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 FDEA201805231270Seat Track · gougedMAIN DECK SEAT TRACK AT BS 1014, RBL 8.5, FOUND THE CROWN DAMAGED. REPLACED FROM BS 989 TO 1069, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201805231299Doubler · crackedRIGHT WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 668 WAS CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201805231298Doubler · crackedRIGHT WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 700 WAS FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201805231297Skin · crackedRIGHT WING FIXED LEADING EDGE COMPARTMENT XOS 547 PANEL CUTOUT WAS FOUND CRACKED. REPAIRED IAW SRM 51-31-01-06, DRAWING ARB2933, REV AJ, AND SRM 51-35-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201805231296Stiffener · crackedRIGHT WING FIXED LEADING EDGE COMPARTMENT STIFFENER AT XOS 542 WAS FOUND CRACKED. THE STIFFINER WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G, DRAWING ARB2918, REV G. AND SRM 51-33-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201805231295Doubler · crackedRIGHT WING FIXED LEADING EDGE COMPARTMENT DOUBLER WAS FOUND CRACKED AT XOS 789. THE DOUBLER WAS REMOVED AND REPLACED IAW DRAWING ARB3954, REV K.AND SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201805231294Doubler · crackedRIGHT WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT XOS 906 WAS FOUND CRACKED. THE DOUBLER WAS REMOVED AND AND A NEW DOUBLER WAS FABRICATED IAW DRAWING ARB3954, REV K. INSTALLED THE DOUBLER IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2May 23, 2018 · N620FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201805231287Skin · crackedLEFT WING LEADING EDGE, NR 1 PYLON LT SIDE ADJACENT AREA LOWER SUPPORT PLATE FOUND CRACKED. THE SKIN WAS REMOVED IAW SRM 51-35-01-0G, AND FABRICATED A NEW SKIN IAW DRAWING ARB2363, REV C, AND INSTALLED IAW SRM 51-35-01-0G. THE REPAIR WAS CLASSIFIED AS MAJMay 23, 2018 · N620FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201805231281Seat Track · corrodedMAIN DECK SEAT TRACK AT BS 1431, RBL 8.5 WAS FOUND CORRODED. THE CORROSION WAS FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK FROM BS 1391 TO EXISTING SPLICE AT BS 1451 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. May 23, 2018 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201805231278Seat Track · gougedMAIN DECK SEAT TRACK AT BS 1285, LBL 47.5, FOUND TO CROWN DAMAGED. REPLACED THE SEAT TRACK FROM BS 1248 TO 1312, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201805231293Web · crackedCOCKPIT RT OBSERVER`S SEAT FLOOR SUPPORT CUTOUT WEB FOUND CRACKED AT BS 365, RBL 3.5. THE WEB WAS REPAIRED IAW SRM 53-10-51-2R, FIG 202, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201805231292Frame · damagedFRAME AT BS 535, LONGERON 23L FOUND WITH A REPAIR ANGLE DAMAGED. REPAIRED IAW SRM 53-20-07-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201805231291Seat Track · crackedMAIN DECK SEAT TRACK CRACKED AT BS 635, RBL 47.5. REPLACED THE SEAT TRACK FROM EXISTING SPLICES BS 625 TO 665 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201805231290Seat Track · crackedMAIN DECK FLOOR SEAT TRACK CRACKED AT BS 695, RBL 27.5. REPLACED THE SEAT TRACK FROM EXISTING SPLICES BS 625 TO 745 IAW SRM 53-00- 52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201805231285Seat Track · gougedMAIN DECK SEAT TRACK CROWN AT BS 5-113, RBL 47.5 FOUND GOUGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK FROM BS 5-83 TO EXISTING SPLICE AT BS 5-123 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAMay 23, 2018 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201805231284Seat Track · corrodedMAIN DECK SEAT TRACK AT BS 5-43, RBL 8.5 WAS FOUND CORRODED. FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK FROM EXISTING SPLICE BS 5-0 TO 5-83 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASMay 23, 2018 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201805231283Seat Track · corrodedMAIN DECK SEAT TRACK AT BS 1471, LBL 8.5 WAS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK FROM BS 1411 TO EXISTING SPLICE AT BS 5-0 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLMay 23, 2018 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201805231275Doubler · crackedLEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 701 FOUND CRACKED. REPAIRED DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201805231274Doubler · crackedLEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 664 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201805231273Doubler · crackedLEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 646 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201805231272Doubler · crackedLEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 613 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201805231268Seat Track · crackedMAIN DECK SEAT TRACK AT BS 635, LBL 47.5 FOUND CRACKED. REPLACED FROM EXISTING SPLICES BS 625 TO 705 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201805231303Skin · damagedLEFT WING, LOWER FUEL TANK ACCESS PANEL 538AB CUTOUT FOUND DAMAGED. REPAIRED IAW SRM 57-20-02-2R, FIG 201, REPAIR 5. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201805231289Seat Track · crackedMAIN DECK SEAT TRACK CRACKED AT BS 635, RBL 27.5. REPLACED THE SEAT TRACK FROM EXISTING SPLICES BS 625 TO 645 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201805231288Seat Track · crackedMAIN DECK SEAT TRACK CRACKED AT BS 635, RBL 8.5. REPLACED THE SEAT TRACK FROM EXISTING SPLICES AT BS 625 TO 645 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201805231277Seat Track · damagedMAIN DECK SEAT TRACK AT BS 775, X= 75.25, FOUND THE CROWN DAMAGED. REPLACED THE SEAT TRACK FROM EXISTING SPLICES BS 765 TO 816, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201805231269Seat Track · gougedMAIN DECK SEAT TRACK AT BS 880, RBL 8.5, FOUND THE CROWN DAMAGED. REPLACED FROM BS 869 TO 909, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2018060130225Intercostal · crackedDURING REMOVAL OF THE PNEUMATIC DUCT IAW NRC 379144, FOUND AN INTERCOSTAL GOUGED & CRACKED, BS 1781 - 1801. FABRICATED A REPLACEMENT INTERCOSTAL IAW DWG AGA7177. AND INSTALLED.May 22, 2018 · N257UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2018053030179Web · crackedWHILE ACCOMPLISHING EO MD11-5710-65285-C APPX. B, STEP 5. ONE CRACK DETECTED ON THE RT WEB OTBD LOWER STIFFENER .250 IN LENGTH, DEPTH GREATER THAN .050. REPAIRED THE FUEL TANK WEB IAW EO MD11-5710-68621-A. MAJOR.May 22, 2018 · N257UP · Doug MD11F · Fuel StorageSDR FDEA201805221312Cylinder · leakingHYD ELEV 3 OFF AT 4.9 QUANTITY IN HYD SYSTEM 3. TURNED LT & RT HYD 3 PUMPS OFF. QUANTITY CONTINUED TO DECREASE. HYD 3 OFF ILLUMINATED AT 2.5, SELECTED HYD AUTO AND QUANTITY CONTINUED TO DECREASE. HYD 3 QUATITY AT .8 WHEN LANDING GEAR LOWERED NORMALLY. REMay 22, 2018 · N528FE · Doug MD11F · Hydraulic System, MainSDR IPXA201805239879Battery Pack · inoperativeFOUND THE EMERGENCY LIGHT TEST FAILED. R & R THE BATTERY PACK IAW AMM 33-51-01/401. PERFORMED AN EMERGENCY LIGHT TEST, FOUND TO BE SATISFACTORY.May 22, 2018 · N270UP · Doug MD11F · Emergency LightingSDR SRXR201805220025Cargo Track · corrodedAFT CARGO BAY, CARGO TRACK AT BS 1849, RBL 15 IS CORRODED. REMOVED, FABRICATED, LOCATED, DRILLED, AND REPLACED THE CARGO TRACK IAW DWG AG3855, REV P, SRM 51-21-01, AND EA 011-5300-52-A7254.May 22, 2018 · N415JN · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2018060130223Floor Panel · corrodedRCB AREA FLOOR PANEL WSP0788-502 HAD CORROSION BETWEEN BS 476 - 480, RBL 37. REPAIRED THE FLOOR PANEL IAW EA 011-5330-01-A7289, REV IR, AND EO MD11-5330-68700-A.May 20, 2018 · N257UP · Doug MD11F · Fuselage Floor PanelSDR IPXA201805219798Panel · damagedLOWER VERTICAL STABILIZER RIGHT SIDE REAR PANEL DAMAGED. REPAIRED THE PANLE IAW EO MD11-5530-67901-B.May 20, 2018 · N288UP · Doug MD11F · Vertical Stabilizer, Plate/SkinSDR SRXR201805200024Skin · corrodedNUMEROUS AREAS OF CORROSION ON RT WING LOWER SKIN AT XORS 346 AND XORS 402 STRINGER 31 TO 40. ACCOMPLISHED REPAIR AT RT WING LOWER SKIN AT XORS 346 TO XORS 402 BETWEEN STRINGER 31 TO STRINGER 40 PER EA 011-5720-52-A7220 IR REF NRC A040473.May 20, 2018 · N415JN · Doug MD11F · Wing, Plate/SkinSDR IPXA2018060643312Skin · crackedNR 2 ENGINE, RT CORE COWL HAD A CRACK ON THE OUTER SKIN AT THE FWD LATCH. REPAIRED THE DAMAGE IAW EA 011-5430-01-A7295, REV I/R, AND EO MD11-5430-68739-A.May 18, 2018 · N257UP · Doug MD11F · Nacelle/Pylon, Plate/SkinSDR IPXA2018060430281Cap · crackedLEFT UNDERWING BARREL CANTED PANEL CAP IS CRACKED AT BS 1278 AND Z -100. REPAIRED THE PANEL CAP IAW EA 011-5310-01-A7281, REV I/R, AND EO MD11-5340-68712-A. MAJOR.May 18, 2018 · N257UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2018060430280Spar Cap · corrodedRIGHT WING REAR SPAR UPPER CAP HAD CORROSION BETWEEN XORS. 666.2 TO 680.7. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A7288, REV I/R, AND EO MD11-5710-68701-A.May 18, 2018 · N257UP · Doug MD11F · Wing SparSDR IPXA201806040270Support Angle · damagedLEFT WING LOWER T/E PANEL SUPPORT ANGLE WAS CHAFED, ADJACENT TO PANEL 551BB. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT SUPPORT ANGLE IAW DWG ARC0744, AND SRM 51-33-01.May 18, 2018 · N257UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2018060130222Spar Cap · corrodedCORROSION UNDER THE RT WING UPPER AFT T/E PANEL AT WS 593 - 678. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A7287, REV IR, AND EO MD11-5710-68702-A.May 18, 2018 · N257UP · Doug MD11F · Wing SparSDR IPXA2018052529997Angle · crackedLEFT WING T/E PANEL 551AB SUPPORT ANGLE WAS CRACKED, OTBD OF INBD AILERON. REMOVED, FABRICATED, AND REPLACED THE SUPPORT ANGLE IAW DWG.ARC0872, AND SRM 51-33-01.May 18, 2018 · N257UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2018060430290Tail Cone · chafedTAILCONE LT SIDE THE UPPER PRODUCTION DOUBLER HAD DEEP CHAFE WEAR AT BS 2165.061 AND LBL 36.5. REPAIRED THE TAILCONE IAW EA 0115350-01-A7278, REV I/R, AND EO MD11-5350-68582-A.May 17, 2018 · N257UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2018060430282Spar Cap · corrodedLEFT WING REAR UPPER SPAR CAP HAD CORROSION BETWEEN XORS. 595.5 TO 612. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A7286, REV I/R, AND EO MD11-5740-68724-A.May 17, 2018 · N257UP · Doug MD11F · Wing SparSDR IPXA2018060130219Skin · chafedLEFT WING DROOP LE SKIN, FWD EDGE HAS PREVIOUS REPAIR CHAFED THROUGH. REMOVED THE REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW SRM 57-40-01, REPAIR 15, FIGURE 202. MAJOR.May 17, 2018 · N257UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2018060130221Doubler · crackedRIGHT WING SKIN SPLICE DOUBLER AT XORS 799 WAS CRACKED. REMOVED AND REPLACED THE DOUBLER IAW DWG ARB3954, SRM 51-21-01, 51-31-01, 51-33-01, AND 51-35-01.May 17, 2018 · N257UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2018052930139Angle · crackedINSPECTION TYPE:4C, RT WING L/E INTERNAL "L" ANGLE IS CRACKED AT APPROX XORS 480. REMOVED AND REPLACED RT WING L/E INTERNAL "L" ANGLE AT XORS 480 IAW DWG ARB2931 AND SRM 51-31-01, 51-33-01 & 51-35-01.May 17, 2018 · N257UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2018053029137Rib · crackedRIGHT WING NR 2 SLAT OTBD CLOSURE RIB WAS CRACKED. REMOVED AND REPLACED THE RIB IAW DWG ARB1647, SRM 51-31-01, AND 51-35-01.May 17, 2018 · N257UP · Doug MD11F · Leading Edge DevicesSDR IPXA2018053030176Floor Panel · corrodedMAIN CABIN FLOOR PANEL AT BS 475 AND RCB FLOOR FITTING NR 5 HAD HEAVY CORROSION . REPAIRED MAIN CABIN FLOOR PANEL AND RCB FLOOR FITTING IAW EA 011-5330-01-A7284, REV IR, AND EO MD11-5320-68679-A.May 17, 2018 · N257UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2018052963027Angle · crackedNR 1 PYLON L ANGLE WAS FOUND CRACKED ABOVE AFT END OF THE PRECOOLER. REMOVED AND REPLACED THE ANGLE IAW SRM 54-01-42.May 17, 2018 · N257UP · Doug MD11F · Nacelle/Pylon Miscellaneous StructureSDR IPXA2018052529996Floor Panel · corrodedMAIN CABIN FLOOR PANEL AT BS 475 AND RCB FLOOR FITTING NR 2 HAD HEAVY CORROSION. REMOVED AND REPLACED THE FLOOR PANEL IAW AMM 53-21-10-400-801.May 17, 2018 · N257UP · Doug MD11F · Fuselage Floor Panel
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