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 IPXA201810245287Battery Pack · inoperativeAN EMERGENCY LIGHT TEST FAILED, EMERGENCY LIGHT BATTERY 1 LOW. R & R THE BATTERY PACK IAW MM 33-51-01. OPS CHECKED GOOD.SDR FDEA201810222970Warning System · false activationGOT MOMENTARY TRITONE AND CARGO FIRE LWR ALERT. WENT OUT WE COULD READ IT ALL. NO INDICATIONS ON OVERHEAD OR AIR SYNOPTIC. CHECKED CARGO AREA AND PERFORMED LOWER CARGO HEAT DETECTORS OPERATIONAL TEST AND THEN NO FAULTS FOUND IAW AMM 26-14-02-5.SDR FDEA201810222968Web · damagedLT INBD FLAP SKIN PANEL DAMAGED. REPLACED -3 WEB ASSY WITH A -23 WEB ASSY IAW PRODUCTION DWG ARC2305. COMPLIED WITH EA1-5730-T0343042.SDR IPXA2018102235250Pan · crackedBULK CARGO DOOR LOWER AFT CORNER WAS DEFLECTED AND THE PAN HAD A 1 INCH CRACK THAT ENDS IN A RIVET HOLE. REPAIRED IAW EO MD11-5230-70321-A.SDR IPXA2018102935444Retainer · crackedCENTER CARGO FLOOR SUPPORT RETAINER WAS CRACKED AT BS 1541. REMOVED, FABRICATED, AND REPLACED THE FLOOR SUPPORT RETAINER IAW DWG AEA0341, AND SRM 51-35-01. MINOR.SDR FDEA201810212965Pan · corrodedCABIN UPPER CARGO DOOR CORROSION ON UPPER DOOR PAN AT STATION 664.75-STATION 685. CABIN-UPPER CARGO DOOR CORROSION ON UPPER DOOR PAN AT STATION 664.750 - STATION 685 REMOVED AS PER SRM 51-21-01-OG AND FOUND EXCEEDED LIMIT AS PER SRM 52-00-00-2R FIGURE 202. UPPSDR FDEA201810202962Seat Track · corrodedCABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK CORROSION AT LEFT HAND STATION 6-80, X = 8.5. SEAT TRACK SECTIONAL REPAIR CARRIED OUT FROM STATION 6-0 TO STATION 6-100, X = 8.5 PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. RSDR FDEA201810202961Seat Track · corrodedCABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK CORROSION AT RIGHT HAND STATION 1300, -8.5. SEAT TRACK SECTIONAL REPAIR CARRIED OUT FROM STATION 1229 TO STATION 1331, X=-8.5 PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFESDR IPXA2018111205854Longeron · corrodedINSPECTION TYPE: 3C, EXFOLIATED CORROSION ON EXTERNAL LONGERON 28L UNDER WING TO BODY FAIRING, BELOW THE L3 DOOR AT BS 1300. REPAIRED THE LONGERON IAW EA 011-5310-01-A7528, REV IR, AND EO MD11-5310-70581-A. MAJOR.SDR FDEA201810192952Support Fitting · corrodedLEFT HAND OUTBOARD FLAP VANE HORN FITTING "D" MOUNT HOLE CORRODED. CORROSION AT LEFT HAND OUTBOARD FLAP VANE HORN FITTING "D" MOUNT HOLE REWORKD BY MACHINING AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED SLOT BUSHING FABRICATED BSDR FDEA201810192951Support Fitting · corrodedLEFT HAND OUTBOARD FLAP VANE HORN FITTING "F" MOUNT HOLE CORRODED. CORROSION AT LEFT HAND OUTBOARD FLAP VANE HORN FITTING "F" MOUNT HOLE REWORKD BY MACHINING AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED SLOT BUSHING FABRICATED BSDR FDEA201810192950Support Fitting · corrodedLEFT HAND OUTBOARD FLAP VANE HORN FITTING "C" MOUNT HOLE CORRODED. CORROSION AT LEFT HAND OUTBOARD FLAP VANE HORN FITTING "C" MOUNT HOLE REWORKD BY MACHINING AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED SLOT BUSHING FABRICATED BSDR FDEA201810192949Support Fitting · corrodedLEFT HAND OUTBOARD FLAP VANE HORN FITTING "E" MOUNT HOLE CORRODED. CORROSION AT LEFT HAND OUTBOARD FLAP VANE HORN FITTING "E" MOUNT HOLE REWORKD BY MACHINING AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED SLOT BUSHING FABRICATED BSDR FDEA201810192948Support Fitting · corrodedLEFT HAND OUTBOARD FLAP VANE HORN FITTING "B" MOUNT HOLE CORRODED. CORROSION AT LEFT HAND OUTBOARD FLAP VANE HORN FITTING "B" MOUNT HOLE REWORKD BY MACHINING AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED SLOT BUSHING FABRICATED BSDR FDEA201810192947Hinge Bracket · corrodedLEFT HAND OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) BARREL NUTS HOLE SURFACE CORROSION. CORROSION AT LEFT HAND OUTBOARD FLAP INBOARD FORWARD HINGE(WING SIDE) BARREL NUT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER DRAWING ARC0502 REV BF AND COMPONSDR IPXA2018111205853Floorbeam · corrodedINSPECTION TYPE 3C, AFT CARGO COMPARTMENT FLOORBOARD FLOORBEAM WAS CORRODED AROUND THE NUT PLATES, BS 1841, LBL 7 - LBL 22. REPAIRED THE FLOORBEAM IAW EA 011-5310-A7527, REV IR, AND EO MD11-5310-70498-A. MAJOR.SDR IPXA2018111215871Stringer · crackedINSPECTION TYPE:3C, STRINGER 46 WAS CRACKED. REPAIRED STRINGER IAW EA 011-5710-01-A7529, REV I/R, AND EO MD11-5710-70582-A. MAJOR.SDR IPXA2018110985799Rib · brokenLEFT ELEVATOR L/E RIB UPPER AFT INBD FLANGE WAS BROKEN OFF INSIDE PANEL 335CT. REPAIRED THE RIB AT XE 125.8 IAW EA 011-5520-01-A7521, REV IR, AND EO MD11-5520-70541-A. MAJOR.SDR IPXA2018110735746Stringer · crackedSTRINGER 45 WAS CRACKED. REPAIRED THE STRINGER IAW SRM 57-10-03, REPAIR 1, FIG 201. MAJOR.SDR IPXA2018110735745Stringer · crackedSTRINGER 47 WAS CRACKED. REPAIRED THE SRTINGER IAW SRM 57-10-03, REPAIR 1, FIG 201. MAJOR.SDR IPXA2018110213561Skin · crackedRT WING LOWER SKIN ACCESS PANEL 636AB LANDING HAD CRACKS AT 2 FASTENER HOLES BETWEEN XORS. 683.4 - 713.650. REPAIRED RT WING LOWER SKIN LANDING IAW SRM 57-20-02, REPAIR 5, FIG 201.SDR IPXA2018103105513Skin · crackedLEFT LOWER WING SKIN ACCESS PANEL 536AB LANDING HAD TWO CRACKED FASTENER HOLES. REPAIRED THE ACCESS PANEL LANDING IAW SRM 57-20-02, REPAIR 5, FIG 201. MINOR.SDR IPXA2018103105510Mount · damagedL1 DOOR FWD SLIDE MOUNT FITTING WAS WORN AND CHAFED. REMOVED, FABRICATED, AND REPLACED THE MOUNT FITTING IAW DWG ABA8513, AND SRM 51-33-01. MINOR.SDR IPXA2018103105509Mount · damagedL1 DOOR AFT SLIDE MOUNT FITTING WAS WORN AND CHAFED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG ABA8513, AND SRM 51-33-01. MINOR.SDR IPXA2018101835118Bottle · low pressureFOUND RT PASSENGER DOOR PNEUMATIC BOTTLE WITH LOW PRESSURE. PERFORMED SERVICING OF R1 DOOR PNEUMATIC BOTTLE IAW AMM 12-25-04 PB301 REV 91 01.SDR FDEA201810182938Idler Link · corrodedLEFT WING INBOARD FLAP INBOARD IDLER LINK HOLE BORE CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP INBOARD IDLER LINK HOLE BORE REWORKED AS PER COMPONENT MAINTENANCE MANUAL 57-52-03 AND FOUND EXCEED LIMIT AS PER DRAWING ARC2761 REV K. REPLACEMENT BUSHING SDR FDEA201810182937Hinge Fitting · corrodedRIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUTS HOLE SURFACE CORROSION CORROSION AT RIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUTS HOLE SURFACE REWORKED AS PER COMPONENT MAINTENACE MANUAL 57-44-09. REPAIR SHIM SDR IPXA2018102935468Support Bracket · crackedRIGHT OTBD FLAP, INBD FWD HINGE FAIRING CENTER PANEL SUPPORT BRACKET WAS CRACKED. REMOVED, FABRICATED, AND REPLACED THE SUPPORT BRACKET IAW DWG ARC0504, AND SRM 51-33-01. MINOR.SDR IPXA2018110535630Longeron · crackedLONGERON 27R WAS CRACKED UNDER THE R3 DOOR. REMOVED, FABRICATED, AND REPLACED THE LONGERON IAW DWG AEA7127, SRM 51-35-01, AND SRM 51-33-01.SDR IPXA2018110213563Tee Fitting · crackedMAIN CABIN, BS 1321, LONGERON 15L TEE FITTING WAS CRACKED. REMOVED, FABRICATED, AND REPLACED THE LONGERON TEE FITTING IAW DWG AEA7568, AND SRM 51-33-01.SDR IPXA2018110213562Tee Fitting · crackedMAIN CABIN, BS 1321, LONGERON 15R, TEE FITTING CRACKED. REMOVED, FABRICATED, AND REPLACED THE LONGERON TEE FITTING IAW DWG AEA7568, AND SRM 51-33-01.SDR IPXA2018110213551Fuel Tank · corrodedCENTER WING TANK UPPER CENTER SKIN HAD CORROSION AT XCW=-17, AND BETWEEN STRINGERS 14 & 15. REPAIRED THE TANK IAW 011-5730-01-A7523, REV I/R AND EO MD11-5730-70469-A.SDR IPXA2018110213554Intercostal · crackedTAILCONE LT UPPER BOX FITTING INTERCOSTAL WAS CRACKED. REMOVED, FABRICATED, AND REPLACED THE INTERCOSTAL IAW DWG AKC7520, AND SRM 51-31-01.SDR IPXA2018102935463Web · crackedRIGHT WW FUEL TANK UPPER AFT WEB WAS CRACKED AT AT BS 1372, RBL 80. REPAIRED THE WEB IAW EO MD11-5710-70319-A. MAJOR.SDR IPXA2018102935476Skin · crackedRIGHT LOWER WING SKIN ACCESS PANEL 636AB LANDING HAD 9 CRACKED HOLES, BETWEEN XORS 683.4, AND 713.6. REPAIRED THE ACCESS PANEL LANDING IAW EA 011-5730-01-A7516, REV I/R, AND EO MD11-5730-70430-A. MAJOR.SDR IPXA2018102935475Skin · crackedLEFT LOWER WING SKIN ACCESS PANEL 536AB LANDING HAD 15 CRACKED HOLES BETWEEN XORS 683.4 AND XORS 713.6. REPAIRED THE ACCESS PANEL LANDING IAW EA 011-5730-01-A7517, REV I/R, AND EO MD11-5730-70429-A. MAJOR.SDR IPXA2018102635378Door Frame · crackedL3 DOOR FRAME LOWER WEB WAS CRACKED AT BS 1251, Z -15. REPAIRED THE DOOR FRAME IAW SRM 53-40-15, REPAIR 3, FIG 201. MAJOR.SDR IPXA2018102635377Beam · chafedTAIL CONE HORIZONTAL BEAM HAD DEEP CHAFE DAMAGE ON THE RT SIDE. REPAIRED THE HORIZONTAL BEAM IAW DWG AKC7520, AND SRM 51-35-01. MINOR.SDR IPXA2018101765072Solenoid · inoperativeL1 DOOR LOCK PIN RELEASE SOLENOID INOPERATIVE. R & R THE L1 DOOR LOCK PIN RELEASE SOLENOID IAW MM 52-10-16, OPS CHECKED GOOD.SDR IPXA2018101735091Altimeter · malfunctionedPASSING FL 180 DURING CLIMB, THE FIRST OFFICER LOST ALL CONTROL OF HIS BARO ALTIMETRY, ALT DISPLAYED BOTH EAD'S, ALT WINDOW ON AFS PANEL WENT BLANK, NO CONTROL WITH ALTITUDE KNOB. AIRSPEED HDG ALSO BLANKED WITH NO CONTROL, AUTO THROTTLES LOCKED. AIR TURN BSDR FDEA201810162920Bracket · corrodedRIGHT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE CORROSION. CORROSION AT RIGHT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE ( HOLE 'A' AND 'B' ) REWORKED AND FOUND EXCEED LIMIT AS PER COMPONENT MAINTESDR FDEA201810162919Bracket · corrodedRIGHT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE CORROSION. CORROSION AT RIGHT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE ( HOLE 'G' AND 'F' ) REWORKED AND FOUND EXCEED LIMIT AS PER COMPONENT MAINTENASDR FDEA201810162918Bracket · corrodedLEFT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE CORROSION. CORROSION AT LEFT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER COMPONENT MAINTENANCE MSDR FDEA201810162917Bracket · corrodedLEFT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE CORROSION. CORROSION AT LEFT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER COMPONENT MAINTENCE MANUALSDR FDEA201810162916Bracket · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE SURFACE CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE SPOTFACE REWORKED AS PER COMPONENT MAINTENANCE MANUAL 57-44-07 AND FOUND WITHINSDR FDEA201810162915Bracket · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE (HOLE 3) REWORKED AND FOUND WITHIN LIMIT AS PER COMPONENT MAINTENANCE MANUAL 57-44-SDR FDEA201810162914Bracket · corrodedRIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE (HOLE 3) REWORKED AND FOUND EXCEED LIMIT AS PER COMPONENT MAINTENCE MANUAL 5SDR FDEA201810162913Hinge Bracket · corrodedLEFT HAND OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE CORROSION. CORROSION AT LEFT HAND OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE (8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER COMPONENT MAINTESDR FDEA201810162912Hinge Bracket · corrodedLEFT HAND OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE CORROSION. CORROSION AT LEFT HAND OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE (8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER COMPONENT MAINTENCSDR FDEA201810162911Hinge Bracket · corrodedLEFT HAND OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) FORWARD MOUNT OUTBOARD HOLE BORE CORROSION. CORROSION AT LEFT HAND OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) FORWARD MOUNT OUTBOARD HOLE BORE (6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER COMPON
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