. - [SDR MWEA020024](https://openairdocs.org/sdr/MWEA020024.md): Channel · corroded · Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous Structure > CORROSION 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. - [SDR MWEA020023](https://openairdocs.org/sdr/MWEA020023.md): Channel · corroded · Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous Structure > CORROSION 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. - [SDR MWEA020022](https://openairdocs.org/sdr/MWEA020022.md): Frame · damaged · Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, Frame > STATION 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. - [SDR MWEA020021](https://openairdocs.org/sdr/MWEA020021.md): Frame · damaged · Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, Frame > STATION 1038 RIGHT FRAME CAP (P/N 9912246-105) HAS TWO OVERSIZED HOLES WHERE THE AFT UPPER ENGINE PYLON STRAP ATTACHES. FABRICATED AND INSTALLED DOUBLER. - [SDR MWEA020020](https://openairdocs.org/sdr/MWEA020020.md): Frame · cracked · Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, Frame > KEEL AREA FRAME AT STATION 637 IS CRACKED AT OUTBOARD END ON LEFT SIDE. FABRICATED AND INSTALLED REPAIR ANGLE. - [SDR MWEA020019](https://openairdocs.org/sdr/MWEA020019.md): Web · corroded · Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous Structure > WEB 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. - [SDR MWEA020018](https://openairdocs.org/sdr/MWEA020018.md): Longeron · chafed · Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, Longeron/Stringer > LONGERON 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. - [SDR MWEA020017](https://openairdocs.org/sdr/MWEA020017.md): Frame · cracked · Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, Frame > FUSELAGE FORMER CRACKED BELOW LONGERON 15 RIGHT VIEW FROM FORWARD SIDE OF FUSELAGE FRAME 1038. REMOVED AND REPLACED FORMER. - [SDR MWEA020014](https://openairdocs.org/sdr/MWEA020014.md): Floor Support · corroded · Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous Structure > FLOORBOARD SUPPORT AT STATION 200 HAS CORROSION BEYOND LIMITS LOCATED BETWEEN NR 3 SEAT TRACK AND NR 4 SEAT TRACK. REMOVED AND REPLACED FLOOR SUPPORT. - [SDR MWEA020013](https://openairdocs.org/sdr/MWEA020013.md): Floor Support · corroded · Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous Structure > FLOORBOARD SUPPORT AT STATION 200 HAS CORROSION BEYOND LIMITS LOCATED BETWEEN CENTER FLOOR SUPPORT AND NR 3 SEAT TRACK. REMOVED AND REPLACED FLOOR SUPPORT. - [SDR MWEA020012](https://openairdocs.org/sdr/MWEA020012.md): Floor Support · corroded · Jan 4, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous Structure > FLOORBOARD 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 SUPPOR - [SDR MWEA020010](https://openairdocs.org/sdr/MWEA020010.md): Frame · chafed · Jan 4, 2002 · N212ME · Doug DC932 · Fuselage Main, Frame > FUSELAGE FRAME 1059 HAS CHAFE DAMAGE ON UPPER LEG AT LONGERON 21 RIGHT. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED, FIT, DRILLED AND INSTALLED REPAIR. - [SDR MWEA020009](https://openairdocs.org/sdr/MWEA020009.md): Web · damaged · Jan 4, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous Structure > SUBFLOOR 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. - [SDR MWEA020008](https://openairdocs.org/sdr/MWEA020008.md): Seat Track · corroded · Jan 4, 2002 · N212ME · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings > NUMBER 3 SET TRACK HAS HEAVY CORROSION FROM STATION 218 TO 248. CUT AND REMOVED SEAT TRACK. LOCATED, DRILLED AND INSTALLED SEAT TRACK. - [SDR MWEA020007](https://openairdocs.org/sdr/MWEA020007.md): Floor Support · corroded · Jan 4, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous Structure > CENTER 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. - [SDR MWEA020006](https://openairdocs.org/sdr/MWEA020006.md): Skin · cracked · Jan 4, 2002 · N212ME · Doug DC932 · Fuselage Main, Plate/Skin > STATION 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. - [SDR MWEA020002](https://openairdocs.org/sdr/MWEA020002.md): Panel · delaminated · Jan 4, 2002 · N212ME · Doug DC932 · Wing, Plate/Skin > RIGHT 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. - [SDR MWEA011487](https://openairdocs.org/sdr/MWEA011487.md): Longeron · chafed · Dec 17, 2001 · N212ME · Doug DC932 · Fuselage Main, Longeron/Stringer > KEEL AREA LONGERON 27 LEFT HAS A CHAFE AT STATION 655 AB5. REMOVED, DRILLED AND INSTALLED LONGERON. - [SDR MWEA011490](https://openairdocs.org/sdr/MWEA011490.md): Longeron · cracked · Dec 6, 2001 · N212ME · Doug DC932 · Fuselage Main, Longeron/Stringer > CABIN LONGERON 4 LEFT IS CRACKED AT FRAME STATION 200. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SECTION OF LONGERON. - [SDR MWEA011489](https://openairdocs.org/sdr/MWEA011489.md): Longeron · cracked · Dec 6, 2001 · N212ME · Doug DC932 · Fuselage Main, Longeron/Stringer > CABIN LONGERON 4 LEFT IS CRACKED AT FRAME STATION 160. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SECTION OF LONGERON. - [SDR MWEA011352](https://openairdocs.org/sdr/MWEA011352.md): Control Box · faulty · Sep 24, 2001 · N212ME · Doug DC932 · Landing Gear Position and Warning > IN 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 PROXIMIT - [SDR MWEA011272](https://openairdocs.org/sdr/MWEA011272.md): Web · chafed · Sep 15, 2001 · N212ME · Doug DC932 · Fuselage Main, Structure > FOUND MINOR CHAFE ON WEB IN NOSE WELL. -- BLENDED CHAFE AND REPAIRED WITH DOUBLER REPAIR. - [SDR MWEA011240](https://openairdocs.org/sdr/MWEA011240.md): Light · departed · Sep 1, 2001 · N212ME · Doug DC932 · Exterior Lighting > AFTER 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. - [SDR MWEA011001](https://openairdocs.org/sdr/MWEA011001.md): Pressure Switch · failed · Jun 26, 2001 · N212ME · Doug DC932 · Engine Oil Pressure > ON 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 - [SDR MWEA010580](https://openairdocs.org/sdr/MWEA010580.md): Switch · inoperative · Apr 13, 2001 · N212ME · Doug DC932 · Landing Gear Brake System > TAKE OFF WARNING HORN CAME ON AT 105 KNOTS DURING TAKE OFF ROLL. ABORTED TAKE OFF. MAINTENANCE FOUND PARKING BRAKE SWITCH INOPERATIVE AND REPLACED SWITCH. - [SDR MWEA010512](https://openairdocs.org/sdr/MWEA010512.md): Transducer · inoperative · Apr 1, 2001 · N212ME · Doug DC932 · Stall Warning System > STALL INDICATOR FAILURE ANNUNCIATOR CAME ON AT CLIMBOUT WITH INTERMEDIATE WINDSHEAR INOP LIGHT. REPLACED LEFT ANGLE OF ATTACH VANE. - [SDR MWEA010161](https://openairdocs.org/sdr/MWEA010161.md): Clip · broken · Feb 19, 2001 · N212ME · Doug DC932 · Aerodynamic Fairings > TAIL CONE AFT INTERIOR HANDLE HAS A BROKEN CLIP AND FAILS PULL CHECK (25 - 35 LBS). REMOVED AND REPLACED CLIP. - [SDR MWEA010166](https://openairdocs.org/sdr/MWEA010166.md): Skin · dented · Feb 19, 2001 · N212ME · Doug DC932 · Rudder, Plate/Skin > RUDDER LEFT SKIN HAS.75 INCH BY.75 INCH DENT.010 INCH DEEP AT ZR 28.936. REMOVED AND REPLACED DOUBLER. - [SDR MWEA010165](https://openairdocs.org/sdr/MWEA010165.md): Skin · damaged · Feb 19, 2001 · N212ME · Doug DC932 · Fuselage Main, Plate/Skin > AFT 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. - [SDR MWEA010164](https://openairdocs.org/sdr/MWEA010164.md): Belt · corroded · Feb 19, 2001 · N212ME · Doug DC932 · Fuselage Main, Structure > NR 20 LEFT WINDOW FRAME CORRODED IN BOTH LOWER, INNER CORNERS. REMOVED AND REPLACED WINDOW BELT. - [SDR MWEA010162](https://openairdocs.org/sdr/MWEA010162.md): Panel · dented · Feb 19, 2001 · N212ME · Doug DC932 · Wing, Plate/Skin > LEFT WING UPPER TRAILING EDGE PANEL IS DENTED, STATION 419, 4 INCHES AFT OF REAR SPAR. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER. - [SDR MWEA010160](https://openairdocs.org/sdr/MWEA010160.md): Ring · cracked · Feb 19, 2001 · N212ME · Doug DC932 · Passenger Compartment Windows > LEFT WINDOW RING CRACKED, STATION 639 - 658. REMOVED AND REPLACED WINDOW RING. - [SDR MWEA010159](https://openairdocs.org/sdr/MWEA010159.md): Skin · dented · Feb 19, 2001 · N212ME · Doug DC932 · Fuselage Main, Plate/Skin > FUSELAGE SKIN DENTED STATION 980, 2 INCHES BELOW LONGERON 2 RIGHT. FABRICATED AND INSTALLED DOUBLER. - [SDR MWEA010154](https://openairdocs.org/sdr/MWEA010154.md): Web · cracked · Feb 13, 2001 · N212ME · Doug DC932 · Nacelle/Pylon, Main Frame > VERTICAL WEB CRACKED IN RIGHT PYLON OUTBOARD OF 13TH STRINGER. BLEED NUT ACCESSIBLE THROUGH PANEL 8204A. FABRICATED AND INSTALLED REPAIR DOUBLERS. - [SDR MWEA010153](https://openairdocs.org/sdr/MWEA010153.md): Longeron · corroded · Feb 13, 2001 · N212ME · Doug DC932 · Fuselage Main, Longeron/Stringer > CORROSION ON LONGERON 12 LEFT AT STATION 1104. FABRICATED AND INSTALLED LONGERON AND ANGLE. - [SDR MWEA010152](https://openairdocs.org/sdr/MWEA010152.md): Floor Panel · cracked · Feb 13, 2001 · N212ME · Doug DC932 · Fuselage Floor Panel > FLOOR PANEL E-6 IS CRACKED ON AFT OUTBOARD CORNER. FABRICATED AND INSTALLED DOUBLER. - [SDR MWEA010151](https://openairdocs.org/sdr/MWEA010151.md): Angle · cracked · Feb 13, 2001 · N212ME · Doug DC932 · Fuselage Miscellaneous Structure > CRACK AT STATION 1121 AT LONGERON 17 RIGHT. DRILLED AND INSTALLED REPAIR ANGLES. - [SDR MWEA010148](https://openairdocs.org/sdr/MWEA010148.md): Fitting · cracked · Feb 9, 2001 · N212ME · Doug DC932 · Nacelle/Pylon, Attach Fittings > FITTING CRACKED AT VERTICAL WEB AT LEFT ENGINE PYLON STRUCTURE, VIEWED THROUGH PANEL 8105A. REMOVED AND REPLACED FITTING. Next page: https://openairdocs.org/deregistered/N212ME-2003-12-17/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N212ME-2003-12-17/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.