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 FDEA201211264158Seat Track · corrodedBS 1385, "X"= 8.5. SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211264157Seat Track · corrodedBS 1451, "X"= 8.5, SEAT TRACK FOUND CORRODED. REPAIRED AS PER SRM 53- 00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211264160Seat Track · corrodedBS 1641, "X"=-8.5, SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED MAJOR AS IAW GMM 6-2-100 REVISION 115.SDR FDEA201211264159Seat Track · corrodedBS 1884 TO 1887, "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 IPXA2M76316B-Nut · looseDIVERSION - NR 1 ENGINE OIL QUANTITY DECREASED AT APPROX 1 QT IAW 30 MINUTES FOUND LOOSE B-NUT ON OIL PRESSURE TRANSMITTER. RETORQUED AND LEAK CHECKED OK.SDR FDEA201211244147Skin · crackedLT WING L/E LOWER SURFACE ACCESS PANEL 518FB CUT-OUT CORNER FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIG 202, REPAIR 7, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.SDR FDEA201211244146Skin · crackedRT WING L/E FOUND LOWER FIXED PANEL NR 11 SLAT TRACK CUT-OUT SKIN EDGE CORNER CRACKED. REPAIRED IAW SRM 57-40-02, FIGURE 201, REPAIR 7, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211244145Cargo Track · corrodedMAIN DECK CARGO TRACK BS 1827, X= 8.5 FOUND WITH SURFACE CORROSION. CARGO TRACK REPLACEED FROM BS 1791 TO 1887, IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211244144Cargo Track · corrodedMAIN DECK CARGO TRACK BS 1661, X= -8.5 FOUND WITH SURFACE CORROSION. CARGO TRACK REPLACEED FROM BS 1531 TO 1671, IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211244143Cargo Track · corrodedMAIN DECK CARGO TRACK BS 1841, X= -27 FOUND WITH SURFACE CORROSION. CARGO TRACK REPLACED FROM BS 1791 TO 1887, IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211244142Cargo Track · corrodedMAIN DECK CARGO TRACK BS 1541, X= -8.5 FOUND WITH SURFACE CORROSION. CARGOTRACK REPLACED FROM BS 1531 TO 1671, IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.SDR FDEA201211244141Cargo Track · corrodedMAIN DECK CARGO TRACK, BS 1745, X= -27 FOUND WITH SURFACE CORROSION. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.SDR FDEA201211244140Cargo Track · corrodedMAIN DECK CARGO TRACK BS 1541, X= -27 FOUND WITH SURFACE CORROSION. CARGO TRACK REPLACED FROM STATION 1531 TO 1571, IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.SDR FDEA201211244139Skin · crackedLEFT WING NR 11 L/E SLAT TRACK CUT-OUT FOUND CRACKED AT XOS 720. REPAIRED IAW SRM 57-40-02, FIG 201, REPAIR 7, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.SDR FDEA201211244138Skin · crackedRT WING L/E NR 8 SLAT OTBD INNER SKIN FOUND CRACKED. REPAIRED IAW EA 1-5750-165172, PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211244148Battery · inoperativeDURING SERVICE CHECK, FOUND L1 DOOR ESCAPE SLIDE PRESS TO TEST LIGHT NOT ILLUMINATING. GAINED ACCESS TO L1 SLIDE PRESS TO TEST BATTERIES. REPLACED BATTERIES, RESECURED SLIDE COVER, OPS CK GOOD REF AMM 25-61-15-4.SDR FDEA201211234130Cargo Track · damagedMAIN DECK CARGO TRACK AT BS 1092, "X"= 47, FOUND CROWN ELONGATED. CARGO TRACK REPLACED FROM BS 1009 TO 1109, "X"= 47, IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211234129Cargo Track · damagedMAIN DECK CARGO TRACK AT BS 1035, "X"= 47", FOUND CROWN ELONGATED. REPAIRED IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211234136Dadc · failedFIRST OFFICER LOST AIRSPEED INFORMATION DURING TAKEOFF ROLL, SUSPECT DADC FAILURE. AT 300FT AGL, CAPTAIN LOST FLT DIRECTOR CONTROL OF FCP ALT-SELECTOR AIRSPEED SEEMED OK. WHEN F/O SWITCH TO CAPTAIN'S ADC, CAPTAIN'S SIDE GOT FLT DIRECT, AUTO PILOT, AUTO THROTSDR FDEA201211234131Access Panel · corrodedLEFT WING, T/E LOWER ACCESS PANEL NR 541JB CUTOUT FORWARD EDGE LOWER CAP. LOWER SURFACE FOUND CORRODED. CUTOUT FORWARD EDGE LOWER CAP DAMAGED. R & R WITH NEW CAP IAW SRM 51-31-01, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.SDR FDEA201211234128Cargo Track · corrodedMAIN DECK CARGO TRACK AT BS 873, "X"=-8.5", FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211234127Seat Track · corrodedMAIN DECK CARGO TRACK AT BS 873, "X"= 8.5, FOUND WITH CORROSION. REPAIRED IAW SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211234132Web · canningCENTER LANDING GEAR LT KEEL WEB AT BS 1431 OIL CANNING FOUND EXCEED SRM ALLOWABLE LIMITS. REPAIRED IAW EA 1-5310-163532. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211224124Door Frame · crackedCENTER CARGO DOOR, UPPER DOOR FRAME BEAM AT BS 1743, "X" =-106 CRACKED. REPAIRED IAW EA 1-5310-165169. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201211224123Vane · delaminatedLEFT WING, INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED IAW MM 27-50-22-4, REVISION 74.1. ADJUSTMENT CARRIED OUT IAW MM 27-50-22-830-801, REVISION 74.1 AND FOUND SATISFACTORY. FLAP OPS TEST CARRIED OUT IAW MM 27-50-00-860-801, REVISISDR FDEA201211224122Skin · misrepairedSKIN MISREPAIRED AT BS 1846, LONGEON 42 TO 44 RIGHT. REPAIRED IAW EA 1-5330-163536. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211214115Web · crackedRT OBSERVER SEAT, LOWER FLOOR WEB FOUND EDGE CRACKED. REPAIR CARRIED OUT IAW SRM 53-10-51, REPAIR 1, FIGURE 202, REVISION 51. REPAIR PARTS INSTALLED IAW SRM 51-35-01, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 115.SDR FDEA201211214107Frame · crackedFRAME END CAP AT BS 555, NEAR LONGERON 32R, IN AIR CONDITION PACK NR 3 COMPARTMENT, FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-35- 01, REVISION 51.. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 115.SDR FDEA201211194084Hinge Bracket · damagedRIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND EXCEEDED LIMITS AFTER BUSHING REMOVED. REPAIRED PER EA 1-5750-75980 REVISION A PART 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211194097Skin · looseLEFT WING INBD FLAP UPPER SURFACE RIVETS FOUND LOOSE. REPAIRED IAW SRM 57-50-01, FIGURE 201, REPAIR 4, REVISION 51 AND EA 1-5750-163534, STEP 4, PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211194096Skin · looseRIGHT WING INBD FLAP UPPER SURFACE RIVETS FOUND LOOSE. REMOVED AND REPAIRED PER SRM 57-50-01, FIGURE 201, REPAIR 4, REVISION 51 AND EA 1-5750-163535. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 115.SDR FDEA201211194095Hinge Bracket · scratchedLEFT WING INBD FLAP FORWARD HINGE BRACKET PIVOT BORE OTBD SPOT FACE FOUND SCRATCHED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-07, REVISION 74. REPAIR ACCOMPLISHED PER EA 1-5750-162397, PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 1SDR FDEA201211194094Hinge Bracket · corrodedRIGHT WING INBD FLAP, FORWARD HINGE BRACKET PIVOT LUG BORE INBD AND OTBD SPOT FACE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-07 REVISION 74. REPAIR ACCOMPLISHED AS PER EA 1-5750-163542, PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6SDR FDEA201211194092Hinge Bracket · corrodedDURING BUSHING REMOVAL, LEFT WING INBD FLAP, AFT OTBD HINGE BRACKET PIVOT OTBD LUG BORE FOUND CORRODED BEYOND LIMITS. ACCOMPLISHED BUSHING REPAIR PER EA 1-5750-162394 PART 1. REPAIR CLASSIFIED A MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211194091Skin · chafedSKIN CHAFED AT BS 889, LONGERON 40 - 41R. REPAIRED AS PER SRM 53-00-15 FIGURE 202 REPAIR 8 REVISION 51. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201211194090Skin · chafedSKIN CHAFED BS 1009, LONGERON 40 - 41R. REPAIRED AS PER SRM 53-00-15 FIGURE 202 REPAIR 8 REVISION 51. EO 1-5100-7-5001 B2 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201211194085Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BORE FOUND EXCEEDED LIMIT AFTER BUSHING REMOVED. REPAIRED IAW EA 1-5750-75980 REVISION A PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211194082Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD FORWARD HINGE BRACKET SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW CMM 20-10-6 REVISION 74. FOUND ACCEPTABLE IAW EA 1-5750-162398 PART 1. SHIM FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 74. REPAIR CARRIED OUT PER ESDR FDEA201211194089Rib · crackedON REMOVAL OF RT WING NR 8 SLAT, CRACKS WERE FOUND ON RIB AT STATION XOS =1141.2. R & R IAW DWG ARB1954 REV NC AND EA 1-5750-163529, STEP 5 THRU STEP 10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201211194088Rib · crackedON REMOVAL OF RT WING NR 8 SLAT, CRACKS FOUND ON RIB AT STATION XOS =1146.8. REMOVED AND REPLACED AS PER DRAWING ARB1954 REVISION NC AND E.A. 1-5750-163529 STEP 5 THRU STEP 10. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201211194087Rib · crackedON REMOVAL OF RT WING NR 8 SLAT, CRACKS FOUND ON RIB AT STATION XOS =1135.6. REMOVED AND REPLACED IAW DRAWING ARB1954 REVISION NC AND EA 1-5750-163529 STEP 5 THRU STEP 10. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201211194086Rib · crackedON REMOVAL OF RT WING NR 8 SLAT, CRACKS FOUND ON RIB AT STATION XOS =1152.4. REMOVED AND REPLACED IAW DRAWING ARB1955 REVISION D AND EA 1-5750-163529 STEP 5 THRU STEP 10. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201211194083Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET LOWER MOUNT OTBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-08 REVISION 74. REPAIRED IAW EA 1-5750-162398 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211194081Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-09 REVISION 74. REPAIRED IAW EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, 6, 9 AND 10. REPAIR CLASSIFIED AS MAJORSDR FDEA201211194080Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 REVISION 74. REPAIRED IAW EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, 6, 9 AND 10, . WASHER AT OUTBOARD HINSDR FDEA201211194079Fitting · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE BRACKET SIDE LOAD FITTING LOWER BORE SURFACE FOUND CORRODED. REWORKED AS PER CMM 20-10-6 REVISION 74. REPAIRED IAW EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, AND 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION SDR FDEA201211194078Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE LOAD FITTING UPPER BORE SURFACE FOUND CORRODED. REWORKED AS PER CMM 20-10-6 REVISION 74. REPAIRED PER EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, AND 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVSDR FDEA201211194077Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE LOAD FITTING LOWER BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 REVISION 74. REPAIRED PER EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, 7, 9 AND 10. REPAIR CLASSIFIED AS MSDR FDEA201211194076Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE LOAD FITTING UPPER BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITD AS PER CMM 57-44-09 REVISION 74. . REPAIRED PER EA 1-5750-162400 PART 1, STEP 1, 2, 3, 4, 5, 7, 9 AND 10. REPAIR CLASSIFIED AS MASDR FDEA201211194075Hinge Bracket · corrodedRT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET LOWER MOUNT INBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44- 09 REVISION 74. . REPAIRED PER EA 1-5750-162400 PART 1, STEPS 1, 2, 3, 4, 5, 8, 9 AND 10. REPAIR CLASSIFIED AS MAJOR PER
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