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 IPXA2016060604308Bulkhead Web · corrodedINSPECTION TYPE:3C, FORWARD CARGO COMPARTMENT AFT BULKHEAD WEB IS CORRODED AT BS 6-73.5 ABOVE LONGERON 42 RT. REMOVED, FABRICATED AND INSTALLED REPLACEMENT CHORD IAW DWG ADA7667 AND SRM 51-35-01.SDR IPXA2016060604304Skin · corrodedINSPECTION TYPE:3C, CENTER WING UPPER AFT SKIN HAS CORROSION ABOVE STR 5 AND 6 AT BS XCW =- 113. REPAIRED IAW EA 011-5730-A6270, REV I/R AND EO MD11-5730-60877-A.SDR IPXA2016060304196Door Frame · crackedINSPECTION TYPE: 3C, AFT CARGO DOOR AFT FRAME LOWER LIGHTNING HOLE IS CRACKED. REPAIRED AFT CARGO DOOR AFT FRAME LOWER LIGHTNING HOLE IAW EA 011-5231-01-A6284 AND EO MD11-5230-60907-A.SDR IPXA2016053104045Intercostal · crackedINSPECTION TYPE: 3C, FWD CARGO COMPARTMENT AT BS 6-10 TO 6-30, INTERCOSTAL BETWEEN LONGERON 42R-43R IS CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL AT BS 6-10 TO 6-30 LONGERON 42R TO 43R IAS DWG ACA7049 AND SRM 51-33-01.SDR IPXA2016053104043Intercostal · crackedINSPECTION TYPE:3CFWD, CARGO AT BS 655 TO 675 LONG 42R-43R, INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL AT BS 655 TO 675 LONGERON 42R-43R IAW DWG ACA7049 AND SRM 51-35-01.SDR IPXA2016052904000Longeron Splice · crackedINSPECTION TYPE:3C, LONGERON SPLICE FITTING IS CRACKED IN FWD. CARGO COMPARTMENT AT BS 869, LONGERON 35 LT. R & R CRACKED LONGERON 35 LT SPLICE FITTING AT BS 869 IAW DWG ADA8423 AND SRM 51-33-01.SDR FDEA201605171649Skin · crackedON WALK AROUND, FOUND RT WING LE CRACK, APPROX 3.5" AT INBD SIDE OF NR 6 SLAT. REPAIRED IAW EA 1-5730-T0325373 PART 1 & 2.SDR FDEA201605171648Doubler · crackedRIGHT WING FIXED LE COMPARTMENT, AT STATION XOS 795, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201605171647Doubler · crackedRIGHT WING FIXED LE COMPARTMENT, STATION XOS 768, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR AS IAW GMM 6-2-100.SDR FDEA201605171646Doubler · crackedRIGHT WING FIXED LE COMPARTMENT, AT APPROX STATION XOS 697, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201605171645Doubler · crackedRIGHT WING FIXED LE COMPARTMENT, AT STATION XOS 665, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201605171644Doubler · crackedRIGHT WING FIXED LE COMPARTMENT, AT STATION XOS 656, BEADED DOUBLER FOUND CRACKED. REPAIR CLASSIFIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201605171643Doubler · crackedRIGHT WING FIXED LE COMPARTMENT, AT STATION XOS 614, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201605171642Doubler · crackedLEFT WING FIXED LE COMPARTMENT AT APPROX STATION XOS 545, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201605171641Doubler · crackedLEFT WING FIXED LE COMPARTMENT AT APPROX STATION XOS 675, BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201605171640Fitting · corrodedLEFT WING, OTBD FLAP VANE HORN FITTING B FWD HOLE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02-2R, FIG 201, EXISTING SIZE: LENGTH 0.915", WIDTH: 0.621". FINAL SIZE: LENGTH 1.0395", WIDTH: 0.7395", MAXIMUM ALLOWABLE SIZE: LENGTH 0.9SDR FDEA201605171639Fitting · corrodedLEFT WING, OTBD FLAP VANE HORN FITTING C FWD HOLE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02-2R, FIG 201, EXISTING SIZE: LENGTH 0.918", WIDTH: 0.653". FINAL SIZE: LENGTH 1.019", WIDTH: 0.718", MAXIMUM ALLOWABLE SIZE: LENGTH 0.940SDR FDEA201605171638Fitting · corrodedLEFT WING, OTBD FLAP VANE HORN FITTING D FWD HOLE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02-2R, FIG 201, EXISTING SIZE: LENGTH 0.858", WIDTH: 0.598", FINAL SIZE: LENGTH 0.9495", WIDTH: 0.649", MAXIMUM ALLOWABLE SIZE: LENGTH 0.940SDR FDEA201605171637Hinge · corrodedRIGHT WING, INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE OTBD BORE CORROSION. CORROSION REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING DIA: 1.282", FINAL DIA: 1.315", MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IAW SDR FDEA201605171636Hinge · corrodedRIGHT WING, INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE INBD BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING DIA: 1.283", FINAL DIA: 1.315". MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLED ISDR FDEA201605171635Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 1.282", FINAL DIA: 1.288", MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLEDSDR FDEA201605171634Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 1.250", FINAL DIA: 1.254", MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED BY MACHINING ASDR FDEA201605171633Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 0.708", FINAL DIA: 0.722". MAXIMUM ALLOWABLE DIA: 0.709". SHOULDER BUSHING FABRICATED BY MACHISDR FDEA201605171632Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 0.708", FINAL DIA: 0.722". MAXIMUM ALLOWABLE DIA : 0.709". SHOULDER BUSHING FABRICATED BY MACHSDR FDEA201605171631Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, UPPER MOUNT OTBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 0.943", FINAL DIA: 0.953". MAXIMUM ALLOWABLE DIA: 0.944". REPAIRED BUSHING, FABRICATED BY MACSDR FDEA201605171630Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 1.251 INCH, FINAL DIAMETER 1.254 INCH & MAX ALLOWABLE DIAMETER 1.220 INCH;. REPAIRED BUSHING, FASDR FDEA201605171629Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.382 INCH, FINAL DIAMETER 0.410 INCH & MAXIMUM ALLOWABLE DIAMETER 0.391 INCH. RSDR FDEA201605171628Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER HOLE BORE CORROSION. CORROSION HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.382 INCH, FINAL DIAMETER 0.410 INCH & MAX ALLOWABLE DIAMETER 0.391 INCH. REPAIREDSDR FDEA201605171627Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE 3 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.598 INCHES, FINAL DIAMETER 0.604 INCHES, MAX ALLOWABLE DIAMETER 0.584 INCHES. REPSDR FDEA201605171626Hinge · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION AT HOLE 3 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.598 INCHES, FINAL DIAMETER 0.604 INCHES, MAX ALLOWABLE DIAMETER 0.584 INCHES. REPSDR FDEA201605171625Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT INBD HOLE BORE CORROSION. CORROSION HOLE NR 2 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.944 INCHES, FINAL DIAMETER 0.951 INCHES, MAX ALLOWABLE DIAMETER 0.944 INCHES. REPSDR FDEA201605171624Hinge · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE OTBD BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-03. EXISTING DIAMETER 1.222 INCH, FINAL DIAMETER 1.237 INCH & MAX ALLOWABLE DIAMETER 1.220 INCH. REPAIRED BUSHING, FABRICASDR FDEA201605171623Hinge · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE INBD BORE CORROSION. CORROSION AT HOLE INBD BORE REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-03. EXISTING DIAMETER 1.2235 INCH, FINAL DIAMETER 1.237 INCH & MAX ALLOWABLE DIAMETER 1.220 INCH. REPAIRSDR FDEA201605171622Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 1.218 INCH, FINAL DIAMETER 1.226 INCH & MAXIMUM ALLOWABLE DIAMETER 1.220 INCH. REPAISDR FDEA201605171621Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE. BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 1.252 INCH, FINAL DIAMETER 1.255 INCH & MAXIMUM ALLOWABLE DIAMETER 1.220 INCH. REPSDR FDEA201605171620Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE SURFACE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING THICKNESS 0.437 INCHES, MATERIAL REMOVED FWD SIDE 0.006 INCHES, AFT SIDE 0.016 INCHES, REMAINING THICSDR FDEA201605171619Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-48-08. EXISTING DIAMETER 0.708 INCHES, FINAL DIAMETER 0.731 INCHES, MAX ALLOWABLE DIAMETER 0.709 INCHES. RSDR FDEA201605171618Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 0.727 INCHES, FINAL DIAMETER 0.731 INCHES & MAX ALLOWABLE DIAMETER 0.709 INCHES. REPAIR BUSHINSDR FDEA201605171617Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, UPPER MOUNT HOLE OTBD BORE CORROSION. REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 0.942 INCHES, FINAL DIAMETER 0.950 INCHES & MAX ALLOWABLE DIAMETER 0.944 INCHES. REPAIR BUSHING FABRICATSDR FDEA201605171616Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08, EXISTING DIAMETER 0.627 INCHES, FINAL DIAMETER 0.629 INCHES & MAX ALLOWABLE DIAMETER 0.621 INCHES. REPAIR BUSHINGSDR FDEA201605171615Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, FWD MOUNT INBD HOLE BORE CORROSION. CORROSION AT HOLE NR 6 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 1.2805 INCH, FINAL DIAMETER 1.284 INCH & MAX ALLOWABLE DIAMETER 1.254 INCH. REPAIRESDR FDEA201605171614Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 1.256 INCH, FINAL DIAMETER 1.259 INCH, MAX ALLOWABLE DIAMETER 1.220 INCH. REPAIRED BSDR FDEA201605171613Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBOARD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 1.252 INCH, FINAL DIAMETER 01.259 INCH, MAX ALLOWABLE DIAMETER 1.220 INCH. REPAIRSDR FDEA201605171612Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.665 INCHES, FINAL DIAMETER 0.677 INCHES & MAX ALLOWABLE DIAMETER 0.667 INCHES. REPAIR BUSHING FABSDR FDEA201605171611Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.390 INCHES, FINAL DIAMETER 0.407 INCHES, MAX ALLOWABLE DIAMETER 0.391 INCHES. REPAIR BUSHINSDR FDEA201605171610Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER HOLE BORE FOUND CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.390 INCHES, FINAL DIAMETER 0.407 INCHES, MAX ALLOWABLE DIAMETER 0.391 INCHES. REPAIREDSDR FDEA201605171609Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE FOUND CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.582 INCH, FINAL DIAMETER 0.597 INCHES. MAX ALLOWABLE DIAMETER 0.584 INCHES. SHOULDER SDR IPXA2016061204517Skin · corrodedINSPECTION TYPE:3C, AFT FUSELAGE SKIN HAS CORROSION BETWEEN BS 2125 TO 2163 AND BETWEEN LONG. 33 RT TO 35 RT. REPAIRED CORRODED FUSELAGE SKIN AT SAID LOCATION IAW VT-SAA EA 011-5330-01-A6277 REV I/R AND MD11-5330-61031-A.SDR IPXA2016060804365Seat Track · damagedINSPECTION TYPE:3C, MAIN CABIN CENTER SEAT TRACK HAS AN ELONGATED HOLE AT BS 565. REPAIRED SEAT CENTER SEAT TRACK AT BS 565 IAW VT-SAA EA011-5310-01-A6265, REV. I/R AND EO MD11-5310-60986-A.SDR IPXA2016060704327Structure · corrodedINSPECTION TYPE:3C, AFT CARGO COMPARTMENT AT BS 1902 TO 1967 ABOVE LONGERON 42 RT, T-CHORD HAS CORROSION. REMOVED, FABRICATED AND REPLACED T-CHORD IAW DWG. AGA3857 AND SRM 51-31-01.
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