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 FDEA201905030991Shutoff Valve · failedPDIS 592 29-02 3353 03MAY19 IND FACT U LOGPAGES:3094152 DURING CLIMB OUT TO FL 390 WE RECIVED A LVL 1 HYD 3 ELEV OFF ALERT NO.3 QUANTITY WAS 4.5.W/3-2 NRMP INOP. DURING CRUISE QTY LEVEL WENT TO 4.1. DESCENT INTO IND WE CONFIGURED W/FLAPS 15 ANDSDR IPXA2019050241650Panel · crackedINSPECTION TYPE:4C INSPECTION ON TC 7682 ON RT WING LOWER FUEL PANL 636AB FOUND 3 HOLES WITH CRACKS. REAMED HOLES, FABRICATED AND INSTALLED BUSHINGS ON RT ING FUEL PANEL 636AB PER SRM 57-20-02 REPAIR 5.SDR FDEA201904300970Skin · crackedAFT CARGO DOOR AFT LOWER CORNER SKIN FOUND CRACKED CRACKED SKIN AT AFT CARGO DOOR AFT LOWER CORNER TRIMMED OUT AND CARRY OUT REPAIRED AS PER SRM 52-30-16-2R FIGURE 202 REPAIR 3 AND EA 1-5232-T0346872 P1 TITLE : DOORS - AFT CARGO COMP DOOR - DEVIATIONS TO SRM 5SDR IPXA2019051242012Frame · gougedINSPECTION TYPE:4C FWD. TAIL CONE AFT BULKHEAD RT UPPER FRAME IS GOUGED. REPAIRED TAIL CONE FRAME IAW DWG. AKC7539 AND SRM 53-80-07 REPAIR 4. (MINOR)SDR IPXA2019051242010Stiffener · crackedINSPECTION TYPE:4C AFT CARGO VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LONG. 48R. REMOVED, FABRICATED AND REPLACED VERT. STIFFNER AT STA. 1841 & LONG. 48R IAW DWG. AGA7170 AND SRM 51-33-01. (MINOR)SDR IPXA2019051242011Stiffener · crackedINSPECTION TYPE:4C AFT CARGO VERTICAL STIFFNER IS CRACKED AT STA. 1841 & LONG. 48L. REMOVED, FABRICATED AND REPLACED VERT. STIFFNER AT STA. 1841 & LONG. 48L IAW DWG. AGA7170 AND SRM 51-33-01. (MINOR)SDR FDEA201904300968Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 667 RIB DOUBLER FOUND CRACKED RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 667 CRACKED RIB DOUBLER REMOVED AND INSTALLED WITH FABRICATED PART AS PER SRM 51-33-01-0G. RIB DOUBLER FABRICATSDR IPXA2019050741854Beam · crackedINSPECTION TYPE:4C RT I/B AILERON FWD. LOWER ANGLE SUPPORT/BEAM U-IS CRACKED. REMOVED, FABRICATED AND REPLACED BEAM IAW DG. AKC1313 AND SRM 51-35-01. (MINOR)SDR IPXA2019043041601Battery · dischargedINSPECTION TYPE:N/A EMER LT TEST RECEIVED LVL 1 EMER LT BAT 1 LOW. ITEM TRANSFERRED TO M668740 IAW MEL 33-50-4. DMP ACCOMPLISHED PLACARD INSTALLED. **SUPPLEMENTAL SDR** REPLACED EMERGENCY POWER SUPPLY BATTERY PER AMM 33-51-01. TEST PASSED. NO ALERTS NOTED. THISDR IPXA2019051742214Longeron · corrodedINSPECTION TYPE:4C LONGERON 52 IS CORRODED BETWEEN STA. Y=5.0 AND Y=5-32. REPAIRED CORRODED LONGERON 52 BETWEEN STA. Y=5.0 & Y=5-32 IAW EA 011-5310-01-A7762 REV. I/R AND EO MD11-5330-72574-A. (MAJOR)SDR FDEA201904290963Stringer · corrodedRIGHT HAND WING - FIXED LEADING EDGE COMPARTMENT STATION XOS 667 STRINGER FOUND CRACKED RIGHT HAND WING - FIXED LEADING EDGE COMPARTMENT STATION XOS 667 STRINGER CRACKED REPAIR CARRIED OUT AS PER SRM 57-40-03-2R FIGURE 202 REPAIR 2. REPAIR CLASSIFIED AS MAJOSDR FDEA201904290962Support Fitting · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER.5 SUPPORT FITTING ECCENTRIC HOLE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER. 5 SUPPORT FITTING ECCENTRIC HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201.OVERSIZED ECSDR FDEA201904290961Support Fitting · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER.4 SUPPORT FITTING ECCENTRIC HOLE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER. 4 SUPPORT FITTING ECCENTRIC HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201.OVERSIZED ECSDR FDEA201904290960Support Fitting · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER.2 SUPPORT FITTING ECCENTRIC HOLE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER. 2 SUPPORT FITTING ECCENTRIC HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ESDR FDEA201904290959Support Fitting · corrodedRIGHT WING - OUTBOARD FLAP VANE NUMBER.4 SUPPORT FITTING ECCENTRIC HOLE FOUND CORROSION. CORROSION AT RIGHT WING - OUTBOARD FLAP VANE NUMBER. 4 SUPPORT FITTING ECCENTRIC HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZEDSDR FDEA201904290958Support Fitting · corrodedRIGHT WING - OUTBOARD FLAP VANE NUMBER. 2 SUPPORT FITTING ECCENTRIC HOLE FOUND CORROSION. CORROSION AT RIGHT WING - OUTBOARD FLAP VANE NUMBER. 2 SUPPORT FITTING ECCENTRIC HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZESDR FDEA201904290957Hinge · corrodedRIGHT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. OVERSIZED BUSHING FASDR FDEA201904290956Hinge · corrodedLEFT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. OVERSIZED BUSHING FASDR IPXA2019051141989Rib · bentINSPECTION TYPE:4C RT WING I/B AILERON O/B RIB IS BENT. REMOVED AND REPLACED BENT RT WING I/B AILERON O/B RIB IAW SRM 51-31-01 AND 51-35-01. (MINOR)SDR IPXA2019051041957Skin · chafedINSPECTION TYPE:4C RT I/B AILERON I/B LOWER SKIN HAS DEEP WEAR. REMOVED, FABRICATED AND REPLACED SKIN IAW DWG. ARC1316 AND SRM 51-31-01. (MINOR)SDR FDEA201904290981Control Manifold · failedUNABLE TO MOVE FLAP/SLAT HANDLE TO SLAT RETRACT POSITION AFTER ACCELERATION PAST SR PROMPT. AFTER SEVERAL ATTEMPTS SLAT HANDLE MOVE TO SLAT RETRACT POSITION AFTER BRIEF DISPLAY INDICATION NORMAL ACCELERATION AND TARGET CLIMB SPEED, AMBER OVERSPEED TAPE DROPPEDSDR IPXA2019051642184Fillet · crackedINSPECTION TYPE:4C RT WING SLAT TO FUSELAGE FILLET ASSY. IS CRACKED AT STA. XIS=150.74 CANT. REPAIRED CRACKED RT WING SLAT TO FUSELAGE ASSY. IAW EA 011-5754-01-A7740 REV. I/R AND EO MD11-5720-72474-A. (MINOR)SDR IPXA2019051542138Skin · corrodedINSPECTION TYPE:4C CENTER WING BOX UPPER SURFACE HAS CORROSION AT STRINGER 15 & RBL 85-90. REPAIRED CORRODED CENTER WING UPPER FWD AND CENTER SKIN AT STRINGER 15 ABOVE STA XCW=-86 TO XCW=-100 IAW EA 011-5730-01-A7750 REV. IR AND EO MD11-5730-72515-A. (MINOR)SDR FDEA201904280946Skin · chafedFORWARD CARGO COMPARTMENT DOOR AFT FUSELAGE CUTOUT SKIN AT STATION 999 BETWEEN LONGERON 40 AND LONGERON 42 FOUND WITH CHAFED. CHAFED MARK AT FORWARD CARGO COMPARTMENT DOOR AFT FUSELAGE CUTOUT SKIN STATION 999 BETWEEN LONGERON 40 AND LONGERON 42 TRIMMED OUT ANDSDR IPXA2019051242014Doubler · crackedINSPECTION TYPE:4C RT WING FIXED L/E BEADED DOUBLER IS CRACKED BEYTWEEN SYA. XOS=542.0 TO XOS=547.5. REPAIRED CRACKED RT WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS=542.0 TO XOS=547.5 IAW SRM 57-40-02 PERAIR 15 FIG. 205. (MAJOR)SDR FDEA201904280950Fitting · crackedHFEC INSPECTION CARRIED OUT AT LEFT HAND NOSE LANDING GEAR TRUNNION FITTING AT STATION Y = 595 EXISTING REPAIR FOUND CRACK PROPAGATE 0.2" IN LENGTH BEYOND THE EXISTING TRIM OUT AREA. CRACK AT LEFT HAND NOSE LANDING GEAR TRUNNION FITTING AT STATION Y = 595 REPASDR FDEA201904280949Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 730 BEADED DOUBLER FOUND CRACKED RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 730 CRACKED. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIEDSDR FDEA201904280948Doubler · crackedLEFT HAND WING FIXED LEADING EDGE LOWER STATION XOS 487 DOUBLER FOUND CRACKED LEFT HAND WING - FIXED LEADING EDGE LOWER STATION XOS 487 CRACKED DOUBLER. REMOVED AND REPLACED WITH FABRICATED PART AS PER SRM 51-31-01-0G. DOUBLER FABRICATED AS PER DRAWING ARB1180SDR IPXA2019050941943Skin · gougedINSPECTION TYPE:4C RT WING NR 3 SLAT INNER SKIN IS GOUGED. REPAIRED GOUGED RT WING NR 3 SLAT INNER SKIN BETWEEN STA. XOS=455 TO XOS=498 IAW SRM 57-40-01 REPAIR 3 FIG. 201. (MAJOR)SDR IPXA2019050841896Doubler · crackedINSPECTION TYPE:4C RT WING BEADED DOUBLER IS CRACKED AT LE APPROX. XOS=625 - XOS=629 BEHIND FUELING PANEL. REPAIRED CRACKED RT WING BEADED DOUBLER CRACK AT L/E APPROX. XOS=625 THU XOS=629 IAW SRM 57-40-02 REPAIR 15, FIGURE 205. (MAJOR)SDR IPXA2019042941545Limit Switch · defectiveINSPECTION TYPE:N/A R1 DOOR ELECTRIC OPERATION INTERMITTENT FROM EITHER SWITCH. DEFERRED R1 DOOR ELECTRIC OPERATION INOP PER MEL 52-10-1-2-0-1 ON M668612. DMP C/W. **SUPPLEMENTAL SDR** REPLACED UP LIMIT SWITCH PER SWPM 20-30-00 ( 51-592) AND REPLACED ELECTRIC SDR IPXA2019051942249Frame · crackedINSPECTION TYPE:4C NR 3 O/B T/R CORE COWL INNER HOUSING IS CRACKED AT THE 12 O'CLOCK POS. ON AFT RIB (FRAME). REMOVED AND REPLACED CRACKED AFT RIB (FRAME) ON NR 3 O/B T/R CORE COWL AT 12 O'CLOCK POS. IAW SRM 54-05-41. (MINOR)SDR IPXA2019051542157Cowling · chafedINSPECTION TYPE:4C NR 1 ENG. RT FAN COWL HAS CHAFE DAMAGE ON THE UPPER FWD. DOOR HINGE FITTING.REPAIRED CHAFED RT FAN COWL FWD. HINGE IAW EA 011-7110-01-A7766 REV. I/R AND EO MD11-7110-72596-A. (MINOR)SDR IPXA2019051542137Thrust Reverser · crackedINSPECTION TYPE:4C NR 3 ENGINE I/B CORE COWL (T/R) HAS A CRACK ON OUTER SKIN AT FASTENER AT APPROX. 11 O'CLOCK POS. 4" FROM AFT EDGE. REPAIRED CRACKED NR 3 ENGINE I/B T/R CORE COWL OUTER SKIN AFT FIXED INNER BARREL AT STA. NAC 193 - NAC 197.7 IAW EA 011-7830-0SDR FDEA201904270940Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE REWORKED AND FOUND INBOARD FACE WITHIN LIMIT, OUTBOARD FACE EXCEED LIMIT AS PER CMM 57-44-SDR FDEA201904270939Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE REWORKED AND FOUND INBOARD FACE WITHIN LIMIT, OUTBOARD FACE EXCEED LIMIT AS PER CMM 57-44-07.SDR FDEA201904270938Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSSDR FDEA201904270937Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVESDR FDEA201904270936Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSSDR FDEA201904270935Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57- 52-03. OVERSDR 9WGA2019043001Connector · shortedAFTER TAKEOFF AND CRUISE LVL 1 INTERMITTENT FIRE DETECTOR ENGINE 2 FAIL WITH ENGINE 2 FIRE WARNING. T/S PER FIM 26-11-01 PERFORMED WIRING CHECK LOOP "A" PIN J AND K FOUND SHORTED TO GROUND. CLEAN CONTAMINATION PERFORMED RTS PER AMM 26-11-02 ALL TEST PASS.SDR IPXA2019042974504Skin · delaminatedLEFT TRAILING EDGE LOWER SURFACE DELAMINATED.ISSUED NON ROUTINE CARD 621344 FOR MAJOR REPAIR.SDR FDEA201904260927Fuel Cell · corrodedMAIN DECK APPROX STA.1229 LBL X-8.50 CENTER TANK UPPER SKIN HAS CORROSION. REMOVED CORROSION REF. STEP 2 OF EA 1-5730-T0345575 P1.INSTALLD FASTENERS REF.STEP 8 EA 1-5730-T0345575 P1.SDR FDEA201904260926Fuel Cell · corrodedMAIN DECK APPROX STA.1229, RBL X=47.50 CENTER FUEL TANK UPPER SKIN IS CORRODED. REMOVED CORROSION REF. STEP 2 OF EA 1-5730-T0345575 P2. INSTALLED FASTENERS REF. STEP 11 OF EA 1-5730-T0345575 P2 ( WING-PLATES AND SKINS- CENTER WING UPPER SKIN- REWORK)SDR IPXA2019051141992Longeron · crackedINSPECTION TYPE:4C LONGERON 52 IS CRACKED AT STA. 1706.REPAIRED CRACKED LONGERON 52 BETWEEN STA. 1681 TO 1710 IAW EA 011-5310-01-A7742 REV. I/R AND EO MD11-5330-72553-A. (MAJOR)SDR IPXA2019050141645Doubler · chafedINSPECTION TYPE:4C TAILCONE RT UPPER INTERNAL DOUBLER WORN (CHAFED). REPAIRED TAILCONE RT UPPER INTERNAL DOUBLER CHAFE DAMAGE IAW EO MD11-5350-66790-A. (MINOR)SDR FDEA201904250921Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CSDR FDEA201904250920Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE (#10 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZESDR FDEA201904250919Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMSDR FDEA201904250918Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-4
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