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 FDEA2018051871254Flex Line · brokenON BLOCK IN, ADVISED BY GROUND THAT FLAMES WERE COMING FROM LEFT GEAR . TRYING TO CONFIRM, THE FLAMES HAD STOPPED. HIGHEST BRAKE TEMP NOTED ON CONFIG PAGE WAS 6 AT 473. ALL TEMPS ON LEFT TRUCK WERE MID 400S, ALL TEMPS ON RIGHT TRUCK MID 300S. LIGHT TO MEDMay 17, 2018 · N617FE · Doug MD11F · Landing Gear Brake SystemSDR IPXA2018052963028Fitting · crackedNR 1 ENGINE INBD THRUST REVERSER CENTER ACTUATOR BACK-UP FITTING WAS CRACKED. REPAIRED THE CENTER ACTUATOR BACK-UP FITTING IAW CMM 78-32-02, REPAIR 016.May 16, 2018 · N257UP · Doug MD11F · Engine Thrust ReverserSDR FDEA201805151239Engine · malfunctionedWHILE DOING DELAYED ENGINE START ON ENG 2 (2 START ALL NORMAL) NOTICED ENGINE 3 IDLING HIGHER THAN ENGINE 1. ALL OTHER INDICATIONS ON ENG 3 NORMAL (EGT,FF,ETC.). DECIDED TO SHUT NR 3 DOWN AND RESTART SHUT DOWN NR 3, WAITED UNTIL ALL INDICATIONS WERE ZERO +30 May 15, 2018 · N623FE · Doug MD11F · Engine (Turbine/Turboprop)SDR IPXA2018052530008Skin · dentedFUSELAGE SKIN DENTED BETWEEN BS 1681 - 1701, LONGERONS 34R - 35R. ACCOMPLISHED A PERMANENT REPAIR IAW EA 011-5330-01-A7280, REV IR, AND EO MD11-5330-68624-A.May 15, 2018 · N257UP · Doug MD11F · Fuselage Main, Plate/SkinSDR SRXR201805150019Longeron · corrodedCENTER CARGO LONGERON 38 IS CORRODED BETWEEN STA 5-123 & 5-113. REPAIRED IAW SRM 53-00-05, REPAIR 1, SHEET 1.May 15, 2018 · N415JN · Doug MD11F · Fuselage Main, Longeron/StringerSDR SRXR201805150018Stringer · crackedCENTER AUX FUEL TANK LOWER STRINGER 45 CRACKED AT XCW -17.00 AND XCW 17.00. REPAIRED IAW SRM 57-10-03, REPAIR 1.May 15, 2018 · N415JN · Doug MD11F · Fuel StorageSDR SRXR201805150017Stringer · crackedLEFT WING NR 1 FUEL TANK UPPER STRINGER 10 FOUND CRACKED AT XORS 753. REPAIRED THE STRINGER IAW SRM 57-00-03, REPAIR 5, FIG 202.May 15, 2018 · N415JN · Doug MD11F · Wing, Longeron/StringerSDR SRXR201805150016Angle · corrodedNR 2 PYLON, LT SIDE ACCESS PANEL 457AL COMPARTMENT HAS A CORRODED ANGLE. REMOVED, FABRICATED AND INSTALLED A NEW ANGLE AND DOUBLER IAW SRM 51-31-01.May 15, 2018 · N415JN · Doug MD11F · Nacelle/Pylon Miscellaneous StructureSDR FDEA20180515225Hose · leaking2.5 HOURS INTO FLIGHT, RECEIVED A HYD 3 ELEVATOR OFF, NR 2-3 RMP ALERT. AFTER COORDINATION WITH MOCC, ISOLATED THE NR 3 HYD SYSTEM, FLUID LEVEL CONTINUED TO DECREASE TO 1.7 GALLONS DURING DESCENT. FOLLOWED HYD 3 FAIL CHECKLIST, USED A MANUAL GEAR EXTENSMay 14, 2018 · N610FE · Doug MD11F · Hydraulic System, MainSDR FDEA2018091401208Hydraulic Line · failedHYD 1 FAIL, QTY 0.0. REMOVED AND REPLACED NR 1 ENGINE LEFT PUMP (UPPER) PRESSURE HOSE ASSY REF AMM 20-40-01-2.May 10, 2018 · N603FE · Doug MD11F · Hydraulic System, MainSDR FDEA2018051801206Doubler · crackedLEFT WING FIXED LEADING EDGE LOWER PANEL 519AB, FWD CUTOUT FOUND DOUBLER CRACKED AT XOS 600, INBOARD OF REFUELING PANEL. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-33-01-0G, AND DRAWING ARB2933, REV AJ. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-10May 10, 2018 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018051801205Doubler · crackedLEFT WING FIXED LEADING EDGE LOWER PANEL 518DB FWD CUTOUT FOUND DOUBLER CRACKED AT XOS 490. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-33-01-0G, DRAWING ARB2933, REV AJ. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 10, 2018 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018051501204Stiffener · crackedLEFT WING FIXED LEADING EDGE LOWER PANEL 518GB, OUTBOARD CUTOUT FOUND A STIFFENER CRACKED AT XOS 542 OUTBOARD SIDE OF SLAT DRIVE MECHANISM DOOR. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G, DWG ARB2918, REVISION G AND SRM 51-33-01-0G. THE RMay 10, 2018 · N615FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA2018051801192Seat Track · corrodedBS 1880 RBL 27.5 SEAT TRACK FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED FROM BS 1811 TO 1887 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WASMay 8, 2018 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2018051801191Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 693. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 8, 2018 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018051801190Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER WAS FOUND CRACKED AT XOS 705. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 8, 2018 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018051801189Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 762. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 8, 2018 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018051801188Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER WAS FOUND CRACKED AT XOS 616. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 8, 2018 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018051811187Seat Track · damagedCARGO TRACK CROWN DAMAGED AT 5-10, X= 27.5 UPPER CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 8, 2018 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA201805169619Longeron Splice · crackedINSPECTION TYPE: 3C, WHILE PERFORMING X-RAY INSPECTION OF THE TRANSVERSE SKIN SPLICE AT BS 5-123, DETECTED A CRACK FROM FASTENER TO FASTENER AT LONGERON 3R SPLICE FITTING. REMOVED AND REPLACED THE LONGERON SPLICE FITTING IAW SRM 51-31-01, AND 51-33-01.May 7, 2018 · N276UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2018051429586Skin · corrodedINSPECTION TYPE: 3C, EXTERIOR FUSELAGE SKIN HAD CORROSION, BS 2140 TO 2163, LONGERONS 33R TO 35R. REPAIRED THE SKIN IAW SRM 53-70-01, REPAIR 3, FIG 201. MAJOR.May 4, 2018 · N276UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA201805239893Frame · crackedCOCKPIT INSTRUMENT PANEL FRAME WAS CRACKED. REPAIRED THE INSTRUMENT PANEL FRAME IAW EA 011-3110-01-A7261, REV I/R, AND EO MD11-2510-68485-A.May 3, 2018 · N276UP · Doug MD11F · Fuselage Main, StructureSDR IPXA201805239890Bulkhead · crackedRIGID CARGO BARRIER WALL WAS CRACKED AT BS 488.812 AND RBL 4. REPAIRED THE WALL IAW EA 011-5320-01-A7265, REV I/R, AND EO MD11-5320-68577-A. MAJOR.May 3, 2018 · N276UP · Doug MD11F · Fuselage Main, BulkheadSDR IPXA201805219797Longeron Splice · crackedINSPECTION TYPE: 3C, LONGERON 9L SPLICE FITTING CRACKED AT BS 1531. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT LONGERON SPLICE IAW DWG A5A7112, AND SRM 51-33-01.May 3, 2018 · N276UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA201805189717Pan · damagedINSPECTION TYPE: 3C, MAIN CARGO DOOR FWD LOWER PAN IS CHAFED AND PUNCTURED. REMOVED, FABRICATED, AND REPLACED THE MAIN CARGO DOOR FWD LOWER PAN IAW DWG ACA7301, AND SRM 51-33-01.May 3, 2018 · N276UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2018051429553Fitting · chafedINSPECTION TYPE: 3C, RCB SIDEWALL ATTACHMENT FITTING NR 9 FOUND CHAFED. REPAIRED THE FITTING IAW SREO MD11-5310-48610-B.May 3, 2018 · N276UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2018051409535Web · crackedINSPECTION TYPE: 3C, R3 DOOR FRAME LOWER WEB WAS CRACKED AT BS 1254, Z-18. REPAIRED THE DOOR FRAME LOWER WEB IAW SRM 53-40-15, REPAIR 3, FIG 201. MAJOR.May 2, 2018 · N276UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2018051409534Web · crackedINSPECTION TYPE: 3C, L3 DOOR FRAME LOWER WEB FOUND CRACKED AT BS 1254, Z-18. REPAIRED THE DOOR FRAME LOWER WEB IAW SRM 53-40-15, REPAIR 3, FIG 201. MAJOR.May 2, 2018 · N276UP · Doug MD11F · Fuselage Main, StructureSDR SRXR201805020015Doubler · crackedLEFT WING CUT OUT AREA AFT OF THE NR 5 SLAT AT XORS 696, THE BEADED DOUBLER WAS FOUND CRACKED IN TWO PLACES. FABRICATED AND INSTALLED A REPAIR IAW SRM 57-40-02, REPAIR 15, FIG 205.May 2, 2018 · N415JN · Doug MD11F · Wing, Plate/SkinSDR IPXA2018051629660Intercostal · crackedINSPECTION TYPE: 3C, FWD CARGO BAY SUBFLOOR INTERCOSTAL WAS FOUND CRACKED AT BS 6-73, ABOVE LONGERON 43R. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-31-01, 51-33-01, 51-35-01, AND DWG ADA7667.May 1, 2018 · N276UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA201805169638Floorbeam · crackedINSPECTION TYPE: 3C, FWD CARGO FLOORBEAM CRACKED BS 6-70, AT LONGERON 43R. REPAIRED THE FLOORBEAM IAW SRM 53-40-51, FIGURE 202, REPAIR 1. MAJOR.May 1, 2018 · N276UP · Doug MD11F · Fuselage Main, Floor BeamSDR IPXA2018050129139Microphone · no testRIGHT OBS SEAT OXYGEN MASK MIC WILL NOT TEST. REMOVED MASK IAW AMM 35 13 01 000 802. INSTALLED SVC ASSY IAW 35 13 01 400 802. ESR IPC 35 13 05 01 ITEM 010.May 1, 2018 · N251UP · Doug MD11F · Crew Oxygen SystemSDR IPXA2018050129155Smoke Barrier · not seatedGAP IN SMOKE CURTAIN. CARGO BARRIER VAPOR SEAL RE-INSTALLED IAW AMM 25-59-15-400-801 REV 90.08. SEAL NOW PROPERLY SEATED.May 1, 2018 · N254UP · Doug MD11F · Emergency EquipmentSDR SRXR201805010014Mount Bracket · crackedMAIN CABIN R3 DOOR FRAME UPPER AFT LONGERON 15R HAS A CRACKED MOUNTING BRACKET. REMOVED THE MOUNTING BRACKET IAW SRM 51-00-12. FABRICATED A REPAIR MOUNTING BRACKET IAW DWG AEA7568. INSTALLED THE REPAIR MOUNTING BRACKET, BS 1278 IAW SRM 51-33-01, PG 30, PARAMay 1, 2018 · N415JN · Doug MD11F · Fuselage Main, Attach FittingsSDR SRXR201805010013Mount Bracket · crackedMAIN CABIN L3 DOOR FRAME UPPER AFT LONGERON 15L HAS A CRACKED MOUNTING BRACKET. REMOVED THE CRACKED MOUNTING BRACKET IAW SRM 51-35-01. FABRICATED REPAIR MOUNTING BRACKET IAW DWG AEA7568, AND INSTALLED THE MOUNTING BRACKET, BS 1278 LONGERON 15L IAW SRM 51-35-0May 1, 2018 · N415JN · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA201805239891Bulkhead · crackedRIGID CARGO BARRIER WALL IS CRACKED AT BS 488.812 AND LBL 4. REPAIRED THE BARRIER WALL IAW EA 011-5320-01-A7265, REV I/R, AND EO MD11-5320-68577-A. MAJOR.Apr 30, 2018 · N276UP · Doug MD11F · Fuselage Main, BulkheadSDR IPXA201805189710Closeout Panel · crackedINSPECTION TYPE: 3C, RIGID CARGO BARRIER WALL LOWER FWD CLOSEOUT IS CRACKED AT BS 488.81, LBL 8.5. REPAIRED THE FWD CLOSEOUT IAW SRM 53-20-53, REPAIR 1, FIG 201. MAJOR.Apr 30, 2018 · N276UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA201805189709Closeout Panel · crackedINSPECTION TYPE: 3C, RIGID CARGO BARRIER WALL LOWER FWD CLOSEOUT IS CRACKED AT BS 488.81, LBL 22.5. REPAIRED THE CLOSEOUT IAW SRM 53-20-53, REPAIR 1, FIG 201. MAJOR.Apr 30, 2018 · N276UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA201805189690Skin · chafedINSPECTION TYPE: 3C, FUSELAGE SKIN CHAFED AT BS 1153, LONGERON 44R. REPAIRED THE SKIN IAW SRM 53-40-01, REPAIR 2, FIG 201. MAJOR.Apr 30, 2018 · N276UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA201805189708Closeout Panel · crackedINSPECTION TYPE: 3C, RIGID CARGO BARRIER WALL LOWER FWD CLOSEOUT IS CRACKED AT BS 488.81 LBL 42.5. REPAIRED THE CLOSEOUT IAW SRM 53-20-53, REPAIR 1, FIG 201. MAJOR.Apr 30, 2018 · N276UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA201805189707Closeout Panel · crackedINSPECTION TYPE: 3C, RIGID CARGO BARRIER WALL LOWER FWD CLOSEOUT IS CRACKED AT BS 488.81, LBL 13.5. REPAIRED CLOSEOUT IAW SRM 53-20-53, REPAIR 1, FIG 201. MAJOR.Apr 30, 2018 · N276UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA201805189706Closeout Panel · crackedINSPECTION TYPE: 3C, RIGID CARGO BARRIER WALL LOWER FWD CLOSEOUT IS CRACKED AT BS 488.81, RBL 33.5. REPAIRED THE BARRIER CLOSEOUT IAW SRM 53-20-53, REPAIR 1, FIG 201. MAJOR.Apr 30, 2018 · N276UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2018051409547Attach Bracket · crackedINSPECTION TYPE:3CWING TO BODT FAIRING ATTACH ANGLE CRACKED, RH SIDE, STA. 1361 ABOVE UPPER WING SURFACEREMOVED FABRICATED AND INSTALLED REPLACEMENT ANGLE PER DWG AEA0553 AND SRM 51-33-01 (MINOR)Apr 30, 2018 · N276UP · Doug MD11F · Aerodynamic FairingsSDR IPXA201805149546Attach Bracket · crackedINSPECTION TYPE: 3C, WING TO BODY FAIRING ATTACH BRACKET FOUND CRACKED, LT SIDE, BS 1401 BELOW LONGERON 23L. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT BRACKET IAW DWG AEA0553 AND SRM 51-33-01.Apr 30, 2018 · N276UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2018052329896Stringer · crackedLEFT WING STRINGER 13 WAS CRACKED BETWEEN XORS 562 - 592. REPAIRED CRACKED LT WING STRINGER IAW EA 011-5710-01-A7257, REV I/R AND EO MD11-5710-68576-A. MAJOR.Apr 29, 2018 · N276UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2018052129822Spar Cap · corrodedINSPECTION TYPE: 3C, RT WING REAR SPAR UPPER CAP HAS CORROSION BETWEEN XORS 749 AND 807.5. REPAIRED THE UPPER SPAR CAP IAW EA 011-5710-01-A7267, REV I/R, AND EO MD11-5710-68558-A.Apr 29, 2018 · N276UP · Doug MD11F · Wing SparSDR IPXA2018052129821Skin · corrodedINSPECTION TYPE: 3C, LEFT WING UPPER SKIN HAD CORROSION, XORS 142.25 - 144.25, ABOVE THE FRONT SPAR. REPAIRED THE SKIN IAW EA 011-5730-01-A7269, REV I/R, AND EO MD11-5730-68556-A.Apr 29, 2018 · N276UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2018052129820Skin · corrodedINSPECTION TYPE: 3C, RT WING UPPER SKIN HAS CORROSION AT THE REAR SPAR BETWEEN XORS 786 - 806. REPAIRED THE SKIN IAW EA 011-5730-01-A7268, REV I/R, AND EO MD11-5730-68559-A.Apr 29, 2018 · N276UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2018052129819Skin · corrodedINSPECTION TYPE: 3C, LT WING UPPER SKIN HAS CORROSION AT XORS 751.5, BETWEEN STRINGERS 5 - 6L. REPAIRED THE SKIN IAW EA 011-5730-01-A7271, REV I/R, AND EO MD11-5730-68557-A.Apr 29, 2018 · N276UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2018051879691Stanchion · crackedINSPECTION TYPE: 3C, LT WING T/E SHELF PANEL HAS VERTICAL SUPPORT STANCHION CRACKED BELOW NR 1 SPOILER INBD END. REMOVED, FABRICATED AND REPLACED VERTICAL STANCHION IAW DWG ARC0298-5, AND SRM 51-33-01.Apr 29, 2018 · N276UP · Doug MD11F · Wing Main, Frame Structure
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