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 FDEA201911022825Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE (#10 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZEDSDR FDEA201911022824Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMSDR FDEA201911022823Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FSDR FDEA201911022822Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CSDR FDEA201911022821Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMMSDR FDEA2019113012805Bushing · not reportedWHEN GEAR WAS RETRACTED INITIALLY SHOWED LEFT MAIN GEAR UNSAFE ON BOTH GEAR LIGHT AND CONFIG PAGE. AFTER QRH PROCEDURES, WE THEN HAD LEFT AND RIGHT MAIN GEAR UNSAFE. DURING CRUISE .70 MACH FL340 ONLY RIGHT MAIN GEAR REMAINED UNSAFE. REPALACED LOWER TRASDR IPXA2019110148547Solenoid · inoperativeINSPECTION TYPE:N/A2L DOOR INOP.R&R ED L1 SOLENOID PER AMM 52 10 06 401 DOOR OPERATES NORMAL. OK FOR SERVICE. IPC 52 11 70 01 ITEM 070JSDR IPXA2019112214247Longeron · crackedINSPECTION TYPE:2CAFT CARGO LONGERON 40 R/H IS CRACKED AT STA. 1878.REPAIRED CRACKED LONGERON 40 R/H BETWEEN STA. 1871 TO 1902 IAW VT-SAA EA 011-5310-01-A7941 REV. I/R AND UPS EO MD11-5310-74633-A. (MAJOR)SDR IPXA2019112214244Support Angle · crackedINSPECTION TYPE:2CAFT CARGO SIDEWALL SUPPORT ANGLE IS CRACKED AY STA. 1921 R/H SIDE.REMOVED, FABRICATED AND REPLACED SUPPORT ANGLE IAW DWG. AGA0065 AND SRM 51-35-01.. (MINOR)SDR FDEA2019111932989Web · crackedR/H NLG WHEEL WELL WEB AT STA. 495 HAS A .200 IN. CRACK AT FASTENER HOLE ABOVE HORIZONTAL STIFFENER. (MARKED) REPAIRED RH NLG WHEEL WELL WEB AT STA 495 REF SRM 53-10-13 FIG 201 SH. 8SDR FDEA201911152938Web · crackedL/H NLG WHEEL WELL WEB AT STA. 495 HAS A .200 IN. CRACK AT FASTENER HOLE ABOVE HORIZONTAL STIFFENER. (MARKED) REPAIRED LH NLG WHEEL WELL WEB @ STA 495 REF SRM 53-10-13 FIG 201 SH. 8 'MAJOR REPAIR' JPFSDR FDEA201911152937Skin · crackedL/H LWR WING SKIN AT #16 SLAT TRACK CUT OUT AFT I/B CORNER HAS A .400 IN. CRACK. (MARKED) REPAIR NOTED SKIN CRACK AT SLAT #16 PER SRM 57-40-02-2R REPAIR 7 FIG 201SDR FDEA201911152936Skin · crackedL/H LWR WING SKIN AT #12 SLAT TRACK CUT OUT AFT O/B CORNER HAS A .300 IN. CRACK. (MARKED) REPAIRED NOTED SKIN CRACK AT SLAT TRACK #12 PER SRM 57-40-02-2R REPAIR 7 FIG 201.SDR FDEA201910312795Slide · deployedMDIS 605 52-10 8462 31OCT19 MEM OPEN U L1 DOOR SLIDE DEPLOYED UPON OPENING MEL 31OCT19 08:07 MEM U RELEASED FOR SERVICE PER MEL : 52-10-03-03 CATEGORY : C EXPIRATION : 10NOV19 "MEL 52-10-03-03: L1 CABIN ENTRY SLIDE - INOP EXTENDED OVERWSDR IPXA2019111549029Angle · crackedINSPECTION TYPE:2CCENTER CARGO FLOOR SUPPORT ANGLE IS CRACKED IN 6 PLACES.REMOVED, GFABRICATED AND REPLACED FLOOR SUPPORT ANGLE IAW DWG. AEA0341 AND SRM 51-35-01. (MINOIR)SDR FDEA201910312798Panel · delaminatedLEFT WING UPPER OUTBOARD ISLAND PANEL ARC7201-1 DELAMINATED. REPAIRED DAMGE (DELAMINATED) LEFT WING UPPER OUTBOARD ISLAND PANEL ARC7201-1 PER SRM 57-50-80-2R-0, REPAIR #3 PAGE 39. DRILLING HOLES, PAINTING, AND INSTALLATION WILL BE DONE ON N/R 870.....SDR FDEA201910312794Indication Sys · faultyPDIS 578 28-41 3074 31OCT19 HNL OPEN U LOGPAGES:2605567 APPROX. 2.2 HRS INTO FLIGHT LEVEL 2 FUEL QTY/USED CHK ALERT CAME ON. COMPLIED WITH QRH PROCEDURE FUEL USED CALCULATING FUEL USED HAD FUEL AT 175K. FUEL GAUGES ADDED UP TO 166K. DIFF OF 9SDR FDEA2020040862900Doubler · corrodedRH WING UPPER SURFACE - APPROX XORS 288 AFT SECTION OF LANDING GEAR DOUBLER - CORROSION AROUND FASTENER. REPAIRED PER EA 1-5730-T0350758SDR FDEA2020011600131Web · crackedR/H NLG TRUNNION FITTING WEB AT STA. 590 HAS A .900 IN. CRACK. (MARKED) REPAIRED AS REQUIRED R/H NLG TRUNNION FITTING WEB AT STA 590, PER MD-11 SRM 53-10- 14-2R, FIGURE 202, REPAIR 2, PG 8-10.SDR IPXA2019111879075Bracket · crackedINSPECTION TYPE:2C#1 ENG. O/B T/R FIXED COWL, RIB/ BRACKET IS BROKEN AT FAN AIR VALVE DUCT ATTACH BRACKET.REMOVED AND REPLACED RIB/BRACKET IAW SRM 54-01-42. (MINOR)SDR IPXA2019111328936Skin · corrodedINSPECTION TYPE:2CCENTER WING BOX UPPER SKIN HAS CORROSION AT STR. 15 AND BETWEEN X=46.5 TO X-80.REPAIRED CENTER WING BOX UPPER SKIN AT STR. 15 AND BETWEEN X=46.5 TO X=80 IAW VT-SAA EA 011-5730-01-A7945 REV. I/R AND UPS EO MD11-5730-74604-A. (MINOR)SDR IPXA2019111328934Skin · corrodedINSPECTION TYPE:2CCENTER WING TANK UPPER SKIN HAS CORROSION BETWEEN STA. XCW=101 & XCW=118 AT APPROX. FUSELAGE STA. 1256.REPAIRED CORRODED CENTER WING TANK UPPER SKIN BETWEEN STA. XCW=101 & XCW-118 AT STRINGER 12 IAW VT-SAA EA 011-5730-01-A7944 REV. IR AND UPSSDR FDEA201910302782Stiffener · crackedLANDING GEAR RIGHT HAND MAIN LANDING GEAR WHEEL WELL UNDERWING BARREL TORQUE BOX APPROXIMATELY STA 1441 FORWARD ANGLE STIFFENER FOUND CRACKED APPROXIMATELY 1" RIGHT HAND MAIN LANDING GEAR WHEEL WELL UNDERWING BARREL TORQUE BOX APPROXIMATELY STA 1441 FORWSDR IPXA2019112214246Rib · crackedINSPECTION TYPE:2CR/H W/W AFT CORNER PANEL RIB IS CRACKED.REMOVED, FABRICATED AND REPLACED RIB IAW DWG. ANB7203 AND SRM 51-35-01. (MINOR)SDR IPXA2019111879076Floorbeam · crackedINSPECTION TYPE:2CFWD. CARGO FLOOR BEAM IS CRACKED AT STA. Y=6-70, X=-57.5 AND Z=-98.REPAIRED CRACKED FLOOR BEAM AT STA. Y=6-70, X=-57.5 AND Z=-98 IAW SRM 53-40-51 REPAIR 1 FIG. 202. (MAJOR)SDR IPXA2019111879074Former · crackedINSPECTION TYPE:2CR/H WING FIXED L/E FORMER IS CRACKED AT STA. XOS.558.REMOVED, FABRICATED AND REPLACED FORMER AT STA. XOS=558 IAW DWG ARB1162 AND SRM 51-33-01. (MINOR)SDR IPXA2019111849113Angle · crackedINSPECTION TYPE:2CR/H WING #2 SLAT O/B END UPPER ANGLE IS CRACKED AT AFT END.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. ARB1647 AND SRM 51-31-01 & 51-35-01. (MINOR)SDR FDEA201910292775Skin · chafedLEFT HAND WING - UPPER INBOARD FIXED LEADING EDGE SURFACE BETWEEN XIS 269.9 AND XIS 276.5 FOUND WITH CHAFFING MARK. LEFT HAND WING - UPPER INBOARD FIXED LEADING EDGE SURFACE BETWEEN XIS 269.9 AND XIS 276.5 CHAFFING MARK REPAIRED PER EA 1-5730-T0349969 P1, SDR IPXA2019111549030Stiffener · crackedINSPECTION TYPE:2CL/H MLG W/W AFT SIDE VERTICAL STIFFNER IS CRACKED.REMOVED, FABROICATED AND REPLACED STIFFNER IAW DWG. ANB7230 AND SRM 51-33-01. (MINOR)SDR IPXA2019111549007Former · crackedINSPECTION TYPE:2CR/H WING FIXED L/E FORMER IS CRACKED AT STA. XOS.541.REMOVED, FABRICATED AND REPLACED FORMER IAW DWG. ARB2918 AND SRM 51-31-01. (MOINOR)SDR FDEA201910292776Seat Track · corrodedCABIN - RIGHT HAND STATION 450 - 480 X=-107.25 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND SEAT TRACK STATION 450 TO STATION 480 X = - 107.25 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SDR IPXA2019111148857Stiffener · crackedINSPECTION TYPE:2CR/H W/W CUTOUT AFT SIDE PANEL HAS STIFFNER ANGLE CRACKED.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. ANB7203 AND SRM 51-35-01. (MINOR)SDR IPXA2019111148868Stiffener · crackedINSPECTION TYPE:2CL/H WING FIXED L/E STIFFNER IS CRACKED AT THE I/B FUELING ADAPTER.REMOVED, FABRICATED AND REPLACED ANGLE/STIFFNER IAW DWG. ARB1288AND SRM 51-33-01. (MINOR)SDR FDEA201910292773Seat Track · corrodedCABIN - SEAT TRACK AT STATION 455 TO STATION 475 X = 0 FOUND CORROSION . CABIN AT SEAT TRACK STATION 455 TO STATION 475 X = 0 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REMOVED SDR IPXA2019111148853Door Frame · crackedINSPECTION TYPE:2CCENTER GEAR R/H AFT GEAR DOOR PAN/FRAME IS CRACKED.REMOVED AND REPLACED DOOR PAN/FRAME IAW SRM 51-35-01. (MINOR)SDR IPXA2019103098436Door · unknownINSPECTION TYPE:N/ADFW GROUND CREW REPORTED L1 DOOR WILL NOT CLOSE OR OPENPERFORMED OPERATIONAL TEST OF L1 DOOR IN REF TO MD11 M/M 52-11-02-700-802. OPS CHECKS NORMAL.SDR FDEA201910282768Doubler · wornTAILCONE RH UPPER INTERNAL SKIN IS WORN. INSTALLED REPAIR PER E.A. 1-5340-T0350296 "FUSELAGE-ATTACH FITTINS TAIL CONE UPPER SKIN REPAIR"SDR IPXA2019111328937Skin · corrodedINSPECTION TYPE:2CCENTER WING BOX UPPER SKIN HAS CORROSION AT STR. 3 AND BETWEEN XCW=-101 TO XCW=-110.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT STR 3. AND BETWEEN CXW=-101 AND XCW=-110 IAW VT SAA EA 011-5730-01-A7939 REV. I/R AND UPS EO MD11-5730-74536-SDR FDEA201911152948Tray · corrodedCAC - AREA UNDER BATTERY TRAY HAS SUFACE CORROSION. R AND R REF N/R 1086 AND DWG AAA7086-1 SRM 51-31-01-06SDR IPXA2019111348979Doubler · crackedINSPECTION TYPE:2CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 542 TO XOS. 547.5.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 542 TO XOS. 547.5 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR FDEA201910252747Seat Track · corrodedREWORK : MAIN DECK FLOOR SEAT TRACK FOUND CORROSION AT STATION 1821 X = - 75.25 . MAIN DECK FLOOR AT SEAT TRACK STATION 1821 X = - 75.25 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRASDR FDEA201910252748Seat Track · corrodedREWORK: MAIN DECK FLOOR SEAT TRACK FOUND CORROSION AT STATION 1620 - 1661 , X = 75.25 . MAIN DECK FLOOR AT SEAT TRACK STATION 1620 TO STATION 1661 X = 75.25 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGESDR FDEA201910252745Doubler · crackedLEFT WING LEADING EDGE COMPARTMENT APPROXIMATELY AT STATION XOS 761 , BEADED DOUBLER FOUND WITH CRACKS. LEFT WING LEADING EDGE COMPARTMENT STATION XOS 761 BEADED DOUBLER CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MSDR IPXA2019102868299Door · unwanted deployINSPECTION TYPE:N/ALAV SERVICE COMPANY EMERGENCY DEPLOYED L1 PASSENGER DOOR.RESTORED L1 PASSENGER DOOR TO NORMAL OPERATION. IAW 52-11-04. SERVICED PNEUMATIC STORAGE SYSTEM IAW 12-25-04SDR FDEA201910242742Intercostal · crackedEMPENNAGE LEFT HAND REAR CENTER SPAR TO REAR SPAR INTERCOSTAL FOUND CRACK. EMPENNAGE LEFT HAND REAR CENTER SPAR TO REAR SPAR INTERCOSTAL CARRIED OUT REPAIR AS PER EA #1-5330-T0350369P1. TITLE: STABILIZERS- VERTICAL STABILIZER- REAR CENTER SPAR TO REAR SPARSDR FDEA201910242737Hinge Bracket · corrodedLEFT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR HOLE BORE CORROSION. CORROSION AT LEFT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PSDR FDEA201910242736Hinge Bracket · corrodedLEFT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE CORROSION. CORROSION AT LEFT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PERSDR FDEA201910242740Hinge · corrodedRIGHT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT ASSDR FDEA201910242738Hinge · corrodedRIGHT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PSDR FDEA2019102542744Tail Cone · wornTAILCONE, RH LOWER INTERNAL SKIN HAS WORN GROOVES (15 EA) FROM FASTENERS RIDING CONDITION DOT #10 PERFORMED REPAIR PER EA 1-5352-T0350122
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