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 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" ANSDR 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 SDR 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". NEWSDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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". NESDR 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". NESDR 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 SSDR 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 SDR 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 FASDR 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 DISDR 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 DISDR 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 0.4SDR 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 THISDR 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 DIAMSDR 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 DIAMETESDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 MAJOSDR 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.SDR 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.SDR FDEA201605181662Light · inoperativeL1 LIFE RAFT & SLIDE CIRCUIT CONTINUITY TEST LIGHT DOES NOT ILLUMINATE. RE-LAMPED L1 SLIDE PTT & LOW PRESS INDICATOR.SDR 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.SDR 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 SDR IPXA2016051903601Sign · brokenL1 EXIT SIGN BROKEN. REPLACED THE EXIT SIGN IAW 33-27-05.SDR 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.SDR KO0R201605180054Angle · corrodedCORROSION ON ANGLE AT BS 2033 BETWEEN STRINGER 3L & 3R IN THE UPPER AFT FUSELAGE COMPARTMENT.SDR 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 TAXSDR 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 BSDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.
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