Boeing MD-11F

Service difficulty reports · 31,320

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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 FDEA201806131468Seat Track · crackedFWD CABIN SEAT TRACK FOUND CRACKED AT BS 635 LBL 8.5. REPLACED THE SEAT TRACK BETWEEN BS 625 - 665 IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 13, 2018 · N578FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201806131467Seat Track · corrodedCABIN, MAIN DECK CARGO SEAT TRACK CORRODED, BS 1311, RBL 27.5. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED, BS 1266 TO 1331 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR Jun 13, 2018 · N578FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2018062093832Fitting · corrodedRIGID CARGO BARRIER FLOOR FITTING NR 1 HAD CORROSION. REMOVED AND REPLACED THE RIGID CARGO BARRIER FLOOR FITTING IAW EO MD11-2520-58701-D.Jun 12, 2018 · N279UP · Doug MD11F · Fuselage Main, Attach FittingsSDR FDEA201806121456Web · crackedBS 1841, LONGERON 46L WEB WAS FOUND CRACKED. REPAIRED IAW SRM 53-00-00-2R, FIGURE 211, REPAIR GENERAL. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 12, 2018 · N578FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201806121455Web · crackedBS 1841, LONGERON 46R WEB WAS FOUND CRACKED. REPAIRED IAW SRM 53-00-00-2R, FIGURE 211, REPAIR GENERAL. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 12, 2018 · N578FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201806121454Seal · chafedRT WING DROOP LEADING EDGE INBD METAL SEAL CHAFED AT STA XDLE 310. REPAIR CARRIED OUT AT R WING DROOP LEADING EDGE INBD SIDE AS PER SRM 57-40-01-2R FIGURE 202 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 12, 2018 · N578FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201806121450Doubler · crackedLT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 663 FOUND CRACKED. REPAIR CARRIED OUT AT LT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 663 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 12, 2018 · N578FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201806121449Doubler · crackedRT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 613 WAS FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 12, 2018 · N578FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2018070231236Barrier · corrodedINSPECTION TYPE:2C, RIGID CARGO BARRIER WALL LOWER FWD. FACE HAS CORROSION AT STA 488.812 AND BETWEEN X=-54 THRU X=-78 AND Z=-19. REPAIRED CORRODED RIGID CARGO BARRIER WALL LOWER FWD FACE AT STA 488.812 AND BETWEEN X=-54 THRU X=-78 AND Z=-19 IAW EA 011-5310-01Jun 11, 2018 · N279UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2018062983162Beam · crackedFWD CARGO BAY SUB FLOOR, LT HORIZONTAL BEAM WAS CRACKED AT STA 6-73, ABOVE LONGERON 43L. REMOVED AND REPLACED THE HORIZONTAL BEAM IAW SRM 51-31-01, 51-33-01, AND 51-35-01.Jun 11, 2018 · N279UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2018062531031Stiffener · crackedFWD CARGO BAY SUB FLOOR BEAM, VERTICAL STIFFNER ANGLE WAS CRACKED AT BS 6-70, ABOVE LONGERON 43L. REMOVED, FABRICATED, AND REPLACED THE STIFFNER IAW DWG A6A7092, AND SRM 51-33-01.Jun 11, 2018 · N279UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2018062543988Floor Panel · corrodedMAIN CABIN BS 460 - 475, FLOOR PANEL WAS CORRODED AT RIGID CARGO BARRIER FLOOR FITTING NR 7. REMOVED AND REPLACED THE FLOOR PANEL IAW EO MD11-2520-58701-D.Jun 11, 2018 · N279UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2018062093834Fitting · corrodedRIGID CARGO BARRIER FLOOR FITTING NR 7 HAD CORROSION. REMOVED AND REPLACED THE RIGID CARGO BARRIER FLOOR FITTING IAW EO MD11-2520-58701-D.Jun 11, 2018 · N279UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2018061430668Flap · crackedINSPECTION TYPE:2C, RT IB FLAP T/E SPLIT AT STA XIFH183. REPAIRED FLAP T/E PER SRM 57-50-02 REPAIR 2 AND SRM 51-62-01. (MINOR)Jun 11, 2018 · N279UP · Doug MD11F · Trailing Edge FlapsSDR FDEA201806111445Pdu · failedFWD CARGO COMPARTMENT, "BRAKE ROWS 1,2,7,8,9" CB POPPED AND WILL NOT RESET. FOUND FWD CARGO COMPARTMENT 2L LONGITUDINAL PDU ROLLER M1-2457 TO BE INTERNALLY SHORTED (PIN E TO PIN F). REPLACED NR 2 PDU, OP CHECK GOOD. CB REMAINS SET, MM25-57-10-4-2, WDM 25-52-0Jun 11, 2018 · N610FE · Doug MD11F · Cargo CompartmentsSDR IPXA2018062983161Longeron · corrodedCENTER CARGO, BS 1551 CENTERLINE LONGERON 52 HAD CORROSION, INBD OF THE DRAIN. REMOVED AND REPLACED THE DAMAGED SECTION OF LONGERON BETWEEN BS 1531 - 1561 IAW SRM 51-31-01, 51-33-01, AND 53-50-05.Jun 10, 2018 · N279UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2018062230942Stiffener · chafedTAIL CONE UPPER PATIO DOOR LT SIDE STIFFNER ANGLE, BEHIND SPRING SEAL HAD DEEP WEAR. REMOVED, FABRICATED, AND REPLACED THE STIFFNER ANGLE IAW DWG AKC7868, AND SRM 51-31-01.Jun 10, 2018 · N279UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2018061130480Solenoid · intermittentR1 DOOR ACTAUTOR WAS INTERMITTENT. FOUND THE R1 DOOR LOCK RELEASE SOLENOID WAS INTERMITTENT THROUGH A1 TO A2, REPLACED THE SOLENOID IAW 52-730 IAW MM 52-10-06. FUNTIONAL TESTED GOOD.Jun 10, 2018 · N258UP · Doug MD11F · Service DoorsSDR IPXA2018061430669Flap · crackedINSPECTION TYPE:2C, LT IB FLAP T/E SPLIT AT STA XIFH 233. REPAIRED FLAP T/E PER SRM 57-50-02 REPAIR 2 AND 51-62-01. (MINOR)Jun 10, 2018 · N279UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2018062543986Longeron Splice · crackedMAIN CABIN LONGERON SPLICE 14R WAS CRACKED AT BS 1321. REMOVED, FABRICATED, AND REPLACED THE LONGERON SPLICE IAW DWG AEA7600, AND SRM 51-33-01.Jun 9, 2018 · N279UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2018062543987Tee Fitting · crackedMAIN CABIN LONGERON 15L TEE FITTING WAS CRACKED AT BS 1340. REMOVED, FABRICATED, AND REPLACED THE LONGERON IAW DWG AEA7568, AND SRM 51-33-01.Jun 9, 2018 · N279UP · Doug MD11F · Fuselage Main, Attach FittingsSDR FDEA2018061201433Frame · chafedMAIN DECK CARGO, FRAME CHAFED AT BS 535, LONGERON 24R. THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 9, 2018 · N578FE · Doug MD11F · Fuselage Main, FrameSDR FDEA2018061201432Frame · chafedMAIN DECK CARGO FRAME WAS CHAFED AT BS 535, LONGERON 19R. REPAIRED THE FRAME IAW SRM 53-20-07-2R, FIGURE 202, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 9, 2018 · N578FE · Doug MD11F · Fuselage Main, FrameSDR IPXA2018062213929Longeron · crackedMAIN CABIN LONGERON 18L WAS CRACKED BETWEEN BS 1159 - 1179. REMOVED, FABRICATED, AND REPLACED THE LONGERON IAW DWG AEA0220, AND SRM 51-33-01.Jun 9, 2018 · N279UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2018062230940Tee Fitting · crackedMAIN CABIN LONGERON 15R, TEE FITTING WAS CRACKED AT BS 1340. REMOVED, FABRICATED, AND REPLACED THE LONGERON TEE FITTING IAW DWG AEA7568, AND SRM 51-33-01.Jun 9, 2018 · N279UP · Doug MD11F · Fuselage Main, Attach FittingsSDR SRXR201806090051Channel · corrodedFWD CARGO COMPARTMENT FLOOR CHANNEL IS CORRODED AT STA 999 X=47.75. ACCOMPLISHED REPAIR ON FWD CARGO COMPARTMENT FLOOR CHANNEL AT STA 999 X=47.75 PER EA 011-5310-52-A7272 I/R.Jun 9, 2018 · N415JN · Doug MD11F · Fuselage Miscellaneous StructureSDR SRXR201806090050Longeron · corrodedCENTER FUSELAGE/LONGERON 28R STA 1361 TO STA 1401 HAS CORROSION. ACCOMPLISHED REPAIR ON CENTER FUSELAGE LONGERON 28R BETWEEN STA 1361 TO STA 1401 PER EA 011-5340-52-A7249 I/R REF NRC A040825.Jun 9, 2018 · N415JN · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2018063031234Tail Cone · wornINSPECTION TYPE:2C, TAIL CONE STA 2165.6 HAS DEEP WEAR AT BX=-36.5 AND BETWEEN Z=-35 TO Z=-61.5. REPAIRED TAIL CONE AT SAID LOCATION IAW EA 011-5320-01-A7307 REV I/R AND EO MD11-5350-68943-A. (MINOR)Jun 8, 2018 · N279UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2018062523958Skin · chafedNR 2 ENGINE, LT THRUST REVERSER AFT FIXED INNER BARREL ,OUTER SKIN IS CHAFED THROUGH. REPAIRED THE THRUST REVERSER SKIN IAW EA 011-7830-01-A7303, REV I/R, AND EO MD11-7830-68965-A.Jun 8, 2018 · N281UP · Doug MD11F · Engine Thrust ReverserSDR IPXA2018062523959Skin · chafedNR 2 ENGINE, RT THRUST REVERSER AFT FIXED INNER BARREL OUTER SKIN WAS CHAFED. REPAIRED THE THRUST REVERSER IAW EA 011-7830-01-A7306, REV IR, AND EO MD11-7830-68966-A.Jun 8, 2018 · N281UP · Doug MD11F · Engine Thrust ReverserSDR IPXA2018062543991Doubler · crackedRT WING FIXED L/E BEADED DOUBLER WAS CRACKED AT XOS 494 - 500. REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 205. MAJOR.Jun 8, 2018 · N279UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2018062213930Angle · crackedRT WING NR 2 SLAT OTBD EDGE ANGLE WAS CRACKED. REMOVED, FABRICATED, AND REPLACED THE ANGLE IAW DWG ARB1647, AND SRM 5135-01.Jun 8, 2018 · N279UP · Doug MD11F · Leading Edge DevicesSDR IPXA2018062230941Intercostal · crackedTAIL CONE RT CENTER GUIDE PIN ATTACH INTERCOSTAL AND PLATE WERE CRACKED. REMOVED, FABRICATED, AND REPLACED THE INTERCOSTAL AND DOUBLER IAW DWG AKC7520, AND SRM 53-80-07, REPAIR 7.Jun 8, 2018 · N279UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2018062093825Doubler · crackedLEFT UNDERWING ACCESS PANEL LANDING WAS CRACKED AT XORS 542. REMOVED, FABRICATED, AND REPLACED THE ACCESS PANEL LANDING DOUBLER IAW DWG ARB2933, SRM 51-33-01, AND 51-35-01.Jun 8, 2018 · N279UP · Doug MD11F · Wing, Plate/SkinSDR FDEA201806081440Slat Track · crackedNR 12 RT SLAT TRACK (MOST O/B ON THE NR 5 SLAT) APPEARS TO BE CRACKED FROM L/E OF CUT OUT THROUGH 2 FASTENERS GOING AFT. INSTALLED REPAIR IN REF TO SRM 57-40-02-2R AND PRIMED AND PAINTED REPAIR IN REF TO SRM 51-21-01.Jun 8, 2018 · N597FE · Doug MD11F · Leading Edge DevicesSDR IPXA2018070231215Skin · crackedINSPECTION TYPE:2C, NR 3 I/B T/R AFT UPPER OUTER SKIN HAS A CRACK APPROX 4" FROM AFT EDGE OF UPPER SIDE. REPAIRED NR 3 I/B T/R AFT UPPER OUTER SKIN IAW EA 011-7830-01-A-7305 REV IR AND EO MD11-7830-68876-A. (MINOR)Jun 7, 2018 · N279UP · Doug MD11F · Engine Thrust ReverserSDR IPXA2018060830414Battery Pack · inoperativeEMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 33-51-01-700-802. SYSTEM CHECKED OK.Jun 7, 2018 · N275UP · Doug MD11F · Emergency LightingSDR FDEA201806071413Cable · out of rigATTEMPTED TAKEOFF ON SIN RW 20C AND FOUND RUDDER PEDALS NOT CONNECTED TO STEERING. REJECTED AT LESS THAN 60 KTS AND RETURN TO GATE. TROUBLESHOOT FOUND STEERING FOLLOW UP CABLE OUT OF RIG, CARRIED OUT TENSION ADJUSTMENT OF STEERING FOLLOW UP CABLES PER AMM 32-5Jun 7, 2018 · N620FE · Doug MD11F · Landing Gear Steering SystemSDR IPXA2018061830750Frame · crackedINTERNAL FRAME CRACKED INSIDE THE NR 2 PYLON LOWER AFT FAIRING. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT FRAME IAW DWG AVB7599, AND SRM 54-01-42.Jun 6, 2018 · N281UP · Doug MD11F · Nacelle/Pylon, Main FrameSDR IPXA2018061430671Intercostal · crackedINSPECTION TYPE:2C, UPPER INTERCOSTAL BROKEN INSIDE LT FWD A/C DOOR 113AL. REMOVED FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER DWG ACA3820 AND SRM 51-33-01. (MINOR)Jun 6, 2018 · N281UP · Doug MD11F · Service DoorsSDR IPXA2018061130512Tee Fitting · crackedMAIN CABIN LONGERON 15L TEE FITTING WAS CRACKED AT BS 1340. REMOVED AND REPLACED THE TEE FITTING IAW SRM 51-33-01, 51-35-01, AND DWG AEA 7568.Jun 6, 2018 · N281UP · Doug MD11F · Fuselage Main, Attach FittingsSDR FDEA201806061405Tire · leakingLEVEL 1 LOW TIRE PRESSURE ALERT ON NR 5 TIRE CAME ON DURING CLIMB. FOLLOWED BY LEVEL 2 TIRE FAILURE ALERT. C/W QRH AND RETURNED TO KMEM. REPLD NR 5 AND NR 6 WHEEL ASSY REF AMM 32-41-01-4. INSP WHEEL WELL AND LANDING GEAR AREA. NO DAMAGE FOUND. A/C OK FORJun 6, 2018 · N617FE · Doug MD11F · BrakeSDR SRXR201806060048Skin · corrodedCORROSION FOUND ON THE RT WING FWD UPPER SKIN TO MID SKIN FROM XROS 192 - 216. BLENDED OUT THE CORROISION IAW SRM 52-21-04, PG 4. REPAIRED THE WING SKIN IAW EA 011-5720-52-A7293.Jun 6, 2018 · N415JN · Doug MD11F · Wing, Plate/SkinSDR SRXR201806060047Skin · corrodedRIGHT WING FWD AND CENTER UPPER SKIN HAD CORROSION BETWEEN XORS 145 AND 231, STRINGER 14R. ACCOMPLISHED A BLENDOUT REPAIR IAW EA 011-5720-52-A7293, I/R.Jun 6, 2018 · N415JN · Doug MD11F · Wing, Plate/SkinSDR SRXR201806060046Skin · corrodedCORROSION FOUND ON THE RT WING FWD UPPER SKIN TO MID SKIN FROM APPROX XORS 285 - 318. BLENDED THE CORROSION IAW SRM 51-21-04, PG3. REPAIRED IAW EA 011-5720-52-A7293.Jun 6, 2018 · N415JN · Doug MD11F · Wing, Plate/SkinSDR SRXR201806060045Skin · corrodedRIGHT WING UPPER SKIN HAD CORROSION BETWEEN XORS 91 AND XORS 230, STRINGER 14. ACCOMPLISHED A BLENDOUT REPAIR ON THE RT WING SKIN IAW EA 011-5720-52-A7293, I/R.Jun 6, 2018 · N415JN · Doug MD11F · Wing, Plate/SkinSDR IPXA2018062230939Vertical Support · crackedRIGHT WING T/E VERTICAL SUPPORT WAS CRACKED JUST FWD OF THE NR 1 SPOILER, INBD HINGE. REMOVED, FABRICATED, AND REPLACED THE SUPPORT IAW DWG ARC0297, AND SRM 51-33-01.Jun 5, 2018 · N281UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2018062213914Thrust Reverser · crackedNR 2 ENGINE, RT THRUST REVERSER AFT FIXED INNER BARREL UPPER SKIN IS CRACKED. REPAIRED THE THRUST REVERSER FIXED INNER BARREL UPPER SKIN IAW EA 011-7830-01-A7297, REV I/R, AND EO MD11-7830-68788-A.Jun 5, 2018 · N281UP · Doug MD11F · Engine Thrust ReverserSDR IPXA2018062030875Cap · crackedLT UNDERWING BARREL CANTED PANEL CAP WAS CRACKED AT BS 1236.8, AND Z=-100. REPAIRED THE PANEL CAP IAW EO MD11-5310-68793-A. MAJOR.Jun 5, 2018 · N281UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2018062030874Cap · crackedRT UNDERWING BARREL CANTED PANEL CAP IS CRACKED AT BS 1236.8 AND Z=-100. REPAIRED THE CANTED PANEL CAP IAW EO MD11-5310-68794-A. MAJORJun 5, 2018 · N281UP · Doug MD11F · Fuselage Miscellaneous Structure
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