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.

SDR FDEA201606302200Seat Track · damagedMAIN DECK CARGO LT FLOOR SEAT TRACK AT STA 1259, X= 47.5, FOUND CROWN DAMAGED AS MARKED.Jun 30, 2016 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201606302199Seat Track · damagedMAIN DECK CARGO RT FLOOR SEAT TRACK AT STA 5-53, X=-47.5. FOUND CROWN DAMAGED AS MARKED.Jun 30, 2016 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201606302198Floorbeam · corrodedCENTER CARGO FLOORBEAM UPPER SURFACE FOUND WITH CORROSION AT STA 1701, X=-18 TO X=-24.Jun 30, 2016 · N602FE · Doug MD11F · Fuselage Main, Floor BeamSDR IPXA2016063005232Bracket · damagedDURING PRE FLIGHT, FOUND L1 DOOR GIRT BAR BRACKET HAS COME APART. REINSTALLED L1 DOOR ESCAPE SLIDE GIRT BAR AS REQ'DJun 29, 2016 · N280UP · Doug MD11F · Emergency EquipmentSDR FDEA201606292197Computer · failedRECEIVED AURAL CAWS ALERT, TIRE FAILURE, ON GEAR EXTENSION. ALL OTHER INDICATIONS NORMAL. PERFORMED GO AROUND, QRH CHECKLIST, LANDED. PREMATURE REMOVAL/INSTALLATION. LAST FLIGHT FAULT SHOWED, BTM/TPI CONTROL UNIT COMPUTER FAIL INTERMITTENT. REPLACED THE TJun 29, 2016 · N591FE · Doug MD11F · Landing Gear Brake SystemSDR FDEA201606292192Pitot Line · contaminatedLOST FLIGHT DIRECTORS AND AUTOPILOT/ATS PASSING 16000. F/O AIRSPEED 10 KNOTS LESS THAN CAPTAIN AND STANDBY A/S. ALSO RECEIVED, SELECT ELEVATOR FEEL MANUAL AND SELECT FLAP LIMIT OVER RIDE INDICATIONS. ENTERED A/S UNRELIABLE CHECKLIST. F/O SELECTED AUXILIARJun 29, 2016 · N631FE · Doug MD11F · Pitot/Static SystemSDR FDEA201606292189Hinge · corrodedLT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, EXISTING HOLE DIA: 1.249", FINAL HOLE DIA: 1.252" MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLEDJun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292188Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE D: 0.420", FINAL HOLE D: 0.423", MAXIMUM ALLOWABLE HOLE D: 0.391". REPAIR BUSHING FABRICATED AND INSTALLED IJun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292187Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 0.420", FINAL HOLE: DIA 0.423", MAXIMUM ALLOWABLE HOLE: DIA 0.391". REPAIR BUSHING FABRICATED AND INJun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292186Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE SURFACE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.400", MATERIAL REMOVED: 0.006", FWD FACE; 0.023", AFT FACE, REMAINING THICKNESS: 0.371". MINIMUJun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292185Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE SURFACE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.419", MATERIAL REMOVED: 0.006", FWD FACE; 0.006", AFT FACE, REMAINING THICKNESS: 0.389". MINIMUM Jun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292184Hinge · corrodedLT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.614", FINAL HOLE DIA: 0.620", MAXIMUM ALLOWABLE HOLE DIA: 0.584". REPAIR BUSHING FABRICATED IAW EA: 1Jun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292183Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.614", FINAL HOLE DIA: 0.620", MAXIMUM ALLOWABLE HOLE DIA: 0.584". REPAIR BUSHING FABRICATED IAW EAJun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292182Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.946". MAXIMUM ALLOWABLE HOLE DIA: 0.944". REPAIR BUSHING FABRICATED AND INSTAJun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292181Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT INBD HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.946". MAXIMUM ALLOWABLE HOLE DIA: 0.944". REPAIR BUSHING FABRICATED BY MACHJun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292180Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE PIVOT HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 2.311". FINAL HOLE DIA: 2.316". MAXIMUM ALLOWABLE HOLE DIA: 2.3135". REPAIR BUSHING FABRICATED AND INSTALLED IAWJun 29, 2016 · N602FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606292179Door · stuckDURING PREFLIGHT, R-1 DOOR WOULD NOT OPEN.Jun 29, 2016 · N616FE · Doug MD11F · Passenger/Crew DoorsSDR IPXA2016062905184Light · inoperativeL1 DOOR DISARM LIGHT INOPERATIVE. REPLACED LIGHT INDICATOR ASSY SWPM: 20-84-00, PN OFF-ON: 351-24406-402, SN OFF: NSN, SN ON: TAG 01465838. EFF REF IPC: 52-11-70-01, ITEM:170.Jun 28, 2016 · N257UP · Doug MD11F · Door Warning SystemSDR FDEA201606282177Screw · defectiveCABIN DOOR WOULD NOT ARM AT PUSHBACK. FOUND DOOR CABLE BRACKET LOOSE. REPLACED HARDWARE FOR BRACKET. L1 DOOR OPS CK GOOD AND ARMS. REF AMM 52-11-02-6, FOUND DOOR CABLE BRACKET LOOSE. REPLACED HARDWARE FOR BRACKET. L1 DOOR OPS CK GOOD & ARMS, REF AMM 52-1Jun 28, 2016 · N602FE · Doug MD11F · Passenger/Crew DoorsSDR IPXA2016062805178Power Supply · inoperativeEMERGENCY POWER TEST FAILED, INOPERATIVE. R & R EMERGENCY POWER SUPPLY. OPS CK NORMAL REF AMM 33-51-01 EFF SOURCE IPC 33 51 01, EFF SOURCE IPC 33-51-10-01-005J.Jun 27, 2016 · N257UP · Doug MD11F · Emergency LightingSDR IPXA2016071405860Thrust Reverser · crackedINSPECTION TYPE: 3C. NR 3 ENG. O/B THRUST REVERSER CASCADE FRAME LOWER LUG BORE IS CRACKED. REMOVED AND REPLACED THE THRUST REVERSER HALF IAW AMM 71-13-01-000-868 AND 71-13-01-400-868.Jun 25, 2016 · N285UP · Doug MD11F · Engine Thrust ReverserSDR IPXA2016062605038Skin · damagedL1 DOOR ENTRY DOOR OUTER SKIN DAMAGED. REPAIRED REF EO MD11-5210-61065-B.Jun 25, 2016 · N252UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2016070705511Fitting · corrodedINSPECTION TYPE: 3C, RIGID CARGO BARRIER FLOOR FITTING NR 6 HAS CORROSION. REPAIRED CORRODED RCB FLOOR FITTING NR 6 IAW EA 011-5340-01-A6346 REV. I/R AND EO MD11-5340-61193-A. (MINOR)Jun 24, 2016 · N285UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016070705510Fitting · corrodedINSPECTION TYPE: 3C, RIGID CARGO BARRIER FLOOR FITTING NR 7 HAS CORROSION. REPAIRED THE FLOOR FITTING IAW EA 011-5340-01-A6346 REV. I/R AND EO MD11-5340-61193-A. (MINOR)Jun 24, 2016 · N285UP · Doug MD11F · Fuselage Main, StructureSDR FDEA201606242136Wire Harness · chafedDURING APPROACH, AFTER ALL CHECKLISTS COMPLETED, WE HAD A GREEN BOX ON DU NR 3, BUT THEN, LANDING GEAR, BEGAN FLICKERING IN SIDE THE BOX INTERMITTENTLY. WE LOOKED AT THE LANDING GEAR SYNOPTIC. THE LT GEAR INDICATED RED FOR UNSAFE. WENT AROUND CYCLED GEAR FJun 24, 2016 · N617FE · Doug MD11F · Landing Gear System WiringSDR IPXA2016071505935Frame · crackedINSPECTION TYPE: 3C, FUSELAGE FRAME CRACKED AT BS 469 NEAR X=60. REPAIRED IAW EA 011-5310-01-A6348 REV. IR AND EO MD11-5310-61274-A. MAJOR REPAIR.Jun 23, 2016 · N285UP · Doug MD11F · Fuselage Main, FrameSDR IPXA2016071505933Frame · crackedINSPECTION TYPE: 3C, FUSELAGE FRAME CRACKED AT BS 469 NEAR X 30. REPAIRED IAW EA 011-5310-01-A6348 REV. IR AND EO MD11-5310-61274-A. MAJOR REPAIR.Jun 23, 2016 · N285UP · Doug MD11F · Fuselage Main, FrameSDR IPXA2016070605471Drip Tray · chafedINSPECTION TYPE: 3C, AFT SIDE OF MAIN AVIONICS RACK DRIP SHIELD IS CHAFED. REMOVED, FABRICATED AND REPLACED THE DRIP SHIELD IAW DWG SP11251227 AND SRM 53-00-00.Jun 23, 2016 · N285UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016062805149Fitting · crackedINSPECTION TYPE:3C, RIGID CARGO BARRIER FLOOR FITTING NR 10 IS CRACKED. R & R RCB FLOOR FITTING IAW EO MD11-2520-58701-C.Jun 23, 2016 · N285UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016062405000Actuator · inoperativeL1 ENTRY DOOR WILL NOT LATCH FULL OPEN OR CLOSE. MOTOR IS INTERMITTENT. R & R L1 DOOR ELECTRICAL ACT REF MM 52-11-01. OPS NORMAL, IPC 52-11-05-05.Jun 23, 2016 · N295UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2016071005625Longeron Splice · crackedINSPECTION TYPE: 3C, CENTER CARGO LONGERON SPLICE 33L IS CRACKED AT BS 5-123. REMOVED, FABRICATED AND REPLACED THE LONGERON SPLICE IAW DWG A5A7112 AND SRM 51-33-01. (MINOR)Jun 22, 2016 · N285UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2016071105697Longeron Splice · crackedINSPECTION TYPE: 3C, FWD CARGO LONGERON SPLICE 45L AT BS 685 IS CRACKED. REMOVED AND REPLACED THE LONGERON SPLICE IAW SRM 51-33-01. (MINOR)Jun 22, 2016 · N285UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2016070605498Intercostal · crackedINSPECTION TYPE: 3C, FWD. CARGO BAY BETWEEN BS 6-39 TO 6-59 AND LONGERON 42-43L, INTERCOSTAL IS CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-33-01. (MINOR)Jun 22, 2016 · N285UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016062204929Power Supply · inoperativeEMERGENCY LIGHT BATTERY 1 LOW ALERT ON PREFLIGHT. DEFERRED EMERGENCY LIGHTING SYSTEM IAW MEL 33-50-4. R&R EMERGENCY LIGHT BATTERY POWER SUPPLY MM 33-51-01-00-802 AND 33-51-01-400-802. OPS TEST SATIS MM 33-51-01-700-802.Jun 22, 2016 · N291UP · Doug MD11F · Emergency LightingSDR IPXA2016071505932Skin · corrodedINSPECTION TYPE:3CAFT FUSELAGE EXTERIOR SKIN CORRODEDSTA. 2140 - 2164 L33 - 35L. REPAIRED IAW EA 011-5330-01-A6341 REV. IR AND EO MD11-5330-61287-A. MAJOR REPAIR.Jun 21, 2016 · N285UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016071505931Skin · corrodedINSPECTION TYPE: 3C, AFT FUSELAGE EXTERIOR SKIN CORRODED BS 2120 - 2163 L33 - 35L. REPAIRED IAW EA 011-5330-01-A6341 REV. IR AND EO MD11-5330-61287-A. MAJOR REPAIR.Jun 21, 2016 · N285UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016071505917Skin · corrodedINSPECTION TYPE: 3C, CENTER WING UPPER SKIN CORRODED ABOVE STRINGER 15 BETWEEN XCW -5 AND -20. REPAIRED IAW EA 011-5730-01-A6357 REV. IR AND EO MD11-5730-61284-A.Jun 21, 2016 · N285UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016071505916Skin · corrodedINSPECTION TYPE: 3C, CENTER WING UPPER SKIN CORRODED ABOVE STRINGER 15 NEAR XCW102. REPAIRED NOTED CORROSION IAW EA 011-5730-01-A6357 REV. IR AND EO MD11-5730-61284-A.Jun 21, 2016 · N285UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016071505913Skin · corrodedINSPECTION TYPE: 3C, CENTER WING UPPER SKIN PANEL CORRODED ABOVE S15 BETWEEN XCW -32 AND -45. REPAIRED IAW EA 011-5730-01-A6357 REV. IR AND EO MD11-5730-61284-A.Jun 21, 2016 · N285UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016071505911Longeron · crackedINSPECTION TYPE:3C, LONGERON 27L CRACKED BS 1219 - 1239. REPLACED THE LONGERON IAW EA 011-5310-01-A6343 REV. IR AND EO MD11-5310-61257-A. MAJOR REPAIR.Jun 21, 2016 · N285UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2016071505878Fuel Tank · corrodedINSPECTION TYPE: 3C, MAIN CABIN UNDER FLOOR CENTER TANK UPPER SKIN HAS CORROSION AT XCW=-50 AT STR. 15.REPAIRED CORRODED CTR. WING SKIN AT STA. XCW=-50 IAW EA 011-5730-01-A6345 REV. I/R AND EO MD11-5730-61283-A. MAJOR REPAIR.Jun 21, 2016 · N285UP · Doug MD11F · Fuel StorageSDR IPXA2016071505877Longeron · crackedINSPECTION TYPE: 3C, MAIN CABIN AT BS 1179-1199, LONGERON 27 LT IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE LONGERON IAW EA 011-5310-01-A6344 REV. I/R AND EO MD11-5310-61228-A. MAJOR REPAIR.Jun 21, 2016 · N285UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2016070605500Stringer · crackedINSPECTION TYPE: 3C, CENTER TANK STRINGER 48 HAS AN 8 INCH CRACK AT XCW=32.00. REPAIRED THE STRINGER IAW SRM 57-10-03 REPAIR 1 FIG. 201. (MAJOR)Jun 21, 2016 · N285UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016071505895Longeron · crackedINSPECTION TYPE: 3C, MAIN CABIN LONGERON 27R IS CRACKED BETWEEN BS 1219-1239. REPAIRED THE LONGERON IAW EA 011-5310-01-A6355 REV. I/R AND EO MD11-5310-61227-A. MAJOR REPAIR.Jun 20, 2016 · N285UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2016071505880Frame · dentedINSPECTION TYPE:3C, MAIN CABIN FRAME IS DENTED AT BS 715, LONGERON 12R. REPAIRED THE FRAME IAW EA 011-5310-01-A6350 REV. I/R AND EO MD11-5310-61254-A. MAJOR REPAIR.Jun 20, 2016 · N285UP · Doug MD11F · Fuselage Main, FrameSDR IPXA2016071505879Frame · dentedINSPECTION TYPE: 3C, MAIN CABIN FRAME IS DENTED AT BS 675, LONGERON 12R. REPAIRED THE FRAME IAW EA 011-5310-01-A6349 REV. I/R AND EO MD11-5310-61250-A. MAJOR REPAIR.Jun 20, 2016 · N285UP · Doug MD11F · Fuselage Main, FrameSDR IPXA2016071405839Frame · dentedINSPECTION TYPE: 3C, MAIN CABIN FRAME IS DENTED AT BS 775 LONGERON 12R. REPAIRED THE FRAME IAW EA 011-5310-01-A6352 REV. I/R AND EO MD11 5310-61255-A. MAJOR REPAIR.Jun 20, 2016 · N285UP · Doug MD11F · Fuselage Main, FrameSDR IPXA2016071305797Longeron · chafedINSPECTION TYPE:3C, MAIN CABIN LONGERON 12 LT IS CHAFED BETWEEN STA 1781-1801. REPAIRED CHAFED LONGERON 12 LT BETWEEN STA 1781-1801 IAW EA 011-5310-01-A6353, REV I/R AND EO MD11-5310-61225-A.Jun 20, 2016 · N285UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2016070805539Tube · kinkedINSPECTION TYPE: 3C, RT WING FUEL TRANSFER PIPE HAS A LARGE DENT AT XOS 703.6. REPAIRED THE TRANSFER PIPE IAW EA 011-2820-A6336 REV. I/R AND EO MD11-2820-61199-A. (MINOR)Jun 20, 2016 · N285UP · Doug MD11F · Aircraft Fuel Distribution SystemSDR IPXA2016070605470Longeron Splice · crackedINSPECTION TYPE:3CMAIN CABIN LONGERON 12 L SPLICE FITTING IS CRACKED AT STA 5-123. REMOVED, FABRICATED AND REPLACED THE LONGERON SPLICE IAW DWG A5A7112 AND SRM 51-33-01. (MINOR)Jun 20, 2016 · N285UP · Doug MD11F · Fuselage Main, Longeron/Stringer
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