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 FDEA202005120921Cotter Pin · missingDURING C-11 CHECK WORKCARD 55C0204-02 FOUND ALL 4EA. LOWER AFT RUDDER TIE RODS MISSING SAFETY COTTER PINS AND NUTS WERE NOT TORQUED. GENERATED NON-ROUTINES N00829, N00830, N00831, N00832 GENERATED MSR REPORT. COMPLIED WITH N00829, N00830, N00831, N00832SDR FDEA2020051820952Floorboard · delaminatedL/H MAIN CARGO DECK STA 1039 X= 107.25 FOUND FLOOR BOARD AREA DELAM, RED MARK. FABRICATED NEW FLOOR PANEL, MAIN DECK LEFT HAND SIDE STATION 1039 LBL107 IN REF TO FEDEX DWG SRZ-25-005.SDR FDEA2020051320928Wire · pulledSHORTLY AFTER T.O KIND RCVD LEVEL 1 ALERT "TAT PROB HEAT" FOLLWED QRH PROCEDURES AND DISCOVERED THE ASSOCIATED CIRCUIT BREAKER "POPPED". FOUND RED WIRE B608-3-20 PULLED OUT OF CONTACT #3 ON CONNECTOR P1-1032. REPLACED CONNECTOR SOCKET PER SMP. TAT PROBE SDR FDEA2020051320926Seal · damagedON CLIMB OUT OF KIND R'CVD LEVEL ONE ALERT"AIR SYS 1 OFF". FOLLOWED QRH PROCEDURES. INSTALLED NEW SEAL ON I/B SIDE OF ARROW COUPLING REPOSITIONED COUPLING LEAK CHECKED GOOD, REF AMM 36-14-05-2. ACCOMPLISHED PNEU SYS #1 DECAY CHECK REF AMM SDR FDEA2020051320921Cotter Pin · missingDURING C-11 CHECK WORKCARD 55C0204-02 FOUND ALL 4EA. LOWER AFT RUDDER TIE RODS MISSING SAFETY COTTER PINS AND NUTS WERE NOT TORQUED. GENERATED NON-ROUTINES N00829, N00830, N00831, N00832SDR FDEA2020051310920Frame · crackedRIGHTWING OUTBOARD FLAP, INBOARD HINGE FWD FAIRING FRAME IS CRACKED IN HALF A AND HAS ELONGATED RIVET HOLES. MARKED #58. REMOVED AND REPLACED FAIRING FRAME ON RH WING, OB FLAP INBD HINGE PANEL #635 BR PER DAC BLUE PRINT ARCO504.SDR FDEA202005110917Floor Support · crackedFUSELAGE : FORWARD AVIONICS COMPARTMENT MAIN DECK FLOOR SUPPORT APPOXIMATELY STATION 392 TO STATION 401 X = 30 FOUND CRACKED . FUSELAGE : FORWARD AVIONIC COMPARTMENT , CRACKED MAIN DECK FLOOR SUPPORT AT APPROXIMATELY STATION 392 TO STATION 401 X = 30 , RESDR 9WGA20200511001Warning System · activatedBLEED AIR TEMP ANNUNCIATED. COMPLETED LEVEL 3 CHECKLISTSDR FDEA2020051890961Door · bentDURING WALKAROUND , FOUND BULK CARGO DOOR BENT . MAJOR SHEETMETAL REPAIR PERFORMED PER EA 1-5200-T0354075SDR FDEA202005080913Light · inoperativeL1 EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST LIGHT INOP. RELEASED FOR SERVICE PER MEL : 25-61-02 CATEGORY : C EXPIRATION : 18MAY20 MEL 25-61-02: L1 EVAC SLIDE REMOTE PRESS INDICATOR - INOP. PER MEL 25-61-02, VERIFY AND RECORD IN THE AML, EVAC SLIDE SYSDR IPXA2020051155180Windshield · crackedINSPECTION TYPE:N/AAT 25K ON CLIMBOUT THE F/O WINDSCREEN CRACKED FROM BOTTOM RIGHT MOVING LEFT WHEN I TURNED ON WINDSHIELD ANTI ICE SAW THE ORIGIN POINT SPARKING AND SHUT IT OFF THEN 20 SEC LATER WINDSCREEN SPIDER WEB CRACKED.R&R F/O PANEL ASSEMBLY WINDSHIELD SDR FDEA2020060571129Bracket · crackedCENTER WING LWR FUSELAGE BARREL STRUCT, CRACK ON ATTACH BRACKET AT STA 1278, RT CANTED PANEL. REPLACED CTR WING LWR FUSELAGE BARREL STRUCT, ATTACH BRACKET AT STA 1278 RT REF DAC DRAWING NR AYB7035 AND SRM 51-31-01-0G.SDR FDEA202006051122Spar Cap · corrodedLEFT WING REAR SPAR UPPER CAP, AFT FLANGE UPPER SURFACE HAS CORROSION AT STA XORS 1041. REPAIRED PER EA 1-5710-T0354319 WINGS, BASIC WING STRUCTURE, LT WING REAR SPAR, UPPER CAP, CORROSION AT XORS1042.SDR IPXA2020052645687Skin · dentedINSPECTION TYPE:2CLT WING I/B FLAP LOWER SURFACE HAS A DENT 10.2" FROM T/E AND 44" FROM O/B EDGE REQUIRES PERMANENT REPAIR.REPAIRED LT WING I/B FLAP DENT ON LOWER SURFACE BETWEEN XIFH 261 - 269 IAW VT-SAA EA 011-5750-01-A8177 REV IR AND UPS EO MD11-5750-76600-SDR IPXA2020050655007Battery · dischargedINSPECTION TYPE:N/A** SUPPLEMENTAL SDR ** WHEN TESTING THE L1 SLIDE PRESSURE WITH PUSH TO TEST, THE LIGHT DID NOT ILLUMINATE. ASSINGED TO M 706406 PER MEL 25 61 2 VERIFIED PRESSURE PER DMP.REPLACED REMOTE PRESSURE INDICATOR BATTERIES PERMM 25-61-04-000-801. SYSDR FDEA202005041614Balance Weight · corrodedVERTICAL STABILIZER, UPPER RUDDER MID WEIGHT HAS CORROSION ON INTERNAL AFT SECTION. REMOVED AND REPLACED MID SPAN WEIGHT, IAW EA 1-5540-T0355282 PART 1.SDR FDEA2020072304614Counterweight · corrodedVERTICAL STABILIZER; UPPER RUDDER MID WEIGHT HAS CORROSION ON INTERNAL AFT SECTION. DOT #11 REMOVED AND REPLACED MID SPAN WEIGHT IAW E.A. 1-5540-T0355282 PART 1SDR FDEA2020070841454Longeron · corrodedAFT CARGO AT APPROX STA 1956 RBL 45 LONGERON/STRINGER EXFOLIATED (MARKED) REPAIRED LONGERON AGA7038-501 PER EA # 1-5310-T0354242 .SDR FDEA2020070641057Skin · corrodedAFT CARGO WASTE TANK AT APPROX STA 2000 & LBL 46 LWR INTERIOR SURFACE SKIN AREA EXFOLIATED. REPAIRED PER EA 1-5330-T0354479 TITLED: FUSELAGE - PLATES AND SKINS - AFT BODY KEEL PLANK P/N AJC 7164-503 - CORROSION BETWEEN BS 1997 AND BS 2005 AND BETWEEN L-44L ANSDR FDEA2020062540892Warning System · false activationARRIVED AT AIRCRAFT WITH EMER LIGHT SELECTED ON. AFTER RETURNING SWITCH TO NORMAL AND RUNNING EMER LIGHT TEST, EMER 1 BAT LO ANNUNCIATED TROUBLESHOT AND TESTED THE EMERGENCY LIGHTING SYSTEM. TESTS PASSED. AIRCRAFT OK FOR SERVICE.SDR FDEA2020061041157Support Bracket · corrodedAFT CARGO AT APPROX STA 1956 & RBL 44 LONGERON SUPPORT BRACKET HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED LONGERON SUPPORT BRACKET USING FABRICATED PART REF DAC DRAWING NR NGA6713 AND SRM 51- 31-01-0G.SDR FDEA2020060341116Floorbeam · corrodedCENTER CARGO COMPARTMENT, CORROSION ON FRAME, ON BOTTOM SIDE OF THE FLOOR SUPPORT, AT STA 1781 LBL 46 (MARKED NR 8). COMPLETED REPAIR ON FLOORBEAM STA 1781 LBL 46 PER EA 1-5300-T0354162. TITLE, FUSELAGE, GENERAL CORROSION ON FLOORBEAM STA 1781 UPPER CHORD TASDR FDEA2020052941058Seat Track · corrodedAFT CARGO AT APPROX STA 1841 RT SEAT TRACK FWD AREA HAS MINOR SURFACE CORROSION, MARKED. REPLACED SEAT TRACK AT AFT CARGO BETWEEN STA 1841 TO 1942 IAW DAC DRAWING NR AGA 3855 AND SRM 51-31-01-0G.SDR FDEA2020052941057Skin · corrodedAFT CARGO WASTE TANK AT APPROX STA 2000 & LBL 46 LWR INTERIOR SURFACE SKIN AREA EXFOLIATED, MARKED.SDR FDEA2020052641039Floorbeam · corrodedAFT CARGO AT APPROX STA 1842 FLOORBEAM ON TOP SECTION HAS MINOR SURAFCE CORROSION AT APPROX RBL 50 (MARKED). REMOVED AND REPLACED FLOORBEAM TOP SECTION ( ANGLE SUPPORT ) AT STA APPROX 1842 WITH A NEW PART REF SRM 51-31-01-0G AND DAC DRAWING AGA7170.SDR IPXA2020052055524Seat Track · crackedINSPECTION TYPE:2CMAIN CABIN SEAT TRACK IS CRACKED AND CORRODED AT STA 890 AND X=27.5.REPAIRED CRACKED/CORRODED MAIN CABIN SEAT TRACK AT STA 890 AND X=27.5 IAW MD-11 SRM 53-00-52, REPAIR 1, FIGURE 201. (MAJOR)SDR FDEA202005040886Attach Fitting · corrodedRIGHT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "F" FOUND MOUNT HOLES CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "F" REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED ECCENTRIC BUSHING FABRICSDR FDEA2020070831459Doubler · crackedLT LOWER WING AT ACCESS PANEL AT STA XORS 683.4 TO 713.6 EXISTING REPAIR INTERNAL DOUBLER HAS A .050 INCH CRACK AT HOLE 29 AND .150 IN. CRACK AT HOLE 30. REMOVED AND REPLACED DAMAGED INTERNAL DOUBLER IAW SRM 57-20-02-22 FIG 201 REPAIR 1 SHEET 1.SDR FDEA2020051830879Spar · crackedULTRASONIC INSPECTION FOUND CRACK INDICATION ON LOWER VERTICAL STABILIZER # 4 BANJO FITTING LEFT HAND SIDE FORWARD FLANGE REPAIR AREA AND UNABLE TO DETERMINE THE CRACK LENGTH DUE TO REPAIR BLOCKAGE AT APPROXIMATE STATION Y = 2164 EXISTING CRACK FOUND DURSDR FDEA2020051830878Beam · damagedAGING AIRCRAFT - EXISTING REPAIR AT AFT CARGO STATION 1841 BEAM WEB RIGHT HAND X = -0 TO -13 EXISTING REPAIR AT AFT CARGO STATION 1841 BEAM WEB RIGHT HAND X=-0 TO X=-13 FOUND WEB DAMAGED. REPAIR CARRIED OUT AT AFT CARGO STATION 1841, X=-0 TO X=-17 AS PER SSDR FDEA202005130929Skin · crackedRIGHT WING LEADING EDGE SLAT TRACK #2 CUT OUT HAS A CRACK MARKED #55 TRIMMED OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER AT #3 SLAT RH WING LE PER SRM 57-40-02,FIG 202.SDR FDEA2020050430879Fitting · crackedULTRASONIC INSPECTION FOUND CRACK INDICATION ON LOWER VERTICAL STABILIZER #4 BANJO FITTING LEFT HAND SIDE FORWARD FLANGE REPAIR AREA AND UNABLE TO DETERMINE THE CRACK LENGTH DUE TO REPAIR BLOCKAGE AT APPROXIMATELY STATION Y = 2164SDR FDEA2020062300876Mount · damagedDURING CLIMB OUT RECEIVED A WEATHER FAIL ALERT. SWITCHED TO SYSTEM 1 AND AFTER APPROXYMATELY 3 MINUTES, RECEIVED WEATHER FAIL ALERT FOR THE SECOND WEATHER SYSTEM. SYSTEM 2 WOULD NOT COME BACK. SYSTEM 1 INTERMITTENTLY CAME BACK, THEN FAILED AGAIN. ON APPROACSDR IPXA2020062256771Skin · gougedINSPECTION TYPE:3C WHILE INSTALLING THE LEFT MAIN LANDING GEAR FIXED BRACE ASSEMBLY, GEAR STAND DOOR OPENED AND CONTACTED THE LEFT I/B FLAP LOWER SKIN. REPAIRED GOUGED LT I/B FLAP LOWER SKIN BETWEEN XIFH 190 AND XIFH 213.05 IAW EA 011-5750-01-A8184 AND EO MD1SDR FDEA202005021130Frame · gougedFORWARD AVIONICS’ COMPARTMENT, APPROX STA 449, UNDER RAM AIR DUCTING FOR ACM NR 1 (REF BOOT), 1 SCREW NOT SEATED AND 1 SCREW HAS WORN INTO FRAME RADIUS AT FWD INBD POSITION. DAMAGE TRIMMED OUT AND FRAME REPAIRED. REF SRM53-00-07-2R REPAIR NR 2 FIG 201 SHEETSDR IPXA2020052255569Doubler · crackedINSPECTION TYPE:2CLT WING FIXED L/E SKIN BEADED DOUBLER CRACK REPAIR BETWEEN STA XOS 763.6879 - 768.2704 REQUIRES PERMANENT REPAIR.REPAIRED CRACKED LT WING FIXED L/E BEADED DOUBLER BETWEEN STA XOS 763.6879 - 768.2704 IAW MD-11 SRM 57-40-02, REPAIR 15, FIGURE 2SDR IPXA2020052055522Doubler · crackedINSPECTION TYPE:2CLT WING FIXED L/E SKIN BEADED DOUBLER BETWEEN STA XOS 633 TO 636 REQUIRES PERMANENT REPAIR.REPAIRED CRACKED LT WING FIXED L/E SKIN BEADED DOUBLER BETWEEN STA XOS 633 TO 636 IAW MD-11 SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)SDR FDEA2020051320873Attach Fitting · corrodedLEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "F" FOUND MOUNT HOLES CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "F" REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED ECCENTRIC BUSSDR FDEA2020051320872Attach Fitting · corrodedLEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "E" FOUND MOUNT HOLES CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "E" REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED ECCENTRIC BUSSDR FDEA2020050420889Tire · failedLEVEL 2 "TIRE FAILURE" ON #5 TIRE ON SHORT FINAL. R & R # 5 MLG TIRE ASSY. INSPECTED AREA OF LT MLG, CHECK GOOD. REF MM 32-41-01-4.SDR FDEA2020050420876Pedestal · malfunctionedDURING CLIMB OUT RECEIVED "WEATHER FAIL" ALERT. SWITCHED TO SYSTEM 1 AND AFTER APPROXYMATELY 3 MINUTES RECEIVED "WEATHER FAIL" ALERT FOR SECOND WEATHER SYSTEM. SYSTEM 2 WOULD NOT COME BACK. SYSTEM 1 INTERMITTINGLY COME BACK, THEN FAILED AGAIN. ON APPROACSDR FDEA2020050420873Attach Fitting · corrodedLEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "F" FOUND MOUNT HOLE CORROSION.SDR FDEA2020050420872Attach Fitting · corrodedLEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "E" FOUND MOUNT HOLE CORROSION.SDR IPXA2020052255591Seat Track · corrodedINSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION AT STA 635 AND LBL 75.REMOVED AND REPLACED CORRODED SECTION OF MAIN CABIN SEAT TRACK BETWEEN STA 625 - 645 AT LBL 75.25 IAW MD-11 SRM 53-00-52, REPAIR 1, FIGURE 201. (MAJOR)SDR IPXA2020052055534Seat Track · corrodedINSPECTION TYPE:2CMAIN CABIN SEAT TRACK AT STA 733 & X=-8.5 HAS CORROSION.REPAIRED CORRODED MAIN CABIN SEAT TRACK BETWEEN STA 605 - 745 AT X=-8.5 IAW MD-11 SRM 51-33-01. (MINOR)SDR IPXA2020052055533Seat Track · corrodedINSPECTION TYPE:2CMAIN CABIN SEAT TRACK AT STA 720 & X=8.5 HAS CORROSION.REPAIRED CORRODED MAIN CABIN SEAT TRACK BETWEEN STA 605 - 745 AT X=8.5 IAW MD-11 SRM 51-33-01. (MINOR)SDR FDEA2020050810914Seat Track · damagedMAIN DECK, APPROX STA 1531, X= 8.5, SEAT TRACK DAMAGED BEYOND SRM LIMITS. REPLACED DAMAGED SEAT TRACK AT STA. 1531 REF. SRM 53-00-52 R1SDR FDEA2020050410891Seat Track · damagedMAIN DECK, APPROX STA 775, X= 75.25, SEAT TRACK BLENDED BEYOND SRM LIMITS, MARKED. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK AT STA 775,LBL 75. REF SRM CH 53-70-00, FIG 1.SDR FDEA2020050410890Trim Motor · cracked2:00 INTO FLT, FLT 370 HYD 3 ELEV OFF ALER. HYD SYS 3 WAS AT 3.9 OVER NEXT FIVE MINUTES DROPPED TO 3.6. DEPRESSURIZED SYS UNTIL LANDING. AFTER LANDING QTY WAS DOWN TO 1.0 FOUND HYDRAULIC FLUID MISTING IN TAIL AREA AROUND HORIZONTAL STABILIZER TRIM MOTORSSDR 9WGA2020050101Warning System · activatedLVL 2 HYD 2 FAIL
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