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 IPXA2018110935815Oil System · leakingSTRONG ODOR IN THE COCKPIT. THE ODOR THAT WAS PREVIOUSLY TROUBLESHOT, CAME BACK STRONG DURING CLIMB OUT, CAUSED BURNING EYES, THROAT, LUNGS. COMPLIED WITH AIR CONDITONING PACKS AND DUCTS, RUNNING APU FOR 1.5 HOURS, OIL QUANTITY WAS 8.0, AFTER 1.5 HOURS, THESDR FDEA201811073125Hinge Bracket · corrodedRIGHT HAND WING INBOARD FLAP OUTBOARD AFT (FLAP SIDE) HINGE PIVOT INBOARD HOLE BORE CORROSION. HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-130949C PART5 STEP 2SDR FDEA201811073124Hinge Bracket · corrodedRIGHT HAND WING INBOARD FLAP OUTBOARD AFT (FLAP SIDE) HINGE PIVOT OUTBOARD HOLE BORE CORROSION. HOLE BORE (HOLE B AND A) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-130949CSDR FDEA201811073123Hinge Bracket · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD AFT (FLAP SIDE) HINGE PIVOT OUTBOARD HOLE BORE CORROSION. HOLE BORE (HOLE B AND A) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-130946C PASDR FDEA201811073122Hinge Bracket · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD AFT (FLAP SIDE) HINGE PIVOT INBOARD HOLE BORE CORROSION. HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-130946C PARSDR FDEA201811073121Hinge Bracket · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD FORWARD (WING SIDE) HINGE ACTUATOR OUTBOARD HOLE BORE CORROSION. HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0343SDR FDEA201811073120Hinge Bracket · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD FORWARD (WING SIDE) HINGE ACTUATOR INBOARD HOLE BORE CORROSION. HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T03434SDR FDEA201811073119Hinge Bracket · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD FORWARD (WING SIDE) HINGE LOWER BARREL NUT HOLE BORE CORROSION. HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T03434SDR FDEA201811073117Hinge Bracket · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD FORWARD (WING SIDE) HINGE UPPER BARREL NUT HOLE BORE CORROSION. HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T03434SDR FDEA201811073116Hinge Bracket · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD FORWARD (WING SIDE) HINGE LOWER MOUNT OUTBOARD HOLE BORE CORROSION. HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0343410 P1 STEP 2B AND INSTALLED SDR FDEA201811073115Hinge Bracket · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD FORWARD (WING SIDE) HINGE LOWER MOUNT INBOARD HOLE BORE CORROSION. HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0343410 P1 STEP 2B AND INSTALLED ASDR FDEA201811073114Hinge Bracket · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD FORWARD (WING SIDE) HINGE UPPER MOUNT OUTBOARD HOLE BORE CORROSION. HOLE BORE (NR 2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0SDR FDEA201811073113Hinge Bracket · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD FORWARD (WING SIDE) HINGE PIVOT HOLE BORE CORROSION. HOLE BORE (NR 4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44- 09 AND EA 1-5750-T0343410 P1 STESDR FDEA2018110763108Doubler · crackedLEFT HAND WING - LEFT HAND LEADING EDGE BEADED DOUBLER AT STATION XOS = 708 FOUND CRACKED AS MARKED. REPAIR CARRIED OUT AT LEFT HAND WING LEADING EGDE BEADED DOUBLER AT STATION XOS 708 AS PER STRUCTURE REPAIR MANUAL 57-40-02-2R, FIGURE 203, REPAIR 15. REPSDR IPXA2018111235887Longeron Splice · crackedINSPECTION TYPE: 4C, LONGERON 48L SPLICE FITTING WAS CRACKED AT BS 1541. REMOVED, FABRICATED, AND REPLACED THE LONGERON IAW DWG A5A7124, AND SRM 51-31-01. MINOR.SDR IPXA2018110535633Cover · brokenLIFE VEST COVER BROKEN IN PASSENGER AREA. REMOVED AND REPLACED THE LIFE VEST COVER IAW AMM 25-64-01.SDR IPXA2018111656000Longeron · corrodedINSPECTION TYPE: 4C, LOWER CARGO LONGERON 48L WAS CORRODED BETWEEN BS 1531 - 1551. REPAIRED THE LONGERON BETWEEN BS 1531 - 1551 IAW EA 011-5310-01-A7535, REV I/R, AND EO MD11-5310-70611-A. MAJOR.SDR IPXA2018111235889Retainer · crackedINSPECTION TYPE: 4C, CENTER CARGO FLOOR SUPPORT RETAINER WAS CRACKED AT BS 1521. REMOVED, FABRICATED, AND REPLACED THE RETAINER IAW DWG AEA0341, AND SRM 51-35-01. MINOR.SDR FDEA201811013079Computer · failedCLIMBING THROUGH FL200, RECEIVED A LEVEL 2 STAB OUT OF TRIM WARNING. SWITCHED AUTOPILOT IAW QRH. AUTOPILOT 2 WOULD DISCONNECT BECUASE OF STAB TRIM INOPERATIVE. AUTOPILOT 1 CONTINUED TO DISPLAY STAB OUT OF TRIM. INTERROGATED BOTH FCCS. NR 1 FCC HAS NO FSDR IPXA2018111656007Fairing · crackedINSPECTION TYPE: 4C, RT WING PERFORMANCE FAIRING WAS CRACKED COMMON TO THE ALIGNMENT HOLE AT XIS 150.74. REPAIRED THE FAIRING IAW EA 011-5754-01-A7536, REV I/R, AND EO MD11-5720-70620-A. MINOR.SDR IPXA201811145944Spar Cap · corrodedINSPECTION TYPE: 4C, RT WING REAR SPAR UPPER CAP HAD CORROSION BETWEEN XORS 452.75 - 488.25, AND XORS 523.75 - 544.5. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A7539, REV I/R, AND EO MD11-5710-70589-A. MINOR.SDR IPXA2018111205846Doubler · crackedINSPECTION TYPE: 4C, RT WING LE BEADED DOUBLER WAS CRACKED BETWEEN XOS 783 & 789. REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIGURE 205, REV 65. MAJOR.SDR IPXA2018110935814Floor Panel · delaminatedAFTER REMOVAL OF BALLMAT IN MAIN CABIN, FOUND THE FLOOR PANEL 231HF BADLY DELAMINATED AND SPLINTERED. REMOVED THE FLOOR PANEL, FABRICATED A REPLACEMENT AND INSTALLED IAW DWG WSP0823, AND AMM 53-21-02. MINOR.SDR FDEA201810313067Warning System · activatedJUST AFTER RETRACTING LANDING GEAR IN TAKE OFF, RECEIVED LVL 2 BRAKE OVERHEAT. NR 6 BRAKE TEMP WAS MISSING, FOLLOWED QRH AND EXTENDED LANDING GEAR. AFTER ABOUT 1 MINUTE NUMBER 6 BRAKE FLICKED NUMEROUS HIGH TEMPS AND THEN SHOWED STEADY TEMP OF 375 DEGREE, ABSDR FDEA201810313063Transmitter · failed"TIRE FAIL" ANNUNCIATED WHEN LEVELING AT FL350 LEFT NOSE WHEEL INDICATED LOW PRESS THEN TIRE FAIL. REMOVED AND REPLACED LT NOSE WHEEL TIRE PRESS TRANS, REF AMM 32-46-04-4, OPS CHKD GOOD.SDR IPXA2018111435965Pan · crackedINSPECTION TYPE: 4C, LT MLG DOOR CENTER, LOWER, FWD CORNER PAN WAS CRACKED. REMOVED AND REPLACED THE MLG DOOR PAN IAW SRM 51-35-01, & 51-35-02. MINOR.SDR IPXA201811145951Support Frame · crackedINSPECTION TYPE: 4C, SUPPORT FRAME WAS CRACKED INSIDE 311 ACCESS HOLE AT BS 2122. REMOVED, FABRICATED, AND REPLACED SUPPORT FRAME IAW DWG AJC7372, AND SRM 51-33-01. MINOR.SDR IPXA201811145949Frame Angle · crackedINSPECTION TYPE: 4C, SUPPORT FRAME ANGLE WAS CRACKED INSIDE 311 ACCESS HOLE AT BS 2047. REMOVED AND REPLACED SUPPORT FRAME ANGLE IAW SRM 51-33-01, AND 51-35-01. MINOR.SDR IPXA2018111435948Frame Angle · crackedINSPECTION TYPE: 4C, SUPPORT FRAME ANGLE WAS CRACKED INSIDE 311 ACCESS HOLE ON CEILING AT BS 2065. REMOVED AND REPLACED SUPPORT FRAME ANGLE IAW SRM 51-33-01, AND 51-35-01. MINOR.SDR IPXA2018111205845Web · crackedINSPECTION TYPE: 4C, WEB CRACKED AT BS 1372 & LBL 80. REPAIRED THE WEB IAW EO MD11-5710-70496-A. MAJOR.SDR IPXA2018110935830Skin · crackedLEFT WING FIXED LE SKIN WAS CRACKED AT THE NR 14 SLAT TRACK CUT OUT. REPAIRED THE SKIN AT XOS 889 IAW SRM 57-40-02, REPAIR 7, FIGURE 201, REV 65. MAJOR.SDR IPXA2018110213546Switch · inoperativeLIFE RAFT ON THE L1 DOOR WOULD NOT TEST. R & R THE PRESS TO TEST SWITCH ON THE L1 DOOR IAW AMM 25-61-04. OPS TESTED GOOD.SDR IPXA2018103105483Cylinder · low pressureL1 DOOR EMERGENCY CYLINDER WAS BELOW LIMITS. THE DOOR CYLINDER WAS SERVICED IAW AMM 52-11-04-501, REV 91.02.SDR IPXA2018111656006Skin · chafedINSPECTION TYPE: 4C, LT WING L/E SKIN WAS CHAFED AT XLDE 330.2745. REPAIRED WING SKIN IAW EO MD11-5730-63460-C. MAJOR.SDR IPXA2018111435966Barrier · damagedRIGID CARGO BARRIER WALL PREVIOUS REPAIR WAS CORRODED. NO CORROSION FOUND DURING INSPECTION, REPAIRED RIGID CARGO BARRIER IAW EO MD11-5310-70473-A. MINOR.SDR IPXA2018111205852Fastener · shearedINSPECTION TYPE: 3C, FOUND A SHEARED FASTENER BETWEEN BS 316.9 - 345.7. REMOVED AND REPLACED THE FASTENER IAW EA 011-5730-01-A7537, REV IR, AND EO MD11-5730-70571-A. MINOR.SDR IPXA2018111205844Web · crackedINSPECTION TYPE: 4C, RIGHT OVERWING UPPER FUEL TANK AFT WEB WAS CRACKED AT BS 1372 & RBL 80. REPAIRED THE WEB IAW EO MD11-5710-70497-A. MAJOR.SDR FDEA201810293042Hinge · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE CORROSION. HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE (HOLE 4) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED AND INSTALLED AS PER CSDR FDEA201810293041Hinge · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE CORROSION. HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE (HOLE 4) REWORKED AND FOUND WITHIN LIMIT AS PER COMPONENT MAINTENANCE MANUAL 57-44-07. REPAIR BUSHING FABRICATEDSDR FDEA201810293040Hinge · corrodedRIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE CORROSION. HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE (HOLE 4) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED AND INSTALLED AS PER COSDR FDEA201810293039Hinge · corrodedRIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE CORROSION. HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE (HOLE 4) REWORKED AND FOUND WITHIN LIMIT AS PER COMPONENT MM 57-44-07. REPAIR BUSHING FABRICATED AND INSTALLESDR IPXA2018111235888Stiffener · crackedINSPECTION TYPE: 4C, RIGHT MLG WW, AFT OTBD SIDEWALL STIFFENER WAS CRACKED. REMOVED, FABRICATED, AND REPLACED THE STIFFENER IAW DWG ANB7203, AND SRM 51-31-01. MINOR.SDR IPXA2018103105511Bottle · low pressureLEFT CREW DOOR PNEUMATIC STORAGE PRESSURE WAS LOW. SERVICED THE BOTTLE IAW AMM 12-25-04. ACFT OK FOR SERVICE.SDR FDEA2018102983035Support Bracket · damagedLT MAIN GEAR WHEEL WELL AFT STRUCTURE SUPPORT NEAR I/B SPOILER, BROKEN REPLACED SUPPORT BRACKET.SDR FDEA2018102973032Computer · malfunctionedUNSUCCESFUL AUTOLAND 36L MEMPHIS WIND 240/4, AUTOPILOT FLARE AT 40 FT AGL, AUTOPILOT AGGESSIVELY PITCHED OVER AT 15 FT AGL CAUSING A HARD LANDING, BOUNCE X 2, PORPOSE X 2 AND POSSIBLE NOSE WHEEL FIRST CONTACT WITH RUNWAY, DURING G0-AROUND. R/R NR 1 FCC REF MMSDR FDEA201810263018Brace · crackedL/H MAIN GEAR WHEEL WELL AFT STRUCTURE SUPPORT NEAR I/B SPOILER CRACKED REMOVED AND REPLACED BRACE.SDR FDEA2018102963018Support · crackedLT MAIN GEAR WHEEL WELL AFT STRUCTURE SUPPORT NEAR I/B SPOILER CRACKED IN WORK.SDR FDEA201810242989Power Supply · inoperativeEMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY REF AMM 33-51-01-4. OPS CK GOOD.SDR IPXA2018102655342Door · bindingL1 DOOR WILL NOT CLOSE AND SECURE PROPERLY, AFTER BINDING WITH CREW REST MODULER AND RT DOOR IAW MM 52-11-02-400-800, STEPS D2, & F. OPS CHECKED GOOD.SDR IPXA2018111215872Stringer · crackedINSPECTION TYPE: 3C, LT WING STRINGER 32 WAS CRACKED BETWEEN XORS 896.070 & 917.200. REPAIRED THE STRINGER IAW EA 011-5710-01-A7515, REV I/R, AND EO MD11-5710-70579-A. MAJOR.
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