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 IPXA2018081302649Skin · dentedR1 DOOR EXTERIOR SKIN, FWD EDGE, MID SPAN WAS DENTED. REPAIRED THE DOOR SKIN IAW EA 011-5210-01-A7394, REV IR, AND EO MD11-5210-69510-A.SDR IPXA2018081132664Floorbeam · crackedFWD CARGO BAY FLOORBEAM, BS 6-70, LBL 57.5 WAS CRACKED. REPAIRED THE FLOORBEAM IAW EA 011-5310-01-A7370-IR, AND EO MD11-5310-69482-A.SDR IPXA2018081082591Stringer · crackedINSPECTION TYPE: 3C, CENTER WING TANK STRINGER 47 WAS CRACKED. REPAIRED STRINGER IAW SRM 57-10-03, REPAIR 1, FIG 201. MAJOR.SDR IPXA2018080652442Floorbeam · crackedFWD CARGO FLOORBEAM WAS CRACKED AT STATION 6-70, X -57, & Z -98. REPAIRED THE FLOORBEAM IAW SRM 53-40-51, REPAIR 1, FIG 202. MAJOR.SDR IPXA2018080332359Skin · corrodedINSPECTION TYPE:3C, CORROSION AT CENTER WING BOX UPPER SKIN AT APPROX STRINGER 15 LBL 80 - 90. REPAIRED CENTER WING UPPER SKIN BETWEEN STA XCW =81 AND XCW =-50 AT STRINGER 15 IAW EA 011-5730-01-A7377 REV IR AND EO MD11-5730-69383-A. (MINOR)SDR IPXA2018080332334Skin · corrodedINSPECTION TYPE:3C, CENTER WING TANK UPPER CENTER SKIN HAS CORROSION AT STA XCW=101 & XCW=111 AND ABOVE STR 10. REPAIRED CORRODED CENTER WING TANK CENTER SKIN AT STA XCW=101 & XCW=111 IAW EA 011-5730-01-A7379 REV I/R AND EO MD11-5730-69380-A. (MINOR)SDR IPXA2018080132333Skin · corrodedINSPECTION TYPE:3C, CENTER WING TANK UPPER FWD SKIN HAS CORROSION AT STA XCW=-13 & XCW=-15.5 AND ABOVE STR 16-17. REPAIRED CORRODED CENTER WING TANK UPPER FWD SKIN AT STA XCW=-13 & XCW=-15.5 AND ABOVE STR 16-17 IAW EA 011-5730-01-A7376 REV I/R AND EO MD11-5730SDR IPXA2018080132330Skin · corrodedINSPECTION TYPE:3C, CENTER WING BOX UPPER FWD SKIN HAS CORROSION AT STA XCW=100 & XCW=107 AND ABOVE STR 17 & 18. REPAIRED CORRODED CENTER WING BOX UPPER FWD SKIN AT STA XCW=100 & XCW=107 AND ABOVE STR 17 & 18 IAW EA 011-5730-01 A7378 REV I/R AND EO MD11-5730-6SDR IPXA2018073032192Intercostal · crackedINSPECTION TYPE:3C, FWD CARGO INTERCOSTAL IS CRACKED BETWEEN STA 6-30TO 6-50 ABOVE LONG 43L. REMOVED, FABRICATED AND REPLACED INTERCOSTAL BETWEEN STA 6-30 TO 6-50 AND ABOVE LONG 43R IAW DWG ACA7049 AND SRM 51-33-01. (MINOR)SDR IPXA2018073032190Beam · crackedINSPECTION TYPE:3C, FWD CARGO COMP AT STA 6-73 ABOVE LONG 43R, HORIZ BEAM IS CRACKED. REMOVED, FABRICATED AND REPLACED HORIZ BEAM AT STA 6-73 AND ABOVE LONG 43R IAW DWG ADA7667 AND SRM 51-33-01.SDR IPXA2018073032210Landing · crackedINSPECTION TYPE:3C, LT WING FUEL ACCESS PANEL(536AB) LANDING HAS 7 CRACKS BETWEEN STA XORS 683.4 TO 713.65. REPAIRED CRACKED LT WING FUEL ACCESS PANEL LANDING BETWEEN STA XORS 683.4 TO 713.65 IAW SRM 57-20-02 REPAIR 5 FIG 202. (MINOR)SDR IPXA2018071131586Slide · low pressureR1 DOOR ENTRY/SLIDE PSI BELOW MIN. SERVICED R1 ENTRY DOOR EMERGENCY PNEU IAW MM-12-25-04-600-801. LEAK CK GD.SDR IPXA2018071031563Retaining Clip · brokenINSPECTION TYPE:PS-1, LIFE STOWAGE COMPARTMENT DOOR SUPER SEATS LEFT AND CTR RETAINING CLIPS BROKEN. R&R LIFE VEST STOWAGE COMPARTMENT BETWEEN LEFT AND CTR SUPER SEATS, REF AMM 25-64-01-201.SDR IPXA2018071031547Bottle · low pressureL1 ENTRY DOOR EMERGENCY BOTTLE HAS LOW PSI. DEFERRED L1 DOOR IAW MEL 52 10 3 1 2 1. SERVICED L1 ENTRY DOOR IAW MM 12-25-04-600-801.SDR IPXA2018080832579Pan · gougedMAIN CARGO DOOR L/E PAN WAS DENTED AND GOUGED IN TWO AREAS. REMOVED AND REPLACED THE CARGO DOOR PAN IAW SRM 51-31-01, 51-33-01, AND 51-35-01.SDR IPXA2018073032193Longeron Splice · crackedINSPECTION TYPE:3C, MAIN CABIN LONG 7L SPLICE FITTING IS CRACKED AT STA 5-123. REMOVED, FABRICATED AND REPLACED LONG 7L SPLICE FITTING AT STA 5-123 IAW DWG A5A7112 AND SRM 51-33-01. (MINOR)SDR FDEA201807091656Skin · crackedLT WING FOUND SLAT TRACK NR 14 CUTOUT CORNER CRACKED, STA XOS 881 LT WING SLAT TRACK NR 14 CUTOUT CORNER, STA XOS 881 CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201807091655Skin · crackedRT WING FOUND SLAT TRACK NR 14 CUTOUT CORNER CRACKED, STA XOS 889 RT WING SLAT TRACK NR 14 CUTOUT CORNER, STA XOS 889 CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201807091654Skin · crackedRT WING FOUND SLAT TRACK NR 12 CUTOUT CORNER CRACKED, STA XOS 774 RT WING SLAT TRACK NR 12 CUTOUT CORNER, STA XOS 774 CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201807091649Panel · crackedRT WING OUTBOARD L/E PANEL 626AB CRACKED AT STA XOS 842. REPAIR CARRIED OUT PER EA 1-5730-T0340910 P1. CRACKED RT WING LE DOOR PANEL SKIN REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR IPXA2018072331953Support Angle · crackedINSPECTION TYPE:3C, MAIN CABIN STA 1380 LONG 15 LT HAS A CRACKED TEE SUPPORT ANGLE. REMOVED, FABRICATED AND REPLACED LONG 15 LT TEE SUPPORT ANGLE AT STA 1380 IAW DWG AEA7568 AND SRM 51-33-01. (MINOR)SDR IPXA2018072331952Support Angle · crackedINSPECTION TYPE:3C, MAIN CABIN AT STA 1380 LONGERON 15 RT HAS A CRACKED SUPPORT ANGLE. REMOVED, FABRICATED AND REPLACED LONGERON 15 RT SUPPORT ANGLE AT STA 1380 IAW DWG AEA7568 AND SRM 51-33-01. (MINOR)SDR FDEA201807091653Skin · corrodedAFT ACCESSORY COMPARTMENT RT FUSELAGE SKIN AT STA 2163.685 LONGERON 33R-35R, FOUND CORROSION. CARRIED OUT REPAIR AS PER SRM 53-70-01-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. RT FUSELAGE SKIN AT STA 2163.685 LONGERON 33R - LONGERON 35SDR FDEA201807091652Skin · crackedDURING HFEC INSPECTION, 01 EA CRACK FOUND APPROX 1/8 INCH IN LENGTH AT RT WING CORNER NR 5 SLAT ACTUATOR ACCESS DOOR, FORWARD INBOARD CORNER. REPAIR CARRIED OUT AT RT WING CORNER NR 5 SLAT ACTUATOR ACCESS DOOR FWD INBOARD CORNER AT XOS 490 AS PER SRM 57-40-01-SDR FDEA201807091651Skin · crackedDURING HFEC INSPECTION, 01 EA CRACK FOUND APPROX 1/2 INCH IN LENGTH AS MARKED AT LT WING CORNER NR 13 SLAT TRACK NR 10 CUTOUT, AFT INBOARD CORNER. REPAIR CARRIED OUT AT LT WING CORNER NR 13 SLAT TRACK NR 10 CUTOUT AT XOS 659 AS PER SRM 57-40-02-2R FIG 201 REPASDR FDEA201807091650Wire Harness · shortedON DESCENT, RCVD A LEVEL 1 FIRE DET 2 FAULT. TROUBLESHOT, FOUND INTERMITTENT SHORT TO SHIELD/GROUND ON ENGINE FIRE DETECT HARNESS 420803-0000. REMOVED UNSERVICEABLE HARNESS, AWAITING THERMAL WRAP. REMOVED WIRE HARNESS PN 224W9931-501 SN 4815681045. REPLACED NRSDR FDEA201807091647Light · inoperativeON PREFLIGHT CHECK, FOUND EMERGENCY LIGHT DOES NOT ILLUMINATE DURING EMERGENCY LIGHT TEST AND ALSO WHEN S/W SELECTED ON. IDENTIFIED PARTS EMERG EXIT LIGHTS MPN: 60-4411-5 CPN: 3300197. WHILE TROUBLESHOOTING EMER LIGHTS RAN R-T-S ON MSC, ONCE TEST PASSED OPS CHSDR IPXA201808082552Stiffener · crackedVERTICAL STIFFENER WAS CRACKED ON THE LT WING T/E, BEHIND PANEL 541JB, AT XORS 433. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-31-01, AND SRM 51-33-01.SDR IPXA2018080632458Rub Strip · chafedRIGHT INBD AILERON L/E RUBSTRIP WAS HEAVYLY CHAFED. REMOVED AND REPLACED THE RT AILERON IAW AMM 27-10-20-401.SDR IPXA2018080632457Rub Strip · chafedLEFT INBD AILERON L/E RUB STRIP WAS HEAVYLY CHAFED. REMOVED AND REPLACED THE LT INBD AILERON IAW AMM 27-10-20-401.SDR IPXA2018080332357Skin · chafedINSPECTION TYPE:3C, LT I/B FLAP VANE CENTER TRACK CUT OUT ON I/B FLAP SKIN IS CHAFED AT I/B & O/B SIDES. REPAIRED LT I/B FLAP SKIN AT CENTER FLAP VANE TRACK CUT OUT STA XIFH =216.3 IAW EA 011-5753-01-A7382 REV IR AND EO MD11-5750-69441-A. (MINOR)SDR IPXA2018080332376Strap · crackedINSPECTION TYPE:3C, LT WING LOWER T/E STRAP (SILL) AT APPROX STA XORS 410 IS CRACKED. REPAIRED LT WING LOWER T/E STRAP (SILL) AT XORS 420.375 IAW EA 011-5720-01-A7366 REV IR AND EO MD11-5720-69423-A. (MINOR)SDR IPXA2018080132245Skin · damagedINSPECTION TYPE:3C, LT I/B FLAP CENTER AFT LOWER SKIN IS DENTED AND CREASED AT STA XIFH183.3 TOXIFH189.3. REPAIRED FLAP LOWER SKIN AT STA XIFH 183.3 TO XIFH 189.3 IAW EA 0115753-01-A7367 REV I/R AND EO MD11-5750-69384-A. (MAJOR)SDR SRXR201807080002Doubler · crackedRT WING L/E BEADED DOUBLER IS CRACKED AT XOS 610. ACCOMPLISHED REPAIR ON RT WING L/E BEADED DOUBLER AT XOS 610 PER SRM 57-40-02 REPAIR 15 FIG 205 REF NRC A042951.SDR IPXA2018080132252Skin · chafedINSPECTION TYPE:3C, RT O/B FWD PYLON LOWER SKIN IS CHAFED AT STA XDLE 330.2745. REMOVED, FABRICATED AND REPLACED L/E SKIN AT STA XLDE 330.2745 IAW DWG ARB2363 AND SRM 51-31-01 & 51-33-01. (MINOR)SDR IPXA2018073032123Intercostal · crackedINSPECTION TYPE:3C, LT FWD A/C COMPARTMENT DOOR HAS A CRACKED ANGLE (INTERCOSTAL) AT UPPER CENTER. REMOVED AND REPLACED LT A/C COMPARTMENT DOOR UPPER CENTER ANGLE (INTERCOSTAL) IAW SRM 51-31-01, 51-33-01 AND 51-35-01. (MINOR)SDR IPXA2018073032166Intercostal · crackedINSPECTION TYPE:3C, RT A/C COMP AT STA 545, LONGERON 32 RT INTERCOSTAL WEB IS CRACKED. REMOVED, FABRICATED AND REPLACED LONG 32 RT INTERCOSTAL WEB AT STA 545 IAW DWG ACA3804 AND SRM 51-33-01. (MINOR)SDR IPXA2018073032165Former · crackedINSPECTION TYPE:3C, LT WING L/E FORMER IS CRACKED AT STA XOS 917. REMOVED, FABRICATED AND REPLACED LT WING L/E FORMER IAW DWG ARB2920 AND SRM 51-33-01. (MINOR)SDR IPXA2018072732086Doubler · crackedINSPECTION TYPE:3C, LT WING L/E BEADED DOUBLER IS CRACKED AT STA XOS 685.9-699-12. REPAIRED CRACKED LT WING L/E BEADED DOUBLER BETWEEN STA XOS 685.9-699.12 IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)SDR FDEA201807091645Fuel Nozzle · damagedDURING INITIAL CLIMBOUT FROM LAX AT CLIMB THRUST RECEIVED NR 1 ENGINE FIRE LIGHT. LIGHT WENT OUT WHEN TRUST REDUCED TO IDLE. COMPLETED ENGINE FIRE CHECKLIST AND LANDED LAX. IDENTIFIED PARTS FUEL MSN: 1922860. REMOVED BRACKET AND FUEL NOZZLE FOR 1 O`CLOCK POSITSDR IPXA2018081132663Fitting · crackedLEFT WING OTBD FLAP, INBD FWD HINGE SIDE LOAD FITTING TENSION STRAP WAS BROKEN IN HALF. REPAIRED THE FLAP INBD HINGE SIDE LOAD FITTING TENSION STRAP IAW EA 011-5753-01-A7384-IR, AND EO MD11-5750-69523-A. MAJOR.SDR IPXA2018080832578Pan · crackedRIGHT MLG DOOR FWD OTBD CORNER PAN WAS CRACKED. REMOVED AND REPLACED THE DOOR PAN IAW SRM 51-35-01, AND SRM 51-35-02.SDR IPXA2018080132249Pan · crackedINSPECTION TYPE:3C, RT MAIN GEAR DOOR CENTER FWD CORNER PAN IS CRACKED. REMOVED AND REPLACED RT MAIN GEAR CENTER FWD CORNER PAN IAW SRM 51-33-01 AND SRM 51-35-01. MINORSDR IPXA2018072732088Angle · crackedINSPECTION TYPE:3C, INSIDE ACCESS 311AB COMPARTMENT UPPER AFT ATTIC STA 2046 UPPER CEILING ANGLE (CLIP) IS CRACKED AT FASTENER. REMOVED AND REPLACED ANGLE (CLIP) INSIDE ACCESS 311AB COMPARTMENT UPPER AFT ATTIC STA 2046 UPPER CEILING IAW SRM 51-33-01 AND SRM 51SDR IPXA2018072331954Pan · crackedINSPECTION TYPE:3C, LT MLG DOOR FWD O/B CORNER PAN IS CRACKED. REMOVED AND REPLACED LT MLG DOOR FWD O/B PAN IAW SRM 51-35-01. (MINOR)SDR IPXA2018072031893Stiffener · crackedINSPECTION TYPE:3C, RT MLG WW AFT O/B WALL 2ND VERTICAL STIFFNER IS CRACKED. REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG ANB7203 AND SRM 51-33-01. (MINOR)SDR IPXA2018072031864Web · crackedINSPECTION TYPE:3C, RT OVER WING UPPER FUEL TANK AFT WEB IS CRACKED AT STA 1372 AND X=-80. REPAIRED CRACKED RT OVER WING UPPER FUEL TANK AFT WEB AT STA 1372 AND X=-80 IAW EO MD11-5710-69173-A. (MAJOR)SDR IPXA2018072031892Stiffener · crackedINSPECTION TYPE:3C, LT MLG WW AFT O/B WALL 2ND VERTICAL IS CRACKED IN 2 PLACES. REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG ANB7203 AND SRM 51-33-01. (MINOR)SDR FDEA201807061641Doubler · crackedLT WING FOUND LEADING EDGE CAVITY WITH BEADED DOUBLER CRACKED AS MARKED AT STA XOS 626. LT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 626 CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201807061640Doubler · crackedLT WING FOUND LEADING EDGE CAVITY WITH BEADED DOUBLER CRACKED AS MARKED AT STA XOS 695. LT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 695 CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
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