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 IPXA2020092460590Floor Support · corrodedINSPECTION TYPE: 2C FLOOR PANEL SUPPORT IS CORRODED BETWEEN STA 392-440 AND X= -8.5 TO X= -27.5. REMOVED, FABRICATED, AND REPLACED FLOOR SUPPORT, IAW DWG WSP0668 AND SRM 51-33-01. (MINOR)SDR IPXA2020092360558Fitting · migratedINSPECTION TYPE: 2C LT OUTBOARD ELEVATOR NR 6 MOUNT FITTING OUTBOARD BUSHING IS MIGRATED. REPAIRED LT OUTBOARD ELEVATOR NR 6 MOUNT FITTING OUTBOARD BUSHING BORE, IAW VT-SAA EA 011-5510-01-A8560 REV IR AND UPS EO MD11-5520-77927-A. (MINOR)SDR IPXA2020091416100Handle · inoperativeINSPECTION TYPE: N/A ATB AFTER TO COULD NOT RAISE THE GEAR HANDLE, IAW THE CHECKLIST TRIED TO RAISE WITH HANDLE REC BUTTON DEPRESSED STILL COULD NOT RAISE. DUMPED 69 FUEL AND LANDED AT PANC. BLEED LT MAIN TRIM CYCL, IAW AMM 32-37-01 PER FIM 32-30-23-00. GOUSDR 9WGA2020091105301Engine · power lossTANK 2 PUMPS OFF DURING CRUISE, FOLLOWED BY ENG 2 RPM LOW. SELECTED MAN AND RELIT ENGINE.SDR IPXA2020092860728Channel · corrodedINSPECTION TYPE: 2C CENTER CARGO LOADING SYSTEM CHANNEL HAS CORROSION BETWEEN STA 1571 TO 1611 AND X= -33. REPAIRED CORRODED CENTER CARGO LOADING SYSTEN CHANNEL BETWEEN STA 1571 TO 1611 AND X= -33, IAW UPS EO MD11-2550-77908-A. MAJOR.SDR FDEA202009092155Seat Track · corrodedCABIN - LEFT HAND STATION 6-12 X = 27.5 SEAT TRACK FOUND CORROSION AS MARKED . CABIN LEFT HAND STATION 6-12 X=27.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BSDR IPXA2020092460582Intercostal · crackedINSPECTION TYPE: 2C LOWER FWD CARGO BETWEEN STA 6-30 TO 6-50 & ABOVE L43L INTERCOSTAL IS CRACKED. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL, IAW DWG ACA7049 AND SRM 51-33-01.SDR IPXA2020092260511Intercostal · crackedINSPECTION TYPE: 2C LOWER FWD CARGO BETWEEN STA 6-30 TO 6-50 ABOVE L43R, INTERCOSTAL IS CRACKED IN 3 PLACES. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG ACA7049 AND SRM 51-33-01 MINOR.SDR FDEA202009092154Seat Track · wornCABIN RIGHT STATION 1421 X= -8.5 SEAT TRACK CROWN FOUND WORN, AS MARKED. CABIN RIGHT HAND STATION 1421 X= - 8.5 SEAT TRACK CROWN WORN AREA SMOOTHED OUT AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. WORN SEAT TRACK REPAIRED SDR IPXA2020092460589Floorbeam · crackedLOWER FWD. CARGO FLOOR BEAM IS CRACKED AT STA. 6-70 ABOVE LONG. 43R.REPAIRED CRACKED FLOOR BEAM AT STA. 6-70 ABOVE LONG. 43R ISW SRM 53-40-51 REPAIR 1 FIG. 202. (MAJOR)SDR IPXA2020092660639Tee Fitting · corrodedINSPECTION TYPE: 2C LT WING TRAILING EDGE "T" ANGLE HAS CORROSION AROUND FASTENER HOLES FWD OF INBOARD AILERON. REPAIRED LT WING TRAILING EDGE "T" ANGLE (CAP) CORROSION FWD OF INBOARD AILERON, IAW MD-11 SRM 57-50-02 REPAIR 9, FIGURE 201. MAJOR.SDR IPXA2020092460584Support Beam · crackedINSPECTION TYPE: 2C LT WING OUTBOARD FLAP AFT HINGE FAIRING OUTBOARD SUPPORT BEAM IS CRACKED. REMOVED, FABRICATED, AND REPLACED BEAM, IAW DWG ARC2149 AND SRM 51-35-01 & 51-33-01. (MINOR)SDR IPXA2020092460581Rib · chafedINSPECTION TYPE: 2C NR 1 PYLON LOWER AFT FAIRING V-RIB IS CHAFED AND DAMAGED. REMOVED AND REPLACED V-RIB, IAW SRM 51-33-01 & 51-35-01. (MINOR)SDR IPXA2020092360557Beam · crackedINSPECTION TYPE: 2C LT WING OUTBOARD FLAP AFT HINGE FAIRING INBOARD SUPPORT BEAM IS CRACKED. REMOVED AND REPLACED CRACKED LT WING OUTBOARD FLAP AFT HINGE FAIRING INBOARD SUPPORT BEAM, IAW MD-11 SRM 51-33-01, 51-35-01 AND 51-35-02. (MINOR)SDR IPXA2020092260512Skin · damagedINSPECTION TYPE: 2C LT WING NR 3 SLAT LOWER SKIN HAS DEEP CHAFE DAMAGE. REMOVED AND REPLACED LT WING NR 3 SLAT ON NRC 432092.SDR IPXA2020092260509Beam · damagedINSPECTION TYPE: 2C AFT EXTENDED TAIL CONE LOWER HORZ. BEAM IS DAMAGED. REMOVED, FABRICATED AND REPLACED BEAM IAW DWG AKC7602 AND SRM 51-35-01, MINOR.SDR IPXA2020092160469Doubler · chafedINSPECTION TYPE: 2C LT UNDER WING FUSELAGE SKIN HAS CHAFE DAMAGE AT STA 1153 AND LONG 43L. REMOVED, FABRICATED, AND REPLACED DAMAGED DOUBLER AT STA 1153 AND LONG 43L, IAW SRM 53-40-01 REPAIR 2 FIG 202 (MAJOR).SDR IPXA2020091860357Doubler · crackedINSPECTION TYPE: 2C LT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA XOS 625 TO 629. REPAIRED CRACKED LT WING FIXED L/E BEADED DOUBLER BETWEEN STA XOS 625 TO 629, IAW SRM 57-40-02 REPAIR 15 FIG. 205 (MAJOR).SDR FDEA202009082143Seat Track · corrodedCABIN, LEFT STATION 1551 X=8.5 SEAT TRACK FOUND CORROSION. CABIN LEFT HAND STATION 1551 X=8.5 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 TRACK RSDR FDEA202009082142Seat Track · corrodedCABIN, LEFT STATION 1530 X=8.5 SEAT TRACK FOUND CORROSION. CABIN LEFT HAND STATION 1530 X=8.5 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 TRACKSDR FDEA202009082141Roller Tray · corrodedFUSELAGE-GENERAL-SPLICE REPAIR CARGO COMP ROLLER TRAY-REPAIR COMPLY WITH E.A. 1-5300-T0356398 REV NO. POS. P1, INFO 08SEP20 06:21. ATTACHED TO WORK ORDER 00078083, FACT 08SEP20 06:31, MEM U. COMPLIED WITH EA NR 1-5300-T0356398 PT1 SPLICE REPAIR CARGO COMP RSDR IPXA2020092460583Stiffener · crackedINSPECTION TYPE: 2C 2164 BULKHEAD (AFT SIDE) LOWER HORIZ STIFFNER BEAM IS CRACKED ON THE RIGHT SIDE. REMOVED, FABRICATED, AND REPLACED STIFFNER/BEAM, IAW DWG. AJC7001 AND SRM 51-31-01 & 51-35-01. (MINOR)SDR IPXA2020091660314Tee Fitting · crackedINSPECTION TYPE: 2C MAIN CABIN TEE ANGLE IS CRACKED AT STA 1341 AND LONG 15L. REMOVED, FABRICATED, AND REPLACED TEE ANGLE, IAW DWG AEA7568 AND SRM 51-33-01 (MINOR).SDR IPXA2020091660313Tee Fitting · crackedINSPECTION TYPE: 2C MAIN CABIN TEE ANGLE IS CRACKED AT STA 1341 AND LONG 15R. REMOVED, FABRICATED, AND REPLACED TEE ANGLE, IAW DWG AEA7568 AND SRM 51-33-01.SDR IPXA2020091660291Web · crackedINSPECTION TYPE: 2C L-3 DOOR JAMB LOWER AFT WEB IS CRACKED AT STA 1307 AND Z= -18. REPAIRED CRACKED L-3 DOOR JAMB LOWER AFT WEB AT STA 1307 AND Z= -18, IAW SRM 53-40-15 REPAIR 3 FIG. 201 (MAJOR).SDR IPXA202009160271Frame · chafedINSPECTION TYPE: 2CA FT EXTENDED TAIL CONE LT FRAME AT UPPER GUIDE PIN LOCATION PIN WORE INTO FRAME. REPAIRED LT FRAME ON TAIL CONE AT STA 2165.062 AROUND UPPER GUIDE PIN, IAW SRM 53-80-07 REP 1 FIG 201 (MINOR).SDR IPXA2020090859970Actuator · warning messageATB, LANDED W/O INCIDENT, UPON SLAT RETRACTION RECEIVED A LEVEL 2 "AIL DEFLECT DISAG". RAN QRH PROCEDURE, DID NOT CORRECT PROBLEM. R & R LEFT INBOARD AILERON DEFLECTION ACTUATOR PER AMM 27-16-01. OPS TESTS GOOD PER AMM 27-16-00-700-801, ALL INDICATIONS NORMASDR IPXA2020092360556Angle · crackedINSPECTION TYPE: 2C RT MAIN LANDING GEAR WHEEL WELL VERTICAL ANGLE AT AFT OUTBOARD WALL IS CRACKED. REMOVED AND REPLACED CRACKED RT MAIN LANDING GEAR WHEEL WELL VERTICAL ANGLE AT AFT OUTBOARD WALL, IAW MD-11 SRM 51-33-01. (MINOR)SDR IPXA2020092260510Stiffener · crackedINSPECTION TYPE: 2C RT MLG W/W OUTBOARD SIDE SECOND VERTICAL FROM FWD END IS CRACKED. REMOVED, FABRICATED, AND REPLACED STIFFNER, IAW DWG ANB7203 AND SRM 51-35-01, MINOR.SDR FDEA202009042099Brake · brokenMDIS 596, 32-43, 5023, 04SEP20, MEM, FACT U. NR 5 BRAKE IS COMING APART. FACT 04SEP20 09:42, MEM. REMOVED AND REPLACED NR 5 MLG BRAKE ASSEMBLY, REF AMM 32-43-20-4. A/C OK FOR SERVICE AT THIS TIME.SDR FDEA202009042098Brake · damagedMDIS 596, 32-43, 5024, 04SEP20, MEM, FACT U. NR 6 BRAKE IS COMING APART. FACT, 04SEP20 09:24, MEM. R & R NR 6 BRAKE, REF AMM 32-43-20-4. A/C OK FOR SERVICE.SDR IPXA2020090219764Tee Fitting · crackedINSPECTION TYPE: 2C MAIN CABIN LONGERON 15L TEE ANGLE CRACKED AT STA.1341. FABRICATED AND INSTALLED MAIN CABIN LONGERON 15L TEE ANGLE AT STA. 1341 IAW SRM 51-31-01 AND 51-33-01. (MINOR)SDR IPXA2020090219762Tee Fitting · crackedINSPECTION TYPE: 2C MAIN CABIN LONGERON 15R TEE ANGLE CRACKED AT STA. 1341. FABRICATED AND INSTALLED MAIN CABIN LONGERON 15R TEE ANGLE AT STA.1341 IAW SRM 51-31-01 AND 51-33-01. (MINOR).SDR IPXA2020090219761Tee Fitting · crackedINSPECTION TYPE:2C MAIN CABIN LONGERON 15R TEE ANGLE IS CRACKED AT STA. 1219. FABRICATED AND INSTALLED MAIN CABIN TEE ANGLE AT LONGERON 15R STA.1219 IAW SRM 51-33-01 AND 51-31-01. (MINOR)SDR IPXA2020091436160Former · crackedINSPECTION TYPE: 2C LT OUTBOARD FLAP INBOARD HINGE FRAME, FORMER IS CRACKED. REMOVED, FABRICATED, AND REPLACED FORMER, IAW DWG ARC 0547 AND SRM 51-31-01 (MINOR).SDR IPXA2020083159651Skin · crackedINSPECTION TYPE:2C LT WING LOWER SKIN ACCESS DOOR 536AB CUT-OUT 1 EA FASTENER HOLE CRACK.REPAIRED LT WING CRACKED LOWER SKIN ACCESS DOOR 536AB CUT-OUT IEA FASTENER HOLE IAW SRM 57-20-02 REPAIR 5 (MINOR).SDR IPXA2020083159650Skin · crackedINSPECTION TYPE:2C RT WING ACCESS DOOR 636AB LOWER SKIN CUT-OUT FASTENER HOLE HAS 5 EA CRACKS. REPAIRED RT WING ACCESS DOOR 636AB SKIN CUT-OUT FASTENER HOLES IAW SRM 57-20-02 REPAIR 5 (MINOR).SDR IPXA2020091436174Doubler · wornINSPECTION TYPE: 2C TAIL CONE INTERNAL DOUBLER AT FWD LOWER END HAS DEEP CHAFE WEAR FROM LBL-40 TO RBL-40 Y=2163. REPAIRED CHAFED INNER DOUBLER AND REPLACED 2 EA SPLICE ANGLES ON TAIL CONE AT Y=2163 BETWEEN LBL-40 AND RBL-40, IAW EA 011-5350-01-A8544 AND EO MSDR IPXA2020091196046Channel · chafedINSPECTION TYPE: 2C TAIL CONE PLATFORM LOWER CHANNEL CHAFED JUST FWD OF LT LADDER MOUNT FITTING. REMOVED CHAFED CHANNEL, FABRICATED AND INSTALLED ON TAILCONE PLATFORM, IAW DWG AKC7546 (MINOR).SDR FDEA202008282052Seat Track · corrodedFORWARD CABIN RT SEAT TRACK STATION 430 TO STATION 450 , X = - 85.5 FOUND WITH CORROSION. CORROSION EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REMOVED AND REPLACED WITH NEW SEAT TRSDR FDEA202008282051Seat Track · crackedCABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CRACKED AT STATION 1217 , X = - 75.25. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1169 TO EXISTING SPLICE STATION 1269, X= -75.25, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFSDR FDEA202008272042Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CSDR FDEA202008272041Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMMSDR FDEA202008272040Hinge Fitting · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING - 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 FABRSDR FDEA202008272039Lug · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMSDR FDEA202008272038Lug · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM SDR IPXA2020082859582Sensor · out of adjustINSPECTION TYPE: NA**EMERGENCY DECLARED AS PRECAUTION. NO EQUIPMENT NEEDED**. DURING CLIMB OUT RECEIVED LEVEL 2 "SLAT DISAG" ALERT AND STICK SHAKER. FOLLOWING SLAT DISAG CHECKLIST WITH FLAPS/SLATS UP/RET, ALERT EXTINGUISHED. FOUND RT LEADING EDGE SLAT SENSSDR FDEA202008272036Hinge 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 WITHIN LIMIT AS PER MD-11 CMM 57-52-03. REPASDR FDEA202008262029Frame · dentedCABIN - MAIN DECK UPON REMOVAL OF UPPER SIDEWALL LINER FOR INSPECTION ACCESS ( WORK CARD T1-5310-71733 A P2I ) FOUND FRAME DENTED AT STATION 1601 , LONGERON 12 LEFT . CABIN - MAIN DECK CARGO COMPARTMENT , DENTED FRAME AT STATION 1601 , LONGERON 12 LEFT SDR IPXA2020101061147Doubler · crackedINSPECTION TYPE: 2C RT MLG DOOR INNER LOWER FWD CORNER DOUBLER CRACKED AT RADUIS. REMOVED CRACKED DOUBLER AND INSTALLED NEW CORNER ASSEMBLYY AT RT MLG DOOR LOWER FWD CORNER, IAW SRM 51-31-01 (MINOR).
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