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 IPXA2016072306194Skin · dentedTWO DENTS ALONG UPPER EDGE OF R3 DOOR PLUG CENTERED AT BS 1285. FWD DENT MEASERES 2.0"X.40"X.105" DEEP. OK FOR CONTINUED SERVICE PER VTSAA EA011-5210-01-A6365 REV IR AND EO MD11-5210-61812-A.SDR FDEA201607222594Switch · intermittentL1 DOOR WOULD NOT OPEN AFTER LANDING. FOUND L1 DOOR CONTROL POWER INTERLOCK SWITCH, S1-1090, INTERMITTENT. R & R SAME REF FIM 52-11-03. OBSERVED GIRT BAR ARMED WARNING SWITCH, S1-590, CORRODED. R & R SAME PRECAUTIONARY REF FIM 52-11. L1 DOOR OPS CHECKS SASDR KO0R201607220072Hinge Fitting · wornOTBD LEFT FLAP, OTBD HINGE FITTING OTBD FORWARD LUG IS WORN.SDR KO0R201607220071Frame · chafedCENTER LANDING GEAR WHEEL WELL FORWARD RT FRAME IS CHAFED AT BS 1357 AT RBL 5.SDR KO0R201607220070Support Fitting · wornOTBD RT FLAP, INBD SUPPORT FITTING LOWER LUG IS WORN.SDR KO0R201607220069Bolt · corrodedOTBD RT FLAP, INBD HINGE FITTING UPPER OTBD STUD BOLTS ARE CORRODED.SDR KO0R201607220068Bolt · corrodedOTBD LT FLAP, OTBD HINGE FITTING UPPER INBD STUD BOLT IS CORRODED.SDR KO0R201607220067Hinge · wornFORWARD SEGMENT OF THE UPPER CARGO DOOR HINGE HALF HAS WORN LOBES.SDR KO0R201607220066Hinge · wornMAIN CARGO DOOR FORWARD UPPER HINGE SEGMENT FORWARD LOBES ARE WORN.SDR KO0R201607220065Hinge Fitting · wornOTBD LT FLAP, INBD HINGE FITTING LOWER LUG IS WORN.SDR KO0R201607220064Hinge Fitting · wornOTBD LT FLAP, INBD HINGE FITTING LUG ARE WORN.SDR KO0R201607220063Hinge Fitting · corrodedOTBD LT FLAP, INBD HINGE FITTING LOWER LUGS ARE CORRODED.SDR KO0R201607220062Hinge Fitting · corrodedOTBD RT FLAP, INBD HINGE FITTING LOWER LUGS ARE CORRODED.SDR KO0R201607220061Hinge Fitting · corrodedOTBD RT FLAP, INBD HINGE FITTING UPPER OTBD LUGS ARE CORRODED.SDR KO0R201607220060Hinge Fitting · wornOTBD RT FLAP, INBD HINGE FITTING LUG IS WORN.SDR KO0R201607220059Hinge Fitting · corrodedOTBD LT FLAP, OTBD HINGE FITTING LOWER LUGS ARE CORRODED.SDR KO0R201607220058Hinge Fitting · corrodedOTBD RT FLAP, OTDB HINGE FITTING LOWER LUGS ARE CORRODED.SDR IPXA2016072906461Skin · gougedINSPECTION TYPE: 2C, RT INBD FLAP LOWER SKIN GOUGED NEAR REAR SPAR AT XIFH 168. REPAIRED THE RT INBD FLAP LOWER SKIN IAW EA 011-5753-01-6372 REV. IR AND EO MD11-5750-61379-A.SDR FDEA201607212587Fire Loop · defectiveENGINE FIRE NR 3 INDICATION AT 10K'. COMPLIED WITH QRH, RETURNED TO LAND. T/S AND CHECKED ALL 6 ENGINE LOOPS WITH THEM DISCONNECTED AT RESPONDERS. FOUND LT CORE LOOPS CLOSEST TO THE RESISTANCE LIMIT IS THE TSM. REMOVED AND REPLACED LT CORE LOOP ASSY, A & SDR IPXA2016080306630Structure · dentedINSPECTION TYPE: 1C, AFT EXTENDED TAILCONE IS DENTED AND CRACKED. REPAIRED IAW EA 011-5350-01-A6370 REV I/R AND EO MD11-5350-61344-A.SDR IPXA2016080206623Longeron · corrodedINSPECTION TYPE: 1C, CENTER CARGO LONGERON 52 HAS CORROSION FWD. AND AFT OF BS 1701. REPAIRED CORRODED LONGERON IAW EA 011-5310-01-A6371 REV. I/R AND EO MD11-5310-61430-A. MAJOR.SDR IPXA2016080206621Structure · dentedINSPECTION TYPE: 1C, EXTENDED AFT TAILCONE AFT END IS DENTED AND GOUGED AT AFT STATIC WICK. REPAIRED DAMAGED AFT EXTENDED TAILCONE IAW EA 011-5320-01-A6373 REV. I/R AND EO MD11-5320-61368-A.SDR IPXA2016072806424Door · gougedINSPECTION TYPE:1C, LEFT WING L/E DOOR 518AB GOUGED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOOR 518AB IAW DWG ARB2961 AND SRM 51-21-01.SDR FDEA201607202562Control Panel · odorON FLIGHT CONTROL CHECK. PREMATURE REMOVAL, INSTALLATION OFF MPN: 4059032-901, POS: ON SRL: 94110395, TAG NR: 2676C8 ON MPN: 4059032-901, CPN: 2210019, SRL: 99010475, TAG NR: D61528, REASON CODE: PREMATURE REMOVAL, INSTALLATION OFF MPN: 4059001-908, POS: 1, SSDR FDEA201607202561Battery Pack · abnormalDURING POSTFLIGHT, FOUND PTT ON L1 DOOR SLIDE REMOTE INOPERATIVE. INSPECTED REMOTE PRESSURE INDICATOR AND FOUND THE BATTERIES DEAD. R & R THE BATTERIES IAW AMM 25-61-04-4 , 25-61-04-710-801SDR FDEA201607192527Feeder Cable · damagedAFT FUSELAGE COMPARTMENT AT BS 2033, DURING DEFECT RECTIFICATION, FOUND ONE FEEDER CABLE FOR ENGINE NR 2 WITH DEEP CUT AND ON EWIRING CLAMP WITH SIGN OF ARCING.SDR IPXA2016080106544Former · crackedINSPECTION TYPE: 1C, LEFT OTBD WING L/E COMP. AT XOS 585 FORMER IS CRACKED. REMOVED, FABRICATED AND REPLACED THE FORMER IAW DWG ARB 2931 AND SRM 51-33-01.SDR IPXA2016073106514Stringer · crackedINSPECTION TYPE: 1C, LEFT WING FIXED L/E UPPER STRINGER IS CRACKED AT XOS.667. REPAIRED THE STRINGER IAW SRM 57-40-03, REPAIR 2 FIG. 202. (MAJOR)SDR IPXA2016073006481Intercostal · crackedINSPECTION TYPE: 1C, CRACKED INTERCOSTAL IN LT MLG WW, INBD BULKHEAD, BS 1441 - 1461. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-33-01, AND 51-35-01.SDR IPXA2016072906441Doubler · crackedINSPECTION TYPE:1C, LEFT WING L/E BEADED DOUBLER CRACKED AT STA XOS 650. ACCOMPLISHED PERMANENT REPAIR ON LT WING L/E BEADED DOUBLER FROM STA XOS 636-653 IAW SRM 57-40-02. REPAIR 15, FIGURE 203.SDR IPXA2016072806407Doubler · crackedINSPECTION TYPE:1C, LT WING FIXED L/E SKIN INNER SPLICE DOUBLER CRACKED XOS 667. R & R DOUBLER IAW SRM 51-33-01.SDR IPXA2016072806403Support · crackedINSPECTION TYPE:1C, RT WW INBD GEAR DOOR RETRACT CYLINDER SUPPORT INTERCOSTAL CRACKED BETWEEN STA 1441-1461. CRACKED SUPPORT REPAIRED IAW SRM 53-40-12, REPAIR 3 FIG 201.SDR IPXA2016072806402Doubler · crackedINSPECTION TYPE:2C, LEFT WING FIXED L/E SKIN INNER SPLICE DOUBLER CRACKED AT XOS 906. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SPLICE DOUBLER IAW DWG ARB2954 AND SRM 51-33-01.SDR IPXA2016072706385Doubler · crackedINSPECTION TYPE: 1C. RIGHT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS 494 - 500. THE DOUBLER WAS REPAIRED IAW SRM 57-40-02 REPAIR 15 FIG. 206 MAJOR REPAIR.SDR IPXA2016072706384Doubler · crackedINSPECTION TYPE: 1C, RIGHT WING FIXED L/E SKIN SPLICE DOUBLER CRACKED ALONG XOS 789. REMOVED FABRICATED AND INSTALLED REPLACEMENT SPLICE DOUBLER IAW DWG ARB2954 AND SRM 51-33-01.SDR IPXA2016072006079Skin · damagedRIGHT WING FIXED LE SKIN DAMAEGD AT XIS 207.844. COMPLETED TEMP REPAIR PER EO MD11-5720-59485-BSDR FDEA201607182498Skin · crackedRIGHT WING, FIXED LEADING EDGE NR 10 SLAT TRACK INBOARD CUTOUT SKIN CENTER FOUND CRACKED AT XOS 657. REPAIR CARRIED OUT IAW EA 1-5730-T0326737, PART 1, TITLE: WINGS, PLATES AND SKINS. REPAIR FOR RT WING FIXED L/E NR 10 SLAT TRACK CUTOUT SKIN CENTER AREA CRASDR IPXA2016080306631Structure · gougedINSPECTION TYPE: 1C, NR 1 ENGINE INBD FAN COWL FWD UPPER FITTING IS GOUGED. REPAIRED THE NR 1 FAN COWL IAW EA 011-7110-01-A6375 REV. I/R AND EO MD11-7110-61394-A.SDR IPXA2016072806413Intercostal · crackedINSPECTION TYPE:1C, INTERCOSTAL CRACKED IN CAC CEILING RT SIDE BETWEEN STA 6-90 AND 1139. REMOVED FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW DWG ADA7652 AND SRM 51-33-01.SDR IPXA2016072906443Trunnion · crackedINSPECTION TYPE:1C, NLG LT TRUNION FITTING CRACKED ACCOMPLISHED REPAIR ON NLG LT TRUNION FITTING STA 582, Z=-114, X= -24 IAW SRM 53-10-14, REPAIR 2, FIGURE 202.SDR IPXA2016071705969Indicator · inoperativeL1 SILDE REMOTE PRESSURE PRESS TO TEST INDICATOR INOPERATIVE. REPLACED THE BATTERIES & REMOTE PRESSURE INDICATOR ASSY. IAW AMM 25-61-04. OPS. CHECKED NORMAL.SDR IPXA2016071806023Indicator · inoperativeL1 DOOR SLIDE REMOTE PRESSURE PRESS TO TEST INDICATION SYS IS INOPERATIVE. REPLACED BATTERIES AND REMOTE PRESSURE INDICATOR ASSY IAW AMM 25-61-04. OPS CHECKED NORMAL.SDR FDEA201607152450Brake · failedDURING NR 10 TIRE CHANGE, FOUND BRAKE DISKS ARE COMING APART. PREMATURE REMOVAL/INSTALLATION, OFF MPN: 2609472-4, POS: 10, SRL B1471, TAG NR: 1540E0 ON MPN: 2609472-4B, CPN: 3200378, SRL B2599. R & R BRAKE ASSY, REF AMM 32-43-20-4, LEAK AND PRESSURE CHECK GSDR IPXA2016100809083Strap · crackedINSPECTION TYPE: 3C, RIGHT WING LOWER T/E ACCESS PANEL SILL STRAP CRACKED AT XORS 468. SILL STRAP REPAIRED IAW EA 011-5720-01-A6457 REV. IR AND EO MD11-5720-62060-A.SDR IPXA2016071505871Circuit Breaker · trippedBUSS LT EMERGENCY DC OFF. INSPECTION FOUND THE LT EMERGENCY DC BUSS FEED TR 1 C/B OUT. PERFORMED RESET OF C/B AND CARRIED OUT OPS CHECK OF THE DC TIE SWITCH LIGHTS IAW AMM TASK 24-08-02-700-803REV 86.00. OPS CHECKED OK. PERFORMED EPCU R-T-S PER AMM 24-08-01SDR FDEA201607132370Skin · crackedAGING AIRCRAFT, EXISTING REPAIR AT RT WING INBD FLAP SEGMENT UPPER SURFACE AT XIFH 171.3 -XIFH 177.3. EVALUATED AND FOUND CRACK COMMON TO SKIN. RIGHT WING INBD FLAP, INBD FLAP SEGMENT UPPER SURFACE XIFH 171.3-XIFH 177.3. CARRIED OUT REPAIR IAW EA 1-5750-T03SDR FDEA201607132433Hinge · corrodedRIGHT WING, INBD FLAP OTBD FWD HINGE, WING SIDE, PIVOT BORE FOUND, CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-07. EXISTING HOLE DIA: 2.531", FINAL HOLE DIA: 2.536" AND MAXIMUM ALLOWABLE HOLE DIA: 2.531". NEW REPAIR BUSHING FABRICATED AND INSSDR FDEA201607132432Hinge · corrodedRIGHT WING, INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.289", FINAL HOLE DIA: 1.328" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED ANSDR FDEA201607132431Hinge · corrodedRIGHT WING, INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT INBD BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.290", FINAL HOLE DIA: 1.328" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRSDR FDEA201607132430Hinge · corrodedRIGHT WING, OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR ATTACH OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.221", FINAL HOLE DIA: 1.225", MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRICATED
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