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 IPXA201811306386Lens · damagedL1 DOOR EMERGENCY EXIT LENS HOUSING WAS DAMAGED. ACCOMPLISHED EO MD11-02520-70732-A SECTION 6.A.SDR FDEA201811283392Rod · shearedCOMPRESSOR STALL CLIMBING OUT OF 12,000 FT NR 1 ENG FL330 2ND COMPRESSOR STALL. WHILE ON DESCENT FOR LANDING OBSERVED THE FOLLOWING AT 6000 NR 1 EGT 512 EGT, 85% N1, NR 2 38 EGT, 77 %, NR 3 351 EGT 77%. CREW DEBRIEF, NR 2 ENG EGT WAS 358 NOT 38. NR 1 ENG THROSDR FDEA201811273378Transponder · inoperativeAT 1 30 HRS INTO FLIGHT, RECEIVER LEVEL 1 TRANSPONDER 1 FAIL. SWITCHED TO TRANS 2 AND RECEIVED TRNSP 2 FAIL. BOTH TRANSPS INTERMITTENTLY FAILED REMAINING FLIGHT. TRANSPORTER 1 REPLACED SYSTEM 1 AND 2 FIM TASK 34-54-00-1, TEST OK. NO FAULTS REV NOV 1/2010. REPLSDR FDEA201811273373Longeron · corrodedFOUND CORROSION ON LONGERON 50R AT STA 1681. COMPLIED WITH E.A. 1-5310-T0343744; PART 1; REPAIR FOR LONGERON 50R STA. 1681.SDR FDEA201811273372Longeron · corrodedFOUND CORROSION ON LONGERON 49R AT STA 1681. COMPLIED WITH E.A. 1-5310-T0343744; PART 1; MAINFRAME AFT INTERMEDIATE FUSELAGE; BOTTOM; STA. 1671-1691; R/H LONGERONS L49 & L50 CORROSION REPAIR..SDR FDEA201811263370Intercostal · crackedEMPENNAGE, DURING REMOVAL ACCESS FOR BANJO FITTING REPAIR, RIGHT HAND SIDE LOWER VERTICAL STABILIZER REAR CENTER SPAR TO REAR SPAR INTERCOSTAL FOUND CRACK. INTERCOSTAL AT STATION 2164 REPAIR CARRIED OUT AS PER SRM 55-30-02-2R FIGURE 204 REPAIR 7. REPAIR CLASSISDR FDEA201811253379Transponder · failedPDIS 594 34-54 1175 25NOV18 ATH FACT U LOGPAGES:3042743 AT 1 30 HRS INTO FLIGHT RECIEVER LEVEL 1 TRANSPORNDER 1 FAIL.SWITCHED TO TRANS 2 AND RECIEVED TRNSP 2 FAIL.BOTH TRANSPS INTERMITENTLY FAILED REMAINING FLIGHT . FACT 25NOV18 10:37 ASDR FDEA201811253369Probe · failedON CLIMBOUT FLIGHT DIRECTOR WAS GIVING INACCURATE INFO, BUT IT STARTED WORKING AT ALTITUDE IAS COMPARATOR WITH MOMENTARY ELEVN & YAW WARNING ACCOMPANIED BY AUTO-PILOT FAIL. ON RETURN RECEIVED FADEC ALT ALERT. QRH DIRECTED AIRSPEED UNRELIABLE CHECKLIST. SELECTESDR FDEA201811233360Tire · failedTIRE FAIL LEVEL 1 ALERT AT APPROX 80 KTS WITH AUDIBLE BANG DURING ROLLOUT FROM CAT 3 ILS AUTO LAND. CLEARED RUNWAY AND WAITED FOR MAINTENANCE INSPECTION. LATER ANNUNCIATORS, BRAKE DIFF TEMP AND ANTI-SKID ILLUMINATED. MAINTENANCE ADVISED TO TAXI SLOW. TAXIED TSDR FDEA201811233355Finger Doubler · detachedRIGHT WING FINGER DOUBLER FOUND DETACHED AT ISLAND UPPER SKIN OUTBOARD OF INBOARD AILERON AT STATION XW 375 AND E 65.00. REPAIR CARRIED OUT ON STATION XW 375, E 65.00 TO E 70.00 AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-SDR FDEA201811233354Finger Doubler · detachedLEFT WING FINGER DOUBLER FOUND DETACHED AT ISLAND UPPER SKIN OUTBOARD OF INBOARD AILERON AT STATION XW 375 AND E 65.00. REPAIR CARRIED OUT AT STATION XW 375, E 65.00 TO E 70.00 AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-SDR IPXA2018112636313Lamp · inoperativeEMERGENCY POWER OFF ANNUNCIATOR LAMPS INOPERATIVE. REPLACED THE LAMPS, PERFORMED AN OPS CHECK IAW MM 24-34-00-501, LIGHTS OPS CHECKED NORMAL.SDR IPXA2018112626216Battery Pack · inoperativeEMERGENCY LIGHT BATTERY 1 LOW FOUND DURING A PREFLIGHT. THE BATTERY PACK WAS R & R IAW AMM 33-51-01 PB 401, AMM REV 91.02.SDR FDEA201811223349Doubler · crackedNR 1 RAM AIR EXHAUST CUTOUT DOUBLER SUSPECT CRACKED STATION 561 LONGERON 48 LEFT. CRACKED DOUBLER REMOVED AND REPLACED WITH NEW DOUBLER AS PER SRM 51-35-01-0G. NEW DOUBLER FABRICATED AS PER DRAWING ACA 3850 REVISION AA. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-1SDR FDEA201811223347Skin · crackedLOWER CENTER CARGO DOOR FORWARD LOWER EDGE CRACKED AT STATION XIFH 1713.9. REPAIRED AS PER EA 1-5230-T0343643 P1. FWD LOWER CORNER OUTER SKIN CRACK REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201811223345Rail · corrodedLOWER CENTER CARGO COMPARTMENT DURING UPON ACCOMPLISH EA 1-5310-T0338224 P3 TO CARRY OUT PERMANENT REPAIR CENTER CARGO JAMB RAIL AT STATION 1717. REPAIRED AS PER EA #: 1-5310-T0338224 A P3 TITLE: FUSELAGE - MAINFRAME - CENTER CARGO DOOR LOWER JAMB - CORROSISDR FDEA201811213328Support · corrodedRIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING 'F' ECCENTRIC HOLE BORE CORROSION. TEE FITTING 'F' HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0343646 P1 STEP 1B. TRACK SUPPOSDR FDEA201811213327Support · corrodedRIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING 'E' ECCENTRIC HOLE BORE CORROSION. TEE FITTING 'E' HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0343646 P1 STEP 1A. TRACK SUPPOSDR FDEA201811223344Seat Track · corrodedFORWARD CABIN FLOOR SEAT TRACK AT STATION 440 X = 18" FOUND WITH SURFACE CORROSION. CORROSION REMOVED AS PER SRM 51-21-01-0G AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REMOVED AND REPLACED FROM STATIONSDR FDEA201811223342Seat Track · corrodedFORWARD CABIN FLOOR SEAT TRACK AFT OF LAVATORY MODULE STATION 428 X = -27" FOUND WITH CORROSION. CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REMOVED AND REPLACED FROM STATION 421 TO STATSDR FDEA2018112103322Hinge Bracket · corrodedRIGHT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE SURFACE FOUND CORROSION CORROSIONS AT RIGHT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE SURFACE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR EVALUATED AND SDR FDEA2018112103321Hinge Bracket · corrodedRIGHT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORROSION CORROSIONS AT RIGHT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED BUSHINGSDR FDEA2018112103320Hinge Bracket · corrodedLEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE SURFACE FOUND CORROSIONS. CORROSIONS AT LEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR EVALUATED AND SDR FDEA2018112103319Hinge Bracket · corrodedLEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORROSIONS. CORROSIONS AT LEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED BUSHINGSDR FDEA2018112103318Hinge Bracket · corrodedLEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT LEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SDR FDEA201811203326Support Fitting · corrodedRIGHT WING OUTBOARD FLAP VANE NR 4 SUPPORT FITTING ECCENTRIC BORE HOLE FOUND CORROSION. SUPPORT FITTING HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. REPAIR BUSHING FABRICATED AS PER EA 1-5750-T0343705 P1 STEP 1A. TRACK SUPSDR FDEA201811203325Support Fitting · corrodedRIGHT WING OUTBOARD FLAP VANE NR 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSIONS. SUPPORT FITTING HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. REPAIR BUSHING FABRICATED AS PER EA 1-5750-T0343705 P1 STEP 1A. TRACK SUSDR FDEA201811203324Support Fitting · corrodedLEFT WING OUTBOARD FLAP VANE NO. 4 SUPPORT FITTING ECCENTRIC BORE HOLE FOUND CORROSIONS. SUPPORT FITTING HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0343882 PART 1 STEP 1A. TSDR FDEA201811203323Support Fitting · corrodedLEFT WING OUTBOARD FLAP VANE NR 2 SUPPORT FITTING ECCENTRIC BORE HOLE FOUND CORROSION. SUPPORT FITTING HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0343882 PART 1 STEP 1A. TRASDR FDEA201811203310Frame · dentedRIGHT MAIN DECK COMPARTMENT FRAME AT STATION 1641 FOUND DENTED AT LONGERON 12 RIGHT. FRAME REPAIRED AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201811203309Seat Track · corrodedMAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 1359 X = -8.75 FOUND WITH CORROSION AS MARK. SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRASDR FDEA201811203307Floor Support · crackedFUSELAGE : FORWARD AVIONICS COMPARTMENT APPROXIMATELY STATION 383-420, X=90, MAIN DECK FLOOR STRUCTURE SUSPECTED CRACKED. FUSELAGE FORWARD AVIONICS COMPARTMENT APPROXIMATELY STATION 383 - 420 , X= 90 , MAIN DECK FLOOR SUPPORT REMOVED AND REPLACED AS PER MDSDR FDEA201811193298Bracket · corrodedRIGHT WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSIONS. CORROSION AT RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM SDR FDEA201811193297Bracket · corrodedRIGHT WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE) LOWER MOUNT INBOARD LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CSDR FDEA201811193296Bracket · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) INBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMMSDR FDEA201811193295Bracket · corrodedRIGHT WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SDR FDEA201811193300Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. ACTUATOR LUG HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-57SDR FDEA201811193299Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) PIVOT BORE HOLE FOUND CORROSIONS. HINGE HOLE BORE (HOLE 4) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0343678 P1 STEP 2A SDR FDEA201811193294Hinge Bracket · corrodedRIGHT HAND INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION. HOLE BORE (HOLE 3) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA #: 1-5750-T0331061 A PSDR FDEA201811193293Hinge Bracket · corrodedLEFT HAND INBOARD FLAP OUTBOARD FORWARD HINGE ( WING SIDE ) PIVOT HOLE BORE CORROSION. CORROSION AT LEFT HAND INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATSDR IPXA2018112106145Battery Pack · inoperativeEMERGENCY LIGHT BATTERY 1 LOW. R & R EMERGENCY POWER SUPPLY BATTERY IAW AMM 33-51-01-401.SDR FDEA201811193292Doubler · chafedMAIN DECK CARGO COMPARTMENT LEFT HAND 9G NET SUPPORT YOKE FRAME AT STATION 535, LONGERON 24 LEFT, EXISTING REPAIR CHAFED. CHAFED EXISTING REPAIR REMOVED AS PER SRM 51-33-01-0G AND REPAIR CARRIED OUT AS PER SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIEDSDR FDEA201811193304Transmitter · false activationTIRE FAIL AFTER GEAR RETRACTION. REMOVED AND REPLACE TIRE PRESSURE TRANSMITTER. OK FOR SERIVCESDR FDEA201811183273Doubler · crackedRIGHT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 667 FOUND CRACK. DOUBLER REMOVED AS PER SRM 51-31-01-0G AND REPLACED WITH NEW RIB DOUBLER AS PER SRM 51-33-01-0G. FABRICATED RIB DOUBLER AS PER DWG ARB3954 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10SDR IPXA2018112196109Connector · inoperativeEMERGENCY LIGHT TEST FAILED. REPLACED THE POWER SUPPLY IAW 33-51-01-501, TEST FAILED. THE EMERGENCY LIGHTS WOULD NOT GO OFF. INSTALLED THE ORIGINAL POWER SUPPLY. RESEATEDA LOOSE CONNECTOR. OPS CHECKED GOOD IAW AMM 33-50-00.SDR IPXA2018111986080Light · malfunctionedEMERGENCY LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY IAW MM 33-51-01-501, TEST FAILED. EMERGENCY LIGHTS WOULD NOT TURN OFF. INSTALLED THE ORIGINAL POWER SUPPLY.SDR FDEA2018111973268Floor Support · corrodedMAIN DECK CARGO COMPARTMENT AFT FLOOR PANEL SUPPORT FOUND WITH CORROSION AT STATION 1897 X = 58. MAIN DECK CARGO AFT FLOOR PANEL SUPPORT AT STATION 1897, X = 58. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R, FIGURE 206. FLOOR PANEL SDR IPXA2018111976053Bottle · low pressureR1 DOOR PNEUMATIC BOTTLE WAS UNDER THE LIMITS. SERVICED AND VERIFIED PNEU BOTTLE WAS IN THE GREEN BAND IAW AMM 52-11-02-200-804.SDR FDEA201811163256Hmu · unknownPDIS 609 25-50 7809 WRI CLOSED, NEW WRI 72-00 7812. LOGPAGES:3040677 ON CLIMB OUT 5000 FEET, EXPERIENCED A VERY PRONOUNCED JOLT ON THE ENTIRE AIRCRAFT. TROUBLE SHOT, FOUND NO REASON FOR PROBLEM. DECIDED TO CONTINUE CLIMB, HAD SAME INDICATION CLIMBINSDR IPXA2018112196105Flap · brokenR1 DOOR LOWER HINGE SPRING PANEL REMOVED DUE TO DAMAGE. DURING OPS CHECK OF THE EMERGENCY PNEUMATIC FUNCTION OF THE R1 DOOR SLIDE, LOWER FLAP CONTACTED FLOOR AND BROKE OFF THE DOOR AND SLIDE FUNCTIONED NORMALLY.
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