Boeing MD-11F
Service difficulty reports · 31,320
Newest first. General aviation reporting is voluntary.
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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.SDR 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.SDR 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.SDR 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.SDR 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 FABRISDR 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". OVERSISDR 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". SHOUSDR 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". SHOSDR 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 BUSHISDR 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 0.369SDR 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 BUSHISDR 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 BUSHINGSDR 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 FABRICATESDR 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 FABRICATEDSDR 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". OVERSSDR 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 0.442SDR 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 0.320SDR 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 BSDR 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". OVESDR 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". OVERSDR 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", MSDR 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", MSDR 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". SSDR 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", MISDR 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.SDR 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.SDR 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.SDR 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.SDR 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 MD11-5730-430SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 FLOSDR 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 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.SDR 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 CONSDR IPXA2015090393064Frame · dentedINSPECTION TYPE: 4C, MAIN CABIN FRAME DENTED, BS 735 AT L12R. REPAIRED IAW SRM 53-00-07, REPAIR 2, FIG 201.SDR IPXA2015081792435Indicator · obstructedL1 SLIDE PRESSURE NOT VISABLE. CLEARED VIEWING GLASS.SDR 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.SDR 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.SDR 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.SDR 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 201SDR 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.SDR 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.SDR 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 5SDR 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.
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