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 FDEA201610043449Rib · crackedRIGHT HAND WING FIXED LEADING EDGE CAVITY AT STA XOS 667 RIB DOUBLER FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01-0G, DWG #ARB3954 REV K. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201610043448Rib · crackedRIGHT HAND WING FIXED LEADING EDGE CAVITY AT STA XOS 584 RIB FORMER FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01-0G, DWG #ARB2931 REV 'H'. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR IPXA2016102910016Spar · corrodedINSPECTION TYPE: 3C, UPPER FORWARD RUDDER FRONT SPAR WEB CORRODED BETWEEN STA. ZFR 449 - 454REPAIRED RUDDER WEB CORROSION PER VTSAA EA 011-5540-01-A6527 REV. IR AND UPS EO MD11-5540-62321-A (MAJOR)SDR IPXA2016102910015Support · corrodedINSPECTION TYPE: 3C, RT WING TO FUSELAGE FILLET SUPPORT RIB CORRODED AT Y=5-53. REPAIRED THE SUPPORT RIB IAW EA 011-5350-01-A6526 REV. IR AND EO MD11-5350-62318-A.SDR IPXA2016102509884Fastener · shearedINSPECTION TYPE:3C, NR 4 BANJO FITTING HAS 1 SHEARED FASTENER COMMON TO THE CARRY THROUGH CAP STRAP AFT OF STA 2164. REPLACED FASTENER AT NR 4 BANJO FITTING IAW EA 011-5530-01-A62-512 REV I/R AND EO MD11-5530-62247-A. (MINOR)SDR IPXA2016102209704Spar Cap · corrodedINSPECTION TYPE: 3C, LT WING REAR SPAR UPPER CAP AFT FLANGE CORRODED XORS 671 - 825. THE SPAR FLANGE WAS REPAIRED IAW EA 011-5730-01-A6523 REV. IR AND EO MD11-5710-62218-A.SDR IPXA2016101909587Stiffener · corrodedINSPECTION TYPE:3C, RT WING TO FUSELAGE RIB AT STA 5-113 AND 11" FROM LOWER END IS CORRODED. REPAIRED CORRODED WING TO FUSELAGE RIB INSTALLATION AT SAID LOCATION IAW EA 011-5320-01-A6516 REV I/R AND EO MD11-5320-62171-A. MINOR.SDR IPXA2016101709449Strap · corrodedINSPECTION TYPE: 3C, ACCESS PANEL LANDING IS CORRODED ON RT INBD FLAP OTBD HINGE AFT FAIRING. REMOVED, FABRICATED AND REPLACED IAW DWG ARC7540 AND SRM 51-31-01.SDR IPXA2016101209280Angle · crackedINSPECTION TYPE: 3C, LT WING T/E VERTICAL TEE ANGLE IS CRACKED AT XW 371.549. REMOVED AND REPLACED THE TEE ANGLE IAW SRM 51-33-01.SDR IPXA2016100308905Cable · failedL1 DOOR INOPERATIVE. REPLACED THE DRIVE CABLE AND SUPPORT ASSEMBLY. OPS OK. IAW MM 52-11-09-000-801.SDR IPXA2016100508968Gate · damagedL1 ENTRY DOOR HAS A DAMAGED EXTERIOR DOOR HANDLE FLAPPER. THE FLAPPER ASSY REPLACED IAW AMM 20-11-00.SDR IPXA2016100308916Lamp · inoperativeRT EMERGENCY LIGHT ABOVE COURIER SEAT OUT. REPLACED THE LAMP, OPS CHECKED GOOD IAW AMM 33-50-00.SDR FDEA201610033437Doubler · crackedRT WING FIXED LEADING EDGE CAVITY AT STA XOS 639 BEADED DOUBLER FOUND CRACKED. CARRIED OUT INNER DOUBLER REPAIR PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201610033436Doubler · crackedLT WING FIXED LEADING EDGE CAVITY AT STA XOS 627 BEADED DOUBLER FOUND CRACKED. CARRIED OUT INNER DOUBLER REPAIR PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201610033435Doubler · crackedLT WING FIXED LEADING EDGE CAVITY AT STA XOS 693 BEADED DOUBLER FOUND CRACKED. CARRIED OUT INNER DOUBLER REPAIR PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201610033434Doubler · crackedLT WING FIXED LEADING EDGE CAVITY AT STA XOS 755 BEADED DOUBLER FOUND CRACKED. CARRIED OUT INNER DOUBLER REPAIR PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201610033433Doubler · crackedLT WING FIXED LEADING EDGE CAVITY AT STA XOS 733 BEADED DOUBLER FOUND CRACKED. CARRIED OUT INNER DOUBLER REPAIR PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201610033432Doubler · crackedLT WING FIXED LEADING EDGE CAVITY AT STA XOS 766 BEADED DOUBLER FOUND CRACKED. CARRIED OUT INNER DOUBLER REPAIR PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201610033431Doubler · crackedRT WING FIXED LEADING EDGE AT STA XOS 606 PANEL SUPPORT DOUBLER FOUND CRACKED. DOUBLER REMOVED AND REPLACED WITH NEW FABRICATED DOUBLER PER SRM 51-31-01-0G AND DRAWING ARB2933 REV 'AJ' AND REV 'T'. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201610033430Doubler · crackedLT WING FIXED LEADING EDGE LOWER SURFACE AT STA XOS 548 PANEL SUPPORT DOUBLER FOUND CRACKED. DOUBLER REMOVED AND REPLACED WITH NEW FABRICATED DOUBLER PER SRM 51-31-01-0G AND DRAWING ARB2933 REV 'AJ' AND REV 'T'. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR IPXA2016102409831Skin · chafedINSPECTION TYPE:3C, RT WING FIXED LEADING EDGE LOWER SKIN AT STA XDLE 309 HAS CHAFE DAMAGE. REPAIRED CHAFED RT WING FIXED L/E LOWER SKIN AT STA XDLE 309 IAW EA 011-5730-01-A6500 REV I/R AND EO MD11-5730-62243-A. (MAJOR)SDR IPXA2016101309324Stiffener · crackedINSPECTION TYPE: 3C, NR 3 PYLON VERTICAL SUPPORT WEB ATTACH STIFFNER IS CRACKED. REMOVED, FABRICATED AND REPLACED NR 3 PYLON VERTICAL SUPPORT STIFFNER IAW DWG AUB7564 AND SRM 51-35-01.SDR FDEA201610023429Light · inoperativeUPON DISARMING L1 DOOR AT CRK THE DISARM LIGHT DID NOT COME ON. USED R1 FOR ENTRY. FOUND SLIDE WAS NOT DISARMED. FOUND "DISARM" BULBS BURNED OUT. RELAMP AND CHECKED NML. OPERATION CHECK ARM/DISARM SEVERAL TIMES NML PER AMM 52-11-02-6.SDR IPXA2016100208835Skin · damagedLEFT INBD FLAP SKIN INTERIM REPAIR. REPAIRED IAW EO MD11-5750-61915-BSDR IPXA2016100308918Clamp · leakingMANIFOLD 2 FAILED WARNING RECEIVED IN FLIGHT. FOLLOWED AOM CHECKLIST, THE NR 2 ENGINE THRUST REDUCED TO EXTINGUISH WARNING. NOTE - THE NR 2 BLEED VALVE INDICATED OPEN THE ENTIRE TIME. EMERGENCY DECLARED. PERFORMED FIM 36-23-03, FOUND SEVERAL CLAMPS ON SDR FDEA201610023425Seat Track · corrodedMAIN DECK RT STA 1099, X=-27 SEAT TRACK ASSEMBLY FOUND WITH FOUND SURFACE CORROSION AS MARKED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1009 TO STA 1129 X = -27 PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201610023424Seat Track · corrodedMAIN DECK STA 1099, X= 27 SEAT TRACK ASSEMBLY FOUND WITH FOUND SURFACE CORROSION AS MARKED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1069 TO STA 1129 X = 27 PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201610023423Seat Track · corrodedMAIN DECK RT STA 1039, X=-47 SEAT TRACK ASSEMBLY FOUND WITH FOUND SURFACE CORROSION AS MARKED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1009 TO STA 1049 X = -47 PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR IPXA2016102209701Spar Cap · corrodedINSPECTION TYPE: 3C, RT WING REAR SPAR UPPER CAP AFT FLANGE CORRODED BETWEEN XORS 672 - 738. THE SPAR FLANGE WAS REPAIRED IAW EA 011-5730-01-A6518 REV. IR AND EO MD11-5710-62206-ASDR IPXA2016102209700Spar Cap · corrodedINSPECTION TYPE: 3C, RT WING REAR SPAR UPPER CAP AFT FLANGE CORRODED BETWEEN XORS 765 - 826. SPAR REPAIRED IAW EA 011-5730-01-A6517 REV. IR AND EO MD11-5710-62207-A.SDR IPXA2016102009625Support Frame · crackedINSPECTION TYPE: 3C, SUPPORT FRAME IS CRACKED INSIDE ACCESS HOLE 311AB BS 2065. REMOVED, FABRICATED AND REPLACED SUPPORT FRAME IAW DWG. AJC7029 AND SRM 51-33-01.SDR IPXA2016101809532Support Angle · crackedINSPECTION TYPE:3C, LT WING FIXED L/E INNER RIB SUPPORT ANGLE CRACKED AT XOS.1089. REMOVED FABRICATED AND INSTALLED REPLACEMENT ANGLE PER DWG ARN2920 AND SRM 51-35-01. MINOR.SDR IPXA2016101309327Skin · brokenINSPECTION TYPE: 3C, RIGHT WING L/E SKIN IS BROKEN OFF AT SLAT TRACK NR 8. REPAIRED THE SKIN IAW EA 011-5730-01-A6504 REV. I/R AND EO MD11-5730-62115-A.SDR IPXA2016101209284Doubler · crackedINSPECTION TYPE: 3C, RT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS.783. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG. 203. (MAJOR)SDR IPXA2016101209282Former · crackedINSPECTION TYPE: 3C, RT WING FIXED L/E BAY HAS A CRACKED FORMER AT XORS. 455. REMOVED, FABRICATED, AND REPLACED THE FORMER IAW DWG ARB1162 AND SRM 51-33-01.SDR IPXA2016093008780Drive System · stuckL1 DOOR WILL NOT OPEN. REPLACED DRIVE CABLE AND SUPPORT ASSY. OPS CHECKED GOOD IAW MM 52-11-09-000-801.SDR IPXA2016101909586Nose Cowl · gougedINSPECTION TYPE: 3C, NR 1 ENGINE NOSE COWL ASSY. UPPER RT SKIN SEGEMENT IS GOUGED AT THE 2 O'CLOCK POSITION.REPAIRED GOUGED #1 ENG. NOSE COWL ASSY. UPPER R/H SKIN SEGEMENT AT 2 O'CLOCK POS. IAW VT-SAA EA 011-7110-01-A6511 REV. I/R AND UPS EO MD11-7110-62176-A.SDR IPXA2016101909584Trunnion · crackedINSPECTION TYPE: 3C, LEFT NOSE LANDING GEAR TRUNNION FITTING IS CRACKED.REPAIRED CRACKED. L/H NOSE LANDING GEAR TRUNNION FITTING IAW SRM 53-10-14 REPAIR 2 FIG. 202. (MAJOR)SDR IPXA2016101909583Trunnion · crackedINSPECTION TYPE: 3C, RT NOSE LANDING GEAR TRUNNION FITTING IS CRACKED. REPAIRED CRACKED NOSE LANDING GEAR TRUNNION FITTING IAW SRM 53-10-14 REPAIR 2 FIG. 202. (MAJOR)SDR IPXA2016100108816Smoke Detector · malfunctionedCABIN SMOKE ALERT DURING CLIMB THROUGH 7000 FT. ALERT WAS MOMENTARY AND RETURNED AGAIN MOMENTARILY TROUBLESHOT IAW FIM 26-15-00-101 FIG 108. R & R IAW MM 31-42-01-741. OK TO CONTINUE.SDR IPXA2016100709057Intercostal · corrodedINSPECTION TYPE: 3C, INTERCOSTAL CORRODED BS 1039 - 1059 ALONG L43L. REMOVED FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW DWG ACA7049 AND SRM 51-33-01.SDR IPXA2016101109216Stiffener · corrodedINSPECTION TYPE: 3C, THE LEFT NLG SUPPORT BEAM STIFFNER HAS CORROSION AT BS 541.667. REPAIRED THE SUPPORT BEAM STIFFNER IAW EA 011-5310-01-A6503 REV. I/R AND EO MD11-5310-62095-A.SDR IPXA2016101109214Door Frame · corrodedINSPECTION TYPE: 3C, LT FUSELAGE NLG DOOR FRAME CORRODED AT BS 547.250 AND BS 541.667. REPAIRED THE DOOR FRAME IAW EA 011-5310-01-A6502 REV. I/R AND EO MD11-5310-62096-A.SDR FDEA201609273379Brake Assy · failedDURING TAXI OUT, RECEIVED A TIRE DIFF TEMP ALERT. NR 3 & 4 TEMPS WERE 79 FOR NR 3 & 518 FOR NR 4. TAXIED TO PARKING, RECEIVED A LEVEL 2 TIRE PRESSURE LOW, FOLLOWED BY A TIRE FAIL. R & R THE NR 4 BRAKE IAW MM 32-43-20-04.SDR FDEA201609273372Vane · corrodedLEFT WING OTBD FLAP VANE HORN FITTING-D, BUSHING BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R, FIG 201. REPAIR SLOT BUSHING FABRICATED IAW EA 1-5750-T0328435 PART 1 STEP 1A AND INSTALLED IAW AMM 27-50-32-4.SDR FDEA201609273371Vane · corrodedRIGHT WING OTBD FLAP VANE HORN FITTING-C, BUSHING BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R, FIG 201. A REPAIR SLOT BUSHING WAS FABRICATED IAW EA 1-5750-T0328433 PART 1 STEP 2B AND INSTALLED IAW AMM 27-50-32-4.SDR FDEA201609273370Vane · corrodedRT WING OTBD FLAP VANE HORN FITTING E, BUSHING BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R FIG.201. SLOT BUSHING FABRICATED IAW EA 1-5750-T0328433 PART 1 STEP 2A AND INSTALLED IAW AMM 27-50-32-4.SDR FDEA201609263368Battery · failedEMERGENCY POWER TEST FAIL ON PREFLIGHT CHECK. PREMATURE REMOVAL/INSTALLATION, OFF MPN: 31433-001, POS: 2, SRL: 10200007, TAG NR: F40369 ON MPN: 31433-001, CPN: 2412387, SRL: 10103712, TAG NR: 384D35, REASON CODE: PREMATURE REMOVAL/INSTALLATION, OFF MPN: 3143SDR FDEA201609253359Panel · missingON ARRIVAL, FOUND NR 1 INBOARD ENGINE MOUNT COVER WAS FOUND MISSING, ALSO FWD NUT PLATEWAS MISSING AND REAR NUT PLATE ATTACH RIVET HEAD MISSING. REPAIRED IAW 1-5450-T0328547 A PART 2, REPLACED INTERIM PANEL WITH NEW IAW AMM,SRM, IAW DRAWINGS AUB7726. OK FORSDR IPXA2016100809098Skin · chafedINSPECTION TYPE: 3C, LEFT DROOP L/E FLEXIBLE SKIN PANEL CHAFED. REMOVED AND REPLACED THE SKIN PANEL IAW AMM 27-80-10.
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