Boeing MD-11F
Service difficulty reports · 31,317
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 FDEA2020081091844Skin · damagedFORWARD AVIONICS DOOR AFT SKIN HAS DAMAGE REPAIRED AVIONICS DOOR PAN IAW SRM CH 53-00-00, FIG 210 AND EA 1-5310-T0355764.SDR FDEA2020081091843Seat Track · damagedMAIN DECK CARGO COMPARTMENT, FOUND THE SEAT TRACK AT BS 1521, X- 75.25 HAD CROWN DAMAGE.SDR FDEA2020081091842Seat Track · damagedCABIN - MAIN DECK CARGO COMPARTMENT , FOUND SEAT TRACK AT STATION 5-10 , X = 47.5 CROWN DAMAGED .SDR FDEA2020081091841Seat Track · damagedMAIN DECK CARGO COMPARTMENT, FOUND SEAT TRACK AT BS 1541, X - 47.5 CROWN DAMAGED .SDR FDEA2020081091840Seat Track · damagedCABIN - MAIN DECK CARGO COMPARTMENT , FOUND SEAT TRACK AT STATION 1700 , X = 47.5 CROWN DAMAGED .SDR FDEA2020081091839Seat Track · damagedMAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT BS 585 , X = - 8.5 .SDR FDEA2020081091838Seat Track · damagedMAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT STATION 535 , X = - 8.5 .SDR FDEA2020081091837Access Panel · crackedCRACK INDICATION FOUND DURING HFEC INSPECTION ON THE LEFT WING FIXED LEADING EDGE CORNER OF FUEL ACCESS DOOR, FORWARD INBOARD CORNER APPROXIMATELY 1/4 INCHES LENGTH AT XOS 610 .SDR FDEA2020081091836Seat Track · damagedMAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN DAMAGED AT BS 755 , LBL 27.5. DAMAGE REMOVED AND FOUND WITHIN LIMITS IAW SRM 53-00-52-1A. FIGURE 101. ALLOWABLE DAMAGE 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR IPXA2020081098810Angle · crackedINSPECTION TYPE:2CUPPER CARGO COMPT. T-ANGLE CRACK AT LON 15R STA.1341. REMOVED AND INSTALLED CRACKED T-ANGLE AT LON 15R STA.1341 IAW SRM 51-33-01 AND 51-35-01. (MINOR)SDR IPXA2020081098808Angle · crackedINSPECTION TYPE:2C, UPPER CARGO BAY TEE ANGLE CRACKED AT END OF LONGERON 15L, BS 1341. REMOVED AND INSTALLED A NEW ANGLE IAW SRM 51-35-01, AND 51-33-01. (MINOR)SDR FDEA202009081828Support · corrodedRT WING, OUTBOARD FLAP VANE NR 4 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT RT WING, OUTBOARD FLAP VANE NR 4 SUPPORT FITTING ECCENTRIC HOLE BORE. REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT, AS PER MD-11 SRM 57-50-02-2R FIGURE 201 SDR FDEA2020090881827Support · corrodedRT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT RT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE. REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT, AS PER MD-11 SRM 57-50-02-2R FIGURE 201 SDR FDEA2020090481824Support Fitting · corrodedLT WING, OUTBOARD FLAP VANE NR 5 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LT WING, OUTBOARD FLAP VANE NR 5 SUPPORT FITTING ECCENTRIC HOLE BORE. REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 RSDR FDEA2020090481822Support · corrodedLT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE. REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 RSDR FDEA2020082781818Spar · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013, PER DRAWING NUMBER SN10550000 REVISION C, ON LT SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, CRACK INDICATION FOUND ON THIRD FASTENERS FROMSDR FDEA2020082781817Spar · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013, PER DRAWING NUMBER SN10550000 REVISION C, ON LT SIDE OF THE LOWER VERTICAL STABILIZER AFT FLANGE OF UPPER REAR SPAR CAP CRACK INDICATION FOUND BETWEEN FOURTH AND THIRD FASTENESDR FDEA2020082681832Finger Doubler · delaminatedLEFT HAND WING-TRAILING EDGE FINGER DOUBLER AT #541KB AT XW 375 FOUND DELAMINATED. LEFT HAND WING - TRAILING EDGE AT XW 375 #541KB DELAMINATED FINGER DOUBLER REPAIRED AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100SDR FDEA2020082181831Finger Doubler · delaminatedRT WING TRAILING EDGE FINGER DOUBLER AT #641KB FOUND DELAMINATED AT XW 375. RT WING TRAILING EDGE AT XW 375 #641KB DELAMED FINGER DOUBLER REPAIRED AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100 .SDR FDEA2020082081830Doubler · crackedLEFT HAND WING - FIXED LEADING EDGE CAVITY AT STATION XOS = 669 BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .SDR FDEA202008081829Doubler · crackedLT WING FIXED LEADING EDGE CAVITY AT STATION XOS = 653 BEADED DOUBLER FOUND CRACK. LT WING FIXED LEADING EDGE CAVITY AT STATION XOS = 653 DOUBLER REPAIR. CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .SDR FDEA2020082081826Doubler · crackedLEFT HAND WING - FIXED LEADING EDGE CAVITY AT STATION XOS = 638 BEADED DOUBLER FOUND CRACKED . REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .SDR FDEA2020082181825Doubler · crackedLT WING - FIXED LEADING EDGE CAVITY AT STATION XOS = 630 BEADED DOUBLER FOUND CRACK . LT WING - FIXED LEADING EDGE CAVITY AT STATION XOS = 630 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-SDR FDEA2020082081823Doubler · crackedRIGHT HAND WING - FIXED LEADING EDGE CAVITY AT STATION XOS = 962 BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 57-40-02-2RFIGURE 203 REPAIR 15 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .SDR FDEA2020082081821Doubler · crackedRIGHT HAND WING - FIXED LEADING EDGE CAVITY AT STATION XOS = 960 BEADED DOUBLER FOUND CRACK . REPAIR CARRIED OUT AS PER SRM 57-40-2-2R FIGURE 203 REPAIR 15 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .SDR FDEA2020082081820Doubler · crackedRIGHT HAND WING - FIXED LEADING EDGE CAVITY AT STATION XOS = 655 BEADED DOUBLER FOUND CRACK . RIGHT HAND WING - FIXED LEADING EDGE CAVITY AT STATION XOS = 655 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15 . REPAIR CLASSIFIED AS MASDR FDEA2020082081819Doubler · crackedRIGHT HAND WING - FIXED LEADING EDGE CAVITY AT STATION XOS = 650 BEADED DOUBLER FOUND CRACK . RIGHT HAND WING - FIXED LEADING EDGE CAVITY AT STATION XOS = 650 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15 . REPAIR CLASSIFIED AS MASDR FDEA2020081081832Doubler · detachedLEFT WING TRAILING EDGE DOUBLER AT 541KB WAS FOUND DETACHED AT XW 375.SDR FDEA2020081081831Finger Doubler · detachedRIGHT WING LEADING EDGE FINGER DOUBLER AT 641KB WAS FOUND DETACHED AT XW 375.SDR FDEA2020081081830Doubler · crackedLEFT HAND WING FIXED LEADING EDGE CAVITY AT XOS 669 BEADED DOUBLER WAS FOUND CRACKED.SDR FDEA2020081081829Doubler · crackedLEFT WING FIXED LEADING EDGE CAVITY AT XOS 653 BEADED DOUBLER WAS FOUND CRACKED.SDR FDEA2020081081828Support Fitting · corrodedRIGHT WING OUTBOARD FLAP VANE NR 4 SUPPORT FITTING ECCENTRIC HOLE BORE WAS FOUND CORRODED.SDR FDEA2020081081827Support Fitting · corrodedRIGHT WING OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORRODED.SDR FDEA2020081081826Doubler · crackedLEFT WING FIXED LEADING EDGE CAVITY AT XOS 638 BEADED DOUBLER FOUND CRACKED.SDR FDEA2020081081824Support Fitting · corrodedLEFT WING OUTBOARD FLAP VANE NR 5 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORRODED.SDR FDEA2020081081823Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 962 BEADED DOUBLER CRACKED.SDR FDEA2020081081822Vane · corrodedLEFT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORRODED.SDR FDEA2020081081821Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 960 BEADED DOUBLER CRACKED.SDR FDEA2020081081820Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 655 BEADED DOUBLER FOUND CRACKED.SDR FDEA2020081081819Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 650 BEADED DOUBLER FOUND CRACKED .SDR FDEA2020081081817Structure · crackedDURING ULTRASONIC INSPECTION FOUND VERTICAL CRACKS BEHIND SERVICE REPAIR ON LEFT SIDE OF THE LOWER VERTICAL STABILIZER AFT FLANGE OF UPPER REAR SPAR CAP.SDR 9WGA2020081089901Warning Message · illuminatedENG FIRE DETECTION 3 FAIL ALERT JUST AFTER TAKE-OFF.SDR IPXA2020081759134Intercostal · crackedINSPECTION TYPE:2C, LOWER FWD. CARGO INTERCOSTAL IS CRACKED AT STA. 6-30 AND LONG. 41 R/H. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG. ACA7049 AND SRM 51-33-01. (MINOR)SDR IPXA2020081759133Support · crackedINSPECTION TYPE:2C, RT LOWER WINGLET WEB SUPPORT IS CRACKED. REMOVED, FABRICATED AND REPLACED WEB IAW DWG. ARB7774 AND SRM 51-33-01. (MINOR)SDR FDEA202008071796Floorbeam · corrodedUPON REMOVAL OF LAVATORY MODULE IN THE CABIN, RIGHT. BS 420, X -20 - X -27, THE FLOORBEAM STRUCTURE WAS FOUND CORRODED. FLOOR SUPPORT REMOVE AND REPLACED BY FABRICATION PER DOUGLAS DRAWING # WSP0668 REVISION 'B' AND INSTALLED PER MD - 11 AMM 20-50-02 . REPSDR FDEA202008071795Floor Panel · corrodedFORWARD MAIN DECK CARGO COMPARTMENT FLOOR PANEL EDGE FOUND WITH CORROSION AT LEFT BS 475 - 503 , X 19.5 TO X 26.5. REMOVE AND REPLACED AS PER SRM 51-31-01-OG . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202008071794Floor Panel · corrodedFORWARD MAIN DECK CARGO COMPARTMENT FLOOR PANEL EDGE FOUND WITH CORROSION AT RIGHT, BS 475 - 503 ,X -37 TO X -46.5. REMOVED AND REPLACED PER SRM 51-31-01-OG . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202008071793Floor Panel · corrodedFORWARD CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL EDGE FOUND CORRODED AT LEFT, BS 475 -503 , X 1 TO X 8. REMOVE AND REPLACED PER SRM 51-31-01-OG . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202008071792Floor Panel · corrodedFORWARD CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL EDGE FOUND CORROSION AT BS 475 - 503 , X -74.5 TO X -94. REMOVE AND REPLACED AS PER SRM 51-31-01-OG . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202008071791Floor Panel · corrodedFOWARD CABIN MAIN DECK CARGO FLOOR PANEL EDGE FOUND CORRODED BETWEEN 475 - 503 ,X = -28 TO X = -35. REMOVE AND REPLACED PER SRM 51-31-01-OG . REPAIR CLASSIFIED AS MAJOR , PER GMM 6-2-100.
Back to Boeing MD-11F