Boeing MD-11F

Service difficulty reports · 31,317

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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 = 'MD11F'
  ORDER BY difficulty_date DESC"

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SDR IPXA2020062967017Skin · corrodedINSPECTION TYPE:2CCENTER WING BOX UPPER SKIN AT STRINGER 3 AND XCW 101 HAS CORROSION.REPAIRED CENTER WING BOX UPPER SKIN CORROSION AT STRINGER 3 AND XCW 101 IAW VT-SAA EA 011-5730-01-A8361 REV IR AND UPS EO MD11-5730-77002-A. (MINOR)Jun 10, 2020 · N257UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020072057976Cargo Track · corrodedINSPECTION TYPE:3C, RIGHT SIDE O/B SEAT TRACK HAS CORROSION UNDERNEATH FASTENER HOLES BETWEEN STA 1530 AND 1545 X = -107.REPAIRED CORRODED SEAT TRACK IN MAIN CARGO BETWEEN STA 1530 - 1572.5 X= -107 IAW SRM 53-00-52 REPAIR 1 FIG 201 REV.66. (MAJOR)Jun 9, 2020 · N262UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020071091163Frame · crackedEMPENNAGE - ACCESS PANEL 364QR FOUND CUT OUT CRACKED UPON PANEL REMOVAL. AT STATION 2164 RIGHT HAND ZID = 75.5 , XID = 9.0 . EMPENNAGE ACCESS PANEL 364QR AT STATION 2164 RIGHT HAND ZID = 75.5 , XID = 9.0 CRACKED SKIN PANEL REMOVED PER SRM 51-31-01-OG . NEWJun 9, 2020 · N617FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA2020071091162Frame · crackedEMPENNAGE - ACCESS PANEL 363ML FOUND CUT OUT CRACKED UPON PANEL REMOVAL. AT STATION 2164 LEFT HAND , ZID = 72.0 , XID = 9.0 . ACCESS PANEL 363ML AT STATION 2164 LEFT HAND ZID = 72.0 XID = 9.0 CRACK FRAME REMOVED AND REPLACED AS PER EA # 1-5500-T0354594P1.Jun 9, 2020 · N617FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA2020062391159Floorbeam · damagedAGING AIRCRAFT - EXISTING REPAIR FOUND AT CENTER CARGO COMPARTMENT FLOORBEAM WEB STATION 1841 BETWEEN X = - 30 TO X = - 57. EXISTING REPAIR AT CENTER CARGO COMPARTMENT FLOORBEAM WEB AT STA 1841 BETWEEN X= -30 TO X= -57 EVALUATED AND FOUND DAMAGE AT WEB AREA SJun 9, 2020 · N602FE · Doug MD11F · Fuselage Main, Floor BeamSDR FDEA2020062391155Doubler · damagedAGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE UPPER SKIN XIS 247. EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE UPPER SKIN XIS 247 EVALUATED AND FOUND EXISTING REPAIR DOUBLER DAMAGED. LEFT HAND WING FIXED LEADING EDGE XIS 2Jun 9, 2020 · N602FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2020061756622Beam · crackedINSPECTION TYPE:2C RT O/B FLAP I/B HINGE AFT I/B FRAME IS CRACKED. REMOVED, FABRICATED AND REPLACED BEAM IAW DWG ARC2149 AND SRM 51-33-01. (MINOR)Jun 9, 2020 · N276UP · Doug MD11F · Trailing Edge FlapsSDR FDEA2020061091163Skin · crackedEMPENNAGE - ACCESS PANEL 364QR FOUND CUT OUT CRACKED UPON PANEL REMOVAL.Jun 9, 2020 · N617FE · Doug MD11F · Vertical Stabilizer, Plate/SkinSDR FDEA2020061091162Skin · crackedEMPENNAGE ACCESS PANEL 363ML FOUND CUT OUT CRACKED UPON PANEL REMOVAL. ACCESS PANEL 363ML AT STATION 2164 LEFT HAND ZID 72.0 CRACK FRAME REMOVED AND REPLACED AS PER EA 1-5500-T0354594 TITLE : STABILIZERS - GENERAL - PYLON CARRY THRU PANEL FRAME AJC 7593-51 ALJun 9, 2020 · N617FE · Doug MD11F · Vertical Stabilizer, Plate/SkinSDR IPXA2020062977048Attach Fitting · migratedINSPECTION TYPE:2CLT I/B AILERON ACTUATOR ATTACH FITTING I/B BUSHING IS MIGRATED.REPAIRED LT I/B AILERON ACTUATOR ATTACH FITTING I/B MIGRATED BUSHING IAW VT-SAA EA 011-5751-01-A8375 REV. IR AND UPS EO MD11-5750-76997-A. (MINOR)Jun 8, 2020 · N257UP · Doug MD11F · AileronsSDR IPXA2020062657012Bushing · migratedINSPECTION TYPE:2C RT I/B AILERON ACTUATOR MOUNT FITTING BOTH BUSHINGS ARE MIGRATED. REPAIRED RT I/B AILERON ACTUATOR MOUNT FITTING MIGRATED BUSHINGS IAW EA 011-5752-01-A8355 REV IR AND EO MD11-5750-76992-A. (MINOR)Jun 8, 2020 · N257UP · Doug MD11F · AileronsSDR FDEA202006081150Floor Panel · damagedCABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL 231EF TOP SURFACE DAMAGED AT STATION 495 TO STATION 595 LEFT HAND SIDE. DAMAGED FLOOR PANEL REMOVED AS PER AMM 53-21-04. FLOOR PANEL 231EF FABRICATED AS PER DWG SRZ-25-005 REV R. FABRICATED FLOOR PANEL 231EF IJun 8, 2020 · N620FE · Doug MD11F · Fuselage Floor PanelSDR 9WGA2020060988101Flight Dir · failedLEVEL FCC 2A DATA FAULT. ASSOCIATED FD 2 FAILED, SWITCHED SOURCE TO NR 1.Jun 8, 2020 · N581JN · Doug MD11F · Autopilot SystemSDR FDEA202006081149Floor Panel · damagedCABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL 231 HF TOP SURFACE DAMAGED AT STATION 595 TO STATION 675 LEFT HAND SIDE. DAMAGED FLOOR PANEL 231 HF AT CABIN STATION 595 - STATION 675 (LT) REMOVED AS PER AMM 53-21-04. FLOOR PANEL 231 HF FABRICATED AS PER DWG SJun 8, 2020 · N620FE · Doug MD11F · Fuselage Floor PanelSDR IPXA2020070157206Bushing · migratedINSPECTION TYPE:2C RT I/B ELEVATOR NR 3 HINGE FITTING I/B BUSHING IS MIGRATED. REPAIRED RT I/B ELEVATOR NR 3 HINGE FITTING I/B MIGRATED BUSHING IAW EA 011-5520-01-A8366 REV IR AND EO MD11-5520-76960-A. (MINOR)Jun 7, 2020 · N257UP · Doug MD11F · Elevator StructureSDR IPXA2020070157204Hinge Fitting · damagedINSPECTION TYPE:2C RT DETACHABE ELEVATOR NR 1A HINGE FITTING IS DAMAGED. REMOVED AND REPLACED RT DETACHABLE ELEVATOR IAW EO MD11-2700-74700-C. (MINOR)Jun 7, 2020 · N257UP · Doug MD11F · Elevator StructureSDR IPXA2020070157203Bushing · migratedINSPECTION TYPE:2C RT I/B ELEVATOR NR 2 HINGE FITTING I/B BUSHING IS MIGRATED. REPAIRED RT I/B ELEVATOR NR 2 HINGE FITTING I/B MIGRATED BUSHING IAW EA 011-5520-01-A8362 REV IR AND EO MD11-5520-76980-A. (MINOR)Jun 7, 2020 · N257UP · Doug MD11F · Elevator StructureSDR IPXA2020062967024Fitting · migratedINSPECTION TYPE:2CLT I/B ELEVATOR #2 HINGE FITTING A/C SIDE I/B BUSHING IS MIGRATED.REPAIRED LT I/B ELEVATOR #2 HINGE FITTING A/C SIDE MIGRATED BUSHING IAW VT-SAA EA 011-5520-01-A8363 REV IR AND UPS EO MD11-5520-76970-A. (MINOR)Jun 7, 2020 · N257UP · Doug MD11F · Elevator StructureSDR IPXA2020061976699Longeron Splice · crackedINSPECTION TYPE:2C, CENTER CARGO LONGERON 48L SPLICE ANGLE BETWEEN STA 5-113 - 1541 IS CRACKED/CORRODED.FABRICATED REPLACEMENT LONGERON 48L SPLICE ANGLE BETWEEN STA 5-113 - 1541 IAW DAC DWG A5A7124. INSTALLED ON NRC 423387. (MINOR).Jun 7, 2020 · N257UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2020061756680Fitting · wornINSPECTION TYPE:2C LT DETACHABLE ELEVATOR IB CAM FITTING IS WORN. REPAIRED LT DETACHABLE ELEVATOR WORN IB CAM FITTING IAW EA 011-5520-01-A8342 REV IR AND EO MD11-5520-76847-A. (MINOR)Jun 7, 2020 · N257UP · Doug MD11F · Elevator Miscellaneous StructureSDR IPXA2020061756679Fitting · wornINSPECTION TYPE:2C LT IB ELEVATOR OB CAM FITTING IS WORN. REPAIRED LT IB ELEVATOR WORN OB CAM FITTING IAW EA 011-5520-01-A8342 REV IR AND EO MD11-5520-76847-A. (MINOR)Jun 7, 2020 · N257UP · Doug MD11F · Elevator Miscellaneous StructureSDR IPXA2020061756678Fitting · wornINSPECTION TYPE:2C RT OB ELEVATOR CAM FITTING IS WORN IB OF NR 9 BEARING. REPAIRED RT OB ELEVATOR WORN CAM FITTING IB OF NR 9 BEARING IAW EA 011-5520-01-A8342 REV IR AND EO MD11-5520-76847-A. (MINOR)Jun 7, 2020 · N257UP · Doug MD11F · Elevator Miscellaneous StructureSDR IPXA2020061756677Fitting · wornINSPECTION TYPE:2C LT OB ELEVATOR CAM FITTING IS WORN OB OF NR 7 BEARING. REPAIRED LT OB ELEVATOR WORN CAM FITTING OB OF NR 7 BEARING IAW EA 011-5520-01-A8342 REV IR AND EO MD11-5520-76847-A. (MINOR)Jun 7, 2020 · N257UP · Doug MD11F · Elevator Miscellaneous StructureSDR FDEA2020060871143Hinge · damagedCENTER CARGO COMPARTMENT DOOR SIDE HINGE MOST AFT 2 EACH HOLES FOUND EXCEEDED MAXIMUM DIAMETER LIMIT. CENTER CARGO COMPARTMENT DOOR SIDE HINGE MOST AFT 2 EACH HOLES REWORKED AS PER SRM 52-30-16-1A FIGURE 101 SHEET 1 AND FOUND HOLES EXCEEDED LIMIT. REPAIR BUSHIJun 7, 2020 · N620FE · Doug MD11F · Cargo/Baggage DoorsSDR 9WGA2020060874101Unknown · vibrationRETURNED BACK TO ANC SECOND TIME. PASSING 1000 FEET, LOUD BANG SHOOK WHOLE AIRPLANE AND FLIGHT CONTROLS.Jun 7, 2020 · N411SN · Doug MD11F · Fuselage Structure (General)SDR IPXA2020062967023Rib · crackedINSPECTION TYPE:2CEXTENDED TAILCONE L/H FAIRING SUPPORT RIB IS CRACKED.REMOVED AND REPLACED CRACKED EXTENDED TAILCONE L/H FAIRING SUPPORT RIB IAW MD-11 SRM 51-31-01 & 51-35-01. (MINOR)Jun 6, 2020 · N257UP · Doug MD11F · Fuselage Main, StructureSDR FDEA2020060861138Skin · chafedCENTER CARGO COMPARTMENT DOOR FORWARD LOWER CORNER DOOR STATION 1640 FOUND CHAFING. CHAFING DAMAGE REPAIRED AS PER ENGINEERING AUTHORIZATION 1-5230-T0354334 PART 1 TITLE " DOORS - CARGO DOOR / HYD SYS - CENTER CARGO DOOR - DAMAGES FOUND ON OUTER SKIN AND INNERJun 6, 2020 · N620FE · Doug MD11F · Cargo/Baggage DoorsSDR FDEA2020060861137Door Frame · corrodedAFT CARGO COMPARTMENT DOOR AFT JAMB STATION 1959 FOUND CORRODED. AFT CARGO COMPARTMENT DOOR AFT JAMB CORRODED FRAME AT STATION 1959 REMOVED AND REPLACED WITH NEW FRAME AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jun 6, 2020 · N620FE · Doug MD11F · Fuselage Main, StructureSDR 9WGA2020060641101Unknown · vibrationRETURN TO ANC DUE TO STRONG VIBRATIONS OF FRONT FUSELAGE.Jun 6, 2020 · N411SN · Doug MD11F · Fuselage Structure (General)SDR IPXA2020070157158Frame · damagedINSPECTION TYPE:2C TAIL CONE LT PATIO DOOR AFT FRAME IS BENT AND DAMAGED. REMOVED, FABRICATED AND REPLACED FRAME IAW DWG AKC7820 AND SRM 51-35-01. (MINOR)Jun 5, 2020 · N257UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2020062977046Frame · crackedINSPECTION TYPE:2CFWD TAILCONE AFT R/H FRAME HAS 2 CRACKS IN RADIUS AT UPPER AND LOWER LATCH FITTINGS.REMOVED AND REPLACED CRACKED FWD TAILCONE AFT R/H FRAME IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)Jun 5, 2020 · N257UP · Doug MD11F · Fuselage Main, FrameSDR IPXA2020062656961Intercostal · crackedINSPECTION TYPE:2C LOWER VERTICAL STABILIZER REAR CENTER SPAR TO LOWER PANEL INTERCOSTAL RT SIDE IS CRACKED AT STA YID= 375 AND XID= -7.1. REPAIRED CRACKED LOWER VERTICAL STABILIZER REAR CENTER SPAR TO LOWER PANEL INTERCOSTAL RT SIDE AT STA YID= 375 AND XID= Jun 5, 2020 · N257UP · Doug MD11F · Vertical Stabilizer Miscellaneous StructureSDR IPXA2020062656972Cap · crackedINSPECTION TYPE:2C RT UNDER WING CANTED PANEL CAP IS CRACKED AT STA 1236.8 AND Z= -100. REPAIRED CRACKED RT UNDER WING CANTED PANEL CAP AT STA 1236.8 AND Z= -100 IAW EO MD11-5310-76799-A. (MAJOR)Jun 5, 2020 · N257UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020062456949Frame · chafedINSPECTION TYPE:2CTAILCONE FWD UPPER FRAME (BEAM) IS CHAFED IN 4 AREAS.REPAIRED TAILCONE FWD UPPER FRAME (BEAM) CHAFE DAMAGE IAW MD-11 SRM 53-00-00 FIG. 210. (MINOR)Jun 5, 2020 · N257UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2020062957109Cap · corrodedINSPECTION TYPE:2CL/H WING T/E LOWER CAP HAS CORROSION BETWEEN STA. XW= 276.029 TO XW= 328.00.REPAIRED CORRODED L/H WING T/E LOWER CAP BETWEEN STA XW= 276.029 TO XW= 328.00 IAW SRM 57-50-02 REPAIR 9 FIG. 201. (MAJOR)Jun 4, 2020 · N257UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2020062967022Support · crackedINSPECTION TYPE:2CLT WING I/B FLAP I/B HINGE FWD O/B UPPER SUPPORT IS CRACKED.REMOVED AND REPLACED CRACKED LT WING I/B FLAP I/B HINGE FWD O/B UPPER SUPPORT IAW MD-11 SRM 51-33-01 & 51-35-01. (MINOR)Jun 4, 2020 · N257UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2020062657011Longeron · corrodedINSPECTION TYPE:2C CENTER CARGO LONGERON 48L IS CORRODED BETWEEN STA 1531 TO 1551. REPAIRED CORRODED LONGERON 48L BETWEEN STA 1531 TO 1551 IAW EA 011-5310-01-A8338 REV I/R AND EO MD11-5310-76915-A. (MAJOR)Jun 4, 2020 · N257UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2020062656973Longeron · corrodedINSPECTION TYPE:2C CENTER CARGO LONGERON 44R HAS CORROSION AT STA 1611. REPAIRED CORRODED LONGERON 44R BETWEEN STA 1610 TO 1632 IAW SRM 53-00-05 REPAIR 1 FIG 201. (MAJOR)Jun 4, 2020 · N257UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2020062256792Skin · gougedINSPECTION TYPE:2C LT I/B AILERON LOWER L/E SKIN IS GOUGED AT O/B END. REMOVED AND REPLACED GOUGED LT I/B AILERON LOWER L/E SKIN IAW SRM 51-31-01. (MINOR)Jun 4, 2020 · N257UP · Doug MD11F · AileronsSDR IPXA2020061756676Longeron · corrodedINSPECTION TYPE:2C CENTER CARGO LONGERON 48R HAS EXFOLIATION CORROSION AT APPROX STA 1609. REPAIRED CENTER CARGO LONGERON 48R CORROSION BETWEEN STA 1601 - 1621 IAW EA 011-5310-01-A8330 REV IR AND EO MD11-5310-76874-A. (MINOR)Jun 4, 2020 · N257UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA2020060541125Longeron Splice · crackedCENTER CARGO COMPARTMENT, UPON REMOVAL OF LONGERON ACCESS LONGERON SPLICE AT STATION 1531 LONGERON 39 RIGHT HAND FOUND CRACK. LONGERON SPLCE REMOVED AND REPLACED AS PER SRM 51-33-01-0G. LONGERON SPLICE FABRICATED AS PER DRAWING A5A7114 , REVISION J. REPAIR CLAJun 4, 2020 · N620FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2020070357253Angle · crackedINSPECTION TYPE:3C LT WING T ANGLE SUPPORT BETWEEN UPPER AND LOWER T/E SKIN IS CRACKED APPROX 12" FWD OF O/B L/E I/B AILERON. REMOVED CRACKED T ANGLE, FABRICATED AND INSTALLED ON LT WING BETWEEN UPPER AND LOWER T/E SKIN 12" FWD OF O/B L/E OF I/B AILERON IAW SJun 3, 2020 · N262UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2020070157194Doubler · crackedINSPECTION TYPE:3C BEADED DOUBLER ON LT WING FIXED L/E IS CRACKED AROUND FASTENER HOLES AT STA XORS 616. REPAIRED CRACKED BEADED DOUBLER AT LT WING FIXED L/E AT STA XORS-616 IAW SRM 57-40-02 REPAIR 15 FIG 205 REV 66. (MAJOR)Jun 3, 2020 · N262UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020062977054Doubler · crackedINSPECTION TYPE:3C, BEADED DOUBLER ON FIXED LE IS CRACKED ON LH WING XOS=637 TO XOS=643 INSIDE FUEL ACCESS PANEL 519CB.REPAIRED CRACKED BEADED DOUBLER ON LH WING FIXED L/E BETWEEN XOS=637 TO XOS=643 INSIDE FUEL ACCESS PANEL 519CB IAW SRM 57-40-02 REPAIR 15 FIGJun 3, 2020 · N262UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020062977051Doubler · crackedINSPECTION TYPE:3C, RH WING O/B FLAP UPPER SURFACE I/B FWD CORNER PRODUCTION DOUBLER IS CRACKED.REMOVED CRACKED DOUBLER, FABRICATED AND INSTALLED IN RH WING O/B FLAP UPPER SURFACE I/B FWD CORNER IAW DRWG NRC6753. (MINOR)Jun 3, 2020 · N262UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2020062967021Beam · crackedINSPECTION TYPE:2C, RT WING O/B FLAP I/B FWD HINGE FAIRING BEAM IS CRACKED.REMOVED AND REPLACED CRACKED RT WING O/B FLAP I/B FWD HINGE FAIRING BEAM IAW MD-11 SRM 51-33-01. (MINOR)Jun 3, 2020 · N257UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2020062256823Skin · crackedINSPECTION TYPE:3C LT WING FIXED L/E LOWER SKIN HAS A CRACK AROUND NR 11 SLAT TRACK AT STA XOS 717. REPAIRED CRACKED LT WING L/E LOWER SKIN AROUND NR 11 SLAT TRACK AT STA XOS 717 IAW SRM 57-40-02 REPAIR 7, FIG 201. (MAJOR)Jun 3, 2020 · N262UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020062256791Intercostal · crackedINSPECTION TYPE:2C TAILCONE INTERCOSTAL IS CRACKED AT FWD UPPER GUIDE PIN. REMOVED AND REPLACED CRACKED INTERCOSTAL AT UPPER FWD TAILCONE GUIDE PIN IAW SRM 51-33-01 AND 51-35-01. (MINOR)Jun 3, 2020 · N257UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2020062256864Skin · crackedINSPECTION TYPE:2C LT OUTER WING LOWER FUEL ACCESS PANEL (536AB) LANDING HAS 8 EA FASTENER HOLES CRACKED BETWEEN STA XORS 683.40 TO 713.65. REPAIRED CRACKED LT OUTER WING LOWER FUEL ACCESS PANEL (536AB) LANDING BETWEEN STA XORS 683.40 TO 713.65 IAW SRM 57-20-Jun 3, 2020 · N257UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020062256863Skin · crackedINSPECTION TYPE:2C RT OUTER WING LOWER FUEL ACCESS PANEL( 636AB) LANDING HAS 7EA FASTENER HOLES CRACKED BETWEEN STA XORS 683.40 TO 713.65. REPAIRED CRACKED RT OUTER WING LOWER FUEL ACCESS PANEL LANDING BETWEEN STA XORS 683.40 TO 713.65 IAW SRM 57-20-05 REPAIRJun 3, 2020 · N257UP · Doug MD11F · Wing, Plate/Skin
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