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 FDEA2020010970032Rib · crackedRIGHT WING - NUMBER 1 LEADING EDGE SLAT CRUISE PERFORMANCE FILLET RIB FOUND CRACK AT STATION XIS 150.74 RIGHT WING - NO 1 LEADING EDGE SLAT CRUISE PERFORMANCE FILLET CRACKED RIB AT STATION XIS 150.74 CARRIED OUT REPAIR AS PER SRM 57-40-71-2R FIGURE 201 REPSDR IPXA202002051802Mount · gougedINSPECTION TYPE:3CL1 DOOR LOWER AFT SLIDE MOUNT (SUPPORT) IS GOUGED.REMOVED AND REPLACED GOUGED L1 DOOR LOWER AFT SLIDE MOUNT (SUPPORT) IAW MD-11 SRM 51-33-01 & 51-35-01. (MINOR)SDR IPXA2020020315648Stiffener · crackedINSPECTION TYPE:3CLT MLG W/W AFT O/B WALL 3RD VERTICAL STIFFENER FROM FWD IS CRACKED.REMOVED AND REPLACED CRACKED LT MLG W/W AFT O/B WALL 3RD VERTICAL STIFFENER FROM FWD IAW MD-11 SRM 51-35-01. (MINOR)SDR IPXA2020012975473Stringer · crackedINSPECTION TYPE:3CCENTER WING BOX STRINGER # 47 IS CRACKED AT STA. XCW=-17 & XCW=-46.5.REPAIRED CRACKED CENTER WING BOX STRINGER # 47 BETWEEN STA. XCW=-4.25 TO XCW=-58.0 IAW SRM 57-10-03 REPAIR 1 FIG. 201. (MAJOR)SDR IPXA2020012975472Stringer · crackedINSPECTION TYPE:3CCENTER WING BOX STRINGER #45 IS CRACKED AT STA. XCW= -17.REPAIRED CRACKED CENTER WING BOX STRINGER # 45 BETWEEN STA. XCW=-4.25 & XCW=-29.0 IAW SRM 57-10-03 REPAIR 1 FIG. 201. (MAJOR)SDR FDEA2020010970037Doubler · crackedLEFT HAND WING FIXED LEADING EDGE AT STATION XOS 668 BEADED DOUBLER FOUND WITH CRACK LEFT HAND WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 668 CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15 . REPAIR CLASSIFIED AS MAJOR PSDR FDEA2020010970036Doubler · crackedLEFT HAND WING FIXED LEADING EDGE AT STATION XOS 601 BEADED DOUBLER FOUND WITH CRACK LEFT HAND WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 601 CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15 . REPAIR CLASSIFIED AS MAJOR PSDR FDEA2020010970035Doubler · crackedLEFT HAND WING FIXED LEADING EDGE AT STATION XOS 789.6 RIB DOUBLER FOUND WITH CRACK LEFT HAND WING FIXED LEADING EDGE CRACKED RIB DOUBLER AT STATION XOS 789.6 REMOVED AS PER SRM 51-33-01-0G . FABRICATE RIB DOUBLER AS PER DOUGLAS DRAWING # ARB 3954 REV KSDR FDEA2020010970034Doubler · crackedLEFT HAND WING FIXED LEADING EDGE AT STATION XOS 543 BEADED DOUBLER FOUND CRACKED LEFT HAND WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 543 CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15.REPAIR CLASSIFIED AS MAJOR PER GMSDR IPXA2020012251218Intercostal · crackedINSPECTION TYPE:3CFWD CARGO INTERCOSTAL BETWEEN STA 6-30 - 6-50 AND L42L - L43L IS CRACKED AT AFT END.REMOVED AND REPLACED CRACKED FWD CARGO INTERCOSTAL BETWEEN STA 6-30 - 6-50 AND L42L - L43L IAW MD-11 SRM 51-31-01 AND 51-33-01. (MINOR)SDR IPXA2020020551848Floorbeam · crackedINSPECTION TYPE:3CLOWER FWD. CARGO FLOOR BEAM IS CRACKED AT STA. 6-73 AND X=-57.5.REPAIRED CRACKED LOWER FWD. CARGO FLOOR BEAM AT STA. 6-73 AND X=-57.5 IAW VT-SAA EA 011-53140-01-A7985 REV. I/R AND UPS EO MD11-5340-75221-A. (MAJOR)SDR FDEA202001060029Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMMSDR FDEA202001060028Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-SDR FDEA202001060027Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- SDR FDEA202001060026Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 5SDR FDEA202001060025Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- SDR FDEA202001060024Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRISDR IPXA2020020311654Doubler · damagedINSPECTION TYPE:3CLT WING FIXED L/E FWD SPAR DOUBLER HAS A DRILL START AT STA XOS 1177.5.REPAIRED DAMAGED LT WING FIXED L/E FWD SPAR DOUBLER AT STA XOS 1177.5 IAW VT-SAA EA 011-5710-01-A7998 IR AND UPS EO MD11-5710-75384-A. (MAJOR)SDR IPXA2020012751360Fuel Tank · corrodedINSPECTION TYPE:3CCENTER WING TANK UPPER SKIN HAS CORROSION BETWEEN XCW=-99.5 TO XCW= 66.5 AT STRINGER 15.REPAIRED CORRODED CENTER WING TANK UPPER SKIN BETWEEN XCW -99.5 TO XCW 66.5 AT STRINGER 15 IAW VT-SAA EA 011--5730-01-A7979 IR AND UPS EO MD11-5730-75203-SDR IPXA2020012751359Fuel Tank · corrodedINSPECTION TYPE:3CCENTER WING TANK UPPER SKIN HAS CORROSION BETWEEN XCW=-99.5 TO XCW= 66.5 AT STRINGER 15.REPAIRED CORRODED CENTER WING TANK UPPER SKIN BETWEEN XCW -99.5 TO XCW 66.5 AT STRINGER 15 IAW VT-SAA EA 011-5730-01-A7979 IR AND UPS EO MD11-5730-75203-ASDR IPXA2020012751358Fuel Cell · corrodedINSPECTION TYPE:3CCENTER WING TANK UPPER SKIN HAS CORROSION BETWEEN XCW=-99.5 TO XCW= 66.5 AT STRINGER 15.REPAIRED CORRODED CENTER WING TANK UPPER SKIN BETWEEN XCW -99.5 TO XCW 66.5 AT STRINGER 15 IAW VT-SAA EA 011-5730-01-A7979 IR AND UPS EO MD11-5730-75203-ASDR IPXA2020012451332Skin · corrodedINSPECTION TYPE:3CCENTER WING UPPER SKIN HAS CORROSION BETWEEN XCW=100 TO XCW=105 AT STRINGER 17.RERPAIRED CORRODED CENTER WING UPPER SKIN BETWEEN XCW 100 TO XCW 105 AT STRINGER 17 IAW VT-SAA EA 011-5730-01-A7984 REV. IR AND UPS EO MD11-5730-75216-A. (MINOR)SDR IPXA2020020765878Skin · crackedINSPECTION TYPE:3CR/H WING #2 SLAT UPPER O/B SKIN IS CRACKED AT EXISTING REPAIR DOUBLER STA. XIS=328.106.REPAIRED R/H WING #2 SLAT UPPER SKIN AT STA. XIS= 328.106 IAW VT-SAA EA 011-5754-01-A8005 REV. I/R AND UPS EO MD11-5750-75285-A. (MAJOR)SDR IPXA2020012985501Skin · crackedINSPECTION TYPE:3CR/H WING L/E LOWER SKIN IS CRACKED AT THE CORNER AT STA. XOS.=610.844.REPAIRED CRACKED R/H WING L/E LOWER SKIN AT STA. XOS.=610.844 IAW SRM 57-40-01 REPAIR 18 FIG. 201. (MAJOR)SDR IPXA2020012985494Former · crackedINSPECTION TYPE:3CLT WING FIXED L/E HAS A CRACKED ANGLE (FORMER) I/B OF #9 SLAT TRACK AT XOS 584.REMOVED AND REPLACED CRACKED LT WING FIXED L/E ANGLE (FORMER) I/B OF #9 SLAT TRACK AT XOS 584 IAW MD-11 SRM 51-33-01. (MINOR)SDR IPXA2020020321696Skin · gougedINSPECTION TYPE:3C#3 ENG. I/B T/R FIXED INNER BARREL UPPER SKIN IS GOUGED.REPAIRED #3 ENG. I/B T/R IAW VT-SAA EA 011-7830-01-A8004 REV. I/R AND UPS EO MD11-7830-75326-A. (MINOR)SDR IPXA2020012985502Intercostal · crackedINSPECTION TYPE:3CR/H MLG W/W INTERCOSTAL IS CRACKED AT STA. Y=1437AND X=38.5.REMOVED, FABRICATED AND REPLACED INTERCOSTAL AT SAID STA. IAW DWG. AEA0218 AND SRM 51-33-01. (MINOR)SDR IPXA2020020351753Fitting · gougedINSPECTION TYPE:3C#1 ENG. WING PYLON MOUNT I/B SIDE TRUSS FITTING IS GOUGED AT STA. YWN 200, ZWN=23 AND X=2.4.REPAIRED DAMAGED #1 ENG., WING PYLON I/B SIDE TRUSS FITTING AT NOTED LOCATION IAW VT-SAA EA 011-5410-01-A7976 REV. I/R AND UPS EO MD11-5410-75173-A. (SDR IPXA2020012251217Bracket · brokenINSPECTION TYPE:3C, NR 3 ENG. PYLON O/B SIDE OF ENGINE MOUNT FRAME SUPPORT BRACKET IS BROKEN.REMOVED AND REPLACED BROKEN #3 ENG. O/B SIDE OF ENGINE MOUNT FRAME SUPPORT BRACKET IAW MD-11 SRM 54-05-41. (MINOR)SDR IPXA2020012095159Trunnion · crackedINSPECTION TYPE:3CL/H NOSE W/W TRUNNION FITTING IS CRACKED AT STA. Y=582.5, Z=-114 & X=24.REPAIRED CRACKED L/H NOSE W/W TRUNNION FITTING AT STA. Y=582.5, Z=-114 & X=24 IAW SRM 53-10-14 REPAIR 2 FIG. 202. (MAJOR)SDR FDEA202001030008Doubler · corrodedRIGHT HAND WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER FOUND CORROSION AT YW 467. RIGHT HAND WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER AT YW 467 CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 57-20-01-1ASDR FDEA202001030007Doubler · corrodedLEFT HAND WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER FOUND CORROSION AT YW 467. LEFT HAND WIING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER AT YW 467 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 57-20-01-1A ALLOSDR FDEA202001030011Floor Panel · corrodedMAIN CARGO DECK, STA1219 LBL98, CENTER WING UPPER PANEL HAS CORROSION (MARKED) REMOVED FASTENER, REMOVED CORROSION, NDT CHECKED FOR REMAINING MATERIAL THICKNESS & CHECKED THE OPENED HOLE FOR ANY INDICATIONS WITH NO DEFECTS NOTED IN REF TO: EA # 1-5730-T0SDR FDEA202001030016Structure · corrodedUPPER CARGO COMPARTMENT; X=100 Y=1211 UNDER FLOOR UPPER INTERNAL STRUCTURE HAS LEVEL 2/3 CORROSION 1" X 1". DOT #2 REMOVED FASTENERS, BLENDED THE CORROSION WHICH WENT OUT OF LIMITS IN REF TO SRM 57-10-01, FIG 101 SHEETS 1-2. DOUBLER WAS FABRICATED & INSTSDR FDEA202001030015Structure · corrodedMAIN CARGO DECK, STA1231 LBL105, CORROSION ON CENTER WING UPPER PANEL BY OVERWING FUEL TANK (MARKED) REMOVED FASTENERS, REMOVED THE CORROSION, NDT CHECKED FOR MATERIAL LOSS, FOUND TO BE WITHIN ALLOWABLE LIMITS IN REF TO SRM 57-10-01 FIG 101 PAGES 1-2, AREASDR FDEA202001030014Structure · corrodedUPPER CARGO COMPARTMENT; X=98-106 Y=1225-1231 UNDER FLOOR UPPER INTERNAL STRUCTURE HAS LEVEL 2/3 CORROSION 5" X 7". REMOVED FASTENERS, REMOVED THE CORROSION, NDT CHECKED FOR MATERIAL LOSS AFTER BLENDING, HOLES WERE ALSO CHECKED WITH NO DEFECTS NOTED, AREASDR FDEA202001030013Structure · corrodedUPPER CARGO COMPARTMENT; X=58 Y=1227 UNDER FLOOR UPPER INTERNAL STRUCTURE HAS LEVEL 2/3 CORROSION 1" X 1". DOT #5 REMOVED FASTENERS, REMOVED CORROSION, NDT CHECKED FOR THE REMAINING MATERIAL THICKNESS, OPEN HOLES WAS ALSO CHECKED WITH NO DEFECTS NOTED, ARESDR FDEA202001030012Structure · corrodedUPPER CARGO COMPARTMENT; X=86 Y=1228 UNDER FLOOR UPPER INTERNAL STRUCTURE HAS LEVEL 2/3 CORROSION 1" X 1". DOT #3 REMOVED FASTENERS, REMOVED CORROSION, NDT CHECKED FOR THE REMAINING MATERIAL THICKNESS, OPEN HOLES WAS ALSO CHECKED WITH NO INDICATIONS NOTED,SDR FDEA202001030010Actuator · malfunctionedDURING APPROACH TO KMEM, WITH AUTOPILOT ENGAGED AND AIRCRAFT FULLY CONFIGURED, AIRPLANE BEGAN A SIGNIFICANT RHYTHMIC PULSING WITH CORRESPONDING YOKE MOVEMENT. WENT AROUND TO TROUBLESHOOT & PULSING STOPPED. FULLY CONFIGURED EARLY WITH NO PULSING. PASSING 1200' SDR FDEA202001030009Structure · corrodedMAIN CARGO DECK, STA1200 LBL106 CORROSION AROUND THE FASTENER (MARKED) REMOVED FASTENER, REMOVED THE CORROSION, NDT CHECKED THE REMAINING MATERIAL THICKNESS AND ALSO CHECKED THE OPENED HOLE FOR ANY INDICATIONS, FOUND NO DEFECTS, AREA WAS TREATED, PRIMED, FSDR IPXA2020011765980Doubler · crackedINSPECTION TYPE:3CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS= 610.8-616.6.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA XOS-= 610.8-616.6 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR IPXA2020011751012Doubler · crackedINSPECTION TYPE:3CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.= 636-643.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS.= 636-643 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR IPXA2020011751011Doubler · crackedINSPECTION TYPE:3CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.=625-629.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS.=625-629 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR IPXA2020010315551Skin · crackedFUSELAGE SKIN CRACK AT RH SIDE PACK DOOR UPPER AFT AREA. CORRECTIVE ACTION: REPAIRED IAW E.O. MD11-5330-75031-A. THIS IS A MAJOR REPAIR.SDR FDEA2019123183323Panel · corrodedMAIN CARGO DECK, STA1319 LBL105, CENTER WING UPPER PANEL ANGLE TO FUEL TANK HAS CORROSION (MARKED) REMOVED FASTENERS, REMOVED CORROSION, NDT CHECKED THE MATERIAL LOSS AND FOUND THE ALL AREAS WERE WITHIN ALLOWABLE LIMITS PER SRM 57-10-01-1A FIG 101, HOLESSDR FDEA2019123183321Panel · corrodedMAIN CARGO DECK, STA1890 LBL110, CENTER WING UPPER PANEL HAS CORROSION (MARKED) CORRECTION: STA # IS: STA 1296 @ LBL110 - REMOVED FASTENERS, REMOVED CORROSION, NDT CHECKED FOR MATERIAL LOSS AND FOUND AREA TO BE WITHIN ALLOWABLE LIMITS PER SRM 57-10-01-1ASDR FDEA2019123183320Panel · corrodedMAIN CARGO DECK, STA1393 LBL105 TO LBL111, CENTER WING UPPER PANEL HAS CORROSION (MARKED) CORRECTION: STA # IS: STA 1299LBL105 TO LBL 111 - REMOVED FASTENERS, REMOVED CORROSION, NDT CHECKED FOR MATERIAL LOSS AND FOUND TO BE WITHIN ALLOWABLE LIMITS PER SSDR FDEA2019123183319Panel · corrodedMAIN CARGO DECK, STA1321 LBL108, CENTER WING UPPER PANEL HAS CORROSION (MARKED) REMOVED FASTENERS, REMOVED CORROSION, NDT CHECKED FOR THE REMAINING THICKNESS, FOUND TO BE WITHIN ALLOWABLE LIMITS, HOLES WERE ALSO CHECKED AND NO DEFECT WERE NOTED. AREA WAS SDR FDEA2019123183318Panel · corrodedMAIN CARGO DECK, STA1361 LBL107, CENTER WING UPPER PANEL HAS CORROSION (MARKED) REMOVED FASTENERS, REMOVED CORROSION, NDT CHECKED FOR REMAINING MATERIAL THICKNESS AND FOUND AREA TO BE WITHIN ALLOWABLE LIMITS PER SRM 57-10-01-1A FIG 101, OPEN HOLES WERE ALSDR FDEA2019123183317Panel · corrodedMAIN CARGO DECK, STA1346 LBL108, CENTER WING UPPER PANEL HAS CORROSION (MARKED) REMOVED FASTENERS, REMOVED CORROSION, NDT WAS CALLED OUT TO DO A REMAINING THICKNESS CHECK, FOUND AREA TO BE WITHIN ALLOWABLE LIMITS OF SRM 57-10-01-1A FIG 101 & INSPECTED AL
Back to Boeing MD-11F