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 FDEA200908082956Stop Fitting · crackedRT WING OTBD FLAP ASSY UP-STOP FITTING FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 51-31-01 REVISION 41 AND SRM 51-33-01 REVISION 41. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 107.SDR FDEA200908082955Structure · corrodedBARREL NUT HOLES INSPECTION/ REPAIR - BOLT HOLE 31 LEFT HAND BORE HOLE FOUND CORRODED. REPAIR CARRIED OUT AS PER E.A. 1-5510-131653, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200908082954Structure · corrodedBARREL NUT HOLES INSPECTION/ REPAIR - BOLT HOLE 27 LEFT BORE HOLE FOUND CORRODED. REPAIR CARRIED OUT AS PER E.A. 1-5510-131653, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200908082953Fitting · crackedRIGHT WING - LEADING EDGE STRUCTURE RIB 16 XOS= 1005 FOUND CRACKED. RT WING - L/E STRUCTURE RIB NR16 AT XOS 1005 REMOVED IAW SRM 51-31-01 REVISION 41 AND REPLACED IAW SRM 51-33-01 REVISION 41. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REVISION 107.SDR FDEA200908072935Skin · dentedFUSELAGE SKIN AT AFT OF FWD CARGO DOOR CUTOUT S38R TO S423 FOUND EDGE DEFORMED AT SEVERAL LOCATIONS. TRIMMED OUT DAMAGED AREA IAW SRM 53-00-15, FIGURE 202, REVISION 41. REPAIR PARTS FABRICATED IAW SRM 53-00-15, FIGURE 202, REVISION 41 AND INSTALLED IAW SRMSDR FDEA200908072936Fitting · corrodedBARREL NUT HOLES INSPECTION/ RPR - RIGHT HAND NR 26 FITTING FOUND BORE HOLE CORROSION. REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 41. FABRICATED NEW FITTING AS PER DRAWING ALC8107 REVISION D. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200907282810Skin · corrodedHORIZONTAL STABILIZER RT UPPER PLANK NR 34R BARREL NUT BORE SIDEWALL BEARING SURFACE CORROSION REWORKED. FOUND EXCEEDED EO LIMITATIONS. REPAIRED AS PER E.A. 1-5510-131624, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200907272768Skin · cloggedRT WING - AFTER REMOVAL OF RUBSTRIP AND GANG CHANNEL ON FUEL TANK PANEL CUTOUT NR 639CB, 01 EACH FASTENER HOLE FOUND PLUGGED. REPAIR CARRIED OUT AS PER E.A. 1-5730-132661, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200907222702Skin · misrepairedEXISTING REPAIR AT RT WING OTBD AILERON UPPER SKIN. EXISTING REPAIR AT RT WING OTBD AILERON UPPER SKIN EVALUATED AND FOUND NOT IAW SRM REPAIR. RT WING OTBD AILERON UPPER SKIN REPAIRED IAW EA NR 1-5750-132127, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISDR WRLA2009195Engine · failedDURING CLIMBOUT, NR 1 ENGINE FAILED CAUSING DAMAGE TO THE LEFT INBOARD AILERON AND LEFT OUTBOARD HORIZONTAL STABILIZER LEADING EDGE. REPLACED NR 1 ENGINE, LEFT INBOARD AILERON, AND LEFT OUTBOARD SECTION OF THE HORIZONTAL STABILIZER LEADING EDGE.SDR WRLA2009194Charger · inoperativeDURING PREFLIGHT CREW DISCOVERED THAT THE EMERGENCY LIGHTING WAS INOPERATIVE. REPLACED EMERGENCY LIGHTING BATTERY CHARGER.SDR WRLA2009189Engine · vibrationNR 1 ENGINE HI VIBRATION/LOW RPM IN INITIAL CLIMB OUT. HIGH EGT 917C. DURING SHUTDOWN ENGINE FIRE AGENT DISCHARGED.SDR FDEA200907092555Attach Fitting · corrodedRT WING - OTBD T/E FLAP VANE FOUND ATTACHMENT FITTING 'F' (NR 4 FITTING FROM INBD) HOLE CORROSION. REWORKED AS PER E.A. 1-5750-132681, REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100, REVISION 107.SDR FDEA200907092554Support · corrodedLT WING OTBD T/E FLAP AT FLAP VANE FOUND VANE ATTACHMENT FITTING "E" (NR 2 FITTING FROM INBD) CORRODED. REWORKED AS PER E.A. 1-5750-132680. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 107.SDR FDEA200906302397Rub Strip · corrodedRT WING/LWR WING FUEL TANK ACCESS DOOR NR 639CB CUTOUT/RUB STRIP CORRODED. RT WING LWR WING FUEL TANK ACCESS DOOR NR 639CB CUTOUT CORRODED. RUB STRIP REMOVED AND REPLACED IAW SRM 51-42-04 VOLUME II REVISION 40. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 RESDR FDEA200906302396Skin · corrodedREFERENCE EO 1-5510-7-5000D1 PT.1: HOR STAB LT UPPER PLANK NR 08L BARREL NUT BORE CORROSION REWORKED EXCEEDED EO LIMITATIONS. REPAIR CARRIED OUT IAW EA 1-5510-131625, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 107.SDR FDEA200906302391Skin · corrodedREFERENCE EO 1-5510-7-5000D1 PT.1: HOR STAB LT UPPER PLANK NR 16L BARREL NUT BORE CORROSION REWORKED EXCEEDED EO LIMITATIONS. REPAIR CARRIED OUT IAW EA 1-5510-131623, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 107.SDR FDEA200906302390Skin · corrodedREFERENCE EO 1-5510-7-5000D1 PT 1: HOR STAB LT UPPER PLANK NR 06L BARREL NUT BORE CORROSION REWORKED EXCEEDED EO LIMITATIONS. REPAIR CARRIED OUT IAW NR 1-5510-131625, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 107.SDR FDEA200906302389Skin · corrodedEO 1-5510-7-5000D1 PT.1: HOR STAB LT UPPER PLANK, NR24L BARREL NUT BORE CORROSION REWORKED EXCEEDED EO LIMITATIONS. REPAIR CARRIED OUT IAW EA NR1-5510-131623, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 107.SDR FDEA200906292384Spar Cap · corrodedRT WING T/E REAR SPAR UPPER CAP AREA AROUND XORS 1042 FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER E.A. 1-5710-132655, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906272352Spar Cap · corrodedHORIZONTAL STABILIZER LEFT HAND UPPER PLANK NR 36 LEFT BARREL NUT BORE CORROSION REWORK FOUND EXCEEDED E.O. NR 1-5510-7-5000 D1 PART 1 LIMITATION. HORIZONTAL STABILIZER LEFT HAND UPPER PLANK NR 36 LEFT BARREL NUT BORE CORROSION REPAIRED PER E.A. NR 1-5510SDR FDEA200906272351Spar Cap · corrodedCORROSION-LT WING REAR SPAR UPPER CAP OTBD OF NR 5 SPOILER PANEL INBD AROUND XORS 799. REPAIR CARRIED OUT AS PER E.A. 1-5710-132654, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906272350Spar Cap · corrodedCORROSION-LT WING REAR SPAR UPPER CAP FWD OF NR5 SPOILER PANEL INBD AREA BETWEEN XORS 714 TO 738. REPAIR CARRIED OUT AS PER E.A. 1-5710-132654, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906272349Fitting · corrodedHORIZONTAL STABILIZER RT OPERATING BULKHEAD REQUIRED TO TRIM APPROX 0.190" AND FOUND EXCEEDED EO 1-5510-7-5000D1 PT1 LIMITATION (MAX 0.150 INCH) WHILE FACILITATE OVERLAPPED NR 35R BARREL NUT BORE REWORK. REPAIRED AS PER E.A. 1-5510-131629, REPAIR CLASSIFIED SDR FDEA200906272348Trunnion · crackedCRACK-LOWER FASTENER HOLE AT 5:00 POS ON LONGERON APPROX .1250 INCH UPON CRACK AREA REMOVAL FROM NLG TRUNNION FITTING. NOSE LANDING GEAR TRUNNION FITTING LT LOWER LONGERON FABRICATED IAW DWG ACA3796 REVISION A. LONGERON REMOVED AND REPLACED IAW SRM 51-31-01, SDR FDEA200906262312Skin · corrodedAFT ACCESSORY COMPARTMENT RT SKIN, (ACCESS PANEL 347DF LWR 2 EACH ANCHOR NUT MOUNTING AREA) FOUND SEVERE CORROSION. REPAIR CARRIED OUT AS PER E.A. 1-5330-132667, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906262311Longeron Splice · corrodedFWD CARGO COMPARTMENT BILGE AREA STA 1119 THRU 6-10 LONGERON 52 SPLICE FITTING FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II REVISION 40. SPLICE FITTING FABRICATED AS PER DRAWING ADA8424 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-SDR FDEA200906252309Hinge Bracket · corrodedLT WING OTBD FLAP INBD HINGE (WING SIDE) LWR ATTACHMENT INBD BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER E.A. 1-5750-132122, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906252308Hinge Bracket · corrodedLT WING OTBD FLAP INBD HINGE (WING SIDE) LWR ATTACHMENT OTBD BORE FOUND CORRODED. COMPLIED WITH E.A. 1-5750-132122, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906252307Hinge Bracket · corrodedLT WING OTBD FLAP INBD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBD BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER E.A. 1-5750-132121, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906252295Skin · corrodedHORIZONTAL STABILIZER RT UPPER PLANK NR 1 BARREL NUT BORE CORROSION REWORKED, FOUND EXCEEDED EO 1-5510-7-5000 PART 1 LIMITATIONS. REPAIR CARRIED OUT AS PER E.A. 1-5510-131620, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906252294Skin · corrodedHORIZONTAL STABILIZER RT UPPER PLANK NR 15R BARREL NUT BORE CORROSION REWORKED, FOUND EXCEEDED EO 1-5510-7-5000, PART 1 LIMITATIONS. REPAIRED AS PER E.A. 1-5510-131622, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV. 107SDR FDEA200906252293Longeron Splice · corrodedCTR CARGO BILGE AREA AT STA 5-113 TO STA 1541 SPLICE FITTING ON LONGERON 52 FOUND CORROSION. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906252292Longeron · corrodedCTR CARGO BILGE AREA AT STA 1621 LONGERON 52 FOUND CORROSION. REPAIR CARRIED OUT AS PER E.A. 1-5310-131626, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906252291Skin · crackedRT WING DROOP L/E UPPER SURFACE OTBD END TO FASTENER HOLE, FOUND CRACKED. RIGHT HAND WING DROOP LEADING EDGE UPPER SKIN REPAIRED AS PER SRM 57-10-00 FIGURE 30 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906242278Web · crackedCRACK INDICATION FOUND ON SECOND LAYER WEB AT 2 O'CLOCK POSITION DURING HFEC OPEN HOLE INSP ON 0.520 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 7 SUPPORT FITTING AT HOLE NR B. MAIN CARGO DOOR LOWER JAMB NO.7 SUPPORT FITTING AT HOLE NO. B SECOND LAYER WEB RSDR FDEA200906242277Web · crackedCRACK INDICATION FOUND ON FIRST LAYER WEB AT 5 O'CLOCK POSITION DURING HFEC OPEN HOLE INSP ON 0.520 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 7 SUPPORT FITTING AT HOLE NR B. REAMED TO DIAMETER 0.540 INCH IAW SRM 51-31-01 VOLUME II, REVISION 40. REPAIR CARRIEDSDR FDEA200906232244Structure · corrodedBARREL NUT HOLES INSPECT/REPAIR - LT NR 26 FITTING FOUND BORE HOLE CORROSION. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906232243Skin · crackedLT WING NR 3 SLAT, WING L/E TELESCOPIC DUCT DOOR CUT-OUT AREA FOUND CRACKED AT INBD AND OTBD SIDE. REPAIR CARRIED OUT AS PER E.A. 1-5730-131723, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906232242Skin · crackedRT WING NR 3 SLAT, WING L/E TELESCOPIC DUCT DOOR CUT-OUT AREA FOUND CRACKED AT INBD AND OTBD SIDE. REPAIR CARRIED OUT AS PER E.A. 1-5730-131722, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906222235Hinge Bracket · corrodedRT WING - OTBD FLAP OTBD HINGE (WING SIDE) LOWER ATTACHMENT OTBD BORE FOUND CORRODED. RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) LOWER ATTACHMENT OUTBOARD BORE REWORKED & FOUND EXCEEDED LIMIT AS PER CMM 57-44-09 REVISION 64. . REPAIR CARRIED OUT AS SDR FDEA200906222234Hinge Bracket · corrodedRT WING INBD FLAP OTBD HINGE (FLAP SIDE) PIVOT PIN ATTACHMENT INBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03 REVISION 64. REPAIR CARRIED OUT AS PER EA 1-5750-130979, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISSDR FDEA200906222233Hinge Bracket · corrodedRT WING INBD FLAP OTBD HINGE (FLAP SIDE) PIVOT PIN ATTACHMENT OTBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03 REVISION 64. REPAIR CARRIED OUT AS PER EA 1-5750-130979, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISSDR FDEA200906222232Hinge Bracket · corrodedLT WING INBD FLAP OTBD HINGE (FLAP SIDE) PIVOT PIN ATTACHMENT OTBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03 REVISION 64. REPAIR CARRIED OUT AS PER EA 1-5750-130978, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6- 2-100 RESDR FDEA200906222231Hinge Bracket · corrodedLT WING INBD FLAP OTBD HINGE (FLAP SIDE) PIVOT PIN ATTACHMENT INBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03 REVISION 64. EXISTING HOLE DIAMETER = 1.1885", FINAL HOLE DIAMETER = 1.252". REPAIR CARRIED OUT AS PER EA 1-5750SDR FDEA200906192174Longeron · corrodedFWD CARGO COMPARTMENT BILGE AREA RT LONGERON 51R FOUND CORRODED AT STA 6-30. REPAIR CARRIED OUT AS PER E.A. 1-5310-131616, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906192173Longeron · corrodedFWD CARGO COMPARTMENT BILGE AREA LONGERON 52 AND SPLICE FITTING FOUND CORRODED AT STA 1119 TO 6-30. REPAIR CARRIED OUT AS PER E.A. 1-5310-131617, . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906192172Skin · chafedFWD CARGO COMPARTMENT DOOR CUT-OUT AFT LOWER SECTION FOUND EDGE CHAFING. CARRIED OUT DOUBLER REPAIR AS PER SRM 53-50-00 FIGURE 17 VOLUME I REVISION 40. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906192171Fitting · corrodedBARREL NUT HOLES INSPECT/REPAIR - RT NR 26 FITTING FOUND BORE HOLE CORROSION. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II REV 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 107SDR FDEA200906192170Fitting · corrodedBARREL NUT HOLES INSPECT/REPAIR - RT NR 14 FITTING FOUND BORE HOLE CORROSION. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.
Back to Mcdonnell Douglas MD-11