Mcdonnell Douglas MD-11
Service difficulty reports · 7,956
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 = 'MD11' 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 = 'MD11' 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 FDEA201311262878Life Vest · missingFIRST OFFICER`S LIFE VEST IS MISSING. INSTALLED NEW LIFE VEST AT FIRST OFFICER'S SEAT LOCATION IAW FX MD11, SERVICE CHECKED ACFT OK FOR FLIGHT.SDR FDEA201311252866Indicator · inoperativeMDIS 63125-60 0009630 23NOV13 ANC CLOSE R1 DOOR SLIDE REMOTE PRESS INDICATOR INOPERATIVE. FACT 23NOV13 22:53. ANC R RELAMPED R1 DOOR REMOTE PRESS INDICATOR IAW MM 25-61-04-4, OK FOR SERVICE.SDR WRLA20130922602Apu · shutdownDURING DEPARTURE, APU SHUTDOWN AT NR2 ENGINE START. ENGINE AROUND 22 PERCENT N2 WHEN APU STARTED TO ROLL BACK AND COULD NOT SUSTAIN THE ENGINE START. SHUT IT DOWN AND REQUESTED AN AIR START. GROUND PERSONNEL REPORTED SMOKE COMING FROM THE NR 2 ENGINE. MX SDR FDEA201304270870Electrical Sys · malfunctionedEMERGENCY POWER ON ALERT 1:15 INTO FLIGHT IAW QRH CYCLED SWITCH OFF THEN BACK TO ARM. EMERGENCY POWER ON LIGHT REMAINED. NO OTHER ALERTS DISPLAYED. DEPLOYED ADG IAW QRH. STOWED ADG (WRI 24-00/9915) ELECTRICAL SYS RETURNED TO NORMAL. RAN ALL THREE ENGINESDR WRLA20130401588Connector · unsecureUPON ARRIVAL AT STATION KTIK, FWD ZONE EMERGENCY LIGHTS CAME ON AND WOULD NOT SHUT OFF. PROBLEM WAS CORRECTED BY RESECURING OF THE EMERGENCY BATTERY CONNECTOR. NO FURTHER FAULTS NOTED.SDR WRLA20130304586Door · nickedCRACK - DURING 4C CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND TWO NICKS ON THE SKIN OF LEFT WING SLAT ACTUATOR DOOR PANEL 518FB.SDR WRLA20130304585Skin · corrodedCRACK - DURING 4C CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CORROSION ON THE UPPER SURFACE OF FWD UNDERWING BARREL LOWER SKIN BETWEEN STA 1521 AND STA 5-00/1531, LONGERON 51R AND 50R.SDR WRLA20130301584Longeron · crackedCRACK - DURING 4C CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CORROSION ON THE LONGERON L-40R AT STA Y=1987.SDR WRLA20130301583Seat Track · crackedCRACK - DURING 4C CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CORROSION ON CABIN SEAT TRACK AT STA Y=522, X=-75.25.SDR WRLA20130301582Skin · crackedCRACK - DURING 4C CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CORROSION ON UPPER SKIN UPPER SURFACE OF CENTER WING AT STA Y=1240, X=107.25 AND STA Y=1250, X=107.25.SDR WRLA20130224579Unknown · smokeAIR RETURN - SMOKE IN COCKPIT. REMOVED ALL DU'S, GLARESHIELD, AND OPENED ALL CB PANELS FOR INSPECTIONS. FOUND NO CHAFING WIRES OR BURN INDICATIONS. PERFORMED RTS OF ALL SYSTEMS THRU CFDS, ALL TESTS PASSED. REPLACED 3 COALESCER BAGS.SDR WRLA20130111578Unknown · odorELECTRICAL BURNING ODOR DURING, SMOKE/ FUME CHECKLIST COMPLIED WITH , ODOR DISSIPATED WHEN ELEC/AIR SWITCH PLACED TO THE 3/1 POSITION. MAINTENANCE RETURNED ALL ELECTRICAL SYSTEMS TO NORMAL ACCOMPLISHED INSPECTION OF THE FWD AVIONICS BAY ELECTRICAL BOXES NO ABSDR WRLA20121229577Battery Pack · failedDURING PRE-FLIGHT INSPECTION FOUND NR 2 EMERGENCY BATTERY PACK FAILED TEST (NOTE: NR 2 BATTERY PACK REMOVED). REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY NR 2 BATTERY IAW MM 33-51-01. OPS CHECK OK.SDR WRLA20121117564Web · crackedCRACK - DURING C04 CHECK, EGAT MECHANIC FOUND CRACK ON RIGHT WEB PN: ACA3804-27 AT AIR CONDITION DOOR JAMB, STA Y=555, L-36. REPAIRED PER EGAT EI: W2012A53B-2619, R00,R01. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR WRLA20121117563Skin · crackedCRACK - DURING C04 CHECK, EGAT MECHANIC FOUND CRACKS ON RIGHT FAIRING SKIN OF TAIL PYLON LWR AFT SECTION. REPAIRED PER EGAT EI: W2012A54B-2664,R01. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR WRLA20121117562Seat Track · corrodedCORROSION - DURING C04 CHECK, EGAT MECHANIC FOUND CABIN SEAT TRACK CORROSION AT STA 1351, X= -75.25. REPAIRED DAMAGED AREA PER MD-11 SRM 53-00-52, REPAIR 1, REV 50. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR WRLA20121117561Seat Track · corrodedCORROSION - DURING C04 CHECK, EGAT MECHANIC FOUND CABIN SEAT TRACK CORROSION AT STA 460, X= -27.5. REPAIRED DAMAGED AREA PER MD-11 SRM 53-00-52, REPAIR 1, REV 50. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR WRLA20121117559Longeron · corrodedCORROSION - DURING C04 CHECK, EGAT MECHANIC FOUND LONGERON 51LT LOCATED AT STA 1701 TO STA 1721 ON CENTER CARGO COMPT. REPAIRED DAMAGED AREA PER MD-11 SRM 53-00-05, REPAIR 1, REV 50. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR WRLA20121117558Cargo Track · corrodedCORROSION - DURING C04 CHECK, EGAT MECHANIC FOUND LONGERON SURFACE LOCATED ON CENTER CARGO UNDER FLOOR AT LONGERON 51 LEFT AT STA 1601 TO STA 1621. REPAIRED DAMAGED AREA PER MD-11 SRM 53-00-05, REPAIR 1, REV 50. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR WRLA20121116565Skin · dentedDENT - DURING C04 CHECK, EGAT MECHANIC FOUND TWO DENTS ON FUSELAGE SKIN BETWEEN STA Y -495 AND Y=515, L-25L AND L-28L. REPAIRED PER EGAT EI: W2012A53B-2668, R00, R01, R02, R03. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR WRLA20121116560Frame · crackedCRACK - DURING C04 CHECK, EGAT MECHANIC FOUND CRACKS ON FRAME (P/N: AGA7098-3) AND CAP (AGA7098-7) AT STA Y=1841.SDR WRLA20121110566Web · corrodedCORROSION - DURING C04 CHECK, EGAT MECHANIC FOUND CORROSION ON HORIZONTAL WEB (P/N: NCA6048-3) OF NOSE WHEEL WELL AT STA Y=515. REPAIRED PER EGAT EI:W2012A53B-2699, R00, R01, R02. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR WRLA20120602546Skin · gougedGOUGE / DENT FOUND DURING PRIMARY INSPECTION AT FUSELAGE STA 755 L-24 & L25 MEASURED 3.00 X .133. ACCOMPLISHED HFEC INSPECTION ON DENT, NO CRACKS FOUND FOLLOWING BLEND-OUT OF THE EFFECTED AREA ACCOMPLISHED UT INSPECTION OF EFFECTED AREA AND FOUND SKIN THICKNESDR WRLA20120524545Structure · corrodedCORROSION ON TOP OF CENTER WING BOX AT STA 1249 BETWEEN X=75.25 AND X=709.25 RT.SDR WRLA20120521544Fitting · crackedCRACK - FOUND NOSE LANDING GEAR TRUNNION FITTING ON LEFT SIDE HAD CRACK STA Y=595 L=0.5". IAW AMM 32-21-01-000-801 REV B REMOVED NOSE LANDING GEAR ASSY. REPAIR THE CRACK AREA IAW SRM 53-10-14 FIGURE 202 RE. 49 REPAIR 2 IAW AMM 32-21-01-400 REINSTALLED NOSE LSDR WRLA20111226529Ballast · defectiveELECTRICAL SMOKE SMELL IN A ZONE. PULLED CEILING LIGHTS OUTBOARD CIRCUIT BREAKER AND THE SMELL WENT AWAY. FWD CABIN LIGHT INOP. ITEM PUT IN DMI LOG DMI M33DE2011-214 MEL 33-10-01-01 CAT "C", DUE ON -01-12 C ON BALLAST DISC AND C/B PULLED ON CEILING LIGHT POSDR WRLA20111212527Oven · malfunctionedGALLEY BUS 3 OFF ALERT CAME ON WHEN F/A STARTED OVENS IN AFT GALLEY. SUSPECT OVENS 1 AND 2. F/A HEARD A POP SOUND AND SAW SPARKS FROM OVEN. SHUT OVENS 1 AND 2 OFF AND RESET GALLEY BUS 3.SDR WRLA20111118525Light · inoperativeEMERGENCY FLOOR LIGHTING INOP AT 4-6 HJK. ITEM PLACED ON MEL - DMI REF NO NM31101811-103 DUE DATE 28 NOV 2011, PLACARD INSTALLED CAT-C MX CONT NOTIFIED.SDR WRLA20111020524Light · no testEMERGENCY LIGHT TEST FAILED.SDR WRLA20111009523Strap · crackedSTRAP ON RT WING L/E CRACKED FROM BOLT HOLE ABOUT 1" XOS 608. REMOVED DAMAGED STRAP IAW SRM 51-35-01 REV.47. FABRICATED STRAP IAW EI W2011P57B-2164 REV 00 AND REV 01. REPLACED DAMAGED STRAP IAW SRM 51-35-01 REV 47.SDR WRLA20111009522Skin · crackedRT WING SKIN SURFACE L/E CRACKED. REPAIRED CRACK IAW EI W2011A57B-2156, REV 00 AND REV 01.SDR WRLA20111007521Skin · crackedDURING 3C+A12 CHECK, A 0.5 INCH CRACK WAS FOUND ON RT WING L/E SKIN AT LWS 889. REPAIRED CRACK IAW EI W2011A57B-2129 REV.00, REV.01 AND REV.02.SDR WRLA20111005519Intercostal · crackedINTERCOSTAL CRACKED STA 2141, L9R. PERFORMED EI NO: W2011A53B-2141 REV.00 AND REV.01.SDR WRLA20111005520Door · damagedREMOVE EXISTING DOUBLER FOR INSPECTION DUE NO REPAIR DOCUMENTATION. AIR CONDITIONING EQUIP SYS 3 ACCESS DOOR UPPER FWD DOOR CORNER SKIN REF: EGAT N/R U05004. RMV THE DOUBLER IAW SRM 51-35-01 REV. 47. REPAIR DAMAGED AREA IAW SRM 52-40-01. REPAIR 1 FIGURE 201SDR WRLA20111004516Structure · damagedAFT CARGO DOOR LWR AFT CORNER DAMAGED. REPAIRED DAMAGE AREA IAW EI: W2011A52B-2148 REV. 00, REV.01 REV.02.SDR WRLA20111003518Trunnion · crackedFOUND NOSE LANDING GEAR TRUNNION FITTING ON LT SIDE HAS CRACK STA Y=595 L=0.6. REPAIRED IAW SRM 53-10-14, REPAIR 2, FIG 202, REV. 47 AND EI W2011A53B-2159. REV. 00SDR WRLA20111003515Seat Track · corrodedCORROSION FOUND LT MAIN DECK SEAT TRACK CORROSION STA Y535 X = 75.25. REPAIRED SEAT TRACK IAW SRM 53-00-52 REPAIR 1 REV.47 AND EI W2011A53B-2224, REV.00.SDR WRLA20111003514Seat Track · corrodedCORROSION FOUND ON RT MAIN DECK SEAT TRACK STA Y = 535 X = 75.25. REPLACED DAMAGED TRACK WITH NEW PART IAW SRM 53-33-01 AND 51-35-01 REV 47.SDR WRLA20110920510Skin · dentedAIRCRAFT DAMAGE FOUND AT SCHEDULE A-6 CHECK INITIAL WALKAROUND, DENT ON FUSELAGE FORWARD OF L-2 DOOR BETWEEN Y715 AND Y736, AT Z27. DENT WAS 4 INCH LONG, 0.750 WIDE, 0.145 DEEP. BEING REPAIRED PER SRM 53-00-01.SDR WRLA20110826509Battery · dischargedEMER LT 1L TEST FAIL. REMOVED AND REPLACED EMER LIGHT BATT SYSTEM, OPS CHECK GOOD MM 33-50.SDR WRLA20110806499Vent · corrodedAFT RT FUSELAGE FWD LAV EXH VENT CORRODED AND POPPED RIVET AT 6 O'CLOCK POSITION. FWD VENT STA 1895 BETWEEN LONGERON 39 AND 40 RT.SDR WRLA20110730497Pin · defectiveFLOOR EMERGENCY LIGHTS, ZONE B, LIT, SEAT 19D AND FWD INOP. CLEANED ALL CONNECTIONS ON FLOOR AND REPLACED AP5660023 PINS ON WIRES FRH-20WH. LIGHTS CHECK NORMAL PER MM 33-52, TROBLESHOOTING PER WDM 33-52-06.SDR FDEA201107262961Seat Track · wornMAIN DECK SEAT TRACK LOBE WORN AT STA 755 X=-8. REPAIRED AS PER SRM 53-00-52 FIG 201 REV 47. SEAT TRACK FABRICATED AS PER DRAWING ADA7321. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.SDR FDEA201107262960Skin · dentedRT WING INBD FLAP, INBD SEGMENT UPPER SKIN FOUND SEVERAL DENTS. DENTED AREAS ARE ACCEPTABLE AND WITHIN ALLOWABLE DAMAGED LIMIT OF 0.060" AS PER SRM 51-80-01 REV 47 AT RIGHT HAND WING INBOARD FLAP INBOARD SEGMENT UPPER SKIN. HFEC INSPECTION CARRIED OUT AS PERSDR WRLA20110726496Mount · brokenREPORT R3 DOOR DISARMED LIGHT ILLUMINATED ON LANDING. UPON INSPECTION FOUND THE AFT GIRT BAR MOUNT BROKEN. SWAPPED NR 4R GIRT-BAR BRACKET WITH DOOR 3R. ALL FASTENERS TORQUED IAW 20-50-00 - SLIDES REFITTED IAW 25-61-22. OPS CHECK OF R3 DOOR ARM INDICATION SSDR WRLA20110720494Battery Pack · failedNR 1 EMERGENCY BATTERY FAILED TEST. REMOVED AND REPLACED NR 1 EMERGENCY LT BATTERY PACK ALL TEST PASSED.SDR WRLA20110717493Bottle · low pressureL-1 DOOR BOTTLE LOW. SERVICED L-1 DOOR ASSIST BOTTLE.SDR WRLA20110615492Fire Loop · failedLEVEL 3 FIRE WARNING, NR 3 ENG INTERMITTENT ON CLIMBOUT. ON/OFF SEVERAL TIMES, FOLLOWED BY LEVEL 1 ENG 3 FIRE DET FAIL. SECOND ALERT WAS INTERMITTENT FOR 20 MINS. BOTH WERE OFF IN CRUISE. ISSUED DMI PER MEL 26-11-01-01 CAT C LOOP "B" FAIL DM: M26JU1111-76SDR FDEA201105121812Seat Track · corrodedCABIN BETWEEN STA 5-113 TO 1541, X = 7.5 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. TRIMMED OFF CORROSION IAW SRM 52-00-52, REV 46, FIG 201. NEW SEAT TRACK REPAIR SECTION AND SPLICE FABRICATED IAW SRM 53-00-52, REV 46, FIG 201 AND INSTALLED IASDR WRLA20110506479Spacer · crackedCRACK: LT WINGLET AFT FITTING SPACER PN: ARB7602-3 CRACK, NRC U05087 ISSUED.
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