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 IPXA2017022814518Skin · crackedINSPECTION TYPE: 3C, LEFT WING LOWER SKIN CRACKED AROUND FASTENER HOLES THRU PANEL LANDING 536AB XORS 683 - 713. REPAIRED IAW SRM 57-20-02 REPAIR 5.SDR IPXA2017022814521Skin · chafedINSPECTION TYPE: 3C, RT WING FIXED L/E EXTERIOR SKIN CHAFED AT OTBD END OF THE NR 8 SLAT, XOS 1191. REPAIRED THE DAMAGE IAW SRM 57-40-01, REPAIR 16.SDR IPXA2017022514414Door Frame · crackedINSPECTION TYPE: 3C, THE L3 DOOR FRAME INTERIOR FWD WEB CRACKED AT LIGHTENING HOLE, BS 1254. REPAIRED THE DOOR FRAME WEB IAW SRM 53-40-15 REPAIR 3, FIG. 201.SDR IPXA2017022514413Door Frame · crackedINSPECTION TYPE: 3C, R3 DOOR INTERIOR FWD FRAME WEB CRACKED AT THE LIGHTENING HOLE. REPAIRED THE DOOR FRAME WEB IAW SRM 53-40-15 REPAIR 3 FIG. 201.SDR IPXA2017022314361Skin · crackedINSPECTION TYPE: 3C, RT WING ACCESS PANEL 636AB LANDING CRACK INDICATIONS. REPAIRED IAW SRM 57-20-02, REPAIR 5, FIG. 201.SDR IPXA2017022014225Bracket · crackedINSPECTION TYPE: 3C, LOWER AUX TANK UNDERWING FRAME ATTACH BRACKET BROKEN, RT SIDE, BS 1278. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT BRACKET IAW DWG AYB7035 AND SRM 51-33-01.SDR IPXA2017022014224Skin · corrodedINSPECTION TYPE: 3C, RIGHT WING UPPER SKIN CORRODED AROUND FASTENER HEAD XORS 901, ABOVE STRINGER 2. REPAIRED THE SKIN IAW EA 011-5730-01-A6650 REV. IR AND EO MD11-5730-63313-A.SDR IPXA2017021514072Pan · crackedINSPECTION TYPE: 3C RT MLG DOOR OTBD FWD CORNER PAN IS CRACKED. REMOVED AND REPLACED THE DOOR PAN IAW SRM 51-35-01, & 51-35-02.SDR FDEA201702020341Vane · corrodedRIGHT WING OTBD FLAP VANE NR 2 FITTING BUSHING HOLE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R FIG 201. A SLOT BUSHING WAS FABRICATED IAW EA 1-5750-T0331241, PART 1, STEP 2 AND INSTALLED IAW AMM 27-50-32-4.SDR FDEA201702020340Hinge Bracket · corrodedRIGHT WING OTBD FLAP AFT HINGE, FLAP SIDE, PIVOT OUTBD HOLE BORE FOUND CORRODED. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-132706 D, PART 4, STEP 2 & 3.SDR FDEA201702020339Hinge Bracket · corrodedRIGHT WING OTBD FLAP AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE FOUND CORRODED. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-132706 D, PART 4, STEP 2 & 3.SDR FDEA201702020338Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE, WING SIDE, ACTUATOR INBD HOLE SURFACE CORRODED. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1.SDR FDEA201702020337Hinge · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE, WING SIDE, ACTUATOR OUTBD HOLE BORE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1C.SDR FDEA201702020336Hinge · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1C.SDR FDEA201702020335Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE SURFACE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1.SDR FDEA201702020334Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE SURFACE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1.SDR FDEA201702020333Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE CORRODED. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1, AND STEP 1B.SDR FDEA201702020332Hinge Bracket · corrodedRIGHT HAND WING OUTBD FLAP FWD INBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE CORRODED. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1, AND STEP 1B.SDR FDEA201702020331Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1A.SDR FDEA201702020330Hinge Bracket · corrodedRIGHT WING OUTBD FLAP INBD FWD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133 PART 1, STEP 1A.SDR FDEA201702020329Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) ACTUATOR OUTBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331132, PART 1, STEP 1B.SDR FDEA201702020328Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331132, PART 1, STEP 1B.SDR FDEA201702020327Hinge · corrodedRIGHT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331132, PART 1, STEP 1, AND STEP 1A.SDR FDEA201702020326Hinge · corrodedRIGHT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331132, PART 1, STEP 1, AND STEP 1A.SDR FDEA201702020325Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) ACTUATOR OUTBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331077, PART 1, STEP 1B.SDR FDEA201702020324Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331077, PART 1, STEP 1B.SDR FDEA201702020323Hinge Bracket · corrodedLEFT WING OTBD FLAP FWD INBD HINGE (WING SIDE) UPPER MOUNT OUTBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331077, PART 1, STEP 1A.SDR FDEA201702020322Hinge Bracket · corrodedLEFT WING OTBD FLAP FWD INBD HINGE (WING SIDE) UPPER MOUNT INBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331077, PART 1, STEP 1A.SDR FDEA201702020321Hinge Bracket · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331076, PART 1, STEP 1B.SDR FDEA201702020320Hinge · corrodedLEFT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) ACTUATOR OUTBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44- 09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331076, PART 1, STEP 1B.SDR FDEA201702020319Hinge · corrodedLEFT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE SURFACE CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. TWO SHOULDER BUSHINGS AND REPAIR SHIMS FABRICATED AND INSTALLED IAW EA 1-5750-T0331076, PART 1, STEP SDR FDEA201702020318Hinge Bracket · corrodedLEFT WING INBD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBD HOLE BORE FOUND WITH CORROSION. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-132705 C, PART 4, STEP 2A & 2C. CLASSIFIESDR FDEA201702020317Hinge Bracket · corrodedLEFT WING INBD FLAP OTBD AFT HINGE (FLAP SIDE) PIVOT OUTBD HOLE BORE FOUND WITH CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW CMM 57-52-03. OVERSIZE BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-132705 C, PART 4, STEP 2A & 2C. REPAIR CLASSSDR FDEA201702020316Frame · chafedMAIN DECK CARGO BAY FRAME CHAFED AT LT BS 535, LONGERON 19L. REPAIRED IAW SRM 53-20-07-2R, FIG 202, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR IPXA2017022814531Stringer · crackedINSPECTION TYPE: 3C, LT WING STRINGER 15 FOUND CRACKED OTBD OF XORS 433. REPAIRED THE STRINGER IAW EA 011-5710-01-A6636 REV. IR, AND EO MD11-5710-63428-A. (MAJOR)SDR IPXA2017022714450Spar Cap · corrodedINSPECTION TYPE: 3C, LEFT WING UPPER SPAR CAP AFT FLANGE CORRODED BETWEEN XORS 673 & 789. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A6665 REV. IR AND EO MD11-5710-63374-A.SDR IPXA2017022314347Trunnion · damagedINSPECTION TYPE: 3C, LT NLG TRUNNION INBD BUSHING LOOSE. REPAIRED THE TRUNNION IAW SRM 53-10-14, REPAIR 1, FIG. 201.SDR IPXA2017022314350Longeron · corrodedINSPECTION TYPE: 3C, MAIN CARGO HAS CORROSION ON LONGERON 18L BS 1461. REMOVED AND REPLACED THE LONGERON IAW SRM 51-33-01.SDR IPXA2017022314349Longeron · corrodedINSPECTION TYPE: 3C, MAIN CARGO HAS CORROSION ON LONGERON 18L, BS 1501. REMOVED AND REPLACED THE LONGERON IAW SRM 51-33-01.SDR IPXA2017022314348Longeron · corrodedINSPECTION TYPE :3C, MAIN CARGO HAS CORROSION ON THE BS 1481 LONGERON 18L. REMOVED AND REPLACED THE LONGERON IAW SRM 51-33-01.SDR IPXA2017022114270Stringer · crackedINSPECTION TYPE: 3C, STRINGER 47 CRACKED IN RADIUS AT XCW 46. REPAIRED THE STRINGER IAW SRM 57-10-03, REPAIR 1, FIG. 201. (MAJOR)SDR IPXA2017030114591Beam · gougedINSPECTION TYPE: 3C, FWD EXTENDED TAIL CONE AT BS 2165, BEAM HAS GOUGE DAMAGE. REPAIRED THE TAIL CONE BEAM IAW EA 011-5320-01-A6615 REV I/R, AND EO MD11-5350-63293-A.SDR IPXA2017030214623Skin · chafedINSPECTION TYPE: 3C, RIGHT WING FIXED L/E SKIN IS CHAFED AT XIS. 164.317 TO XIS 168.660. REPAIRED THE L/E SKIN IAW EA 011-5740-01-A6624 AND EO MD11-5730-63307-A. (MAJOR)SDR IPXA2017022814526Frame · damagedINSPECTION TYPE: 3C, TAILCONE FWD FRAME CHAFED AT THE LT UPPER GUIDE PIN. REPAIRED THE DAMAGE IAW SRM 53-00-00, REPAIR GENERAL FIG. 210.SDR IPXA2017022814525Frame · damagedINSPECTION TYPE: 3C, TAILCONE FWD FRAME CHAFED AT THE RT UPPER GUIDE PIN. REPAIRED THE DAMAGE IAW SRM 53-00-00, REPAIR GENERAL FIG. 210.SDR IPXA2017022814524Frame · damagedINSPECTION TYPE: 3C, TAILCONE FWD FRAME CHAFED AT THE RT CENTER GUIDE PIN. REPAIRED THE DAMAGE IAW SRM 53-00-00, REPAIR GENERAL FIG. 210.SDR IPXA2017022814522Skin · chafedINSPECTION TYPE: 3C, CHAFE DAMAGE TO LOWER L/E SKIN OF LT INBD AILERON. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT LOWER L/E SKIN PANEL IAW DWG NRC6043 AND SRM 51-33-01.SDR IPXA2017022514415Skin · damagedINSPECTION TYPE: 3C, RIGHT SIDE EXTENDED TAILCONE SKIN AND LONGERON GOUGED, EXISTING REPAIR CHAFED, BS 2165 RBL 36. REPAIRED IAW EA 011-5320-01-A6621 REV. IR AND EO MD11-5350-63205-A.SDR IPXA2017022514412Skin · damagedINSPECTION TYPE: 3C, CHAFE DAMAGE IN FUSELAGE EXTERIOR SKIN, BS 1170, LONGERON 44R. REPAIRED THE SKIN IAW EA 011-5330-01-A6626 REV. IR AND EO MD11-5330-63375-A.SDR IPXA2017022514411Skin · damagedINSPECTION TYPE: 3C, CHAFED EXISTING REPAIR DOUBLER. REPAIRED THE TAILCONE SKIN IAW EA 011-5320-01-A6621 RV. IR AND EO MD11-5350-63205-A.
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