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 WRLA2009020Structure · crackedDURING C-CHECK INSPECTION IN TPE - CRACK WAS FOUND AT LT WING INBOARD FLAP XIFH230 LOWER TRAILING EDGE L=4 INCHES. REPAIRED CRACK AREA IAW SRM 57-20-00 VOL I FIG 2 REV 40. REF EGAT N/R U05011.SDR WRLA2009019Stiffener · crackedDURING C-CHECK INSPECTION IN TPE - FOUND ZEE STIFFENERS OF LT WING INBOARD FIXED L/E UPPER PNL 516ET CRACKED. REPAIRED CRACK AREA IAW SRM VOL 1 57-10-00 REV 40. REF EGAT N/R U05012.SDR WRLA2009018Stiffener · crackedDURING C-CHECK INSPECTION IN TPE - FOUND ZEE STIFFENERS OF RIGHT WING INBOARD FIXED L/E UPPER PNL 616ET CRACKED. REPAIR CRACK AREA IAW MD-11 SRM VOL 1 57-10-00 REV 40. REF EGAT N/R U05013.SDR WRLA2009017Web · damagedDURING C-CHECK INSPECTION IN TPE - FOUND LT WING LEADING EDGE WEB HAS IMPACT DAMAGE AT FUELING STATION X0RS524. REPAIR DAMAGE AREA IAW MD-11 SRM VOL I 57-00-01 FIG 8 REV 40. REF EGAT N/R U05014.SDR WRLA2009013Slide · inoperativeDURING C1 CHECK INSPECTION, TEST DEPLOYED L2 DOOR SLIDE, WHEN HANDLE WAS PULLED AND DOOR RAISED SLIDE DETACHED AND FELL STRAIGHT ONTO THE CABIN FLOOR AND DID NOT INFLATE. REF C1 TASK CARD 1095. REMOVED AND REPLACED L2 DOOR SLIDE/RAFT IAW WOA TASK CARD 1095.SDR WRLA2009007Mount · corrodedNR 3 ENG MOUNT ISOLATOR, INSIDE FAN CASE, HAS RED POWDERY SUBSTANCE DRIPPING OUT ONTO COMPRESSOR, A-07 CHECK. REMOVED NR 3 ENG FWD MOUNT ISOLATOR IAW MM 71-00-39 PW ENG MANUAL. INSP, OK TO INSTALL. 01-09-09 REPLACED MOUNT WITH SERVICEABLE MOUNT IAW ENG MANUASDR WRLA2009001Engine · defectiveIN CRUISE RECEIVED A LVL 2 ENG 2 OIL FILTER ALERT. NOTICED INCREASING EVM COMP INDICATION AND RECIEVED A LVL 1 ENG 2 VIB HI ALERT. LATER MODERATE A/C VIB NOTICED, EVM COMP OF 5.0, A LVL 2 SEL FADEC ALT ALERT AND A DROP IN N1 OF NR 2 ENG COMPLETED IFSD PROCEDURSDR FDEA200812265297Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 6 SUPPORT FITTING AT HOLES A, B AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOSDR FDEA200812265296Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING AT HOLE D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJORSDR FDEA200812265295Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB, NR 4 SUPPORT FITTING AT HOLES A, B, C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED ASDR FDEA200812265292Support Fitting · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 1 SUPPORT FITTING AT HOLES NR A, NR C AND NR D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIESDR WRLA2008105Flap · debondedDURING 1C+12A CHECK, EGAT MECHANIC FOUND LEFT WING OUTBOARD FLAP VANE LOWER SKIN DISBOND AT XOFH=499 ~ XOFH=533 (34 X 9.5 ), REFER TO EGAT NRC U01027. OPENSDR WRLA2008104Repair · debondedDISBOND-DURING 1C+12A CHK, EGAT MECHANIC FOUND LEFT WING INBOARD FLAP VANE LWR SKIN EXISTING REPAIR DISBOND & EXTEND TO THE ORIGINAL SKIN AT XIFH=152~XIFH=213(61 X 19), THE EXISTING REPAIR:(70 X31) AND XIFH=243~XIFH=258 (15X23) REFER TO EGAT NRC U01026. OPENSDR ASM2008F00007Hinge · corrodedAFTER REWORK OF RT OB FLAP, IB AFT HINGE PN ARC 1984-502, OB PIVOT LUG BORE HAS BEEN FOUND OUT OF LIMITS PER CMM 57-52-04 PAGE 624 AND 625. FOUND 1.162" INSTEAD OF 1.150". NR 1-1032193304-2 APPROVE TO INSTALL AN OS BUSHING.SDR ASM2008F00008Hinge · corrodedAFTER REWORK OF OB FLAP, IB AFT HINGE PN ARC 1984-501, IB PIVOT LUG BORE HAS BEEN FOUND OUT OF LIMITS PER CMM 57-52-04 PAGE 624 AND 625. FOUND 1.172" INSTEAD OF 1.150". BOECOM NR 1-1024128699-4 APPROVE TO INSTALL AN OS BUSHING.SDR 08FDEA04090Attach Fitting · scratchedRIGHT WING OUTBOARD FLAP INBOARD HINGE AFT MOUNTING LOWER OUTBOARD MOUNTING BORE HOLE INNER FACE FOUND WITH SCRATCH MARKS.SDR WRLA2008073Skin · corrodedDURING INSPECTION FOUND FUSELAGE SKIN AND REINFORCING DOUBLER CORRODED AT AFT LAV EXHAUST PORT STA 1959 BETWEEN LONGERONS LS9R AND L40R. CORRECTIVE ACTION: REF. DELTA ERA 47026114 REMOVED DAMAGED AREA, PERFORMED HF EDDY CURRENT INSPECTION AS REQUIRED, FABRICASDR WRLA2008071Doubler · crackedCENTER MLG WW RT BULKHEAD CUTOUT DOUBLER CRACKED AT RT FWD CORNER.SDR 08FDEA03512Skin · cracked11 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS= 690 AND STA XORS= 700. 11 EACH FASTENER HOLES CRACK AT RT WING LOWER SKIN ACCESS. REPAIR CARRIED OUT AS PER EA 1-5710-122425A, SDR 08FDEA03511Skin · cracked15 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LH WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS= 690 AND STA XORS= 700. 15 EACH FASTENER HOLES ON LEFT HAND WING LOWER SKIN ACCESS BETWEEN XORS = 690 TO XORS = 700 REPAISDR 08FDEA03517Skin · crackedLEFT WING - NR 6 LEADING EDGE SLAT OUTBOARD TRACK CUTOUT CORNER FOUND SUSPECTED CRACK. LEFT WING NR 6 LEADING EDGE SLAT OUTBOARD TRACK CUTOUT OUTBOARD CRACKED CORNER TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIEDSDR WRLA2008064Actuator · odorFLT 1000 (KIAH/FNLU) ITEM: DURING FLIGHT, SMOKE/FUMES IN CABIN IN VICINITY OF ROW 16 & 17. MAINTENANCE FOUND LARGEST ACTUATOR AT SEAT 18G AS SOURCE OF ELECTRICAL ODOR. DEACTIVATED CONTROL BOX FOR SEATS 18 D&G BY STOWING CONNECTORS AND PULLED C/B. REMOVED ASDR 08FDEA02849Support Fitting · crackedDURING OPEN-HOLE HFEC INSPECTION ON 0.460" HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDICATIONS AT HOLES A, C AND D. MAIN DECK CARGO DOOR LOWER JAMB FITTING NR 4 REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. THIS REPAIR CLASSDR WRL2008F00005Fitting · corrodedDURING LANDING GEAR REPLACEMENT, MAINT FOUND CORROSION ON CENTER LANDING GEAR LT PILLOW BLOCK AFT UPPER SURFACE OF PILLOW BLOCK AFT BOLT HOLE CORRODED. REWORKED AREA IAW SRM 53-40-00 FIG 16 IAW SERVICE REQUEST ID 1-8801879663.(K)SDR WRLA2008054Trunnion · corrodedDURING LANDING GEAR REPLACEMENT MAINTENANCE FOUND CORROSION ON CENTER LANDING GEAR LT PILLOW BLOCK AFT UPPER SURFACE OF PILLOW BLOCK AFT BOLT HOLE CORRODED. (S)SDR 08FDEA02375Trunnion · corrodedDURING CENTER LANDING GEAR REMOVAL FOR REPLACEMENT, THE RIGHT TRUNNION FITTING AFT ATTACHMENT BOLT HOLE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5310-122488, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR WRLA2008053Coffeemaker · odorAFT GALLEY COFFEEMAKER 5 OR 8 HAS STRONG ELECTRICAL SMELL. BOTH SHUT OFF IN FLIGHT. FOUND COFFEEMAKER NR 8 POPPED. NR 5 COFFEEMAKER OPS CHECK OK PER MM 25-32-15. CHECKED OPERATION, OPERATES NORMAL NEF ITEM N25JU1808-721 CLEARED. (S)SDR UPS08M52611Structure · corrodedINSPECTION TYPE-C, AIR CON SYS NR 1 COMPARTMENT INTERIOR, AFT BILGE AREA, EXISTING ANGLE DOUBLER FOUND CORRODED. ATTACH CORROSION FRAME SUPPORTS AND RIB REMOVED IAW SR M51-31-01 VII R35. FRAME, SUPPORTS AND RIB CORROSION REMOVED IAW SRM 51-21-01 VII R35. RESDR UPS08M52460Floorbeam · crackedINSPECTION TYPE:C CTR CARGO COMPT - UPON REMOVING OF PHENOLIC SPACER AT STATION 5-73,X-33 FOUND FLOORBEAM CRACKED. CRACK BEAM REMOVED AND NEW BEAM P/N AFA0039-5N INSTALLED AS PER SRM 51-31-01 VOL II REV 35.SDR WRLA2008049Chiller · malfunctionedKDFW/KATL: FORWARD CHILLER POPS C/B IN FLIGHT WITH ASSOCIATED ODOR OF ELECTRICAL SMOKE. REMOVED AND REPLACED FWD GALLEY CHILLER, OPS CHECK SATISFACTORY PER MD-11 25-37-82. (A)SDR UPS08M52538Hinge · corrodedINSPECTION TYPE:C RHW O/B FLAP I/B HINGE (FLAP MOUNTED) UPPER FWD MOUNTING SPOT FACE FOUND CORRODED. CORROSION REMOVED PER BSOPM20-11-02REV60 ORIG THK 0.751" REMAIN THK 0.746" MAT`L REMOVED 0.005". FPI C/OUT PER DAC NDTSPMREV13PT8 NO CORROSION EVIDENT. RHW SDR 08FDEA01766Frame · dentedCABIN : AFT CABIN AT APPROXIMATELY STATION 1741 LT LONGERON 12 FOUND FRAME DENTED. REPAIRED PER SRM 53-30-00 FIG.1, VOL.I. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PERSDR UPS08M52412Skin · corrodedINSPECTION TYPE:C AFT FUSELAGE EXTERIOR, RIGHT SIDE AT STA 2033 BETWEEN LONGERONS L39 & L 40, CORROSION FOUND SURROUNDING FASTENER HOLE. ATTACH FASTENERS & INNER SUPPORTS REMOVED PER SRM 51-31-01 V II R35. SKIN CORROSION REMOVED PER SRM 51-21-01 VII R35. DASDR UPS08M52413Web · corrodedINSPECTION TYPE:C CABIN LT L27 STA 1946-1986 CHORD WEB AREA FOUND SURFACE CORRODED AS MARKED. LT L27 STA 1946-1986 CORROSION ON WEB SURFACE REMOVED PER SRM 51-21-01 VII R35. CABIN - LT 27 STA 1946-1986 CHORD WEB REMOVED PER SRM 51-31-01 VII R35. NEW WEB FABSDR UPS08M52459Doubler · crackedINSPECTION TYPE:C RT WING FIXED L/E COMPT AT STA XORS 538 APPROX FOUND UPPER DOUBLER CRACKED AS MARKED. DAMAGED AREA AT RT WING FIXED L/E COMPT STA 538 UPPER DOUBLER AREA TRIMMED OFF AS PER SRM 57-10-00 VI FIG 27 R40. NEW REPAIR DOUBLER, REPAIR FILLER & 03EASDR UPS08M52458Seat Track · corrodedINSPECTION TYPE:C CABIN STA 1961 CURVE SEAT TRACK CROWN AREA, X=107.25 FOUND CORROSION AS MARKED. CURVE SEAT TRACK CORROSION REMOVED PER SRM 51-21-01 VII R35. ORIGINAL THICKNESS REMOVED AND FOUND EXCEEDED LIMIT PER SRM 53-70-00 VI R35. CORRODED SEAT TRACK TSDR UPS08M52264Seat Track · corrodedINSPECTION TYPE:C CABIN-STA 839-899 SEAT TRACK CROWN AREA, X=-27.50 FOUND CORROSION AS MARKED. CORROSION AT CABIN STA 839-899 X=-27.5 ON SEAT TRACK CROWN SURFACE AREA REMOVED AS PER SRM 51-21-01 V.II R35. EXISTING SEAT TRACK SPLICE AT STA 816 REMOVED PER SRMSDR UPS08M52263Seat Track · corrodedINSPECTION TYPE:C CABIN-BETWEEN STA 879-899, SEAT TRACK CROWN AREA, X=75.25 FOUND SURFACE CORROSION AS MARKED CORROSION AT CABIN BETWEEN STA 879-899 X=75.25 ON SEAT TRACK CROWN SURFACE AREA REMOVED PER SRM51-21-01 V.II R35. EXISTING SEAT TRACK REPAIR SPLICES SDR CO1Y200800005Skin · crackedFOUND EXISTING REPAIR ON CTR CARGO DOOR FWD LWR CORNER.SDR UPS08M52569Fitting · crackedINSPECTION TYPE:C RHW LOWER WINGLET ASSY AFT FITTING FOUND CRACKED. RHW LOWER WINGLET ASSY ATTACHED BRACKET AND WINGLET FITTING REMOVED. NEW WINGLET FITTING FASTENER HOLES PICKED UP PER SRM 51-31-01VIIR 35. NEW WINGLET INSTALLED PER SRM 51-31-01VIIR35. ATTSDR WRLA2008045Attach Fitting · missingKBGR/EDDP - DURING POST-FLIGHT INSPECTION, MAINTENANCE FOUND AFT LT CENTER GEAR DOOR MECHANICAL ACTUATOR ATTACH FITTING AND HARDWARE MISSING. REPLACED BRACKET ASSY AND R&R ROD END IAW MM 32-59-03, RETRACTED & EXTENDED CRT CREA IAW MM 32-35-00 OPS CK OK LEAK CSDR UPS08M52163Seat Track · corrodedINSPECTION TYPE:C AFT CABIN, CORROSION ON SEAT TRACK CROWN AND CHANNEL AT STA 1761 - 1781 X=-27.5. CORROSION ON AFFECTED AREA REMOVED. MAT'L THK: 0.145 INCH (CROWN), MAT'L REMOVED 0.030 INCH (STA1767), MAT'L REMAINING: 0.115 INCH, FOUND OUT OF LIMIT. DISCRESDR UPS08M52506Support Bracket · crackedINSPECTION TYPE:C LEFT WING L/E TOP PANEL 516ET INTERNAL SUPPORT BRACKETS 03 EA FOUND CRACKED. NR 516ET PANEL INTERNAL (3EA) SUPPORT BRACKETS REMOVED. REPAIR BRACKETS 6EA FAB & HEAT-TREATED. FASTENER HOLES PICK-UP ON 6EA REPAIR SUPPORT BRACKETS. SIX EA REPSDR UPS08M52505Bracket · crackedINSPECTION TYPE:C RHW L/E TOP PANEL NR 616ET INTERNAL SUPPORT BRACKET FOUND CRACKED. INTERNAL SUPPORT BRACKET REMOVED. REPAIR BRACKET FAB 2EA SUPPORT BRACKET HEAT-TREATED AND FASTENER HOLES PICKED UP. REPAIR BRACKETS REPROTECTED AND PAINTED AS PER SRM 51-2SDR UPS08M52547Fitting · crackedINSPECTION TYPE:C RHW LOWER WINGLET (WING MOUNTED) FOUND ATTACH FITTING CRACKED. RHW LOWER WINGLET ATTACH FITTING REMOVED. NEW FITTING FAB WITH FPI C/O, FOUND NO CRACK EVIDENT. NEW FITTING HOLES PICKED UP, PROTECTED AND PAINTED. NEW FITTING INSTALLED AS PESDR UPS08M52431Doubler · crackedINSPECTION TYPE:C RT WING FIXED WING L/E AFT SKIN DOUBLER APPROX STA XORS 550 FOUND CRACKED (2522). AFFECTED SKIN DOUBLER ATTACH PARTS & FASTENERS REMOVED. CRACKED BEADED DOUBLER TRIM OFF. HFEC INSP C/O ON TRIM OFF AREA & FOUND NO CRACK. THREE EACH A REPAISDR UPS08M52411Doubler · crackedINSPECTION TYPE:C RIGHT WING FIXED WING L/E AFT SKIN DOUBLER APPROX STA XORS 556 FOUND CRACKED (2522). RIGHT FIXED WING L/E AFT SKIN DBLR ATTACH PARTS & FASTENERS REMOVED. CRACKED BEADED DOUBLER TRIM OFF. HFEC INSP C/O ON TRIM OFF AREA, FOUND NO CRACK EVIDESDR UPS08M52287Skin · crackedINSPECTION TYPE:C RIGHT WING L/E LWR SURFACE ACCESS PANEL CUTOUT FWD APPROX STA XORS 813 FOUND CRACKED. ATTACH DOOR, FASTENERS & BRACKET REMOVED FROM CRACKED ACCESS PANEL CUTOUT. REPAIR DOUBLER FAB & FASTENER HOLES PICK-UP & PAINTED. REPAIR DOUBLER & ATTACHSDR UPS08M52247Web · dentedINSPECTION TYPE:C CTR CARGO COMPT AT STA 1841, X=-02 & X=-10, WEB FOUND DENTED AS MARKED. DENTED WEB AT STA 1841, RT & ATTACHING FASTENERS REMOVED. NEW WEB FAB USING MAT'L 7075T6 0.050" PER BOEING DWG ACA7170. HOLES PICKED UP & PAINTING DONE ON NEW WEB. NESDR UPS08M52410Skin · crackedINSPECTION TYPE:C, LEFT WING L/E FIXED WING AFT SKIN APPROX STA XORS 538 FOUND CRACKED (2477). LEFT WING NR 4 SLAT CABLE PULLEY REMOVED & L/E FIX WING AFT SKIN FASTENERS REMOVED. INNER SKIN BEADED DOUBLER TRIM OFF. HFEC INSP C/O ON TRIM OFF AREA, FOUND NO C
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