Boeing MD-11F

Service difficulty reports · 31,320

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Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA2017072919900Web · crackedINSPECTION TYPE: SV, OVER WING UPPER FUEL TANK AFT WEB CRACKED BS 1372 AT X=80. REPAIRED CRACKED WEB IAW EA 011-5710-01-A6913 REV IR, AND EO MD11-5710-65091-A. MAJOR.Jul 25, 2017 · N282UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017072919898Web · crackedINSPECTION TYPE: SV, OVER WING UPPER FUEL TANK AFT WEB CRACKED BS 1372 AT X=-80. REPAIRED CRACKED WEB IAW EA 011-5710-01-A6913, REV IR AND EO MD11-5710-65091-A. MAJOR.Jul 25, 2017 · N282UP · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201707242023Fitting · wornATTACH FITTING DAMAGED. REPAIRED IAW EA 1-5340-160080B, P2. REPAIR CLASSIFIED AS MAJOR IAW GMM 602-100.Jul 24, 2017 · N590FE · Doug MD11F · Wing, Attach FittingsSDR IPXA2017080920302Skin · gougedINSPECTION TYPE: 1C, RT NR 3 SLAT LOWER SKIN GOUGED. REPAIRED THE SKIN BETWEEN XOS 475 - 484 IAW EA 011-5754-01-A6921, REV IR, AND EO MD11-5750-65191-A. MAJOR.Jul 24, 2017 · N251UP · Doug MD11F · Leading Edge DevicesSDR IPXA2017080320098Skin · gougedINSPECTION TYPE: 1C, CENTER FUSELAGE LOWER EXTERIOR SKIN PANEL GOUGED BETWEEN BS 1139 - 1168, LONGERONS 43 - 45L. REPAIRED THE DAMAGE IAW EA 011-5330-01-A6915, REV IR, AND EO MD11-5330-65115-A.Jul 24, 2017 · N251UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2017080920305Doubler · damagedINSPECTION TYPE: 1C, EXTENDED TAILCONE LT SIDE INTERNAL REPAIR DOUBLER CHAFED BS 2165 Z=45 - Z=60. REPAIRED IAW EA 011-5350-01-A6914, REV IR, AND EO MD11-5350-65072-A.Jul 23, 2017 · N251UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2017080920320Rib · crackedINSPECTION TYPE: 1C, NR 3 ENGINE INBD CORE COWL AFT RIB CRACKED. REMOVED AND REPLACED IAW AMM 71-14-01.Jul 23, 2017 · N251UP · Doug MD11F · Nacelle/Pylon, Frame/Spar/RibSDR IPXA2017080820263Skin · damagedINSPECTION TYPE: 1C, NR 3 ENGINE OUTBOARD FAN REVERSER INNER BARREL SKIN CHAFED AND CRACKED. REPAIRED THE DAMAGE IAW EA 011-7830-01-A6922, REV IR, AND EO MD11-7830-65185-A.Jul 23, 2017 · N251UP · Doug MD11F · Engine Thrust ReverserSDR IPXA2017080520152Doubler · chafedINSPECTION TYPE:1C, EXTENDED TAILCONE RT SIDE INTERNAL REPAIR DOUBLER CHAFED BS 2165 BETWEEN WL Z=50 AND Z=60.1. REPAIRED IAW EA 011-5350-01-A6912, REV IR, AND EO MD11-5350-65085-A.Jul 23, 2017 · N251UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2017072419707Cable · brokenL1 DOOR OVERHEAD SLIDER CABLE ASSY BROKEN. R & R THE CABLE IAW MM 25-23-23, AND ESR 25-23-15-02.Jul 23, 2017 · N254UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2017080320096Structure · corrodedINSPECTION TYPE: 1C, RCB LOWER AFT FACE SHEET CORRODED AT LBL 22.5 Z=-18. REPAIRED NOTED RCB CORROSION IAW EA 011-5310-01-A6916, REV IR, AND EO MD11-5310-65121-A.Jul 22, 2017 · N251UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017072719836Doubler · crackedINSPECTION TYPE: 1C, LT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS 768.27 - 772.85. REPAIRED THE DOUBLER IAW EA 011-5730-01-A6910, REV I/R, AND EO MD11-5730-65061-A. MAJOR.Jul 22, 2017 · N284UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017072119601Girt Bar · out of positionWITH L1 SLIDE ARMED, EXTERNAL HANDLE PROTRUDING FROM ACFT, WHEN LOOKING THROUGH VIEW WINDOW, GIRT BAR DOES NOT APPEAR TO BE FULLY ARMED. REPOSITIONED THE L1 DOOR FWD VIEW WINDOW FLAPPER DOOR FOR GIRT BAR. DOOR OPERATED NORMAL. OK FOR CONTINUOUS SERVICE.Jul 21, 2017 · N288UP · Doug MD11F · Emergency EquipmentSDR FDEA201708152223Skin · crackedON TOP OF THE LEFT WING DROOPED LEADING EDGE, FOUND A SUSPECTED CRACK COMING FROM THE OUTBOARD MOST FASTNER HOLE. REPAIRED THE DROOPED L/E WITH DOUBLERS IAW SRM 57-40-01, REPAIR 5, FIG 201, SHEET 1-6.Jul 20, 2017 · N528FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2017072719821Spoiler · looseINSPECTION TYPE: 1C, LEFT NR 1 SPOILER LOOSE. REMOVED AND REPLACED THE SPOILER IAW AMM 27-60-20.Jul 20, 2017 · N284UP · Doug MD11F · SpoilersSDR FDEA201707202013Hose · crackedHYD 3 FAILED WHILE AIRBORNE, 1 HR AT FL360 AT BLOCK IN, FOUND HYD FLUID COMING OUT OF NR 3 ENGINE. OPENED THE NR 3 ENGINE COWLINGS AND THRUST REVERSER IAW AMM 71-10-00-2-1. FOUND LEAK COMING FROM CASE DRAIN FILTER TO PYLON HOSE. FOUND CASE DRAIN HOSEJul 20, 2017 · N597FE · Doug MD11F · Hydraulic System, MainSDR FDEA201707202010Hose · failedHYD 3 FAILED WHILE AIRBORNE 1.0 HRS, AT FL360. R & R THE NR 3 ENGINE HYD PUMP. R & R FILTER TO PYLON HOSE ASSY. DRY MOTORED ENGINE. NO LEAKS NOTED ON LT AND RT PUMPS, THE HYD LINE AND ON THE FILTERS. RAN THE NR 3 ENGINE. ALL OPS AND INDICATIONS FOR NRJul 20, 2017 · N597FE · Doug MD11F · Hydraulic System, MainSDR IPXA2017072119594Lens · detachedEXIT SIGN ABOVE THE R1 DOOR FELL OFF. INSTALLED THE LENS IAW AMM 33-52-04. CHECKED NORMAL.Jul 20, 2017 · N257UP · Doug MD11F · Emergency LightingSDR IPXA2017072019529Seal · wornCLIMBING THROUGH 9000 FT MSL, THE WINDOW BEGAN A LOUD VIBRATING HOWL. AT 11000 FT MSL, SOUND WAS UNBEARABLE WITH ATC AND INTERCOCKPIT COMMUNICATIONS EXTREMELY DIFFICULT. FOUND THE RT SLIDING WINDOW SEAL WORN. R & R THE SEAL IAW AMM 56-12-01-8, REV 89.01 07-1Jul 20, 2017 · N287UP · Doug MD11F · Flight Compartment WindowsSDR FDEA201707192090Seat Track · corrodedMAIN DECK SEAT TRACK HAS MINOR SURFACE CORROSION AT BS 1441, LBL 8. REMOVED AND REPLACED THE SECTION OF SEAT TRACK FROM BS 1441 TO 1501 IAW SRM 53-00-52-2R, FIG 201, SHEETS 1-3.Jul 19, 2017 · N528FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201707192002Collar · brokenDURING POSTFLIGHT, FOUND NOSE STRUT LOWER STEERING SUPPORT COLLAR ASSY BROKEN. REMOVAL OF NOSE STRUT LOWER LEG IN PROGRESS AS PER AMM 32-21-01-8 FROM CHAPTER 4 . INSTALLED IAW MM 32-21-01-8 FROM STEP 5.F.11. ALL TEST PASSED INCLUDING NOSE LANDING GEJul 19, 2017 · N617FE · Doug MD11F · Landing Gear Steering SystemSDR FDEA201707192003Skin · scratchedRIGHT WING, UPPER SURFACE, IN THE AREA OF THE NR 8 SLAT, APPEARS TO HAVE A SCRATCH. REPAIRED IAW EA 1-5730-T0334361, REV A.Jul 19, 2017 · N601FE · Doug MD11F · Leading Edge DevicesSDR IPXA2017071919490Longeron · corrodedINSPECTION TYPE:3C, CENTER CARGO COMPARTMENT LONGERON 49L HAS CORROSION AT STA 5-123. REMOVED AND REPLACED LONGERON SECTION 49L PER SRM 53-00-05 REPAIR 1, EA 011-5310-01-A6888 I/R AND EO 5310-64959-A.Jul 18, 2017 · N296UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2017071819485Indicator · inoperativeL1 DOOR REMOTE PUSH TO TEST INDICATOR INOPERATIVE. PRESSURE VERIFIED VIA SLIDE GAUGE PLACARD INSTALLED. R & R PRESSURE INDICATING REMOTE KIT IAW AMM 25-61-04; OPS TESTED GOOD.Jul 18, 2017 · N254UP · Doug MD11F · Emergency EquipmentSDR IPXA2017071819457Battery Pack · inoperativeL1 DOOR SLIDE PRESS TO TEST DOES NOT TEST. PERFORMED DMP 25 61 2 L1 DOOR OPS CHECKS NORAML PERFORMED AN OPS TEST OF SYSTEM FOR BATTERY & LIGHT FUNCTIONS IAW 25-61-04-710-801. REPLACED BATTERIES, OPS TESTED GOOD;Jul 18, 2017 · N254UP · Doug MD11F · Emergency EquipmentSDR FDEA201707181990Trunnion · wornCENTERLINE LANDING GEAR LT AND RT TRUNNION SUPPORT FITTINGS CORRODED. COMPLIED WITH EA 1-5340-T0334405A, PT2. MACHINED FAYING SURFACE. AFTER MACHINING, MINIMUM THICKNESS OF FAYING SURFACE WAS LESS THAN SRM LIMITS.Jul 18, 2017 · N584FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA201707181989Trunnion · wornCENTERLINE LANDING GEAR LT AND RT TRUNNION SUPPORT FITTINGS CORRODED. COMPLIED WITH E.A. 1-5340-T0334405A PT1. MACHINED FAYING SURFACE. AFTER MACHINING, MINIMUM THICKNESS OF FAYING SURFACE WAS LESS THAN SRM LIMITS.Jul 18, 2017 · N584FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR IPXA2017071719419Slide · dislodgedFOUND L1 DOOR SLIDE INADVERTENTLY DISLODGED. REINSTALLED L1 DOOR SLIDE IAW AMM 25-61-15-4 & AMM 25-61-04-400-801.Jul 17, 2017 · N288UP · Doug MD11F · Escape SlideSDR IPXA2017080820262Stiffener · crackedINSPECTION TYPE: 1C, NR 2 ENGINE PYLON AFT UPPER FAIRING INTERNAL STIFFENER CRACKED. REPAIRED THE STIFFENER IAW EA 011-5450-01-A6923, REV IR, AND EO MD11-5450-65160-A.Jul 16, 2017 · N251UP · Doug MD11F · Nacelle/Pylon Miscellaneous StructureSDR IPXA2017071719393Smoke Goggles · damagedDURING PS1 CHECK, FOUND ONE PAIR OF SMOKE GOGGLES BROKEN. R & R.Jul 15, 2017 · N291UP · Doug MD11F · Emergency EquipmentSDR IPXA2017071719383Cable · looseL1 DOOR WILL NOT ARM. DOOR OPERATION ROUGH. DOOR WILL NOT OPEN. DOOR APPEARED TO HAVE A DAMAGED UNLOCK. FOUND ONE CABLE LOOSE IAW AMM 52-11-02-830-801. ADJUSTED THE CABLE. OPEN AND CLOSED L1 DOOR ELECTRICALLY, NORMAL.Jul 15, 2017 · N258UP · Doug MD11F · Passenger/Crew DoorsSDR FDEA201707141936Skin · crackedDURING AN HFEC INSPECTION, FOUND TWO FASTENER HOLES 31 AND 34 WITH CRACK INDICATIONS, AT THE RIGHT WING LOWER PANEL OUTER WING ACCESS DOOR AT XORS 696.730. REPAIRED IAW SRM 57-20-02-2R, FIG 201, REPAIR 5. REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 14, 2017 · N529FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201707141935Skin · crackedDURING HFEC INSPECTION, FOUND ONE FASTENER HOLE 31 HAD A CRACK INDICATION AT RIGHT WING LOWER PANEL OUTER WING ACCESS DOOR AT XORS 696.730. REPAIRED IAW SRM 57-20-02-2R, FIG. 201, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 14, 2017 · N529FE · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2017072719812Fitting · chafedINSPECTION TYPE: 1C, RIGID CARGO BARRIER SIDE FITTING NR 12 HAS CHAFE DAMAGE. REPAIRED RIGID CARGO BARRIER FITTING IAW EA 011-5340-01-A6908, REV I/R, AND EO MD11-5340-65049-A.Jul 13, 2017 · N284UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017072719811Floor Panel · corrodedINSPECTION TYPE :1C, MAIN CABIN FLOOR PANEL HAS CORROSION AT BS 475 AND RBL 30 - 37. REPAIRED THE FLOOR PANEL IAW EA 011-5320-01-A6899, REV I/R, AND EO MD11-5320-65034-A.Jul 13, 2017 · N284UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2017072719809Floor Panel · corrodedINSPECTION TYPE: 1C, MAIN CABIN FLOOR PANEL AT BS 499 AND BETWEEN BL 0 & RBL 8.5 HAS CORROSION. REPAIRED THE FLOOR PANEL IAW EA 011-5320-01-A6905, REV I/R, AND EO MD11-5320-65018-A.Jul 13, 2017 · N284UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2017072719828Doubler · wornINSPECTION TYPE: 1C, TAIL CONE LOWER INTERNAL SKIN DOUBLER HAS DEEP WEAR. REMOVED, FABRICATED AND REPLACED THE DOUBLER IAW DWG AKC7541, SRM 51-35-01, AND 51-33-01.Jul 13, 2017 · N284UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2017072519755Floor Panel · corrodedINSPECTION TYPE: 1C, MAIN CABIN FLOOR PANEL AT BS 475 - 500 AND LBL 19 TO 27.5 HAS CORROSION. REPAIRED THE FLOOR PANEL IAW EA O11-5320-01-A6903, REV I/R, AND EO MD11-5320-65023-A.Jul 13, 2017 · N284UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2017072519751Floor Panel · corrodedINSPECTION TYPE: 1C, MAIN CABIN FLOOR PANEL AT BS 477 - 488, LBL 66 - 76 HAS CORROSION. REPAIRED THE FLOOR PANEL IAW EA 011-5320-01-A6898, REV I/R, AND EO MD11-5320-65019-A.Jul 13, 2017 · N284UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2017072619788Seat Track · corrodedINSPECTION TYPE: 1C, MAIN CABIN SEAT TRACK AT BS 497.175 AND 506.675, RBL 27.5. REPAIRED THE SEAT TRACK IAW EA 011-5310-01-A6904, REV I/R, AND EO MD11-5310-65020-A.Jul 13, 2017 · N284UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2017072319630Floor Panel · corrodedINSPECTION TYPE: 1C, MAIN CABIN FLOOR PANEL HAS CORROSION AT BS 484 AND RBL 59. REPAIRED THE FLOOR PANEL IAW EA 011-5320-01-A6902, REV I/R, AND EO MD11-5320-65014-A.Jul 13, 2017 · N284UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2017072019562Skin · corrodedINSPECTION TYPE: PE, XTERIOR FUSELAGE SKIN HAS CORROSION AT BS 2139 - 2163, LONGERONS 33 - 35R. REPAIRED THE SKIN IAW EO MD11-5330-64948-A. MAJOR.Jul 13, 2017 · N272UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2017072719810Doubler · wornINSPECTION TYPE: 1C, TAIL CONE INTERNAL DOUBLER HAS DEEP WEAR AT BS 2165.06 AND BETWEEN Z 45 TO Z 60.1. REPAIRED THE TAILCONE IAW EA 011-5350-01-A6896, REV I/R, AND EO MD11-5350-64991-A.Jul 12, 2017 · N284UP · Doug MD11F · Aerodynamic FairingsSDR FDEA201707121920Seat Track · damagedMAIN DECK SEAT TRACK AT BS 710, LBL 75.25 CROWN FOUND DAMAGED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 12, 2017 · N529FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201707121933Support · crackedLEFT WING LEADING EDGE LOWER SURFACE SUPPORT FORMER AT XOS 1084 FOUND CRACKED. REMOVED IAW SRM 51-31-01-0G. A NEW SUPPORT FORMER FABRICATED IAW DRAWING ARB2920, REV BB, AND INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 12, 2017 · N529FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201707121924Seat Track · corrodedMAIN DECK SEAT TRACK AT BS 1671, RBL 27.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 12, 2017 · N529FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201707121922Seat Track · corrodedMAIN DECK SEAT TRACK AT BS 1169, LBL 8.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 12, 2017 · N529FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201707121921Seat Track · corrodedMAIN DECK SEAT TRACK AT STATION 5-75, RBL 47.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 12, 2017 · N529FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201707121919Seat Track · damagedMAIN DECK SEAT TRACK AT BS 795, LBL 75.25 CROWN FOUND DAMAGED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 12, 2017 · N529FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201707121923Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT BS 1451, RBL 8.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 12, 2017 · N529FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
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