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 FDEA201211194093Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE OTBD SPOT FACE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 74. EXISTING THICKNESS: 0.263", MATERIAL REMOVED: 0.078", REMAINING THICKNESS: 0.185", MINIMUM THICKNESS: 0.SDR FDEA201211184070Landing Gear · unknownLANDING GEAR DID NOT CYCLE TO GREEN INDICATION. RECYCLED NORMAL GEAR EXTENSION: GREEN. GEAR HANDLE RESISTANCE STIFF, PERFORMED A GENERAL VISUAL INSPECTION OF ALL GEAR DOORS AND ALL LANDING GEAR, ALL FIND NORMAL IAW SMP CLEANED AND INSPECT LANDING GEAR CONTRSDR FDEA201211174062Bracket · corrodedLEFT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 REVISION 74. EXISTING HOLE DIAMETER = 1.224 INCH, FINAL HOLE DIAMETER = 1.228 INCH, MAXIMUM HOLE DIAMETER = 1.220 INCH. RSDR FDEA201211174065Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 REVISION 74. REPAIRED PER EA 1-5750-163540 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211174064Hinge Bracket · corrodedLT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 REVISION 74. REPAIRED PER EA 1-5750-163540 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211174063Bracket · corrodedLT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BORE FOUND CORROSION. FOUND EXCEEDED LIMIT AS PER MD-11 CMM 57-44-09 REVISION 74. EXISTING HOLE DIAMETER = 1.223 INCH, FINAL HOLE DIAMETER = 1.226 INCH, MAXIMUM HOLE DIAMETER = 1.220 ISDR FDEA201211174061Longeron · crackedX-RAY INSPECTION FOUND CRACKED INDICATION APPROX 2" IN LENGTH AT CABIN, STATION 5-123, LONGERON 3 LT AFT SECTION EDGE. REPAIRED AS PER SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 51. NEW LONGERON SEGMENT FABRICATED AS PER DRAWING AFA7771 REVISION C AND INSTSDR WRNA201200015Control Unit · malfunctionedWHILE IN FLIGHT, LEVEL 2 "GEN BUS 3 FAULT" ILLUMINATED. DEPLOYED ADG AND RETURNED TO FIELD (MIA) FOR SAFE LANDING. REPLACED EPCU IAW AMM 24-08-01, GROUND RUN ENGINES, NO DEFECTS NOTED. STOWED ADG IAW AMM 24-25-01. AIRCRAFT RETURNED TO SERVICE.SDR WRNA201200014Engine · bird ingestionAFTER TAKEOFF FROM SUMU, HAD HIGH VIBRATION NR 3 ENGINE. DUMPED FUEL TO MAX LANDING WEIGHT AND RETURNED TO FIELD FOR A SAFE LANDING. AFTER LANDING ENGINE NR 3 WAS SHUT DOWN AS PRECAUTION. ON POST FLIGHT INSPECTION, FOUND 6 DAMAGED FAN BLADES WITH EVIDENCE OSDR FDEA201211164055Skin · misrepairedLT WING NR 2 SLAT INNER SKIN AT XIS 275 MISREPAIRED. REPAIRED PER SRM 57-40-01 FIGURE 201 REPAIR 1 REVISION 51 AND EA 1-5750-163553. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201211164052Skin · misrepairedLT WING INBD FLAP UPPER SURFACE CENTER BOX BETWEEN XIFH 281 AND XIFH 288 MISREPAIRED. REPAIRED IAW SRM 57-00-01 FIGURE 201 SHEET 2 REPAIR 1 REVISION 51 AND EA 1-5750-163534 STEP 2 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201211164051Vane · delaminatedRT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 74.1. ADJUSTMENT AND TEST CARRIED OUT PER AMM 27-50-00-5 REVISION 74.1 FOUND SATISFACTORY. REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211164050Skin · misrepairedLT WING INBD FLAP LOWER SURFACE LOWER SKIN BETWEEN XIFH 269 AND XIFH 288 MISREPAIRED. REPAIRED IAW SRM 57-50-01 FIGURE 201 REPAIR 1 REVISION 51 AND EA 1-5750-163534 STEP 11 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201211164049Skin · misrepairedLT WING INBD FLAP UPPER SURFACE LOWER SKIN BETWEEN XIFH 269 AND XIFH 293 MISREPAIRED. REPAIRED IAW SRM 57-00-01 FIGURE 201 REPAIR 2 REVISION 51 AND E.A. 1-5750-163534 STEP 7 PART 1.SDR FDEA201211164047Seat Track · corrodedBS 1890, X = -3 SEAT TRACK FOUND CORRODED. R & R IW SRM 51-31-01, REV 51. SEAT TRACK FABRICATED IAW DWG AGA7080 REVISION S. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201211164046Seat Track · corrodedLEFT BS 1890, X = 3 SEAT TRACK FOUND CORRODED.SDR FDEA201211154033Frame · misrepairedFRAME MISREPAIRED AT CABIN LT BS 535, 9G NET LOWER SUPPORT YOKE AT LONGERON 24 LT. CARRIED OUT REPAIR IAW SRM 53-20-07, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 115.SDR FDEA201211154032Frame · misrepairedFRAME MISREPAIRED AT CABIN LT BS 535, 9G NET UPPER SUPPORT YOKE AT LONGERON 18 LT. REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 51. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 115.SDR FDEA201211154031Skin · crackedRT WING NR 8 SLAT LOWER SURFACE FOUND CRACKED. REPAIRED IAW SRM 57-40-01, FIG 201 REPAIR 3, REV 51 AND EA 1-5750-163529. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201211154030Skin · misrepairedLT WING NR 3 SLAT ASSY UPPER SKIN XOS 429.446 MISREPAIRED. REPAIRED IAW EA 1-5750-163527. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 115.SDR FDEA201211154037Support Fitting · damagedLEFT WING NR 8 L/E SLAT INBD SUPPORT FITTING FWD HOLE OTBD SIDE SURFACE FOUND STEPPED. SUPPORT FITTING REMOVED AND REPLACED IAW SRM 51-31-01, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GENERAL MM 6-2-100, REV 115.SDR FDEA201211154023Union · leakingAT 118 INTO FLIGHT AT FL 320 GOT LVL 1 "HYD 3 ELEV OFF" ALERT. FLUID LEVEL IN NR 3 WAS 4.3 GALS AND STARTED DECREASING AT A RATE OF .1 GAL EVERY 3 MINUTES. WHEN 3.5 WAS REACHED;, TURNED HYD SYSTEM TO MANUAL AND TURNED OFF HYD 3 LT AND RT PUMPS AND ALSO THESDR FDEA201211144010Seat Track · corrodedBS 1351 'X' = 8.5 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201211144012Seat Track · corrodedBS 1611 'X' = 8.5 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211144011Seat Track · corrodedBS 1805 'X' = -8.5 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211144009Seat Track · corrodedBS 1611 'X' = -8.5 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211144006Support Fitting · chafedLEFT WING NR 8 L/E SLAT, INBD SUPPORT FITTING, AFT HOLE, BOTH SIDES SURFACES FOUND CHAFED. FOUND DURING LT OTBD SLAT DRIVE CABLES TENSION CHECK. SUPPORT FITTING REMOVED IAW STRUCTURAL REPAIR MANUAL 51-31-01 REV 50. HOLES PICKED UP ON NEW SUPPORT FITTING IAW SSDR FDEA201211103935Idg · inoperativeRAN NR 3 ENG FOR IDG DISCONNECT IDG CAME APART DURING RUN. ENGINE NR 3 FIRE INDICATION IN FLIGHTDECK AND 1EA FIRE BOTTLE DISCHARGED, AFTER FURTHER INSPECTION IDG FOUND CRACKED AND INSPECTION ON WIRING AND GEARBOX INWORK. R & R IDG, AIR/OIL HEAT EXCHANGER FLUSDR FDEA201211093918Skin · crackedLEFT WING INBD FLAP UPPER SKIN PANEL ASSY CRACKED AT XIFH 171.3. REPAIRED IAW SRM 57-00-01 REPAIR 1 FIGURE 201 REVISION 50 AND EA 1-5750-163526SDR FDEA201211093915Seat Track · corrodedMAIN DECK SEAT TRACK CLIP NUT HOLE AT BS 5-55, "X" = -107.25 FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 50. REPAIR PARTS FABRICATED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 50. REPAIR PARTS INSTALLED IAW SRM 53-00-52, FIG 201, REPAIR SDR FDEA201211083909Splice · crackedCENTER LANDING GEAR WHEEL WELL RT UPPER FORWARD SPLICE JOINT FOUND CRACKED. SPLICE REMOVED AND REPLACED WITH WITH NEW SPLICE IAW SRM 51-33-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211083908Slat Track · crackedRT WING L/E NR 10 SLAT TRACK CUT OUT INBD CORNER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02 FIGURE 201, REPAIR 7, REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211083907Doubler · crackedLEFT WING L/E COMPARTMENT BEADED DOUBLER AT XOS 666 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02 FIGURE 203, REPAIR 15, TYPE A, REVISION 50. REPAIR CLASSIFIED AS MAJOR GMM REVISION 115.SDR FDEA201211073896Seat Track · corrodedMAIN DECK SEAT TRACK BS 1372, "X" = -8.5 FOUND CORRODED. SEAT TRACK REMOVED IAW SRM 53-00-52, FIG 201. REPAIR 1, REV 50. NEW SEAT TRACK SEGMENT REWORKED IAW SRM 53-00-52, FIG 201, REPAIR 1 REV 50. NEW SEAT TRACK SEGMENT INSTALLED IAW SRM 53-00-52, FIG 201, RESDR FDEA201211073895Seat Track · corrodedMAIN DECK SEAT TRACK BS 1861, "X" = -27.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201 REPAIR 5, REV 50. REPAIR PARTS FABRICATED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 50. REPAIR PARTS INSTALLED IAW SRM 53-00-52, FIG 201, REPAIR 5, REV 50. REPAIR CLASDR FDEA201211073892Frame · dentedDENT FOUND FRAME AT BS 1741, L11R. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211073891Frame · dentedDENT FOUND AT RT SIDE FRAME AT BS 1761, NEAR L11R. REPAIRED IAW SRM 53-00-07 FIGURE 201, REPAIR 2, REVISION 50. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100 REVISION 115.SDR FDEA201211073890Frame · dentedDENT FOUND ON RT SIDE OF CABIN FUSELAGE FRAME AT BS 1641, NEAR L11R. REPAIR CARRIED OUT IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211063867Door Frame · crackedUPPER CENTER CARGO DOOR FRAME, BS 1743 BETWEEN LONGERON 28 - 29R, "X" = 106 FOUND CRACKED. APPROX 1.25" IN LENGTH. REPAIRED IAW EA 1-5310-163524. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211063863Spar Cap · crackedRT WING T/E REAR SPAR LOWER CAP XORS 433 FOUND CRACKED. REMOVED AND REPLACED WITH NEW SILL AS PER SRM 51-34-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211063865Vane · delaminatedRT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 74. FLAP VANE ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REVISION 74. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211063878Longeron Splice · crackedCENTER CARGO BAY BS 5-123, L44L LONGERON SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7116 REVISION D. RESDR FDEA201211063877Longeron Splice · crackedCENTER CARGO BAY BS 5-123 L45R LONGERON SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7116 REVISION D. RESDR FDEA201211063876Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS 683.4 AND XORS 713.6. FOUND CRACK INDICATIONS AT FASTENER HOLES. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 50. REPAIR CLASSIFIED AS MASDR FDEA201211063874Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS 683.4 AND 713.6. FOUND CRACKED INDICATION AT FASTENER HOLES. FASTENER HOLES CRACKED AT RIGHT WING LOWER SKIN ACCESS DOOR COUTOUT REPAIRED IAW SRM 5SDR FDEA201211063872Longeron Splice · crackedCENTER CARGO BAY BS 5-123, L46L LONGERON SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7114 REVISION J. REPASDR FDEA201211063871Longeron Splice · crackedCENTER CARGO BAY BS 5-123, L41L LONGERON SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7115 REVISION D. RSDR FDEA201211063870Longeron Splice · crackedCENTER CARGO BS BS 5-123, LONGERON 40L LONGEORN SPLICE FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7114 REVISIONSDR FDEA201211063869Longeron Fitting · crackedCENTER CARGO COMPARTMENT BS 5-123, LONGERON 44 RT SPLICE FITTING FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7114SDR FDEA201211063868Longeron Splice · crackedCENTER CARGO COMPARTMENT BS 5-123, LONGERON 37 RT SPLICE FITTING FOUND CRACKED. LONGERON SPLICE REMOVED AS PER SRM 51-31-01 REVISION 50 AND INSTALLED WITH NEW FABRICATED SPLICE AS PER SRM 51-33-01 REVISION 50. SPLICE FABRICATED IAW DRAWING A5A7114 REVISION J.
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