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 FDEA201607042253Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK FLANGE LOWER SIDE FOUND CORROSION AT STA 1821-1854, X=-8, INBD. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201607042252Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK FLANGE LOWER SIDE FOUND CORROSION AT STA 1820, X=-8, OTBD. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIG 201 REPAIR 1. REFER TO SNRM N00987 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201607042251Skin · dentedLEFT WING NR 4 SLAT UPPER SURFACE FOUND DENTED AT STA XOS 554.894 TO STA 560.200. DENT EXCEEDED LIMIT OF ALLOWABLE SRM 57-40-02-2R FIG 201 REPAIR 6. DAMAGED AREA TRIM OUT AND REPAIR DOUBLER INSTALLED PER EA 1-5750-T0326476. REPAIR CLASSIFIED AS MAJOR PER GMSDR FDEA201607042269Seat Track · crackedMAIN DECK RT FLOOR SEAT TRACK AT STA 635, X=-47.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625-STA 645X= -47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042268Seat Track · crackedMAIN DECK LT FLOOR SEAT TRACK AT STA 755, X= 8.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 745-STA 785 X= 8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042267Seat Track · crackedMAIN DECK LT FLOOR SEAT TRACK AT STA 755, X=47.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR NR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042266Seat Track · corrodedMAIN DECK RT FLOOR SEAT TRACK AT STA 778, X=-74.5 FOUND CORROSION AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 765-STA 818 X= -74.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. COMPLIED WITH EA 1-5320-T0326733 P1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-SDR FDEA201607042265Seat Track · damagedMAIN DECK LT FLOOR SEAT TRACK AT STA 770, X= 74.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 765-STA 783 X=74.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042264Seat Track · crackedMAIN DECK LT FLOOR SEAT TRACK AT STA 635, X= 47.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625 TO STA 665X=47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042263Seat Track · crackedMAIN DECK LT FLOOR SEAT TRACK AT STA 635, X= 8.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625 TO STA 645 X=8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042262Seat Track · crackedMAIN DECK RT FLOOR SEAT TRACK AT STA 635, X=-8.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625-STA 645 X= -8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042261Seat Track · damagedMAIN DECK RT FLOOR SEAT TRACK AT STA 1425, X=-47.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1390 TO STA 1431 X = -47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042259Seat Track · damagedMAIN DECK RT FLOOR SEAT TRACK AT STA 1285, X=-8.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1264 TO STA 1311 X= -8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100.SDR FDEA201607042258Seat Track · corrodedMAIN DECK LT FLOOR SEAT TRACK AT STA 1643, X= 8.5, FOUND CORROSION AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1570 TO STA 1651 X=8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042257Seat Track · damagedMAIN DECK LT FLOOR SEAT TRACK AT STA 5-5, X= 27.5, FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-0 TO STA 5-63 X=27.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042256Seat Track · damagedMAIN DECK RT FLOOR SEAT TRACK AT STA 5-5, X= -27.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-0 TO STA 5-63 X= -27.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042255Beam · crackedCABIN-L3 DOOR PLUG NR 7 FWD STOP FITTING BEAM FOUND CRACKED. R & R WITH NEW STOP FITTING BEAM IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042247Floor Support · corrodedMAIN DECK, AFT CABIN RT FLOOR SUPPORT AT STA 1887 - STA 2007, X=-25, FOUND CORROSION AS MARKED. R & R WITH NEW FABRICATED FLOOR SUPPORT IAW SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED IAW DWG AGA7087, REV P. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042246Web · crackedMAIN DECK L3 DOOR AFT JAMB LOWER WEB BOX AT STA 1305.25 TO 1315.42, LONGERON L26L TO L27L FOUND CRACKED AS MARKED. CARRIED OUT REPAIR IAW SRM 53-40-15-2R, FIG 201 REPAIR NR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042245Web · crackedMAIN DECK L3 DOOR FWD JAMB LOWER WEB BOX AT STA 1250.75 TO 1256.75, LONGERON L26L TO L27L, FOUND CRACKED AS MARKED. CARRIED OUT REPAIR IAW SRM 53-40-15-2R, FIG 201. REPAIR NR 3 AND EA 1-5310-T0326798A, PT 1 TITLE: FUSELAGE MAIN FRAME, CENTER FUSELAGE, OVERWISDR FDEA201607042244Web · crackedMAIN DECK R3 DOOR FWD JAMB LOWER WEB BOX AT STA 1250.75 TO 1256.75, LONGERON L26R-L27R, FOUND CRACKED AS MARKED. CARRIED OUT REPAIR IAW SRM 53-40-15-2R, FIG 201. REPAIR NR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR IPXA2016070405361Skin · damagedL-1 DOOR OUTER SKIN DAMAGED, REF EO MD11-5210-61106-B FOR REPAIR.SDR IPXA2016070405369Skin · damagedLOWER AFT RUDDER SKIN RT SIDE AT STA ZAR 302.089, 8" AFT OF FWD SPAR HAS A .3750" DIAMETER CHIP IN SKIN COMPLETELY THRU TO INTERNAL DOUBLER. R & R LOWER AFT RUDDER AND COMPLETED SATISFACTORY RANGE ON MOVEMENT CHECK IAW AMM 27-20-20-400-801 AND 27-20-00-710-80SDR FDEA201607032241Bushing · corrodedLEFT WING OTBD FLAP VANE FITTING F, BUSHING HOLE, CORRODED. BUSHING HOLE CORROSION REWORKED PER SRM 57-50-02-2R FIGURE 201 AND FOUND EXCEED LIMIT. EXISTING HOLE SIZE 0.860" X 0.5655", FINAL HOLE SIZE: 0.9565" X 0.6585", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.67SDR FDEA201607032240Web · crackedMAIN DECK R3 DOOR AFT JAMB LOWER WEB BOX AT STA 1305.25-STA 1315.42, LONGERON L26R-L27R FOUND CRACKED AS MARKED. WEB BOX REPAIRED PER SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201607032239Seat Track · crackedMAIN DECK LT FLOOR SEAT TRACK AT STA 755, X= 27.5 FOUND CRACKED AS MARKED. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201607032238Seat Track · crackedMAIN DECK LT FLOOR SEAT TRACK AT STA 755, X=47.5 FOUND CRACKED AS MARKED. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201607032237Bushing · corrodedLT WING OUTBOARD FLAP VANE FITTING 'B' BUSHING HOLE CORROSION. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.935" X 0.650", FINAL HOLE SIZE: 1.0325" X 0.740", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OSDR FDEA201607032236Bushing · corrodedLEFT WING OTBD FLAP VANE FITTING C, BUSHING HOLE CORRODED. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.856" X 0.597", FINAL HOLE SIZE: 0.997" X 0.704", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OVERSISDR FDEA201607032235Bushing · corrodedLT WING OTBD FLAP VANE FITTING D, BUSHING HOLE, CORRODED. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.876" X 0.580", FINAL HOLE SIZE: 0.953" X 0.660", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OVERSIZSDR FDEA201607032250Door · crackedLEFT FWD NOSE GEAR DOOR CRACKED THROUGH 3 RIVETS. APPROXIMATELY 6-8" FROM L/E OF DOOR. REMOVED LT FWD NOSE GEAR DOOR IAW AMM 32-23-03-4. SENT TO SHEETMETAL SHOP. REMOVED DAMAGE ON LT FWD NOSE GEAR DOOR AND REPAIRED IAW SRM 52-00-00-2R.SDR FDEA201607032243Light · brokenL1 DOOR FOLLOWER CEILING PANEL EMERGENCY EXIT LIGHT FRAME ASSY BROKEN.SDR FDEA201607032234Beam · corrodedCABIN MAIN DECK CARGO COMPARTMENT. R3 DOOR PLUG NR 7 LOWER DOOR BEAM DAMAGED.SDR FDEA201607032233Floor Support · corrodedMAIN DECK, AFT CABIN RT FLOOR SUPPORT AT STA 1887 -STA 2007, X=-57 FOUND CORROSION AS MARKED.SDR FDEA201607032232Hinge Bracket · corrodedLEFT WING OTBD FLAP, FLAP SIDE, INBD AFT HINGE PIVOT INBD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT CMM 57-52-04. EXISTING HOLE: DIA 1.154", FINAL HOLE: DIA 1.217", MAXIMUM ALLOWABLE HOLE: DIA 1.150". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA1SDR IPXA2016071205744Door Frame · corrodedINSPECTION TYPE: 3C, AFT CARGO DOOR FRAME HAS CORROSION AT BS 1959 BETWEEN X 30 TO 40 AND Z 80. REPAIRED THE DOOR FRAME IAW EA 011-5310-A6351 REV. I/R AND EO MD11-5310-61221-A. (MINOR)SDR FDEA201607012228Sensor · defectiveENGINE 2 ANTI-ICE DUCT FAIL, PASSING FL 200 TURNED ON ENGINE ANTI-ICE, RECEIVED NR 2 ENGINE DUCT FAILURE NR 2 ANTI-ICE DISAGREE. QRH INDICATED FAILURE OF NR 2 A/I DUCT. RETURNED TO PAN C WHERE ICING DID NOT EXIST. R & R ALL 3, NR 2 ENGINE COWL ANTI-ICE MANISDR IPXA2016070505431Life Vest · openFOUND PASSENGER SEAT LIFE VEST SEAL BROKEN. R&R THE LIFE VEST IAW AMM 25-64-01-2 REV 85.03.SDR FDEA201607012220Skin · crackedTWO CRACK INDICATIONS APPROXIMATE 2.0 INCHES IN LENGTH FOUND DURING X-RAY INSPECTION AT STA 6-0, LONGERON SPLICE 4R AFT SECTION EDGE.SDR FDEA201607012219Hinge · corrodedLEFT HAND WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE LOWER MOUNT OUTBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.706", FINAL HOLE DIA: 0.728", MAXIMUM ALLOWABLE HOLE DIA: 0.709". REPAIR BUSHING FABSDR FDEA201607012218Hinge · corrodedLEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE LOWER MOUNT INBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE: DIA 0.706", FINAL HOLE: DIA 0.728", MAXIMUM ALLOWABLE HOLE: DIA 0.709". REPAIR BUSHING FABRICATEDSDR FDEA201607012214Hinge · corrodedRIGHT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE: DIA 1.330", FINAL HOLE: DIA 1.336", MAXIMUM ALLOWABLE HOLE: DIA 1.220". OVERSIZE BUSHING FABRICATED SDR FDEA201607012213Hinge · corrodedRIGHT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT INBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE: DIA 1.330", FINAL HOLE: DIA 1.336", MAXIMUM ALLOWABLE HOLE: DIA 1.220". OVERSIZE BUSHING FABRICATED IAW SDR FDEA201607012212Hinge · corrodedLEFT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.294", FINAL HOLE DIA: 1.327", MAXIMUM ALLOWABLE HOLE DIA: 1.220", OVERSIZE BUSHING FABRICATED ANDSDR FDEA201607012211Hinge · corrodedLEFT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT INBOARD HOLE BORE CORRODED. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM57-52-03. EXISTING HOLE DIA: 1.294", FINAL HOLE DIA: 1.327", MAXIMUM ALLOWABLE HOLE DIA: 1.220". OVERSIZE BUSHING FABRICATEDSDR FDEA201607012210Bracket · corrodedLEFT HAND WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE ACTUATOR OUTBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.219", FINAL HOLE DIA: 1.235" MAXIMUM ALLOWABLE HOLE DIA: 1.220". OVERSIZE BUSHING FABRICATSDR FDEA201606302205Battery · dischargedR1 DOOR PRESS TO TEST SWITCH INOPERATIVE. REPLACED R-1 DOOR PRESS TO TEST SWITCH BATTERIES. OPS CK GOOD.SDR FDEA201606302203Seat Track · corrodedMAIN DECK CARGO RT FLOOR SEAT TRACK AT STA 492, X=-27.5, FOUND CORROSION AS MARKED.SDR FDEA201606302202Seat Track · damagedMAIN DECK CARGO LT FLOOR SEAT TRACK AT STA 1801, X= 47.5. FOUND CROWN DAMAGED AS MARKED.SDR FDEA201606302201Seat Track · damagedMAIN DECK CARGO LT FLOOR SEAT TRACK AT STA 5-27, X= 47.5. FOUND CROWN DAMAGED AS MARKED.
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