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 IPXA2018091734054Stiffener · crackedNR 3 ENGINE OTBD THRUST REVERSER STIFFENER FITTING CRACKED, AT THE MID SPAN OF THE THRUST REVERSER. REMOVED AND REPLACED THE STIFFENER IAW SRM 54-01-41. MINOR.SDR IPXA2018091233826Battery · dischargedL1 SLIDE PRESSURE LIGHTS INOP. REPLACED BATTERIES. OPS CK GOOD.SDR FDEA201809092426Battery · dischargedR1 EVACUATION SLIDE REMOTE PRESSURE PRESS-TO TEST INDICATION SYSTEM IS INOP ON PREFLIGHT CHECK. R1 EVAC SLIDE REMOTE PRESS INDICATOR INOP. TRIED TO REPLACE IND KIT (26C17528-2) BUT NO HELP. FOUND R1 EVACUATION SLIDE REMOTE PRESSURE PRESS-TO TEST INDICATION SDR FDEA2018091192424Floor Support · corrodedMDCC AFT FLOOR SUPPORT FOUND CORROSION AT STA 2007 X =-25. CORROSION REMOVED PER SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT PER SRM 53-00-00-2R FIG 202. ORIGINAL THK 0.080", MATERIAL REMOVED 0.060", REMAINING THK 0.020". CORRODED FLOOR SUPPORT REMOVED PER AMM 20SDR IPXA2018091033806Skin Panel · damagedLEFT SIDE FUSELAGE SKIN DAMAGE AT STA 655 BETWEEN L41 AND L42. REPAIRED IAW SRM 53-00-01-2R-1, FIG 201, REPAIR 1.SDR FDEA2018091172374Skin · crackedLEFT HAND WING NR 8 SLAT OUTBOARD EDGE INTERIOR LOWER SURFACE AREA FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 57-40-01-2R REPAIR 3 FIGURE 201 AT STA XOS 1180.5 AND PER EA 1-5750-T0342354 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018091172417Fitting · corrodedLT O/B FLAP VANE HORN FITTING 'F' HOLE BORE CORROSION. BORE REWORKED AND FOUND EXCEED LIMIT PER SRM 57-50-02-2R FIG 201 SHEET 1. EXISTING SLOT HOLE: LENGTH 0.852", WIDTH 0.600", FINAL SLOT HOLE: LENGTH 0.960", WIDTH 0.708". REPAIR LIMIT - LENGTH 0.940", WIDTH SDR FDEA2018091172416Fitting · corrodedLT O/B FLAP VANE HORN FITTING 'E' HOLE BORE CORROSION. BORE REWORKED AND FOUND EXCEED LIMIT PER SRM 57-50-02-2R FIG 201 SHT 1. EXISTING SLOT HOLE: LENGTH 0.857", WIDTH 0.581", FINAL SLOT HOLE: LENGTH 0.952", WIDTH 0.652". REPAIR LIMIT - LENGTH 0.940", WIDTH 0.SDR FDEA2018091172415Bracket · corrodedLT WING I/B FLAP I/B DRIVE LINK IDLER BRACKET BORE CORROSION. DRIVE LINK IDLER BRACKET BORE REWORKED PER CMM 57-52-03. EXISTING HOLE DIA 1.00", FINAL HOLE DIA 1.316". REPLACEMENT BUSHING FOR ARC3087-1 & ARC3086-1 FABRICATED PER EA 1-5750-T0342037 P1 STEP 4, 4ASDR FDEA2018091172414Hinge · corrodedLT WING O/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA: 1.148' FINAL HOLE DIA: 1.163" MAXIMUM ALLOWABLE HOLE: 1.150" OVERSIZED BUSHING FABRICATESDR FDEA2018091172413Hinge Bracket · corrodedLT WING O/B FLAP I/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-04. EXISTING HOLE DIA 1.148", FINAL HOLE DIA 1.158", MAXIMUM ALLOWABLE HOLE DIA 1.150". OVERSIZED BUSHING FABRICATSDR FDEA2018091172411Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE CORROSION. HINGE ACTUATOR I/B HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 1.2806", FINAL HOLE DIA 1.284", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSSDR FDEA2018091172410Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE CORROSION. HINGE ACTUATOR O/B HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.223", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSHSDR FDEA2018091172409Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 7) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 0.718". FINAL HOLE DIA 0.727", MAXIMUM HOLE DIA 0.709". REPAIR BUSHING FASDR FDEA2018091172408Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (HOLE 7) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 0.705", FINAL HOLE DIA 0.722", MAXIMUM ALLOWABLE HOLE DIA 0.709". REPAISDR FDEA2018091172407Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED PER CMM 57-44-08. EXISTING THK - UPPER 0.389", LOWER 0.373", MATERIAL REMOVED - UPPER & LOWER 0.005", REMAINING THK - UPPER 0.384", LOWER 0.368SDR FDEA2018091172406Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE CORROSION. HINGE ACTUATOR O/B HOLE BORE (HOLE 8) REWORKED & FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 1.222", FINAL HOLE DIA 1.252", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSSDR FDEA2018091172405Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE CORROSION. HINGE ACTUATOR I/B HOLE BORE (HOLE 8) REWORKED & FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 1.222", FINAL HOLE DIA 1.252", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSSDR FDEA2018091172404Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE SURFACE CORROSION. HINGE LOWER MOUNT O/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING THK 0.400", MATERIAL REMOVED 0.004", REMAINING THK 0.396", MINIMUM ALLOWABLE THK 0.SDR FDEA2018091172402Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE SURFACE CORROSION. HINGE LOWER MOUNT I/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING THK 0.436", MATERIAL REMOVED - FWD FACE 0.004", AFT FACE 0.013", REMAINING THK 0.41SDR FDEA2018091172401Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 7 HOLE) REWORKED & FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 0.709", FINAL HOLE DIA 0.729", MAXIMUM ALLOWABLE HOLE DIA 0.709". OVERSDR FDEA2018091172400Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM57-44-08. EXISTING HOLE DIA 0.708", FINAL HOLE DIA 0.728", MAXIMUM ALLOWABLE HOLE DIA 0.709". OVESDR FDEA2018091172399Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-08, EXISTING THK - UPPER 0.378", LOWER 0.348", MATERIAL REMOVED, UPPER & LOWER 0.005", REMAINING THK - UPPER 0.373", LOWER 0.3SDR FDEA2018091172397Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE PIVOT HOLE BORE CORROSION. HINGE PIVOT HOLE BORE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 2.312", FINAL HOLE DIA 2.317", MAXIMUM ALLOWABLE DIA 2.3135". OVERSIZED BUSHING FABRICATED & INSTALLSDR FDEA2018091172396Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE CORROSION. HINGE ACTUATOR O/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 1.249", FINAL HOLE DIA 1.253", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIRSDR FDEA2018091172395Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE CORROSION. HINGE ACTUATOR I/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 1.249", FINAL HOLE DIA 1.253", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIRSDR FDEA2018091172394Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 0.584", FINAL HOLE DIA 0.596", MAXIMUM ALLOWABLE HOLE DIA 0.584". SHSDR FDEA2018091172393Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 0.584", FINAL HOLE DIA 0.596", MAXIMUM ALLOWABLE HOLE DIA 0.584", SDR FDEA2018091172392Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE UPPER MOUNT O/B HOLE BORE CORROSION. HINGE UPPER MOUNT O/B HOLE BORE (NR 2 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM57-44-09. EXISTING HOLE DIA 0.880", FINAL HOLE DIA 0.948", MAXIMUM ALLOWABLE DIA 0.944". REPAIR BSDR FDEA2018091172391Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE CORROSION. HINGE ACTUATOR O/B HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 1.280", FINAL HOLE DIA 1.1287", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSSDR FDEA2018091172390Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE CORROSION. HINGE ACTUATOR I/B HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09, EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.248", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSHSDR FDEA2018091172389Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED PER CMM 57-44-09. EXISTING THK - UPPER 0.381", LOWER 0.386", MATERIAL REMOVED - UPPER & LOWER 0.010", REMAINING THK - UPPER 0.371", LOWER 0.376SDR FDEA2018091172385Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE UPPER MOUNT O/B HOLE SURFACE CORROSION. HINGE UPPER MOUNT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT PER CMM57-44-09. EXISTING THK 0.715", MATERIAL REMOVED 0.004", REMAINING THK 0.711", MINIMUM ALLOWABLE THK 0.72". SDR FDEA2018091172384Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE UPPER MOUNT HOLE SURFACE CORROSION. HINGE UPPER MOUNT O/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT PER CMM57-44-09. EXISTING THK 0.715", MATERIAL REMOVED 0.004", REMAINING THK 0.711", MINIMUM ALLOWABLE THK 0.72". SDR FDEA2018091172383Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE PIVOT HOLE BORE CORROSION. HINGE PIVOT HOLE BORE (HOLE 4) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 2.300", FINAL HOLE DIA 2.3185", MAXIMUM ALLOWABLE HOLE DIA 2.3135". REPAIR BUSHING FABRICATSDR FDEA2018091172378Hinge · corrodedRT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT O/B HOLE BORE CORROSION. HINGE PIVOT O/B HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.188" - 1.283, FINAL HOLE DIA: 1.3785", MAXIMUM ALLOWABLE DIA: 1.220. REPAISDR FDEA2018091172377Hinge · corrodedRT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.188"-1.290, FINAL HOLE DIA: 1.328", MAXIMUM ALLOWABLE DIA: 1.220. REPAIR BSDR FDEA2018091172376Hinge · corrodedLT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT O/B HOLE BORE CORROSION. HINGE PIVOT O/B HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.188"-1.256, FINAL HOLE DIA: 1.282", MAXIMUM ALLOWABLE DIA: 1.220. REPAIR BSDR FDEA2018091172375Hinge · corrodedLT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA 1.188"-1.220, FINAL HOLE DIA: 1.250", MAXIMUM ALLOWABLE DIA 1.220. REPAIR BUSSDR FDEA201809062370Skin · crackedNR 1 AIR CONDITIONING COMPARTMENT DOOR CUT OUT STA 587, L-32L AFT UPPER CORNER AREA FOUND CRACK. CRACK REPAIRED AS PER SRM 53-20-15-2R FIG 201 REPAIR 3, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR IPXA2018090733647Bottle · low pressureMAIN ENTRY DOOR R1 EMERGENCY PNEUMATIC BOTTLE BELOW GREEN BAND. SVC R1 DOOR BOTTLE TO GREEN BAND AND LEAK CHECK FOUND SATIS PER AMM 12-25-04.SDR FDEA201809062365Controller · failedLEVEL 3 CABIN ALTITUDE WARNING DESCENDING THROUGH 35,000 FEET. CABIN ALTITUDE CLIMBED AS HIGH AS 13,500 FEET. COMPLIED WITH QRH AND PUT CABIN PRESSURE CONTROLLER IN MANUAL. CABIN PRESSURE WAS CONTROLLABLE IN MANUAL. REMOVED AND REPLACED CPC NR 1 IN REF TO AMM SDR FDEA201809052352Seat Track · corrodedMAIN DECK CARGO COMPT FLOOR PANEL OPEN UP FOR SUPRORT REPAIR FOUND SEAT TRACK FLANGE CORROSION AT STA 1681, X= 8.5. CORROSION REMOVED 0.066", REMAIN 0.014", MATERIAL THK 0.080" AND FOUND EXCEEDED LIMIT PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1 AND EXCEEDESDR FDEA2018090652356Tire · separatedPOSTFLIGHT FOUND NR 9 TIRE WITH THROWN TREAD AND TREAD SEPARATION. PER AMM 32-40-00-6 INSPECTION CHECK OF TIRE THAT HAS THROWN TREADS, R&R TIRE. INSPECTED CENTER GEAR TIRE AND WHEEEL PER AMM 32-41-01, NO OTHER DEFECTS FOUND. REMOVED AND REPLACED NR 9 CENTER TISDR FDEA2018090542343Angle · chafedMAIN DECK CARGO EXISTING REPAIR ANGLE FRAME, LONGERON 20L AT STA 535 LEFT HAND FRAME FOUND CHAFFING MARK. EXISTING REPAIR ANGLE FRAME REPAIRED AS PER SRM 53-20-07-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018090542342Seat Track · crackedMAIN DECK CARGO SEAT TRACK AT STA 635, X = 8.5 FOUND CRACK. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM EXISTING SPLICE STA 625 TO STA 665, X= 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018090542341Door Frame · crackedMAIN DECK CARGO LEFT HAND NR 3 DOOR AFT DOOR JAMB WEB AT STA 1315.420 FOUND CRACK. DOOR JAMB WEB REPAIRED AS PER SRM 53-40-15-2R FIGURE 201 REPAIR 3 FROM STA 1305.25 TO STA 1315.420. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10.SDR IPXA2018090533561Battery · dischargedEMERGENCY LIGHT BAT 1 LOW ALERT. R&R EMERGENCY LIGHT BATTERY RE MM 33 51 01 ESR 33 51 01 01.SDR SRXR201809040040Frame · corrodedFWD AVIONICS COMP FRAME AT STA 455 LBL 35 HAS CORROSION. ACCOMPLISHED REPAIR AT FWD AVIONICS COMPARTMENT FRAME AT STA 455 LBL 35 PER SRM 53-00-07 REPAIR 2 FIG 201 REF NRC A043591.SDR SRXR201809040039Fillet · crackedLT PERFORMANCE FILLET IS CRACKED AT OTBD UPPER ATTACH FITTING. ACCOMPLISHED REPAIR ON LT OTBD UPPER ATTACH FITTING SKIN PER SRM 57-40--71 REPAIR 1 REV 64 REF NRC3 A044628.
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