Mcdonnell Douglas MD-11

Service difficulty reports · 7,956

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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 aircraft_model_key = 'MD11'
  ORDER BY difficulty_date DESC"

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SDR WRLA2007110Bracket · corrodedDURING 4C+12A CHECK, FOUND CABIN FLOOR PANEL SUPPORT BRACKET HAS CORROSION AT STA Y=1887 & X=-68. REPLACED WITH NEW PARTS PER MD-11 SRM 51-35-01 VOL.2 REV.40Oct 11, 2007 · N273WA · Doug MD11 · Fuselage Miscellaneous StructureSDR WRLA2007112Tee Fitting · corrodedDURING 4C+12A CHECK, FOUND STA Y=2007 X=57 BULKHEAD TEE CORRODED. REPLACED DAMAGED TEE PER MD11 SRM VOL.II 51-35-01 REV.40. REF EGAT NRC U05041.Oct 11, 2007 · N273WA · Doug MD11 · Fuselage Miscellaneous StructureSDR WRLA2007111Seat Track · crackedDURING 4C+12A CHECK, FOUND AFT CABIN LT FLOOR CURVED SEAT TRACK HAS CORROSION AT STA Y=1964, X=107.25. 10-23-07 REPAIRED THE AFT LT FLOOR CURVED SEAT TRACK PER MD-11 SRM VOL.I 53-70-00 FIG.1 REV.40.Oct 11, 2007 · N273WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS07M51250Structure · corrodedINSPECTION TYPE:C LT HOR STAB NR 1 BARREL NUT HOLE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-21-01V.2R.35. 10X MAGNIFICATION DETAILED VISUAL INSP C/OUT AND FOUND NO CORROSION EVIDENT. BARREL NUT BORE BOTTOM AND BLEND OUT PERIPHERY RADIUOct 10, 2007 · N292UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M51249Structure · corrodedINSPECTION TYPE:C RT HORIZ STAB NR 27 BARREL NUT HOLE FOUND CORRODED. CORROSION REMOVED AT BARREL NUT BORE PER SRM 51-21-01V.2R35.10X MAGNIFICATION DETAILED VISUAL INSP C/OUT FOUND NO CORROSION EVIDENT. BARREL NUT BORE BOTTOM AND BLEND OUT PERIPHERY RADIUS SOct 10, 2007 · N292UP · Doug MD11 · Horizontal Stabilizer StructureSDR WRLA2007109Seat Track · corrodedDURING 4C+12A CHECK, SEAT TRACK CORROSION FOUND AT STA X=-75.25 Y=1870. REPAIRED PER MD-11 SRM 53-70-00 VOL.1 FIG.1 REV.40.Oct 8, 2007 · N273WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2007108Longeron · corrodedDURING 4C+12A CHECK, LONGERON CORROSION FOUND AT STA 1953 L44R. 10-26-07 REPAIRED THE DAMAGED AREA PER MD11 SRM 53-10-00 VOL.I REV.40Oct 8, 2007 · N273WA · Doug MD11 · Fuselage Main, Longeron/StringerSDR WRLA2007107Seat Track · corrodedDURING 4C+12A CHECK, SEAT TRACK CORROSION FOUND AT STA X=-67 Y=517. 10-25-07 REPLACED DAMAGED SEAT TRACK PER MD-11 SRM VOL.I 53-70-00 FIG.8 REV.40.Oct 8, 2007 · N273WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2007106Skin · corrodedDURING 4C+12A CHECK, SEVERAL CORROSION AREAS WERE FOUND ON CENTER WING TANK UPPER SKIN AT XCW=-110 TO XCW=-106 BETWEEN S-15 TO S-22 AND STA XCW=107 BETWEEN S-18 TO S-15. 10-29-07 REPAIRED PER EGAT ENGINEERING INSTRUCTION W2007A57B-638 REV.00.Oct 8, 2007 · N273WA · Doug MD11 · Wing, Plate/SkinSDR WRLA2007104Unknown · odorFLT 1001 FNLU/KIAH. DURING CRUISE FLT 9+20HRS AFTER DEPART ELEC ODOR EMANATING NEAR INSTRUMENT PANEL. NO SMOKE WAS OBSERVED. SOURCE OF ODOR UNKNOWN. ELEC ODOR DISSIPATED OVER TIME. SEL ANNUNCIATOR LIGHT TEST IND MASTER WARNING, MASTER CAUTION AND ABS DISAOct 6, 2007 · N278WA · Doug MD11 · Air Distribution SystemSDR WRLA2007103Ballast · failedEDDP/OKBK ROW 10 & 11 SEATS A, B & C OVERHEAD CEILING LIGHT ABOVE & BEHIND LUGGAGE BIN WAS HOT WITH BURNING PLASTIC ODOR LIGHT WAS DISCONNECTED. 10-18-07 R & R BALLAST.Oct 5, 2007 · N804DE · Doug MD11 · Passenger Compartment LightingSDR WRLA2007102Skin · crackedDURING 4C + 12A CHECK FOUND RIGHT WING FIXED L/E SKIN CRACK AT CORNERS OF CUTOUT L=0.3 INCH, AT STA XOS 464 L=0.5 INCH STA XOS 470. 10-25-07 REPAIRED THE RT WING FIXED LEADING EDGE SKIN CRACK AT CORNERS OF CUTOUT AT STA XOS=464,470 PER MD11 SRM VOL.I 57-Oct 5, 2007 · N273WA · Doug MD11 · Wing, Plate/SkinSDR WRLA2007105Retainer · damagedDURING C-CHECK, FOUND NR 3 PYLON AFT LOWER FAIRING RETAINER DAMAGE. 10-29-07 ACCOMPLISHED ERA NUMBER 07-54-107. REPLACED NR 3 PYLON AFT LOWER FAIRING RETAINER.Oct 4, 2007 · N273WA · Doug MD11 · Nacelle/Pylon Miscellaneous StructureSDR UPS07M51231Web · scratchedINSPECTION TYPE:C PYLON NR 3 WIRING SUPPORT WEB WITH SCRATCHES ABOVE PRECOOLER. REMOVAL C/OUT TO ACCESS SCRATCHES MARK MENTIONED ABOVE, FOUND EXCEEDED LIMIT PER SRM 54-00-01,F1A, V1, .ORI THK 0.032", REMAIN THK 0.012". NEW WEB AT NR 3 PYLON FAB PER P/N AUB7Sep 26, 2007 · N292UP · Doug MD11 · Nacelle/Pylon, Main FrameSDR UPS07M51209Seat Track · corrodedINSPECTION TYPE:C MAIN DECK: FROM BS 820 TO BS 835 (LOCATION :NR 2 DOOR AREA), LT MOST O/B SEAT TRACK FLANGE AREAS FOUND CORRODED. CORROSION AT M/DECK FR BS 820-BS 835 OB SEAT TRACK FLANGE REMOVED PER SRM 51-21-01V.2R.35. FOUND EXCEED LIMIT PER SRM 53-70-00DSep 20, 2007 · N292UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2007090Connector · failedFLT 100 KIAH/FNLU ELECTRICAL ODOR/SMELL EMANATING FROM SEATS 25A-C DURING CRUISE. POWER PLUG SUPPLY PULLED C/B TO AFFECTED ZONES. 10-18-07 R & R 26A-C SEAT CONTROL BOX, REPAIRED DAL NR 68 & NR 14 REF WOA WO D10106.Sep 20, 2007 · N278WA · Doug MD11 · Electrical Power System WiringSDR 07FDEA03953Tee Fitting · corrodedAFTER BUSHING REMOVAL, LEFT HAND WING INBOARD FLAP VANE INBOARD TEE FITTING BORE FOUND CORRODED. LEFT HAND WING INBOARD FLAP VANE INBOARD TEE FITTING REMOVED AND REPLACED AS PER AMM 27- 50-22-4. FLAP OPERATION TEST CARRIED OUT AS PER AMM 27-50-00-860-80Sep 18, 2007 · N618FE · Doug MD11 · Wing, Attach FittingsSDR CO1Y200700007Truss Fitting · corrodedON ENGINE NR 1 FORWARD TRUSS FITTING, FOUND 4EA HOLES WITH CORROSION.Sep 14, 2007 · N702BC · Doug MD11 · Engine Mount SectionSDR CO1Y200700006Truss Fitting · corrodedON ENGINE NR 3 FORWARD TRUSS FITTING, FOUND 4EA HOLES WITH CORROSION.Sep 14, 2007 · N702BC · Doug MD11 · Engine Mount SectionSDR CO1Y200700005Beam · corrodedFOUND CORROSION ON BEAM P/N ADG7032-3.Sep 13, 2007 · N702BC · Doug MD11 · Cargo/Baggage DoorsSDR CO1Y200700003Skin · corrodedLT WING UPPER SURFACE ON SKIN FROM XORS 130 TO XORS 738 FOUND EXFOLIATION CORROSION.Sep 1, 2007 · N702BC · Doug MD11 · Wing, Plate/SkinSDR CO1Y200700004Skin · corrodedRT WING UPPER SURFACE FROM XORS 345 TO XORS 828 FOUND 15EA EXFOLIATION CORROSION POINTS.Sep 1, 2007 · N702BC · Doug MD11 · Wing, Plate/SkinSDR 07FDEA03064Bearing Race · migratedNR 3 PYLON AFT MOUNT BEARING AFT FACE OUTER RACE FOUND MIGRATED. 08-31-07 REMOVED AND REPLACED AS PER FEDEX E.A. 1-5410-112388. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 23, 2007 · N595FE · Doug MD11 · Engine Mount SectionSDR CO1Y200700002Doubler · corrodedMAIN CABIN FROM STA 1321 TO STA 1341 FROM L NR 13 TO L NR 14 RT SIDE ON DOUBLER FOUND CORROSION.Aug 18, 2007 · N702BC · Doug MD11 · Fuselage Main, Plate/SkinSDR CO1Y200700001Longeron · crackedCAC COMPARTMENT AT STA 6-100 ON LONGHERON NR 37LT SIDE FOUND CRACK 1 INCH.Aug 18, 2007 · N702BC · Doug MD11 · Fuselage Main, Longeron/StringerSDR WRLA2007081Engine · overtempKBGR/EINN, IN CRUISE FLIGHT EXPERIENCED MODERATE VIBRATION FOLLOWED BY LEVEL 2 ALERT SELECT FADEC ALT NR 3. RETARDED THROTTLE HALF WAY & SELECTED NR 3 FADEC TO ALT. EGT CONTINUED TO RISE. IN FLIGHT ENGINE SHUT DOWN CHECKLIST WAS ACCOMPLISHED. EMERGENCY DECAug 9, 2007 · N803DE · Doug MD11 · Engine (Turbine/Turboprop)SDR WRLA2007080Structure · crackedDURING 1C+12A CHECK, EGAT MAINT FOUND CRACK ON LT WING ANTI-ICING TELESCOPING DUCT DOOR CUTOUT AT STA XOS=464 & XOS=470. CRACK REPAIRED PER MD-11 SRM VOL 1 57-10-00 FIG 43 REV 39 & EI 2006P20A-124 REV 00. (REPAIR DOUBLER)Aug 4, 2007 · N801DE · Doug MD11 · Wing Miscellaneous StructureSDR WRLA2007079Oven · malfunctionedKBWI/LIMC FWD GALLEY OVENS MADE POPPING SOUND FOLLOWED BY ELECTRICAL SMELL WHILE COOKING. REMOVED POWER FROM OVENS BY PULLING C/B'S. RAN BOTH OVENS FOR ONE HOUR, BOTH OPERATED AS NORMAL IAW MM 25-31-50.Jul 9, 2007 · N801DE · Doug MD11 · Buffet/GalleysSDR 07FDEA02342Frame · dentedMAIN DECK CARGO, RIGHT FRAME 1641 AT STRINGER L12 FOUND DENT. REPAIR CARRIED OUT AT MAIN DECK CARGO, RIGHT FRAME 1641 AT STRINGER L12 AS PER SRM 53-30-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 29, 2007 · N593FE · Doug MD11 · Fuselage Main, FrameSDR 07FDEA02152Rib · crackedRT WING LEADING EDGE RIB NEAR XOS 762 FOUND CRACKED. [06-29-07] REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. RIB FABRICATED AS PER DOUGLAS DRAWING NR ARB2923. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.Jun 15, 2007 · N607FE · Doug MD11 · Wing, Rib/BulkheadSDR 07FDEA02110Longeron · damagedFUSELAGE, CAC COMPARTMENT AT STA 6-100, LONGERON 40L FOUND LONGERON WITH FREEZE PLUG INSTALLED. [06-19-07] REPAIR CARRIED OUT AT FUSELAGE - CAC COMPARTMENT AT STA 6-100, LONGERON 40L AS PER SRM 53 -10-00 FIGURE 2 VOLUME I.Jun 12, 2007 · N578FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 07FDEA02109Splice · damagedAFT CARGO RT L38, STA 1865 FOUND SPLICE DAMAGED. [06-18-07] REPAIR CARRIED OUT AS PER SRM 51-33-01 VOLUME II AND DRAWING AFA7105. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Jun 12, 2007 · N578FE · Doug MD11 · Fuselage Miscellaneous StructureSDR WRLA2007077Fan · noisyFLIGHT 8400 FORWARD CHILLER FAN NOISY - POSSIBLE SOURCE OF ELECTRICAL BURNING ODOR . NR 2 RADAR UNIT (FWD E/E) VERY HOT, POSSIBLE SOURCE OF ELECTRICAL BURNING ODOR. CHECKED CHILLER FOR CHAFED WIRES OR DAMAGE, NONE FOUND. NO ELECTRICAL BURNING ODOR, BUT CHILJun 11, 2007 · N801DE · Doug MD11 · Buffet/GalleysSDR UPS07M50286Longeron Splice · crackedINSPECTION TYPE:C CTR CGO STA 5-113 LONGERON 47 LONGERON SPLICE FITTING FOUND CRACKED AS MARKED NEW SPLICE FITTING FABRICATED PER DWG A5A7114 MATL USED:1D11047. FPI CARRIED OUT PER DPS4.707 REV AW AND FOUND NO CRACK EVIDENT. NEW SPLICE FASTENER HOLES PICK UPJun 8, 2007 · N260UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS07M50069Intercostal · crackedINSPECTION TYPE:C CABIN - FLOOR SUPPORT STRUCTURE STA 1887 - 1902, LBL 18 INTERCOSTAL FOUND CRACKED. CRACK AREA TRIMMED OUT PER SRM 53-00-01 FIG 6 VOL I REV38. HFEC INSP C/OUT FOUND 2 CRACKS APPROX 1" EACH. CRACK AREAS TRIMMED OUT PER SRM 53 -00-01 FIG 6 VOJun 8, 2007 · N288UP · Doug MD11 · Fuselage Miscellaneous StructureSDR 07FDEA02093Skin · corrodedTOP OF CENTER TANK RIGHT SIDE FOUND CORROSION AT STA 1219. CORROSION IN TOP OF CENTER TANK RIGHT SIDE AT STA 1219 CARRIED OUT REPAIR AS PER FEDEX EA NR 1-5710-111114, TITLE: WINGS, CENTER WING FUEL TANK RIGHT SIDE CORROSION REPAIR. REPAIR CLASSIFIED AS MAJJun 8, 2007 · N576FE · Doug MD11 · Wing, Plate/SkinSDR 07FDEA02084Floorbeam · noneEXISTING REPAIR, FUSELAGE STA 6-50 FLOORBEAM REPAIR AT RT BUTT LINE 60", AS SEEN FROM THE FWD LOWER CARGO COMPARTMENT, REPAIR REQUIRES EVALUATION. EXISTING REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-00-01 FIGURE 8 VOLUME I. REPAIR CLASSIJun 7, 2007 · N578FE · Doug MD11 · Fuselage Main, Floor BeamSDR UPS07M50093Frame · crackedINSPECTION TYPE:C AFT FUSELAGE, AFT PRESSURE BULKHEAD, AFT FACE STA 2007, RBL10', UPPER PORTION OF T CHORD FOUND WITH CRACK AT EDGE AS MARKED. AFT FUSELAGE, AFT PRESSURE BULKHEAD, AFT FACE STA 2007 RBL UPP PORTION REMOVED FOR ACCESS REPAIR PER SRM 51-21-01V.RJun 6, 2007 · N260UP · Doug MD11 · Fuselage Main, FrameSDR UPS07M50285Frame · corrodedINSPECTION TYPE:C AFT CGO STA 1841 APPROX LONGERON 44 AREA, FRAME FOUND WITH CORROSION AS MARKED. DAMAGED FRAME REMOVED PER SRM 51-31-01 V.2R.38. NEW FRAME FASTENER HOLES PICKED UP PER SRM51-31-01 V.2R.38. NEW FRAME REPROTECTED AND PAINT TOUCHED UP PER SRM Jun 5, 2007 · N260UP · Doug MD11 · Fuselage Main, FrameSDR 07FDEA02070Frame · noneEXISTING REPAIR, UPPER CARGO COMPARTMENT, LT SIDEWALL STRUCTURE FRAME AT STA 1701, L-12L, FOUND WITH REPAIR DOUBLER. EXISTING REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-Jun 4, 2007 · N578FE · Doug MD11 · Fuselage Main, FrameSDR 07FDEA02068Skin · damagedEXISTING REPAIR, RT WING I/B FLAP UPPER SURFACE FOUND EXISTING PATCH AT XIFH 217 YIFH 65. EXISTING REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 4, 2007 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA02065Skin · damagedEXISTING REPAIR, LT WING I/B FLAP UPPER SURFACE FOUND WITH EXTERNAL PATCH AT XIFH 233 YIFH 17. EXISTING REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 4, 2007 · N578FE · Doug MD11 · Trailing Edge FlapsSDR WRLA2007076Control Unit · smokeFNLU/KIAH FLT 101 05/31/07. SEAT 14G CONTROL INOPERATIVE. SMOKE AND ODOR COMING FROM SEAT WHEN SEAT ACTIVATED. ISOLATED TO POWER CONTROL UNIT. REMOVED POWER CONTROL UNIT, DEACTIVATED SEAT ELECTRICALLY AS PRECAUTIONARY MEASURE. PLACED SEAT ON DMI M25JU0107May 31, 2007 · N278WA · Doug MD11 · Passenger Compartment EquipmentSDR 07FDEA02038Spar Cap · corrodedRIGHT WING, TRAILING EDGE REAR SPAR LOWER CAP FOUND CORROSION AT XORS 1054. [06-18-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-109898. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.May 31, 2007 · N578FE · Doug MD11 · Wing SparSDR 07FDEA02037Spar Cap · corrodedRIGHT WING, TRAILING EDGE REAR SPAR LOWER CAP FOUND CORROSION AT XORS 1067. [06-19-07]May 31, 2007 · N578FE · Doug MD11 · Wing SparSDR 07FDEA02036Hinge · corrodedRIGHT WING, O/B FLAP O/B HINGE AFT FAIRING AFT STRUT FWD BOLT HOLE FOUND CORROSION. [06-18-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-109897. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.May 31, 2007 · N578FE · Doug MD11 · Trailing Edge FlapsSDR 07FDEA02035Seat Track · corrodedUPPER CARGO COMPARTMENT, SEAT TRACK RBL 75 CORRODED AT STA 1301 TO STA 1361. [06-18-07] REPAIR CARRIED OUT AT UPPER CARGO COMPARTMENT, SEAT TRACK RBL 75, STA 1267 TO STA 1391 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER May 31, 2007 · N578FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02034Skin · crackedLEFT WING, NR 1 LEADING EDGE SLAT I/B EDGE FOUND CRACK NEAR ALIGNMENT PIN HOLE. REPAIR CARRIED OUT PER FEDEX EA 1-5710-109891. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.May 31, 2007 · N578FE · Doug MD11 · Leading Edge DevicesSDR 07FDEA02032Control Valve · leakingAFTER 1 HR 30 MINUTES FLIGHT, A/C RETURN BACK TO STN DUE TO NR 3 HYD QTY LOW. FOUND HYD QTY 3 RESERVOIR DEPLETED TO 1.0 AND FOUND EXCESSIVE LEAK FROM THE NR 1 HORIZONTAL STABILIZER CONTROL VALVE UNION. REQUIRES UNION O- RINGS, EDP PUMP AND FILTER MODULE. REMay 31, 2007 · N527FE · Doug MD11 · Rudder Control SystemSDR 07FDEA02014Support · crackedLEFT WING FIXED LEADING EDGE CAVITY INTERIOR UPPER FACE, XORS 562, SUPPORT STRIP FOUND CRACKED. REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5710-111112. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.May 29, 2007 · N576FE · Doug MD11 · Wing Main, Frame Structure
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