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 FDEA201508192613Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, UPPER MOUNT, OTBD HOLE BORE CORRODED. BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0319687 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 19, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508192612Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, UPPER BARREL NUTS HOLE SURFACE CORROSION. REPAIRED IAW CMM 57-44-08. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 19, 2015 · N631FE · Doug MD11F · Trailing Edge FlapsSDR IPXA2015083192973Skin · crackedINSPECTION TYPE: 1C, LEFT WING DROOP L/E SKIN CRACKED. REPAIRED LT DROOP L/E SKIN IAW SRM 57-40-01, REPAIR 5, FIG 201.Aug 17, 2015 · N289UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2015083192903Skin · corrodedINSPECTION TYPE: 1C, LT WING UPPER SKIN CORRODED XORS 433 ABOVE REAR SPAR. REPAIRED IAW EA 011-5722-01-A5940, REV IR AND EO MD11-5730-58572-A.Aug 17, 2015 · N289UP · Doug MD11F · Wing, Plate/SkinSDR FDEA201508172596Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 1.205", FINAL HOLE DIAMETER 1.223", MAX ALLOWABLE DIAMETER 1.220". BUSHING FABRIAug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172595Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, FWD MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 6 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 1.253", FINAL HOLE DIAMETER 1.258", MAX ALLOWABLE HOLE DIAMETER 1.254". OVERSIAug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172594Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.704", FINAL HOLE DIAMETER 0.723", MAX ALLOWABLE HOLE DIAMETER 0.709". SHOUAug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172593Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.703", FINAL HOLE DIAMETER 0.723", MAX ALLOWABLE HOLE DIAMETER 0.709". SHOAug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172592Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, PIVOT HOLE BORE CORROSION. CORROSION AT HOLE 4 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 2.311", FINAL HOLE DIAMETER 2.318", MAX ALLOWABLE HOLE DIAMETER 2.3135". OVERSIZED BUSHIAug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172591Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUT HOLE SURFACE CORROSION. CORROSION REWORKED IAW CMM 57-44-08. EXISTING THICKNESS UPPER 0.376", LOWER 0.376", MATERIAL REMOVED UPPER 0.007", LOWER: 0.007", REMAINING THICKNESS UPPER 0.369", LOWER 0.369Aug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172590Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, UPPER BARREL NUT HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.597", FINAL HOLE DIAMETER 0.631", MAX ALLOWABLE HOLE DIAMETER 0.621". OVERSIZED BUSHIAug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172589Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER BARREL NUT HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.597", FINAL HOLE DIAMETER 0.631", MAX ALLOWABLE HOLE DIAMETER 0.621". OVERSIZED BUSHINGAug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172588Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER BARREL NUT HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 0.390", FINAL HOLE 0.408", MAXIMUM ALLOWABLE HOLE 0.391". OVERSIZED BUSHING FABRICATEAug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172587Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER BARREL NUT HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 0.390", FINAL HOLE 0.407", MAXIMUM ALLOWABLE HOLE 0.391". OVERSIZED BUSHING FABRICATEDAug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172586Hinge Bracket · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE BORE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION AT HOLE 10 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 0.668", FINAL HOLE 0.691", MAXIMUM ALLOWABLE HOLE 0.667". OVERSAug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172585Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE SURFACE CORROSION. CORROSION REWORKED IAW CMM 57-44-09. EXISTING THICKNESS UPPER 0.426", LOWER 0.448", MATERIAL REMOVED UPPER 0.006", LOWER 0.006", REMAINING THICKNESS UPPER 0.420", LOWER 0.442Aug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172584Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE SURFACE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.328", MATERIAL REMOVED 0.013", REMAINING THICKNESS 0.315", MINIMUM ALLOWABLE THICKNESS 0.320Aug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172583Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 1.253", FINAL HOLE 1.257", MAXIMUM ALLOWABLE HOLE 1.220". OVERSIZED BUSHING FABRICATED BAug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172582Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, FWD MOUNT OTBD HOLE BORE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION AT HOLE 6 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 1.258", FINAL HOLE 1.282", MAXIMUM ALLOWABLE HOLE 1.258". OVEAug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172581Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION AT HOLE 8, REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 1.253", FINAL HOLE 1.257, MAXIMUM ALLOWABLE HOLE 1.220". OVERAug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172580Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE SURFACE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.365", MATERIAL REMOVED 0.004", REMAINING THICKNESS 0.361", MAug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172579Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE SURFACE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.357", MATERIAL REMOVED 0.004", REMAINING THICKNESS 0.353", MAug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172578Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION AT HOLE 3 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 0.522", FINAL HOLE 0.591", MAXIMUM ALLOWABLE HOLE 0.584". SAug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508172577Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT OTBD HOLE SURFACE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.723", MATERIAL REMOVED 0.006", REMAINING THICKNESS 0.717", MIAug 17, 2015 · N631FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR IPXA2015081792397Channel · damagedFWD LWR CARGO CEILING SUPPORT DAMAGED AT BS 982 X 14. REPLACED SUPPORT CHANNEL IAW EO MD11-2550-57752-B, PARA 6C AND DWG ADA8012.Aug 17, 2015 · N276UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2015082992860Angle · chafedINSPECTION TYPE: 1C, LT WING T/E PANEL LANDING ANGLE CHAFED NEAR PANEL 551DB. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT LANDING ANGLE IAW DWG ARC0751 AND SRM 51-33-01.Aug 16, 2015 · N289UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2015083192901Skin · corrodedINSPECTION TYPE:1C, RT WING UPPER SKIN CORRODED XORS 622-654, STRINGERS 7-9. REPAIRED THE WING SKIN PANEL IAW EA 011-5722-01-A5941, REV IR AND EO MD11-58573-A.Aug 16, 2015 · N289UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2015083092878Doubler · crackedINSPECTION TYPE: 1C, LEFT WING FIXED L/E BEADED DOUBLER CRACKED AT XOS 762. REPAIRED THE DOUBLER FROM XOS 753 - 768 IAW SRM 57-40-02, REPAIR 15, FIG 203.Aug 16, 2015 · N289UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2015083092876Skin · wornINSPECTION TYPE:1C, RIGHT WING FIXED L/E SKIN AT TELESCOPIC DUCT CUTOUT HAS WEAR DAMAGE ON REPAIR DOUBLER BS XOS 464 TO XOS 470. ACCOMPLISHED PERMANENT REPAIR ON RT WING FIXED L/E SKIN AROUND TELESCOPIC DUCT CUTOUT BS XOS 464 TO XOS 470 IAW SREO MD11-5730-430Aug 16, 2015 · N289UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2015083092875Doubler · crackedINSPECTION TYPE: 1C, LEFT WING FIXED L/E BEADED DOUBLER CRACKED AT BS XOS 792. TEMP REPAIRED BS XOS 789 - 795 IAW SRM 57-40-02, REPAIR 15, FIGURE 206.Aug 16, 2015 · N289UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2015083092874Doubler · crackedINSPECTION TYPE: 1C, LT WING FIXED L/E BEADED DOUBLER CRACKED AT BS XOS 707. TEMP REPAIRED THE DOUBLER BS XOS 703 TO 708 IAW SRM 57-40-02, REPAIR 15, FIG 206.Aug 16, 2015 · N289UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2015083092881Doubler · crackedINSPECTION TYPE: 1C, RT WING FIXED L/E BEADED DOUBLER CRACKED AT BS XOS 731. ACCOMPLISHED A REPAIR ON RT WING FIXED L/E BEADED DOUBLER BS XOS 728.66 TO 734.75 IAW SRM 57-40-02, REPAIR 15, FIG 203.Aug 16, 2015 · N289UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2015083192913Doubler · crackedINSPECTION TYPE: 1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS629. INSTALLED A NEW BEADED DOUBLER REPAIR XOS 621-648 IAW EA 011-5730-01-A5927, REV IR AND EO MD11-5730-58570-A.Aug 16, 2015 · N289UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2015083192912Spar Cap · corrodedINSPECTION TYPE: 1C, RT WING AFT SPAR UPPER CAP AFT FLANGE CORRODED, NUMEROUS LOCATIONS BETWEEN XORS 424 -927. REPAIRED NOTED CORROSION IAW EA 011-5710-01-A5934, REV. IR AND EO MD11-5710-58542-A.Aug 16, 2015 · N289UP · Doug MD11F · Wing SparSDR IPXA2015083192968Skin · corrodedINSPECTION TYPE: 1C, RT WING UPPER SKIN CORRODED ABOVE REAR SPAR, BS XORS 865-909. REPAIRED NOTED CORROSION IAW EA 011-5730-01-A5939, REV. IR AND EO MD11-5730-58559-A.Aug 16, 2015 · N289UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2015082992853Former · crackedINSPECTION TYPE: 1C, RIGHT WING FIXED L/E FORMER CRACKED NEAR BS XES 247. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FORMER IAW DWG ARB3006 AND SRM 51-31-01.Aug 16, 2015 · N289UP · Doug MD11F · Wing SparSDR FDEA201508162575Actuator · malfunctionedAT CRUISE FLIGHT AT FL380, RECEIVED A LEVEL 3 CABIN ALTITUDE. QRH ACTION AVIONICS FAN OVRD CORRECTED PROBLEM. AFTER APPROX 10 MINUTES PROBLEM RETURNED. HAD TO INITIATE DESCENT TO FL320 TO MAINTAIN PRESS. THERE WAS A SLIGHT VIBRATION UNDER THE CAPTAIN'S FLOAug 16, 2015 · N605FE · Doug MD11F · Pressure Regulator/Outflow ValveSDR FDEA201508162566Cap · looseNUMBER 1 ENG OIL PRESS DISPLAYED AN AMBER BOX, 15 MIN AFTER DEPARTURE, CLIMB POWER FL335 TO FL350. AT CRUISE, PRESS WENT INTO GREEN. AMBER BOX APPEARED AGAIN WITH A LOSS OF 3 QTS OIL, 20 INTO FLIGHT. PRECAUTIONARY SHUTDOWN INFLIGHT, WIND MILLED FROM 1422Z Aug 16, 2015 · N574FE · Doug MD11F · Engine Oil Storage (Airframe Furnished)SDR IPXA2015083192969Doubler · crackedINSPECTION TYPE: 1C, LEFT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS 637. REPAIRED THE DOUBLER IAW EA 011-5730-01-A5927 REV IR AND EO MD11-5730-58570-A.Aug 15, 2015 · N289UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2015081792436Unknown · odorAT CRUSE, NOTICED A SLIGHT ODOR OF BURNED RUBBER. SMELL IS CONFINED TO THE COCKPIT ONLY. UNABLE TO DETERMINE ORGIN. CLEARED ABOUT 1 HOUR PRIOR TO TOP OF DESCENT THEN RETURNED IN THE DESCENT, REF PREVIOUS WRITE UP, LOG PG 9806320, 14 AUG 15. OPERATE AIR CONAug 15, 2015 · N286UP · Doug MD11F · Air Distribution SystemSDR IPXA2015090393064Frame · dentedINSPECTION TYPE: 4C, MAIN CABIN FRAME DENTED, BS 735 AT L12R. REPAIRED IAW SRM 53-00-07, REPAIR 2, FIG 201.Aug 14, 2015 · N284UP · Doug MD11F · Fuselage Main, FrameSDR IPXA2015081792435Indicator · obstructedL1 SLIDE PRESSURE NOT VISABLE. CLEARED VIEWING GLASS.Aug 14, 2015 · N282UP · Doug MD11F · Escape SlideSDR IPXA2015081492356Unknown · odorNOTICED A BURNED RUBBER ODOR FROM TOP OF DESCENT. NOT SURE OF ORIGIN. RAN ENGINES, ALSO RAN RTS PACK CONTROLLER IAW MM 21-62-00-501. NO ODOR NOTED AT THIS TIME PACKS RAN ALSO 21-53-00.Aug 14, 2015 · N286UP · Doug MD11F · Air Distribution SystemSDR IPXA2015090593156Channel · chafedINSPECTION TYPE: 4C, NR 2 PYLON SEAL SUPPORT CHANNEL CHAFED YPTN2 = 96.5. REPAIRED IAW EA 011-5400-01-A5947, REV IR AND EO MD11-5420-58618-A.Aug 13, 2015 · N284UP · Doug MD11F · Nacelle/Pylon Miscellaneous StructureSDR IPXA2015090593161Vane · chafedINSPECTION TYPE: 4C, LT OTBD FLAP VANE NR 1 TRACK CHAFE DAMAGE. REPAIRED CHAFE DAMAGE TO NOTED FLAP VANE TRACK IAW EA 011-5753-01-A5951, REV IR AND EO MD11-5740-58634-A.Aug 13, 2015 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2015090293049Door Frame · crackedINSPECTION TYPE: 4C, L3 DOOR FRAME LOWER FORWARD LIGHTNING HOLE CRACKED BS 1250 - 1256. REPAIRED IAW SRM 53-40-15, REPAIR 3, FIGURE 201Aug 13, 2015 · N284UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2015083192967Support · damagedINSPECTION TYPE:4C, R1 DOOR ESCAPE SLIDE FWD SUPPORT CHAFED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SUPPORT IAW DWG ARB9513 AND SRM 51-35-01.Aug 13, 2015 · N284UP · Doug MD11F · Escape SlideSDR IPXA2015083192966Support · damagedINSPECTION TYPE:4C, R1 DOOR ESCAPE SLIDE AFT SUPPORT CHAFED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SUPPORT IAW DWG ABA8513 AND SRM 51-35-01.Aug 13, 2015 · N284UP · Doug MD11F · Escape SlideSDR FDEA201508132542Doubler · crackedRIGHT WING LE COMPARTMENT AT APPROX STATION XOS 789, FOUND WITH CONTOUR LONGITUDINAL FRAME DOUBLER CRACKED. LONGITUDINAL FRAME DOUBLER REMOVED IAW SRM 51-31-01-0G, NEW FRAME DOUBLER FABRICATED IAW DWG ARB3954 REVISION K. NEW FRAME DOUBLER INSTALLED IAW SRM 5Aug 13, 2015 · N529FE · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2015090993294Skin · corrodedINSPECTION TYPE:4C, CORROSION ON CENTER WING UPPER SKIN AT STR 15, XCW 102 ACCOMPLISHED PERMANENT BLEND REPAIR ON CENTER WING UPPER SKIN AT STR 15, XCW 102 IAW EA 011-5730-01-A5933 AND EO MD11-5730-58608-A.Aug 12, 2015 · N284UP · Doug MD11F · Fuselage Main, Plate/Skin
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