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 IPXA2021011964650Skin · chafedINSPECTION TYPE: 3C EXTERIOR FUSELAGE SKIN HAS CHAFE DAMAGE AT STA 1150 AND LONG 44 RT. REPAIRED CHAFED EXTERIOR FUSELAGE SKIN AT STA 1150 AND LONG 44 RT, IAW SRM 53-40-01 REPAIR 3 FIG 201. (MAJOR)SDR IPXA2021011964649Skin · chafedINSPECTION TYPE: 3C EXTERIOR FUSELAGE HAS CHAFE DAMAGE AT STA 1150 AND LONG 44LT. REPAIRED CHAFED EXTERIOR FUSELAGE SKIN AT STA 1150 AND LONG 44 LT, IAW SRM 53-40-01 REPAIR 2 FIG 201. (MAJOR)SDR IPXA2021011964618Cap · crackedINSPECTION TYPE: 3C RT UNDERWING CANTED PANEL CAP IS CRACKED AT STA 1236.8 AND Z= -100. REPAIRED CRACKED RT UNDERWING CANTED PANEL CAP AT STA 1236.8 AND Z= -100, IAW UPS EO MD11-5310-78819-A. (MAJOR)SDR IPXA2021011964616Skin · crackedINSPECTION TYPE: 3C LT WING FIXED LEADING EDGE LOWER SKIN IS CRACKED AT STA XOS 891. REPAIRED CRACKED LT WING FIXED LEADING EDGE LOWER SKIN AT STA XOS 891, IAW SRM 57-40-02 REPAIR 7 FIG 201. (MAJOR)SDR IPXA2021011964613Doubler · crackedINSPECTION TYPE: 3C LT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 661.7 TO 667.67. REPAIRED CRACKED LT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 661.7 TO 667.67, IAW SRM 57-40-02 REPAIR 15 FIG 203. (MAJOR)SDR IPXA2021011964612Doubler · crackedINSPECTION TYPE: 3C LT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 768.2 TO 772.85. REPAIRED CRACKED LT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 768.2 TO 772.85, IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)SDR IPXA2021011964610Doubler · crackedINSPECTION TYPE: 3C LT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 789.6 TO 795.7. REPAIRED CRACKED LT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 789.6 TO 795.7, IAW SRM 57-40-02 TREPAIR 15 FIG 205. (MAJOR)SDR IPXA2021011964607Doubler · crackedINSPECTION TYPE: 3C LT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 555.5 TO 559.4. REPAIRED CRACKED LT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 555.5 TO 559.4, IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)SDR IPXA2021011964655Skin · chafedINSPECTION TYPE: C3 TAILCONE FWD RT LEADING EDGE SKIN IS CHAFED BETWEEN UPPER GUIDE PIN AND FLOOR. REPAIRED TAILCONE CHAFED SKIN AT FWD RT LEADING EDGE, IAW SRM 51-35-01 AND 51-31-01 (MINOR).SDR IPXA2021011964654Skin · chafedINSPECTION TYPE: C3 TAILCONE FWD LOWER LEADING EDGE INNER SKIN CHAFED FROM X=20"LT TO X=44". REPAIRED TAILCONE CHAFED FWD LOWER LEADING EDGE SKIN, IAW SRM 51-35-01 AND 51-35-02 (MINOR).SDR FDEA202012183222Support · corrodedAFT CARGO COMPARTMENT: CORROSION UNDER AND AROUND HOLES FOR LOWER SIDEWALL ATTACH POINTS (BOTTOM OF PANEL) BETWEEN APPROXIMATELY STA 1900-1921, MARKED AND DOT 19. REMOVED & INSTALLED FABRICATED FLOOR SUPPORT AGA 3857, PER DWG AGA 3857 & SRM 51-35-01.SDR FDEA202012183186Sensor · making metalAFTER TAKEOFF PASSING 1000', 5 IN SUCCESSION LOUD BANGS WITH HEAVY SHUTTERS. ENGINE INDICATIONS APPEARED NORMAL AND THERE WAS NO YAW ASSOCIATED WITH THE BANG/SHUTTERING. DURING NR 2 ENGINE INLET AND EXHAUST INSPECTION FOUND LEFT HAND FAN STATOR AFT INNER SEGSDR FDEA202012183184Hmu · failedON TAKEOFF, JUST AFTER LIFTOFF WITH LANDING GEAR IN TRANSIT, HEARD 3 LOUD BANGS AND FELT A LATERAL MOVEMENT. ALL 3 ENGINES APPEARED NORMAL DURING EVENT. WORK PERFORMED PER TSI 72-00/5074.PERFORMED BSI AND NO DEFECT NOTED.REPLASDR IPXA2021012965039Splice Strap · crackedINSPECTION TYPE: 3C RT WING FIXED LEADING EDGE COMP. SPLICE STRAP IS CRACKED AT STA XOS 889. REMOVED, FABRICATED AND REPLACED SPLICE STRAP, IAW DWG ARB3954 AND SRM 51-33-01. (MINOR)SDR IPXA2021012364794Doubler · crackedINSPECTION TYPE: 3C RT WING FIXED LEADING EDGE SKIN SPLICE DOUBLER AT STA XOS 667 IS CRACKED. REMOVED AND REPLACED CRACKED RT WING FIXED LEADING EDGE SKIN SPLICE DOUBLER AT STA XOS 667, IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)SDR IPXA2021012264747Skin · crackedINSPECTION TYPE: 3C RT WING FIXED LEADING EDGE SKIN IS CRACKED AT STA XOS 610.844 INBOARD FWD CORNER OF REFUELLING ACCESS DOOR. REPAIRED CRACKED RT WING FIXED LEADING EDGE SKIN AT STA XOS 610.844 INBOARD FWD CORNER OF REFUELLING DOOR, IAW MD-11 SRM 57-40-01 RSDR IPXA2021011964634Intercostal · crackedINSPECTION TYPE: C3 NR 3 A/C COMPARTMENT INTERCOSTAL CRACK AT STA 595 LON 33R. REMOVED AND REPLACED CRACKED INTERCOSTAL AT NR 3 A/C COMPARTMENT, IAW DWG ACA3804 AND SRM 51-35-01. (MINOR)SDR IPXA2021011964633Stiffener · crackedINSPECTION TYPE: C3 RT WING FIXED LEADING EDGE STIFFENER SUPPORT CRACK AT XOS STA 1005. REMOVED AND REPLACED CRACKED STIFFENER SUPPORT AT RT WING LEADING EDGE, IAW SRM 51-31-01 AND 51-33-01. (MINOR)SDR IPXA2021011964625Attach Angle · damagedINSPECTION TYPE: C3 NR 3 PYLON AFT FAIRING FWD ATTACH ANGLE HAS ELONGATED HOLE. REMOVED AND REPLACED NR 3 PYLON FWD ATTACH ANGLE AT AFT FAIRING, IAW DWG AUB7517 AND SRM 54-01-42. (MINOR)SDR IPXA2021011964611Doubler · crackedINSPECTION TYPE: 3C RT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA, XOS 746.9 TO 753.0. REPAIRED CRACKED RT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 746.9 TO 753.0, IAW SRM 57-40-02 REPAIR 15 BFIG 205. (MAJOR)SDR IPXA2021011964608Doubler · crackedINSPECTION TYPE: 3C RT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 883.7 TO 887.9. REPAIRED CRACKED RT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 883.7 TO 887.9, IAW SRM 57-40-02 REPAIR 16 FIG 205. (MAJOR)SDR IPXA2021011964606Doubler · crackedINSPECTION TYPE: 3C RT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 636.8 TO 643.5. REPAIRED CRACKED RT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 636.8 TO 643.5, IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)SDR IPXA2021011964605Doubler · crackedINSPECTION TYPE: 3C RT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 855.9 TO 861.8. REPAIRED CRACKED RT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 855.9 TO 861.8, IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)SDR IPXA2021011964652Former · crackedINSPECTION TYPE: C3 RT WING FIXED LEADING EDGE RIB (FORMER) CRACK AT STA 584. REMOVED, FABRICATED AND REPLACED CRACKED FORMER, IAW DWG ARB 2931 AND SRM 51-33-01 (MINOR).SDR FDEA202012173175Doubler · crackedFUSELAGE: CENTER LANDING GEAR WHEEL WELL, RIGHT HAND BULKHEAD FORWARD DOUBLER APPROXIMATELY AT STATION 1381, X= -31.50, FLIGHT CONTROL ROD FEED THROUGH POSITION FOUND CRACKED. FUSELAGE CENTER LANDING GEAR WHEEL WELL RIGHT HAND BULKHEAD FORWARD CRACKED DOUBLSDR FDEA202012173174Doubler · crackedFUSELAGE: CENTER LANDING GEAR WHEEL WELL, LEFT HAND BULKHEAD FORWARD DOUBLER APPROXIMATELY AT STATION 1381, X=31.50, FLIGHT CONTROL ROD FEED THROUGH POSITION FOUND CRACKED. FUSELAGE CENTER LANDING GEAR WHEEL WELL LEFT HAND BULKHEAD FORWARD CRACKED DOUBLER APPSDR FDEA202012173178Longeron · crackedFUSELAGE: DURING NOSE LANDING GEAR LEFT HAND TRUNNION FITTING REPAIR, FOUND LONGERON 49 LEFT HAND CRACKED AT STATION Y=595. NOSE LANDING GEAR LEFT HAND STATION Y=595 TRUNNION FITTING CRACKED LONGERON 49 LEFT HAND. REMOVED AND REPLACED, AS PER MD-11 SRM 51-33SDR FDEA202012173177Longeron · crackedFUSELAGE: DURING NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING REPAIR, FOUND LONGERON 49 RIGHT HAND CRACKED AT STATION Y=595. NOSE LANDING GEAR RIGHT HAND STATION Y=595 TRUNNION FITTING CRACKED LONGERON 49 RIGHT HAND. REMOVED AND REPLACED, AS PER MD-11 SRM 5SDR FDEA202012173173Seat Track · crackedCABIN-UNDER SIDE OF SEAT TRACK FROM STATION 939 TO STATION 979, X=8.5 FOUND CRACK. CABIN-AT STATION 939 TO STATION 979, X=8.5 CRACKED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 929 TO EXISTING SPLICE STATION 989 X=8.5, AS PER SRM 5SDR IPXA2020122163636Anti-Ice Valve · warning messageINSPECTION TYPE: N/A DIVERSION ON CLIMBOUT THROUGH 10000 FT HAD LEVEL 2 TAIL A/I DISAG COMBINED WITH LEVEL 1 AIR SYS OFF, AIR SYS OFF CAME UP FIRST THEN THE DISAGREE. RAN QRH PROCEDURES AND DEPARTED ICING. DEFERRED TAIL ANTI ICE VALVE, PER MEL 30-11-1-2. ACSDR IPXA2020121763520Solenoid · inoperativeCREW DOOR LEFT SIDE ELECTRIC DOOR SWITCH INTERMITTENT BOTH IN CABIN AND EXTERIOR SWITCHES INTERMITTENT. DEFERRAL ISSUED, PER MD11 MEL 52-10-3-1-2-1-2 PLACARDS INSTALLED DMI LOG UPDATED. REPLACED L1 DOOR LOCK PIN RELEASE SOLENOID, PER MM 52-10-06, FUNCTIONAL SDR FDEA202012173179Light · no testPDIS 619 25-60 8081. 17DEC20 AFW OPEN U LOGPAGES:3366007. L1 RAFT LIGHT ON DOOR WILL NOT TEST. CANCEL, N/A SDR ENTERED IN ERROR.SDR FDEA201812063450Control Panel · inoperativeREMOVED EMERGENCY LIGHT PANEL FROM OVER L1 DOOR IAW AMM 25-23-23-5. REPAIRED SLIDE PANEL IAW AMM 20-20-03-2. PANEL READY FOR INSTALLATION. REINSTALLED EMRGENCY LIGHT PANEL IAW AMM 25-23-23.SDR FDEA2020121602511Floor Panel · damagedMAIN CABIN FLOOR PANEL 242GF CHAFFING DAMAGE TO UPPER FACE SHEET OF FLOORBOARD. REPLACED PANEL 242GF WITH NEW FLOORBOARD PER DWG SRZ-25-005.SDR FDEA202012160233Floor Panel · damagedMAIN CABIN FLOOR PANEL 242CF CHAFFING DAMAGE TO UPPER FACE SHEET OF FLOOR BOARD. REMOVED AND REPLACED DAMAGED FLOORBOARD 242CF IAW MM 53-21-09-04 FIG 201 AND MM 53-21-06-4.SDR IPXA2021011964636Pan · crackedINSPECTION TYPE: C3 CLG LT FWD DOOR FWD PAN (FRAME) CRACK. REMOVED AND REPLACED CLG LT FWD DOOR CRACKED PAN (FRAME), IAW DWG SE10520012 AND SRM 51-35-01 (MINOR).SDR IPXA2021011964628Intercostal · crackedINSPECTION TYPE: C3 LT MLG WHEEL WELL UPPER BRAKE ACCUMULATOR INTERCOSTAL CRACK. REMOVED AND REPALCED CRACKED INTERCOSTAL AT LT MLG WHEEL WELL BRAKE ACCUMULATOR, IAW SRM 51-33-01 AND DWG AEA0218 (MINOR).SDR FDEA202012150012Skin · crackedRT WING SKIN LOWER ACCESS PANEL CUT OUT (636AB) HAS 3 EA HOLES (NR 15, 33 AND 34) WITH A CRACK INDICATION, MARKED. 3 EA HOLE REAMED AND BUSHED ON LT WING SKIN LOWER ACCESS PANEL, PER SRM 57-20-02 2R REPAIR 5 AND EA: T1-5730-T0358788.SDR FDEA202012150011Skin · crackedLT WING SKIN LOWER ACCESS PANEL CUT OUT (536AB) HAS 1 EA HOLE (NR 7) WITH A CRACK INDICATION, MARKED. 1 EA HOLE REAMED AND BUSHED ON LT WING SKIN LOWER ACCESS PANEL, PER SRM 57-20-02-2R REPAIR 5 AND EA: T1-5730-T0358788.SDR FDEA202012153160Longeron Splice · crackedFORWARD CARGO COMPARTMENT-LONGITUDINAL SPLICE AT STATION 6-0, LONGERON 39 LEFT FOUND CRACK. FORWARD CARGO COMPARTMENT AT STATION 6-0, CRACKED LONGERON 39 LEFT SPLICE. REMOVED AND REPLACED, AS PER SRM 51-33-01-0G. SPLICE FABRICATED BY MACHINING, AS PER DOUGLSDR FDEA202012153156Floor Panel · delaminatedCABIN, FLOOR PANEL NUMBER 231FF FOUND DELAMINATED STATION 595-STA 675. DELAMINATED FLOOR PANEL NUMBER 231FF AT CABIN STATION 595-STATION 675 REMOVED, AS PER AMM 53-21-01-4. FLOOR PANEL NUMBER 231FF FABRICATED, AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FABSDR FDEA202012153161Seat Track · corrodedFORWARD CABIN LEFT HAND SEAT TRACK STATION 430 TO STATION 450, X=85.5 FOUND WITH CORROSION. FORWARD CABIN AT LEFT HAND SEAT TRACK STATION 430 TO STATION 450, X=85.5, CORROSION EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101SDR FDEA202012143209Fuel Tank · corrodedMAIN CABIN, CTR TANK, UPPER SKIN HAS SURFACE CORROSION AT STA. 1229 APPROX. RBL 8. 0000721523 : COLON, LUIS R - 03-FEB-2021 19:30 REPAIRED CORROSION ON CTR TANK UPPER SKIN AT STA 1229 RBL 8 REF E .A.#:1-5730-T0358819 CENTER TANK UPPER SKIN CORROSION. SDR FDEA202012143208Fuel Tank · corrodedMAIN CABIN, CTR TANK, UPPER SKIN HAS SURFACE CORROSION AT STA 1229 APPROXIMATELY RBL 16. REPAIRED CORROSION ON CTR TANK UPPER SKIN AT STA 1229 RBL 16 REF EA # 1-5730- T0358819 CENTER TANK UPPER SKIN CORROSION MAJOR REPAIRSDR FDEA202012143136Longeron Splice · crackedCENTER CARGO COMPARTMENT STATION 5-113 TO 1541 RIGHT HAND LONGERON 39 SPLICE END SUSPECT CRACK, CENTER CARGO COMPARTMENT AT STATION 5-113 TO STATION 1541 RIGHT HAND LONGERON 39. CRACKED SPLICE REMOVED AND REPLACED, AS PER SRM 51-33-01-0G. SPLICE FABRICATED BSDR FDEA202012133135Fitting · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013, PER DRAWING NUMBER SN10550000 REVSION C ON RIGHT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISTING EXISTING CRACK INDICATION FOSDR FDEA202012133134Fitting · crackedFUSELAGE: NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING SUSPECTED CRACK. CRACKED NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING AT STATION Y=595 REPAIRED, AS PER SRM 53-10-14-2R REPAIR 2 FIGURE 202. INITIAL INSPECTION TO BE CARRIED OUT AT 1500 FLIGHT CYCLES SDR FDEA202012133133Fitting · crackedFUSELAGE: NOSE LANDING GEAR LEFT HAND TRUNNION FITTING SUSPECTED CRACK. CRACKED NOSE LANDING GEAR LEFT HAND TRUNNION FITTING AT STATION Y=595 REPAIRED, AS PER SRM 53-10-14-2R REPAIR 2 FIGURE 202. INITIAL INSPECTION TO BE CARRIED OUT AT 1500 FLIGHT CYCLES ANDSDR FDEA202012123128Skin · crackedLEFT HAND WING LEADING EDGE LOWER SURFACE NR 15 SLAT TRACK CUTOUT APPROXIMATELY STATION XOS 994 SKIN FOUND CRACK. LEFT HAND WING LEADING EDGE LOWER SURFACE NR 15 SLAT TRACK CUTOUT APPROXIMATELY STATION XOS 994 SKIN REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R RSDR FDEA202012123127Doubler · crackedRIGHT HAND LEADING EDGE FUEL VALVE PANEL CUTOUT DOUBLER AT STATION XOS 906 FOUND CRACKED. RIGHT HAND LEADING EDGE FUEL VALVE PANEL CUTOUT CRACKED DOUBLER AT STATION XOS 906 REPAIR CARRIED OUT, AS PER SRM 57-40-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS
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