Boeing MD-11F

Service difficulty reports · 31,320

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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 FDEA201605221709Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH SPOT FACE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.408", MATERIAL REMOVED: FWD 0.008", AFT 0.025", REMAINING THICKNESS: 0.375" ANMay 22, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605221708Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.584", FINAL HOLE DIA: 0.613" AND MAXIMUM ALLOWABLE HOLE DIA: 0.584". NEW May 22, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605221707Hinge Bracket · corrodedRIGHT WING, OTBD FLAP OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.584", FINAL HOLE DIA: 0.612" AND MAXIMUM ALLOWABLE HOLE DIA: 0.584". NEWMay 22, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR IPXA2016061204512Skin · brokenINSPECTION TYPE: 3C, LOWER AFT RUDDER LOWER RT SKIN PANEL IS BROKEN OFF. REPAIRED LOWER AFT RUDDER IAW EA 011-5540-01-A6275 REV. I/R AND EO MD11-5540-61013-B.May 21, 2016 · N257UP · Doug MD11F · Rudder, Plate/SkinSDR IPXA2016061104478Skin · gougedINSPECTION TYPE: 1C, LT WING FIXED L/E UPPER SURFACE IS GOUGED BETWEEN XOS 1185 AND 1191. REPAIRED LT WING FIXED L/E UPPER SKIN BETWEEN XOS 1185 AND XOS 1191 IAW EA 011-5730-01-A6296-IR, DATED 06/10/2016 AND UPS EO 5730-61025-A, DATED 06/10/2016.May 21, 2016 · N281UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2016060904421Rub Strip · damagedINSPECTION TYPE: 1C, NR 2 ENGINE LT FAN COWL, T/E RUBSTRIP CHAFE DAMAGE. REPAIRED IAW EA 011-7110-01-A6298, REV. IR AND EO MD11-5420-60987-A.May 21, 2016 · N281UP · Doug MD11F · Nacelle/Pylon Miscellaneous StructureSDR FDEA201605211723Panel · crackedLEFT WING LE HAS CRACK AT LEAST 5 INCHES LONG THAT EXTENDS BENEATH THE NR 7 SLAT. CRACK IS FWD OF FUEL VLV PANEL 526FB. REPAIR COMPLETE IAW WRI 57-10 2352 & EA 1-5710-T0325565 PART 1.May 21, 2016 · N522FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2016060404216Trunnion · crackedINSPECTION TYPE:1C, NLG LT TRUNION FITTING CRACKED ADJACENT TO TRUNION PIN BOSS, BS 582, Z=-114, X=24, REPAIRED CRACKED TRUNION FITTING IAW SRM 53-10-14, REPAIR 2, FIG 202.May 20, 2016 · N281UP · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR IPXA2016060304169Intercostal · crackedINSPECTION TYPE:1C, UPPER INTERCOSTAL CRACKED IN LT MAIN WHEEL WELL. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW DWG AEA0218, SRM 51-33-01, 51-35-01.May 20, 2016 · N281UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016060304199Shear Tie · crackedINSPECTION TYPE:1C, SHEAR TIE CRACKED IN 311 COMPARTMENT CEILING, BS 2084. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SHEAR CLIP IAW DWG AJC7029, SRM 51-33-01, 51-35-01.May 20, 2016 · N281UP · Doug MD11F · Fuselage Internal Mounting StructureSDR IPXA2016060104134Intercostal · crackedINSPECTION TYPE:1C, UPPER INTERCOSTAL CRACKED IN RT WHEEL WELL. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW DWG AEA0218, SRM 51-33-01, 51-35-01.May 20, 2016 · N281UP · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201605201685Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.248", FINAL HOLE DIA: 1.252" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEMay 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201684Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.249", FINAL HOLE DIA: 1.252" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEMay 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201683Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM57-44-08. EXISTING HOLE DIA: 0.709", FINAL HOLE DIA: 0.727" AND MAXIMUM ALLOWABLE HOLE DIA: 0.709". NEW SMay 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201682Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.709", FINAL HOLE DIA: 0.727" AND MAXIMUM ALLOWABLE HOLE DIA: 0.709". NEW May 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201680Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, PIVOT BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM57-44-08. EXISTING HOLE DIA: 2.311", FINAL HOLE DIA: 2.316" AND MAXIMUM ALLOWABLE HOLE DIA: 2.3135". NEW REPAIR BUSHING FAMay 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201679Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH OTBD LUG BORE FOUND CORROSION. NR 8 HOLE CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.219", FINAL HOLE DIAMETER 1.224" & MAXIMUM ALLOWABLE HOLE DIMay 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201678Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, ACTUATOR ATTACH INBD LUG BORE FOUND CORROSION. NR 8 HOLE CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 1.218", FINAL HOLE DIAMETER 1.224" & MAXIMUM ALLOWABLE HOLE DIMay 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201677Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH SPOT FACE FOUND CORROSION. REWORKED & FOUND EXCEEDED LIMIT IAW MM 57-44-09. EXISTING THICKNESS 0.421", MATERIAL REMOVED, FWD FACE 0.009" & AFT FACE 0.009", REMAINING THICKNESS 0.4May 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201676Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH SPOT FACE FOUND CORROSION. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.399", MATERIAL REMOVED 0.009", REMAINING THICKNESS 0.390" & MINIMUM ALLOWABLE THIMay 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201675Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE FOUND CORROSION. NR 3 HOLE CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.581", FINAL HOLE DIAMETER 0.589" & MAXIMUM ALLOWABLE HOLE DIAMMay 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605201674Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE FOUND CORROSION. HOLE 3 CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.596", FINAL HOLE DIAMETER 0.598" & MAXIMUM ALLOWABLE HOLE DIAMETEMay 20, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR IPXA2016061004444Doubler · chafedINSPECTION TYPE: 1C, RT WING FIXED LEADING EDGE EXTERNAL DOUBLER HAS CHAFE DAMAGE BS XOS 442-467 ACCOMPLISHED BLEND REPAIR ON RT WING FIXED L/E EXTERNAL DOUBLER IAW EA 011-5700-01-A6289, REV I/R AND EO MD11-5700-60939-A.May 19, 2016 · N281UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2016061004439Skin · dentedINSPECTION TYPE:1C, REF EO MD11-7830-60613-A NR 2 LT REV INNER BARREL EXTERIOR SKIN. REQUIRES PERMANENT REPAIR. REPAIR NR 2 LT REV SKIN IAW EA 011-7830-01-A6279, REV. IR AND EO MD11-7830-60928-A.May 19, 2016 · N281UP · Doug MD11F · Engine Thrust ReverserSDR IPXA2016060304189Stringer · crackedINSPECTION TYPE:1C, PREVIOUSLY INSTALLED REPAIR AT RT WING L/E STRINGER FOUND CRACKED AT BS XOS.906. R & R REPAIR DOUBLER IN RT WING L/E SRM 57-40-03, REPAIR 1, FIG 201.May 19, 2016 · N281UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2016060304188Stringer · crackedINSPECTION TYPE:1C, LT WING FIXED L/E INNER STRINGER CRACKED NEAR BS XOS906. REPAIRED CRACKED STRINGER IAW SRM 57-40-03, REPAIR 1, FIG 201.May 19, 2016 · N281UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2016060304187Skin · crackedINSPECTION TYPE:1C, LT WING FIXED L/E EXTERIOR SKIN CRACKED AT INBD END OF REFUELING DOOR CUTOUT, BS XOS611. REPAIRED NOTED CRACK IAW SRM 57-40-02, REPAIR 18, FIG 201.May 19, 2016 · N281UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2016060204155Doubler · crackedINSPECTION TYPE: 1C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS 758-763. REPAIRED NOTED BEADED DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 203.May 19, 2016 · N281UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2016060104119Skin · crackedINSPECTION TYPE:1C, LT WING FIXED L/E EXTERIOR SKIN CRACKED AT NR 12 SLAT TRACK CUTOUT BS XOS776. REPAIRED LT WING SKIN BS XOS.776 IAW SRM 57-40-02, REPAIR 7, FIG 201.May 19, 2016 · N281UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2016052903999Skin · crackedINSPECTION TYPE:1C, RT WING FIXED L/E SKIN CRACKED ON LOWER SURFACE NEAR BS XOS 720. REPAIRED L/E SKIN IAW SRM 57-40-02. REPAIR 7, FIG 201.May 19, 2016 · N281UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2016052303740Tire · failedEMERGENCY DECLARED, RECEIVED A LEVEL 2 ALERT FOR TIRE FAILURE. CONTINUED, FOUND TIRE BELOW 50 PSI. REPLACED NR2 MLG WHEEL ASSY IAW MM 32-41-01.May 19, 2016 · N272UP · Doug MD11F · TireSDR FDEA201605191665Doubler · chafedRIGHT WING FIXED LE SKIN, INSPECTION CARRIED OUT IAW WRI 57307476 & FOUND EXISTING REPAIR DOUBLER WITH CHAFED MARK AT STATION XOS 906. CHAFED DAMAGE HAS BEEN REMOVED & NEW REPAIR DOUBLER REPAIR ACCOMPLISHED IAW EA 1-5710-79779C P 2. REPAIR CLASSIFIED AS MAJOMay 19, 2016 · N595FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2016060704348Stringer · crackedINSPECTION TYPE:3C, CENTER WING TANK LOWER STRINGER NR 47 IS CRACKED AT BS X=17, X=-17, X=-46. REPAIRED CRACKED CENTER WING TANK LOWER STR 47 AT SIAD LOCATIONS IAW SRM 57-10-03, REPAIR 1, FIG. 201.May 18, 2016 · N257UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201605181732Seat Track · damagedSEAT TRACK DAMAGED AT POSITION 10L & 9L MCD & LOCK POSITION S1539. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-00-52.May 18, 2016 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201605181662Light · inoperativeL1 LIFE RAFT & SLIDE CIRCUIT CONTINUITY TEST LIGHT DOES NOT ILLUMINATE. RE-LAMPED L1 SLIDE PTT & LOW PRESS INDICATOR.May 18, 2016 · N594FE · Doug MD11F · Emergency EquipmentSDR IPXA2016051803559Panel · out of positionUPON OPENING L1 DOOR, HOOKED ON EXIT SIGN CAUSING DAMAGE. R & R CEILING PANEL IAW MM 52-11-02. OPS CK GOOD.May 18, 2016 · N291UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016051903603Sensor · inoperativeLEVEL 1, ENGINE 2 ANTI-ICE OFF MESSAGE DISPLAYED. R & R NR 2 ENGINE COWL ANTI-ICE MANIF FAILURE SENSING ELEMENT. TESTS OK IAW MM 3022-11/401, 30-22-11-720-801. SENSOR ASSY ON/OFF PN 35512-61 ON SN TAG 1203410B, OFF ELEMENT, X 2, ON/OFF, PN 35519-4-310 ON SN May 18, 2016 · N278UP · Doug MD11F · Air Intake Anti/De-Ice SystemSDR IPXA2016051903601Sign · brokenL1 EXIT SIGN BROKEN. REPLACED THE EXIT SIGN IAW 33-27-05.May 18, 2016 · N291UP · Doug MD11F · Emergency LightingSDR IPXA2016051903599Warning Light · false activationEMERGENCY LIGHT BATTERY ONE LOW, AMM 33-51-01-700-802. OPS TEST BATTERY AND FIM 33-51-00-101 FIG 104, OPS CK GOOD. SYSTEM OK.May 18, 2016 · N276UP · Doug MD11F · Emergency LightingSDR KO0R201605180054Angle · corrodedCORROSION ON ANGLE AT BS 2033 BETWEEN STRINGER 3L & 3R IN THE UPPER AFT FUSELAGE COMPARTMENT.May 18, 2016 · N542KD · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201605181660Pin · shearedAFTER EXITING RNWY, ATTEMPTED NORMAL 90 DEGREE LT TURN, CREW HEARD THUMP & LOST LT TURN AUTHORITY. INITIAL EVALUATION REVEALED BOLT & PIN ATTACHING LT STEERING ACTUATOR TO STEERING COLLAR TO BE MISSING. TOP HALF OF SHEARED BOLT & PIN WAS RECOVERED ON THE TAXMay 18, 2016 · N594FE · Doug MD11F · Landing Gear Steering SystemSDR FDEA201605181659Skin · crackedRIGHT WING LE SLAT EXTERIOR SKIN TE FOUND CRACK AT STATION XOS 816. TRIMMED OUT & DOUBLER REPAIR CARRIED OUT IAW EA 1-5750-T0325443 PART 1 P1. REPAIR CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100. REFER TO WRI 57507879 FOR WORK DETAILS. REPAIR IS A CATEGORY BMay 18, 2016 · N595FE · Doug MD11F · Leading Edge DevicesSDR FDEA201605181658Doubler · corrodedLEFT WING FIXED LE LOWER SKIN ATTACHMENT, DOUBLER FOUND CRACK AT STATION XOS 993. ACCOMPLISHED REPAIR IAW SRM 57-40-03-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 18, 2016 · N595FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201605181657Skin · crackedRIGHT WING FIXED LE SKIN CUT OUT, AT STATION 659.7174, TRACK 10, CORNER 13, FOUND CRACK APPROX 3/16 INCH IN LENGTH. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 201 REPAIR 7. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.May 18, 2016 · N615FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201605181656Longeron · corrodedCENTER CARGO COMPARTMENT, STATION 1701 - 1721 RT SIDE, LONGERON 49R, FOUND CORRODED. CARRIED OUT REPAIR IAW EA 1-5310-T0325527 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 53103729 FOR WORK DETAILS.May 18, 2016 · N615FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2016061104499Stringer · crackedINSPECTION TYPE:3C, RT WING STR 38 CRACKED BEYOND PREVIOUS REPAIR STOP-DRILL XORS 855-XORS 885. REPAIRED STR 38 RT IAW EA 011-5710-01-A6287 REV IR AND EO MD115710-61024-A.May 17, 2016 · N257UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2016061104493Stringer · crackedINSPECTION TYPE:3C, RT WING STRINGER 5 CRACKED XORS 1070-1094. REPAIRED STRINGER 5 RT IAW EA 011-5710-01-A6276, REV.IR AND EO MD11-5710-61017-A.May 17, 2016 · N257UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2016061104491Floorbeam · crackedINSPECTION TYPE:3C, FLOORBEAM CORRODED AND CRACKED IN FWD CARGO COMPARTMENT BS 6-70 AT L43R. REPAIRED FLOORBEAM IAW EA 011-5310-01-A6264, REV. IR AND EO MD11-5310-61007-A.May 17, 2016 · N257UP · Doug MD11F · Fuselage Main, Floor BeamSDR IPXA2016060904405Support Bracket · crackedINSPECTION TYPE:3C, NR 2 PYLON AFT PAN SUPPORT BRACKETS ARE CRACKED. REPAIRED NR 2 PYLON AFT PAN SUPPORT BRACKETS IAW EA 011-5420-A6280, REV I/R AND EO MD11-5420-60903-A.May 17, 2016 · N257UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2016061004440Stringer Clip · crackedINSPECTION TYPE:3C, RT WING STR 11 CLIP IS CRACKED AT BS XORS. 683. REMOVED, FABRICATED AND REPLACED STR. 11 CLIP AT BS XORS. 683 IAW DWG ARB0979 AND SRM 51-33-01.May 17, 2016 · N257UP · Doug MD11F · Wing, Longeron/Stringer
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