Boeing MD-11F
Service difficulty reports · 31,317
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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.
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 IPXA2020021085943Fadec · inoperativeINSPECTION TYPE:N/ADURING SHUTDOWN GOT A LEVEL 2 "SELECT FADEC ALT" ALERT FOR ENG 2. ENG 2 WOULD NOT SHUT DOWN IN ALTERNATE OR NORMAL FADEC MODES. SHUT DOWN USING FIRE HANDLE #2. FUEL SWITCH CYCLED 4 PLUS TIMES NO EFFECT.R&R #2 ENGINE FUEL SWITCH IAW AMM 76-12SDR FDEA202002060277Adc · failedFOLLOWING LIGHT TURBULENCE AND PRECIPITATION AT 370 SIMULTANEOUS AP1 DISCONNECT ACCOMPANIED BY WINDSHEAR DET FAIL, SELECT FADEC ALT, SEL EVEV FEEL MAN SEL FLAP LIM OVRD AND ALT MISCOMPARE ON PFD. RAN QRH AIRSPEED UNRELIABLE CHECK LIST SWAPPED TO AUX ON 1 UPPESDR IPXA2020021095960Floor Panel · corrodedINSPECTION TYPE:S/VMAIN CABIN FLOOR PANEL HAS CORROSION BETWEEN STA. 475-500.175 AND X=0 TO X=8.5.REPAIRED CORRODED FLOOR PANEL AT SAID LOCATION IAW VT-SAA EA 011-5320-01-A8025 REV. I/R AND UPS EO MD11-5330-75449-A. (MINOR)SDR IPXA2020021095959Floor Panel · corrodedINSPECTION TYPE:S/VMAIN CABIN FLOOR PANEL HAS CORROSION BETWEEN STA. 475-500.175 AND X=0 TO X=-8.5.REPAIRED CORRODED FLOOR PANEL AT SAID LOCATION IAW VT-SAA EA 011-5320-01-A8024 REV. I/R AND UPS EO MD11-5320-75447-A. (MINOR)SDR IPXA2020021095958Floor Panel · corrodedINSPECTION TYPE:S/VMAIN CABIN FLOOR PANEL HAS CORROSION BETWEEN STA. 475-500.17 AND X=19 TO X=27.5.REPAIRED CORRODED FLOOR PANEL AT SAID LOCATION IAW VT-SAA EA 011-5320-01-A8026 REV. I/R AND UPS EO MD11-5320-75448-A.SDR IPXA2020020751916Hinge Fitting · gougedINSPECTION TYPE:3CLOWER FWD. RUDDER LOWER HINGE FITTING LUG UPPER SURFACE HAS WEAR DAMAGE.REPAIRED LOWER FWD. RUDDER LOWER HINGE FITTING IAW VT-SAA EA 011-5540-01-A8017 REV. I/R AND UPS EO MD11-5540-75430-A. (MINOR)SDR FDEA202002040261Tire · failedPDIS 615 32-42 8675 03FEB20 CDG FACT U LOGPAGES:3206022 DECELLERATION THROUGH 80 KTS TIRE PRESS DIFF LEVEL 1 ALERT UPON EXITING RUNWAY LEVEL 2 TIRE FAIL ALERT. #8 PRESSURE WENT TO ZERO. INSPECTED BY MAINT. R/I 04FEB20 01:28 CDG U REASONSDR IPXA2020021435103Bulkhead · corrodedINSPECTION TYPE:S/VRIGID CARGO BARRIER WALL HAS HEAVY CORROSION IN MANY PLACES.REMOVED AND REPLACED RIGID CARGO BARRIER ASSY., S/N UP69216 IAW AMM 25-59-13-400-801. (MINOR)SDR FDEA2020020410254Relay · malfunctionedRECEIVED "EMER LT BAT 1 LO" ALERT DURING EMERGENCY LIGHTS TEST. REMOVED AND REPLACED THE R2-5700 EMERGENCY LIGHT BATTERY PACK TEST RELAY PER FIM 33-52-00-1 AND OP'S CHECK WAS GOOD. OK FOR CONTINUED SERVICE.SDR IPXA2020021085939Rib · corrodedINSPECTION TYPE:2CL/H O/B ELEVATOR L/E RIB AT STA. XE=215.120 HAS CORROSION.REMOVED AND REPLACED CORRODED L/H O/B ELEVATOR L/E RIB AT STA. XE=215.120 IAW MD-11 SRM 51-33-01 & 51-35-01. (MINOR)SDR FDEA202001310253Pump · leakingPDIS 612 29-10 9067 31JAN20 PHX OPEN U LOGPAGES:3163545 RECEIVED HYD 1 OFF LEVEL 1 ALERT DURING CRUISE FLIGHT DUE TO DECREASING FLUID QTY IN SYSTEM 1 COMPLIED WITH QRH SHGN 31JAN20 02:29 PHX U #1 HYD QTY AT A/C BLOCK IN WAS 2.2 & PER CREW SDR FDEA202001310252Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM 57-44-08 AND FOUND UPPER AND LOWER BARREL NUT MATISDR FDEA202001300242Rib · crackedRIGHT HAND WING #1 SLAT CRUISE PERFORMANCE FAIRING RIB CRACKED AT XIS 150.7474. RIGHT HAND WING #1 SLAT CRUISE PERFORMANCE FAIRING RIB AT XIS 150.7474 REPAIR CARRIED OUT AS PER EA: 1-5750-T0352236 P1. TITEL: WINGS Ï¿½ FLIGHT SURFACE Ï¿½ RH WING - #1 SLAT SDR FDEA202001300241Longeron Splice · corrodedCENTER CARGO COMPARTMENT STATION 1710 LONGERON 52 SPLICE FITTING FOUND CORRODED. CORROSION ON SPLICE FITTING AT CENTER CARGO COMPARTMENT STATION 1701 LONGERON 52, REMOVED AND REPLACED WITH NEW SPLICE FITTING AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MSDR IPXA2020013151619Transmitter · malfunctionedDIVERSION - LVL 2 "TAIL A/I DISAG" AFTER T.O.D. DIVERT TO KSLC DUE TO ICING CONDITIONS AT DEN. AIRCRAFT REMAINED IN VMC CONDITIONS. TRANSFERRED TAIL ANTI-ICE DIFFERENTIAL PRESSURE SENSORS, M697697 ASSIGNED. SEE ITEM 3 FOR REQUIRED ADDITIONAL DEFERRAL M697701. SDR FDEA202001240221Longeron · corrodedWASTE TANK COMPARTMENT STATION 1968 LONGERON 43 RIGHT FOUND CORRODED. CORROSION AT WASTE TANK COMPARTMENT STATION 1968 LONGERON 43 RIGHT EVALUATED FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 ALLOWABLE DAMAGE. REPAIR CARRIED OUT AS SDR FDEA202001240220Bracket · corrodedRIGHT HAND WING INBOARD FLAP VANE CENTER HINGE FITTING CAVITY WALL CORROSION. RIGHT HAND WING INBOARD FLAP VANE CENTER HINGE FITTING CAVITY WALL CORROSION REMOVED AS PER SRM 51-21-01-0G AND MEASURE REWORKED AREA, ORIGINAL THICKNESS 0.100Ï¿½, MATERIAL REMOVSDR FDEA202001240219Hinge Bracket · corrodedRIGHT HAND WING INBOARD FLAP VANE OUTBOARD HINGE FITTING CAVITY WALL CORROSION. RIGHT HAND WING INBOARD FLAP VANE OUTBOARD HINGE FITTING CAVITY WALL CORROSION REMOVED AS PER SRM 51-21-01-0G AND MEASURE REWORKED AREA. ORIGINAL THICKNESS 0.145Ï¿½, MATERIAL RSDR FDEA202001240218Vane · crackedLEFT HAND WING INBOARD FLAP VANE OUTBOARD LEADING EDGE CRACKED AT STATION XIFH 279.360 . LEFT HAND WING INBOARD FLAP VANE , CRACKED OUTBOARD LEADING EDGE AT STATION XIFH 279.360 REPAIRED AS PER E.A. # : 1-5750-T0338537 A P2 . TITLE : WINGS - FLIGHT SURFASDR FDEA202001240217Longeron · corrodedCENTER CARGO COMPARTMENT BILGE AREA STATION 1701 LONGERON 52 FOUND CORROSION. CORROSION AT LONGERON 52, STATION 1701 CENTER CARGO COMPARTMENT BILGE AREA REMOVED AND FOUND OUT OF LIMIT AS PER SRM 53-00-00-2R FIGURE 202. SEGMENT REPLACEMENT FABRICATED LONGERSDR FDEA202001240216Doubler · crackedLEFT HAND WING LEADING EDGE CAVITY AT XOS 626 Ï¿½ XOS 629 BEADED DOUBLER CRACKED. LEFT HAND WING LEADING EDGE CAVITY AT XOS 626 Ï¿½ XOS 629 BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-SDR FDEA202001240215Doubler · crackedLEFT HAND WING LEADING EDGE CAVITY AT XOS 629 Ï¿½ XOS 633 BEADED DOUBLER CRACKED. LEFT HAND WING LEADING EDGE CAVITY AT XOS 629 Ï¿½ XOS 633 BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-SDR FDEA202001230209Hinge Bracket · corrodedRIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE (HOLE # 3) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-07. RSDR IPXA2020012435262Solenoid · failedCREW ENTRY DOOR WILL NOT CLOSE. TROUBLESHOT TO THE LOCK PIN RELEASE SOLENOID. R & R THE SOLENOID IAW AMM 52-10-06.SDR IPXA2020012751438Control Valve · inoperativeINSPECTION TYPE:N/ADIVERSION - LEVEL 2 STAB OUT, TRIM CLIMBING OUT 4000' WITH A PILOT ON TRIM WORK PERFECT.DEFERRAL WAS APPLIED NOT KNOWING THE SOURCE OF THE STAB OUT MESSAGE HORIZONTAL STAB LVDTS WORKING NORMAL. FOUND #1 PRIMARY TRIM CONTROL VALVE FAULTY. R/RSDR FDEA2020012320194Hinge Bracket · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE SURFACE CORROSION CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR EVALUATED AND FOUSDR FDEA202001210185Angle · chafedCABIN - MAIN DECK CARGO COMPARTMENT FRAME EXISTING OUTER REPAIR ANGLE CHAFFED AT LEFT HAND STATION 535 , LONGERON 24 LEFT . CABIN - MAIN DECK CARGO COMPARTMENT AT LEFT HAND FRAME STATION 535 LONGERON 24 LEFT , CHAFFED MARK AT EXISTING OUTER REPAIR ANGLE FSDR FDEA202001210184Angle · chafedCABIN - MAIN DECK CARGO COMPARTMENT EXISTING OUTER REPAIR ANGLE CHAFFED AT LEFT HAND STATION 535 , LONGERON 19 LEFT . CABIN - MAIN DECK CARGO COMPARTMENT AT LEFT HAND FRAME STATION 535 LONGERON 19 LEFT CHAFFED MARK AT EXISTING OUTER REPAIR ANGLE FOUND TO SDR FDEA202001210183Hinge Bracket · corrodedRIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-5SDR FDEA202001210182Hinge Bracket · corrodedRIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-SDR IPXA2020021215053Thrust Reverser · crackedINSPECTION TYPE:2C#1 ENG. L/H THRUST REVERSER DOOR LAND IS CRACKED.REPAIRED CRACKED #1 ENG. THRUST REVERSER DOOR LAND IAW VT-SAA EA 011-7830-01-A8009 REV. I/R AND UPS EO MD11-7830-75484-A. (MINOR)SDR FDEA202001210187Seat Track · damagedCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT LEFT HAND STATION 745 , X = 75.25 . CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK LEFT HAND STATION 745 X = 75.25 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00SDR FDEA202001210186Seat Track · corrodedCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORROSION AT STATION 1240 , X = - 75.25 . CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE AT STATION 1240 , X = - 75.25 CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 10SDR FDEA2020012100175Hinge Bracket · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52SDR FDEA2020012100174Hinge Bracket · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52- 0SDR FDEA2020012100177Connector · misroutedMDIS 631 27-40 8820 20JAN20 ANC FACT U FOUND ELECTRIC CONNECTORS FOR #1 & #2 HORIZONTAL STABALIZER TRIM MOTORS ROUTED INCORRECTLY AND CROSSED. DISCOVERED WHILE WORKING WRI 27-40/8819 SDR SELECTED DUE POSSIBILITY OF FUTURE TRIMSDR IPXA2020020755856Panel · damagedINSPECTION TYPE:2CR/H WING DROOP L/E PANEL # 617AB HAS GOUGE DAMAGE.REMOVED, FABRICATED AND REPLACED PANEL # 617AB IAW DWG. ARB 1055-18. (MINOR)SDR 9WGA20200120191Tire · leakingIN FLIGHT - L1 TIRE-DIFF PRESS AND TIRE PRESS LOW - THE #6 TIRE SLOWLY DROOP PRESSURE (OVER 30 MINS) TO 49 PSI AND TIRE FAIL L-2 ON #6 ALERT. WE RETURNED TO MIA AND LANDED. FOLLOWED TIRE FAIL CHECKLIST, THE #6 TIRE WAS FLAT BUT NO VISUAL DAMAGE TO AIRCRAFT. INSDR FDEA202001170157Support Fitting · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02- 2RSDR FDEA202001170156Support Fitting · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02- 2SDR IPXA2020020751900Longeron · gougedINSPECTION TYPE:2CEXTENDED TAIL CONE HAS WEB/ZEE LONGERON GOUGED AT R/H HOLE, FWD. END OF PLATFORM.REMOVED, FABRICATED AND REPLACED ZEE/LONGERON IAW DWG. AKC7609 AND SRM 51-31-01. (MINOR)SDR IPXA2020020751899Frame · gougedINSPECTION TYPE:2CTAIL CONE FWD. UPPER MAIN FRAME IS GOUGED ON L/H SIDE.REPAIRED TAIL CONE FRAME IAW SRM 53-00-00 FIG. 210. (MINOR)SDR IPXA2020012071019Connector · dirtyL1 ENTRY DOOR DOES NOT STOP WHEN OPENING DOOR & THE SWITCH IS RELEASED. BOTH INSIDE & OUTSIDE SWITCHES. CLEANED THE DOOR LIMIT SWITCH CONNECTOR PLUG. OPS CHECKED DOOR MULTIPLE TIMES, OPS CHECKED GOOD IAW AMM 52-11-00.SDR FDEA202001160143Stringer · crackedCENTER UPPER AUXILIARY FUEL TANK STRINGER 46 FOUND CRACK FROM XCW 42.5 TO XCW 52.3. CENTER UPPER AUXILIARY FUEL TANK STRINGER 46 FROM XCW 42.5 TO XCW 52.3 CARRIED OUT REPAIR IAW EA # 1-5710-T0352202 PART 1 TITLE :" WINGS - BASIC WING STRUCTURE - CENTER SDR FDEA202001160148Stringer · crackedCENTER UPPER AUXILIARY FUEL TANK STRINGER 47 FOUND CRACK FROM XCW -14.2 TO XCW - 23 CENTER UPPER AUXILIARY FUEL TANK CRACKED STRINGER 47 FROM XCW -14.2 TO XCW -23 CARRIED OUT REPAIR AS PER SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PESDR FDEA202001160147Stringer · crackedCENTER UPPER AUXILIARY FUEL TANK STRINGER 47 FOUND CRACK FROM XCW 14 TO XCW 23.8 CENTER UPPER AUXILIARY FUEL TANK CRACKED STRINGER 47 FROM XCW 14 TO XCW 23.8 CARRIED OUT REPAIR AS PER SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM SDR FDEA202001160146Stringer · crackedCENTER UPPER AUXILIARY FUEL TANK STRINGER 47 FOUND CRACK FROM XCW 37.5 TO XCW 52 CENTER UPPER AUXILIARY FUEL TANK CRACKED STRINGER 47 FROM XCW 37.5 TO XCW 52 CARRIED OUR REPAIR AS PER SRM 57-10-03-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMMSDR FDEA202001160145Stringer · crackedCENTER UPPER AUXILIARY FUEL TANK STRINGER 47 FOUND CRACK FROM XCW -39.4 TO XCW - 52.5. CENTER UPPER AUXILIARY FUEL TANK CRACKED STRINGER 47 FROM XCW -39.4 TO XCW -52.5 CARRIED OUT REPAIR AS PER SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJSDR IPXA2020012985493Access Door · crackedINSPECTION TYPE:2CRT WING TANK ACCESS DOOR 636AB CUTOUT HAS 17 FASTENER HOLES WITH CRACK INDICATIONS.REPAIRED CRACKED RT WING TANK ACCESS DOOR 636AB CUTOUT 17 FASTENER HOLES IAW MD-11 SRM 57-20-02 RERPAIR 5, FIGURE 201. (MINOR)SDR IPXA2020012985492Access Door · crackedINSPECTION TYPE:2CLT WING TANK ACCESS DOOR 536AB CUTOUT HAS 23 FASTENER HOLES WITH CRACK INDICATIONS.REPAIRED CRACKED LT WING TANK ACCESS DOOR 536AB CUTOUT 23 FASTENER HOLES IAW MD-11 SRM 57-20-02 REPAIR 5, FIGURE 201. (MINOR)
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