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 FDEA201709282774Hinge · corrodedRT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT I/B LUG SURFACE CORROSION. RH WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE LUG SURFACE CORROSION REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04 EXISTING THICKNESS 0.447", MATERIAL REMOVSDR FDEA201709282773Hinge · corrodedRT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE CORROSION. RH WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE CORROSION REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04 EXISTING HOLE 1.195", FINAL HOLE 1.200", MAXIMUM ALLOWABLE HSDR FDEA201709282772Hinge · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. RH WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08 EXISTING HOLE: 1.224", FINAL HOLE: 1.229SDR FDEA201709282771Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 1.2235", FINAL HOLE 1.229", MAXIMUM ALLOWABLE HOLE 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EO 1-SDR FDEA201709282770Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE 0.708", FINAL HOLE 0.712", MAXIMUM ALLOWABLE HOLE 0.709". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EO 1-5750-T0SDR FDEA201709282769Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 0.709", FINAL HOLE: 0.712", MAXIMUM ALLOWABLE HOLE: 0.709". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EO 1-5750SDR FDEA201709282768Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) UPPER MOUNT O/B BORE SURFACE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING THICKNESS: 760", MATERIAL REMOVED: 0.050", REMAINING THICKNESS: 0.710", MINIMUM ALLOWABLE THICKNESS: 0.720", REPAIR SDR FDEA201709282767Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) UPPER MOUNT I/B BORE SURFACE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING THICKNESS: 0.729", MATERIAL REMOVED: 0.026" REMAINING THICKNESS: 0.703". REPAIR SHIM FABRICATED AND INSTALLED AS PERSDR FDEA201709282766Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) UPPER MOUNT O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 0.948", FINAL HOLE: 0.951", MAXIMUM ALLOWABLE HOLE: 0.944". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EO 1-575SDR FDEA201709282765Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) UPPER MOUNT I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 0.9535", FINAL HOLE: 0.957", MAXIMUM ALLOWABLE HOLE: 0.944". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EO 1-57SDR FDEA201709282764Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) PIVOT BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 2.317", FINAL HOLE: 2.321", MAXIMUM ALLOWABLE HOLE: 2.3135". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EO 1-5750-T033562SDR FDEA201709282763Hinge Bracket · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE (WING SIDE) LOWER MOUNT, OTBD BORE SURFACE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PT 1, STEP 1.SDR FDEA201709282762Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE (WING SIDE) FWD MOUNT, OTBD LUG SURFACE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIRED IAW EA 1-5750-T0335603, PART 1, STEP 1.SDR FDEA201709282761Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR ATTACH OTBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1E.SDR FDEA201709282760Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR ATTACH INBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1E.SDR FDEA201709282759Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) BARREL NUT HOLE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1F.SDR FDEA201709282758Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1B, AND STEP 1.SDR FDEA201709282757Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) LOWER MOUNT INBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1B, AND STEP 1.SDR FDEA201709282756Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) UPPER MOUNT INBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1A.SDR FDEA201709272750Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) UPPER MOUNT OTBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1A.SDR FDEA201709272749Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) PIVOT BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1C.SDR FDEA201709272748Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE: DIA: 1.222", FINAL HOLE: DIA: 1.228", MAXIMUM ALLOWABLE HOLE: DIA: 1.220". OVERSIZED BUSHING FABRICATED AND INSTASDR FDEA201709272747Hinge Arm · corrodedLT WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE: DIA: 1.224", FINAL HOLE: DIA: 1.228", MAXIMUM ALLOWABLE HOLE: DIA: 1.220". OVERSIZED BUSHING FABRICATED AND INSTASDR FDEA201709272746Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD BORE CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335583, PART 1, STEP 1B, AND STEP 1.SDR FDEA201709272745Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) LOWER MOUNT INBD BORE CORRODED. THE BORE CORROSION WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. FABRICATED AND INSTALLED A REPAIR IAW 1-5750-T0335583, PART 1, STEP 1B, AND STEP 1.SDR FDEA201709272744Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORRODED. CORROSION WAS WORKED IAW CMM 57-44-08. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335583, PART 1, STEP 1.SDR FDEA201709272743Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) PIVOT BORE CORRODED. CORROSION FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335583, PART 1, STEP 1A.SDR FDEA201709272742Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 1.253", FINAL HOLE: 1.259", MAXIMUM ALLOWABLE HOLE; 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1SDR FDEA201709272741Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 1.252", FINAL HOLE: 1.259", MAXIMUM ALLOWABLE HOLE: 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1SDR FDEA201709272740Hinge Arm · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) BARREL NUT HOLE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.692", FINAL HOLE: 0.702", MAXIMUM ALLOWABLE HOLE: 0.667". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T03SDR FDEA201709272739Hinge · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) BARREL NUT LOWER BOLT HOLE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.3255", FINAL HOLE: 0.408", MAXIMUM ALLOWABLE HOLE: 0.391". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER ESDR FDEA201709272738Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.390", FINAL HOLE: 0.408", MAXIMUM ALLOWABLE HOLE: 0.391". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EASDR FDEA201709272737Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.586", FINAL HOLE: 0.597", MAXIMUM ALLOWABLE HOLE: 0.584". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750SDR FDEA201709272736Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.586", FINAL HOLE: 0.597", MAXIMUM ALLOWABLE HOLE: 0.584". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750SDR FDEA201709272735Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) PIVOT BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 2.3165", FINAL HOLE: 2.322", MAXIMUM ALLOWABLE HOLE: 2.3135". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T03356SDR IPXA2017092622058Bulb · wrong partL1 DOOR SLIDE PUSH TO TEST BUTTON NOT ILLUMINATING. REPLACED THE LAMP WITH THE CORRECT BULBS AND OPS CHECKED OK IAW 25-61-05-01.SDR IPXA2017092722086Bulb · wrong partR1 DOOR SLIDE PTT LIGHT INOPERATIVE. TROUBELSHOT IAW FIM 25-61-01, FIG 103. REPLACED THE LAMP IN THE PUSH BUTTON SWITCH WITH CORRECT BULBS, OPS CHECKED OK.SDR FDEA201709262729Skin · chafedLT WING LOWER WING ACCESS PANEL DOOR CUT OUT AT XORS 683 HAS 1 EA DAMAGE ATTACH HOLE AT 6 OCLOCK POSITION AFT REPAIR DOUBLER REF SRM 57-10-00 FIG 69A SHEET 2SDR IPXA2017092722100Relay · inoperativeL1 DOOR DRIVE MOTOR CONTINUES TO RUN AFTER DOOR IS CLOSED CABLES ARE SECURE. R & R THE L1 DOOR RELAY R2177 IAW AMM 20-30-00, AND WDM 52-11-01. OPS CHECKED GOOD IAW AMM 52-10-00-201.SDR FDEA201709252710Hinge Bracket · corrodedRIGHT WING INBD FLAP OTBD FWD HINGE (WING SIDE) PIVOT BORE CORRODED. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T033099 A, PART 1, STEP 1F. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709252709Hinge Bracket · corrodedRIGHT WING INBD FLAP OTBD AFT HINGE (FLAP SIDE) PIVOT OTBD BORE CORRODED. WORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-137533C-PT5, STEP 2B, AND 2A. . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2SDR FDEA201709252708Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE (FLAP SIDE) PIVOT INBD BORE CORRODED. WORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-137533C-PT5, STEP 2B, AND 2A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6SDR FDEA201709252707Hinge Bracket · corrodedLEFT WING INBD FLAP OTBD AFT HINGE (FLAP SIDE) PIVOT OTBD BORE CORRODED. WORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-137533E-PT6, STEP 2B, AND 2A. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GSDR FDEA201709252706Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE (FLAP SIDE) PIVOT INBD BORE CORRODED. WORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-137533E-PT6, STEP 2B, AND 2A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-1SDR FDEA201709252705Hinge Bracket · corrodedLEFT WING INBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR ATTACH OTBD BORE CORRDED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0330993 A, PART 1, STEP 1F. REPAIR CLASSIFEID AS MAJOR IAW SDR FDEA201709252704Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD HINGE (WING SIDE) ACTUATOR ATTACH INBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0330993, PART 1, STEP 1F. REPAIR CLASSIFEID AS MAJOR IAW GMSDR FDEA201709252703Rib · crackedLEFT WING, ON REPLACEMENT OF THE NR 2 SLAT, THE OTBD EDGE ANGLE RIB WAS FOUND CRACKED. REMOVED AND REPLACED THE RIB IAW SRM 51-31-01-OG.SDR IPXA2017092522037Power Supply · no testDURING A PDC EMERGENCY LIGHTS TEST, THE LIGHTS FAILED. R & R THE EMERGENCY LIGHT BATTERY POWER SUPPLY IAW AMM 33-51-01. OPS TEST PASSED.SDR FDEA201709242700Battery · inoperativeDURING A PREFLIGHT INSPECTION, FOUND THE L1 DOOR SLIDE REMOTE PRESS TO TEST LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERIES IAW AMM 25-61-04-4. OPS CHECKED OK. RETURN TO SERVICE.SDR IPXA2017092522021Warning Message · false activationWITH ALL ANTI-ICE SYSTEMS ON IN ICING CONDITIONS, RECEIVED A LEVEL 1 BLEED AIR 2 OFF AND LEVEL 1 PACK 2 OFF. SHORTLY, A LEVEL 2 BLEED AIR 1 FAULT. OUTFLOW VALVE FULLY CLOSED. LEVEL 2 EXTINGUSHED WITH THROTTLE NR 1 ADVANCED TO MCT. COMPLIED WITH A FUNCTIONA
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