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 FDEA2019111532942Hinge · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM57-44-08 AND FOUND EXCEED LIMIT BASE THE DIFFERENSDR FDEA2020011640128Floorbeam · corrodedMAIN CARGO DECK, STA1346 RBL105 CORROSION (MARKED) WORKED ACOMPLISHED ON N/R 664 AND 884 PER EA. 1-5710-T0351898SDR IPXA2019112769431Doubler · damagedINSPECTION TYPE:2CR/H WING I/B FLAP HAS DAMAGED REPAIR DOUBLER AT STA. XIFH=165.3 AND AFT OF YIFH=34.5.REPAIRED DAMAGED R/H I/B FLAP UPPER SKIN AT STA. XIFH=165.3 AND AFT OF YIFH=34.5 IAW VT-SAA EA 011-5753-01-A7954 REV. I/R AND UPS EO MD11-5750-74734-A. (MAJOSDR IPXA2019112219239Skin · damagedINSPECTION TYPE:2CR/H I/B FLAP T/E WEDGE UPPER SKIN HAS REPAIR AT STA. XIFH=171.3 AND 6.5 INCHES FROM EDGE NOT ON REPAIR MAPREPAIRED R/H I/B FLAP T/E WEDGE UPPER SKIN AT STA. XIFH-=171.3 AND 6.5 INCHES FROM EDGE IAW SRM 57-00-01 REPAIR 1 FIG. 201. (MAJOR)SDR IPXA2019112049202Support Web · crackedINSPECTION TYPE:2CCENTER ACC. COMP CIELING AT STA. 6-90 AND RBL 85, SUPPORT WEB IS CRACKED.REMOVED, FABRICATED AND REPLACED WEB IAW DWG. ADA4562 AND SRM 51-35-01. (MINOR)SDR FDEA2019111522923Web · corrodedUPON FLOOR SUPPORT REMOVAL FOR REPAIR - LOWER CENTER CARGO AFT BULKHEAD RIGHT HAND WEB FOUND WITH CORROSION AT STATION 1841 X=-20 TO X=-40 . LOWER CENTER CARGO AFT BULKHEAD RIGHT HAND AT STATION 1841,X=-20 TO X=-40 CORROSION WEB REMOVED AS PER SRM 51-21-01SDR FDEA2019111522922Seat Track · corrodedCABIN - LEFT HAND STATION 455 - 480 X = 107.25 SEAT TRACK FOUND CORROSION . CABIN AT LEFT HAND SEAT TRACK STATION 455 - 480 X = 107.25 , CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACKSDR FDEA201911122921Web · crackedAFT LOWER CARGO COMPARTMENT LEFT HAND FLOOR WEB AT STATION 1841,X=39 UNDERNEATH PANEL 187EF FOUND CRACKED. AFT LOWER CARGO COMPARTMENT LEFT HAND FLOOR AT STATION 1841,X=39 UNDERNEATH PANEL 187EF CRACKED WEB REMOVED AND INSTALLED WITH FABRICATED WEB AS PER SDR IPXA2019111348963Hf Comm · inoperativeINSPECTION TYPE:N/AATB - NEITHER HF 1 OR HF 2 HAVE VOICE CAPABILITY. NO TURNING ABILITY. ALL 3 RADIO HEADS USED TO TRY HF COMM, NO CAPABILITY. ATC ATTEMPTED SELECT CHECK. WE DIDN'T RECEIVE SELCAL.CYCLED BOTH HF1 & HF2 C/B'S. OPS CHK GOOD PER MM 23-11-01. BOTH SDR FDEA2019121313243Doubler · wornRT WING: DROOP L/E, INBD EDGE OF DROOP L/E REPAIR DOUBLER SKIN HAS WEAR MARK WORN INTO SKIN (MARKED AND DOT 36) REPAIRED PER SRM 57-40-01 2RSDR FDEA201911112918Computer · inoperativePDIS 590 22-10 7628 10NOV19 MEM FACT U LOGPAGES:3169806 2100 HOURS INTO FLT @ FL390 LEVEL 2 FCC 2B DATA FAULT. LEVEL 1 SEL YAW UPR B OFF, LEVEL 1 SEL LSAS LOB OFF. COMPLIED WITH QRH. PERFORMED RTS ON FCC #2. ALL TESTS PASSED. REF. FIM 2SDR FDEA2020010600030Skin · chafedRT WING: OUTBD EDGE OF DROOP L/E REPAIR DOUBLER SKIN IS WORN THRU. INSTALLED REPAIR PER SRM 57-40-01-2R INSTALLED DROOP L.E IAW MM 27-80-10-4 OPS CK GOODSDR FDEA2020012493340Frame · wornFWD AVIONICS COMPT: APPROX STA 457, THE FRAME UNDER #1 PACK INLET DUCT. THE DUCT BOOT MOUNT FASTENERS HAVE WORN THRU THE UPPER PART OF THE FRAME. (UNDER THE DUCT BOOT). MARKED. REPAIR IS COMPLIED WITH E.A.#:1-5300-T0351624 PART 1, TITLE: MD-11 N574FE-FUSELSDR FDEA201911092915Doubler · corrodedRH WING UPPER SURFACE - XORS 248 LANDING GEAR DOUBLER - CORROSION AROUND THREE (3) FASTENERS. REPAIRED PER EA 1-5710-T0351593SDR IPXA2019111148871Proximity Sensor · malfunctionedINSPECTION TYPE:N/AATB - AFTER T/O GEAR RETRACTED GOT RED (RIGHT MAIN) GEAR NOT UP INDICATION ON GEAR HANDLE AND CONFIGURATION PG. RAN QRH CHECK LIST 6-56 "GEAR PRIMARY OR SECONDARY LTS ILLUMINATE WITH GEAR HANDLE UP" ATB REQUIREDR&R RH MAIN GEAR UP AND LATCHESDR FDEA2020021480317Angle · corrodedMAIN CARGO DECK, STA1341 RBL104 CORROSION ON ANGLE AT BASE OF OVERWING FUEL TANK (MARKED) WORK ACOMPLISHED ON N/R 664 AND 884 PER EA. 1-5710-T0351898 A P1SDR FDEA2019110980063Bracket · corrodedMAIN CARGO DECK, STA1321 RBL48 UNDER SEAT TRACK, CORROSION BY FASTENER (MARKED) REMOVED AND REPLACED BRACKET PER APB7244SDR FDEA201911082910Support · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE FOUND CORRODED. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 SDR FDEA201911082909Support · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE FOUND CORRODED. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 SDR FDEA201911082908Support · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE FOUND CORRODED. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 SDR FDEA201911082911Support · corrodedRIGHT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE FOUND CORRODED. CORROSION AT RIGHT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR SDR FDEA201911268087Floorbeam · crackedCENTER CARGO COMPT: APPROX STA 1741 , CENTERLINE CARGO STOP. UNDER THE CARGO STOP THE FLOOR BEAM IS CRACKED.(UNDERSIDE OF STOP) REMOVED DAMAGED FLOOR BEAM IN CTR CARGO AT STA 1741. INSTALLED NEW FLOOR BEAM SECTION AND REPAIR PARTS PER SRM 51-31-01-0G.SDR IPXA2019111148877Elevator · malfunctionedINSPECTION TYPE:N/A**SUPPLEMENTAL SDR**EMERGENCY DECLARED -** A/C TAKEN OOS**. ON DESCENT AUTOPILOT WAS MANUALLY SELECTED OFF ELEVATORS WERE EXCESSIVELY HEAVY TO LEVEL OFF THE AIRPLANE. AUTOPILOT REENGAGED WITH AN UNEVENTFUL APPROACH AND LANDING. REMOVED R/H OSDR FDEA201911082912Seal · failedON LANDING ROLLOUT GOT LEVEL 1 ALERT " HYD 1 QTY LO"AFTER CLEARING RUNWAY, GOT LEVEL 2 HYD 1 FAIL OPENED R/H I/B ELEV. ACT. ACCESS PANELS FOR INSPECTION. FOUND O-RING ON FILTER HOUSING BLOWN OUT AGAIN, REMOVED FILTER BOWL AND FOUND IT SPLIT JUST BELOW THSDR FDEA202001170152Cargo Track · crackedCENTER CARGO COMPT: APPROX STA 1721, X=-91.25. O/B CARGO RAIL HAS AN O/B FLOOR BOARD FASTNENER ATTACH EAR CRACKED TWO PLACES. MARKED. PROCESSED NEW CHANNEL PER DWG AJF7011-519, REMOVED AND INSTALLED NEW CHANNEL IN CTR CARGO AT STA 1721, X=-47.25 PER SRM 51SDR FDEA2019122073267Skin · crackedLT LWR VERTICAL STAB FAIRING SKIN AT STA 2160 HAS A .300 IN CRACK PROPAGATING OUT OF THE FASTENER HOLE. BELOW PYLON CARRY THROUGH CAP, REPAIRED SKIN FAIRING PER SRM 55-00-00-2R FIG 204 DWG AJC7582-17.SDR FDEA201911072902Seat Track · crackedWITH REFERENCE TO WRI : 25509452 - CABIN SEAT TRACK CROWN AT STATION 1281 X = 47.5 FOUND CRACKED OFF. CABIN CRACKED SEAT TRACK AT STATION 1281 X = 47.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1311 TO STATION 1229 X = 47.5 AS PER SRM 53-00-52SDR IPXA2019111148861Doubler · wornINSPECTION TYPE:2CTAIL CONE R/H SIDE UPPER LATCH SPOOL FITTING/DOUBLER IS WORN THRU.REMOVED, FABRICATED AND REPLACED FITTING/DOUBLER IAW DWG. AKC7546 AND SRM 51-35-01. (MINOR)SDR FDEA201911072903Seat Track · corrodedCABIN RIGHT HAND STATION 475 X = - 27.5 FOUND CORROSION. CABIN AT RIGHT HAND STATION 475 X= - 27.5 SEAT TRACK, CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REMOVED AND REPLACED FROM STASDR IPXA2019110878739A/C Pack · odorINSPECTION TYPE:N/ATHROUGHT OUT CLIMB AND CRUISE STRONG PACK SMELL WAS NOTED. SELECTED ECON TO CLEAR, THEN SMELL REAPPEARED AND DESCENTCLEANED PACKS AND DUCTS PER 21-53-00 OF EXCESS DE-ICE FLUID OKAY FOR RTSDR FDEA2020022060356Spar · corrodedPERFORMED DETAIL VISUAL INSP. OF THE OUTER WING, UPPER SPAR CAP (P/N ARB7413-2) FROM STATIONS XORS-1041.500 THROUGH XORS-1044.000 PER FOLLOW UP E.A. 1-5720-87643 AND W/C SEQ. #000806, W/C #T-1-5720-87643 P2. FOUND CORROSION BETWEEN AREAS X0RS- 1035.500 TSDR FDEA201912263303Spar · corrodedRIGHT WING T/E REAR SPAR UPPER CAP, LOWER FLANGE IS CORRODED AT STA. XORS 685. BLENDED AND REMOVED CORROSION IAW SRM 57-00-00-2R REFERENCE EA 1-5710-T0350918P1REMOVED FASTENERS THROUGH UPPER SPAR T-CAP LOWER FLANGE FROM XORS 680-690 IAW SRM 51-33-01-0G. RESDR FDEA201911063188Skin · chafedRT WING LWR FIXED L/E SKIN WORN FROM SLAT CONTACT. O/B OF SLAT TRACK NR 10 PERFORMED WING FIXED LEADING EGDE REPAIR IAW SRM 57-40-02-2R FIG 201 REP 5.SDR FDEA2019110762892Doubler · corrodedLEFT WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER FOUND CORROSION AT XORS 254. LEFT WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER STATION XORS 254 CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 57-20-01-1A ALLOWABLE SDR FDEA201911062895Hinge · corrodedLEFT WING FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM57-52-04. OVERSIZED BUSHING FABRICSDR IPXA2019111148881Engine · fodINSPECTION TYPE:N/AATB - A/C TAKEN OOS - **SUPPLEMENTAL SDR** MULTIPLE BIRDSTRIKES DURING CLIMB OUT THROUGH 7000'. HIGH AIRFRAME VIBRATION PRESENT. ALL ENGINES CONTINUED TO OPERATE. VISUAL SHOWS SEVERE DAMAGE TO FUSELAGE, LEFT INBOUND SLAT, AND #1 ENGINE.REPLASDR FDEA2019110762896Hinge · corrodedRIGHT WING FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM57-52-04. OVERSIZED BUSHING FABRSDR FDEA2019110762900Skin · corrodedRH WING UPPER SURFACE - APPROX XORS 288 AFT SECTION OF LANDING GEAR DOUBLER - CORROSION AROUND FASTENER.SDR FDEA2019110752861Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 1190 X=-75.25 FOUND CORROSION. MAIN DECK FLOOR SEAT TRACK AT STATION 1190 X= -75.25 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. ORIGINAL MATERIAL THICKNESS: 0.080 MATERISDR FDEA2019110752856Skin · delaminatedRIGHT WING TRAILING EDGE INBOARD ISLAND FORWARD EDGE UPPER SKIN LOWER SURFACE FINGER DOUBLER AT XW 392 FOUND DETACHED. REPAIR CARRIED OUT AT RIGHT WING TRAILING EDGE INBOARD ISLAND FORWARD EDGE UPPER SKIN LOWER SURFACE AT XW 392 IAW SRM 57-50-01-2R, FIGURE SDR FDEA2019110752865Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 1475 X= 75.25 FOUND FLANGE CORROSION. MAIN DECK FLOOR SEAT TRACK AT STATION 1475 X= 75.25 FLANGE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE101 ALLOWABLE DAMAGE 1. ORIGINAL MATERIAL THICKNESS:SDR FDEA2019110752864Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 1571 TO STATION 1621 X=-107.25 FOUND CORROSION. MAIN DECK FLOOR SEAT TRACK AT STATION 1571 TO STATION 1621 X= -107.25 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE101 ALLOWABLE DAMAGE 1. ORIGINALSDR FDEA2019110752863Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 1441 X= 8.5 FOUND CORROSION. MAIN DECK FLOOR SEAT TRACK AT STATION 1441 X= 8.5 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. ORIGINAL MATERIAL THICKNESS: 0.080 MATERIAL RSDR FDEA2019110752862Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 1256 X=-75.25 FOUND CORROSION. MAIN DECK FLOOR SEAT TRACK AT STATION 1256 X= -75.25 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. ORIGINAL MATERIAL THICKNESS: 0.080 MATERISDR FDEA201911152860Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 475 X=-27.5 FOUND CORROSION. MAIN DECK FLOOR SEAT TRACK AT STATION 475 X= -27.5 FOUND EXFOLIATION CORROSION EXCEED LIMIT AS PER MD11 SRM 53-00-52-1A FIGURE101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT AT STATSDR FDEA2019110752859Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT BS 755 X= 47.5 FOUND CROWN DAMAGED. MAIN DECK FLOOR SEAT TRACK CROWN DAMAGED AT BS 755 X= 47.5, DAMAGED AREA EVALUATED AND FOUND EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT IASDR FDEA2019110752858Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT 755 X=-47.5 FOUND CROWN DAMAGED. DAMAGED AREA EVALUATED AND FOUND EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED ASSDR FDEA2019110752857Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT BS 755 X=-27.5 FOUND CROWN DAMAGED. AREA EVALUATED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED ASDR FDEA2019112243036Skin · corrodedNUMEROUS AREAS OF SURFACE CORROSION ON L/H WING UPPER SURFACE BETWEEN STA XORS-340.00 TO XORS-393.00 / STR-5.5 TO STR. 2...(MRK) REMOVED CORROSION ON L/H WING UPPER SURFACE BETWEEN STA XORS=345.75 TO XORS=298.501 STR 07 TO AFT SPAR REF EA#: 1-5730-T03515SDR FDEA2019112243034Skin · corrodedNUMEROUS AREAS OF SURFACE CORROSION ON L/H WING UPPER SURFACE BETWEEN STA XORS-141.00 TO XORS-166.80 STR.22 TO STR-19....(MRK) REMOVED CORROSION ON L/H WING UPPER SURFACE BETWEEN STA XORS=130.40 TO XORS=163.80 FRONT SPAR TO STR 16 REF SRM 57-00-01-1A
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