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 IPXA2020080258557Door · inoperativeCABIN DOOR FWD RT WONT OPEN AFTER BEING DISARMED. DEFERRED R1 CABIN DOOR PER MEL 52-10-3-1-2-1, DI# M715510 ASSIGNED.T/S PER FIM 52-11-00-810-802. FOUND R1 DOOR UP LIMIT SWITCH INTERMITTENT. R/R SWITCH IAW AMM 20-50-00. VERIFIED SWITCH ADJUSTMENT IAW AMM 52-1SDR FDEA2020080321750Floor Panel · damagedCABIN FLOOR PANEL 262BF FOUND DAMAGED AT RH STA 1159-STA 1239SDR FDEA2020080321749Floor Panel · damagedCABIN FLOOR PANEL 231HF TOP SURFACE DAMAGED AT BS 595 TO 675.SDR FDEA2020080321748Stop Fitting · crackedMAIN DECK CARGO COMPARTMENT R3 DOOR, NR 5 BEAM, FORWARD DOOR STOP NR 5 WAS FOUND CRACKED.SDR KO0R202007310005Light · inoperativeEMERGENCY LIGHTS FAILED TO ILLUMINATESDR FDEA202007311735Brake Assy · overtempWHILE PARKING, RECEIVED A BRAKE OVERHEAT ALERT. NR 5 BRAKE 595 DEGREES C MAX TEMP. FAILED OPS CHECK. & REPLACED WITH SERVICABLE UNIT. FOUND THAT THE BRAKE ASSEMBLY WAS SEIZED ON THE AXLE AND STUCK IN PLACE. THE WHEEL WAS ALSO UNABLE TO ROTATE. NOTED PSDR FDEA202007301727Hinge Fitting · corrodedRIGHT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE FOUND CORRODED. WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR EVALUATED AND FOUND DATA FOR THE PIVOT BORE SHSDR FDEA202007301726Hinge Fitting · corrodedLEFT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORRODED. WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLSDR FDEA202007301724Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON THE LEFT FIXED LEADING EDGE SKIN, AT CORNER NUMBER 13, SLAT TRACK NR 10 CUT OUT AFT INBOARD CORNER FOUND CRACKED APPROXIMATELY 0.4 INCHES IN LENGTH AT XOS 657. REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE SDR FDEA202007301723Doubler · crackedRIGHT WING, LEADING EDGE CAVITY AT XOS 757, BEADED DOUBLER CRACKED. 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 FDEA202007301722Doubler · crackedLEFT WING, LEADING EDGE CAVITY AT XOS 500 BEADED DOUBLER FOUND CRACKED. 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 FDEA202007301721Doubler · crackedRIGHT WING - LEADING EDGE CAVITY AT XOS 751 BEADED DOUBLER FOUND CRACKED. RT WING, LEADING EDGE CAVITY AT STATION XOS=751 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 FDEA202007301720Finger Doubler · detachedRIGHT WING TRAILING EDGE FINGER DOUBLER AT 641KB FOUND DELAMINATED. RT WING, TRAILING EDGE FINGER DOUBLER AT 641KB STATION XW 375.34 REPAIR CARRIED OUT, AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202007291712Engine · damagedDURING CRUISE FLIGHT AT FL 360 WE GOT BANG NOISE SEVERAL TIMES, THEN FELT VIBRATION IN THROTTLE FOR #1 ENGINE FOLLOWED BY ENGINE #1 OVERTEMP FOR OIL ABOVE REDLINE. WE FOLLOWED QRH AND SHUTDOWN ENGINE. #1 SHUTDOWN FINE AND WINDMILLED FOR APPROXIMATELY 40 MSDR FDEA202009101705Frame · dentedCABIN, MAIN DECK CARGO COMPARTMENT FRAME DENTED AT STATION 1621, LONGERON 12 RT. CABIN, MAIN DECK CARGO COMPARTMENT AT STATION 1621, LONGERON 12 RT, DENTED FRAME, REPAIRED AS PER SRM 53-00-07 -2R FIGURE 201 REPAIR 2. REPETITIVE INSPECTION REQUIRED-INITIAL ATSDR FDEA202007291703Hinge Bracket · corrodedRT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE (F AND G HOLE). REWORKED AND FOUND EXCEEDS LIMIT, AS PER MD-11 CMM 57- 52-03.SDR FDEA2020090429701Bracket · corrodedLT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE (F AND G HOLE). REWORKED AND FOUND EXCEEDS LIMIT AS PER MD-11 CMM 57- 52-03SDR FDEA2020082891706Fuel Tank · corrodedMAIN DECK CENTER WING TANK AT S-13, BETWEEN XCW = - 104 AND XCW = -110 AREA FOUND CORROSION. MAIN DECK CENTER WING TANK AT STRINGER - 13, BETWEEN XCW = -104 AND XCW = - 110. REPAIR CARRIED OUT PER FEDEX E.A. # 1-5730-T0355693 P1. TITTLE :- WINGS - PLATES ANSDR FDEA2020082891704Bracket · corrodedRT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE (A AND B HOLE). REWORKED AND FOUND EXCEEDS LIMIT, AS PER MD-11 CMM 57-52-03.SDR FDEA2020082691707Skin · crackedRIGHT WING - FIXED LEADING EDGE AT STATION XOS 1191 FOUND CRACK AS MARKED . RIGHT WING - FIXED LEADING EDGE AT STATION XOS 1191 SKIN REPAIR CARRIED OUT AS PER MD - 11 SRM 57-40-01-2R, FIGURE 201, REPAIR 16 . REPAIR CLASSIFIED AS MAJOR PER GMM 6 - 2 - 100 .SDR FDEA2020082091708Floor Panel · corrodedFOWARD CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL EDGE FOUND CORROSION AT STATION 475 TO STA 503 , BETWEEN X = 37 TO 46.5 . FORWARD CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL AT STATION 475 - STATION 503, BETWEEN X = 37 TO X = 46.5 , CORROSION BLSDR FDEA2020073091712Engine · vibrationDURING CRUISE FLIGHT AT FL 360, BANG NOISE SEVERAL TIMES, THEN FELT VIBRATION IN THROTTLE FOR NR 1 ENGINE FOLLOWED BY ENGINE NR 1 OVERTEMP FOR OIL ABOVE REDLINE. FOLLOWED QRH AND SHUTDOWN ENGINE. NR 1 SHUTDOWN FINE AND WINDMILLED FOR APPROXIMATELY 40 MINSDR FDEA2020073091708Floor Panel · corrodedFOWARD CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL EDGE FOUND CORROSION AT STATION 475 TO STA 503 , BETWEEN X = 37 TO 46.5 .SDR FDEA2020073091707Skin · crackedRIGHT WING - FIXED LEADING EDGE AT STATION XOS 1191 FOUND CRACKED.SDR FDEA2020073091706Fuel Tank · corrodedMAIN DECK - CENTER WING TANK AT STATION 1244 X= - 105 AREA FOUND CORROSION.SDR FDEA2020073091705Frame · dentedCABIN - MAIN DECK CARGO COMPARTMENT FRAME DENTED AT STATION 1621 , LONGERON 12 RIGHTSDR FDEA2020073091704Hinge Fitting · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSIONS.SDR FDEA2020073091703Hinge Fitting · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSIONS.SDR FDEA202007291702Hinge Fitting · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSIONS. REWORKED AND FOUND EXCEED LIMIT, AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A. NR 1-575SDR FDEA2020073091701Hinge Fitting · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSIONS.SDR FDEA202007281690Frame · dentedCABIN - MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR FOUND DENTED AT LEFT STATION 1661 , LONGERON 12 L . REPAIR CARRIED OUT PER MD - 11 SRM 53-00-07 -2R REPAIR 2 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202007281689Frame · dentedCABIN - MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR FOUND DENTED AT LEFT STATION 1721 , LONGERON 12 L . REPAIR CARRIED OUT PER MD - 11 SRM 53-00-07-2R REPAIR 2 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202007281688Skin · corrodedRIGHT WING - UPPER WING SURFACE FOUND CORROSION AT XORS 323, STRINGER 1R. REPAIR CARRIED OUT AS PER FEDEX E.A. # 1-5730-T0355660. P1 . TITTLE : WINGS - PLATES AND SKINS - CORROSION BLENDOUT REPAIRS ON RIGHT OUTER WING , UPPER AFT SKIN PANEL , XORS 345 - SDR FDEA202007281687Skin · corrodedRIGHT WING - UPPER WING SURFACE FOUND CORROSION AT XORS 327, STRINGER 4R. REPAIR CARRIED OUT AS PER FEDEX E.A. # 1-5730-T0355660. P1 . TITTLE : WINGS - PLATES AND SKINS - CORROSION BLENDOUT REPAIRS ON RIGHT OUTER WING , UPPER AFT SKIN PANEL , XORS 345 - SDR FDEA202007281686Skin · corrodedRIGHT WING - UPPER WING SURFACE FOUND CORROSION AT XORS 355 . REPAIR CARRIED OUT, AS PER FEDEX E.A. NR 1-5730-T0355660, P1. TITTLE:WINGS-PLATES AND SKINS-CORROSION BLENDOUT REPAIRS ON RT OUTER WING, UPPER AFT SKIN PANEL, XORS 345-385 STRINGER 1 TO 4. REPAIRSDR FDEA202007281685Doubler · crackedLEFT WING - FIXED LEADING EDGE CAVITY BEADED DOUBLER BETWEEN XFS 990 - XFS 1005 , NEAR SLAT #7 OUTBOARD TRACK FOUND CRACK AS MARK . LEFT WING - FIXED LEADING EDGE CAVITY BEADED DOUBLER BETWEEN XFS 990 - XFS 1005 , NEAR SLAT #7 OUTBOARD TRACK REPAIR CARRIEDSDR FDEA202007281684Seat Track · damagedMAIN DECK - SEAT TRACK AT STATION 1321 X = - 107.25 FOUND DAMAGED. REPAIR CARRIED OUT PER MD-11 SRM 53-00-52-2R . REPAIR 3 . FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .SDR IPXA2020072758276Panel · crackedINSPECTION TYPE:4C, LT WING FIXED L/E PANEL 517AB CRACKED AND TORN. REMOVED, FABRICATED, AND INSTALLED A NEW L/E PANEL 517AB IAW SRM 51-33-01 AND 51-35-01. (MINOR)SDR IPXA2020072758289Relay · failedDURING CRUISE, FL 310, ONE HOUR LEFT IN FLIGHT, HAD A LEVEL 1 CARGO FLOW FWD DISAGREE. NO OTHER INDICATIONS FOUND. TROUBLESHOT IAW FIM 21-27-00-101, STEP 4. R & R RELAY R2-78 IAW WDM 21-43-01 AND AMM 20-30-10. OPS CHECKED GOOD.SDR FDEA202007271674Hinge Fitting · corrodedLT WING, FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT LT WING, FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04. OVERSIZED BUSSDR FDEA202007271673Hinge Fitting · corrodedLT WING, FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE SURFACE FOUND CORROSIONS. CORROSIONS AT LT WING, FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE SURFACE. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04. REPAIR. SDR FDEA202007271672Doubler · corrodedLELEFT WING - UPPER INBOARD SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER SUSPECTED CORROSION NEAR INBOARD EDGE . STA XW 212.2972. LEFT HAND WING UPPER INBOARD SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER NEAR INBOARD EDGE STATION XW 212.2972 CORROSIOSDR FDEA2020082761660Bracket · corrodedRT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR 8 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08SDR FDEA2020082761659Bracket · corrodedRT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR 8 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08SDR FDEA2020082761658Bracket · corrodedRT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE BORE. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BYSDR FDEA2020082761657Bracket · corrodedRT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR 8 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-4SDR FDEA202002761656Bracket · corrodedRT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR 8 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09SDR FDEA2020082761655Bracket · corrodedRT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (NR 3 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-SDR IPXA2020072768240Spar Cap · corrodedINSPECTION TYPE:S/V, RIGHT WING REAR SPAR UPPER CAP AT XORS 735 HAD CORROSION. REPAIRED CORRODED UPPER SPAR CAP BETWEEN XORS 720 - XORS 737 IAW EA 011-5710-01-A8436, REV I/R, AND EO MD11-5740-77265-A. (MINOR)SDR IPXA2020072768239Spar Cap · corrodedINSPECTION TYPE:S/V, RIGHT WING REAR SPAR UPPER FLANGE AT XORS 725 HAD CORROSION. REPAIRED THE RT WING UPPER FLANGE/CAP BETWEEN XORS 720 TO XORS 737 IAW EA 011-5710-01-A8436, REV I/R AND EO MD11-5740-77265-A. MINOR.
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