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 FDEA201909032070Hinge Fitting · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE UPPER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE UPPER MOUNT INBOARD HOLE BORE (#2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57- 44-09. OSDR FDEA201909032069Hinge Fitting · 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 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BYSDR IPXA2019090346261Bottle · low pressureINSPECTION TYPE:N/A**SUPPLEMENTAL INFORMATION** R1 DOOR BOTTLE LOW. DEFERRED PER MEL 52-10-3-1-2-1 PLACARD INSTALLED. SERVICED R1 MAIN ENTRY DOOR PNEU BOTTLE IAW AMM 12-25-04-600-801. THIS CLEARS M681995.SDR FDEA201909022068Hinge Fitting · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE UPPER MOUNT INBOARD HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE UPPER MOUNT INBOARD HOLE BORE (#2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSISDR FDEA201909022067Hinge Fitting · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVSDR FDEA201909022066Hinge Fitting · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVESDR FDEA201909022065Hinge Fitting · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOSDR FDEA201909022064Hinge Fitting · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57- 44-09. SHOSDR FDEA201909022063Hinge Fitting · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MSDR FDEA201909022062Fitting · crackedNOSE LANDING GEAR RIGHT HAND TRUNNION FITTING SUSPECT CRACK AT STA Y = 595 NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING REPAIR CARRIED OUT AS PER SRM 53-10-14-2R REPAIR 2 FIGURE 202 AT STA Y = 595. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. TO CARRY OUT INITSDR FDEA201909022061Fitting · crackedNOSE LANDING GEAR LEFT HAND TRUNNION FITTING SUSPECT CRACK AT STA Y=595 NOSE LANDING GEAR LEFT HAND TRUNNION FITTING REPAIR CARRIED OUT AS PER SRM 53-10-14-2R REPAIR 2 FIGURE 202 AT STA Y = 595. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. TO CARRY OUT INITIAL SDR FDEA201909012060Hinge Fitting · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OSDR FDEA201909012059Hinge Fitting · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVESDR FDEA201909012058Hinge Fitting · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. SHOSDR FDEA201909012057Hinge Fitting · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. SHOULSDR FDEA201909012056Hinge Fitting · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MSDR FDEA201908302045Sensor · malfunctionedAFTER LANDING, RECEIVED A BRAKE DIFF TEMP LVL 1 MESSAGE. BRAKE TEMP ON NR 8 WAS ABOUT 200 COOLER THAN ALL OTHER TEMPS. REMOVED AND REPLACED THE NR 8 BRAKE TEMP SENSOR IAW MM 32-46-01-4. PERFORMED A TEST OF THE BRAKE TEMPERATURE MONITOR AND TIRE PRESSURE INSDR FDEA201908302044Receptacle · fireFIRE AT EXTERNAL POWER CONNECTION BURNED AND MELTED AIRCRAFT EXTERNAL POWER RECEPTACLE AND COMPONENTS. INSTALLED EXTERNAL POWER RECEPTACLE REFERENCE AMM 24-41-03-4. COMPLETED INSTALLATION OF EXTERNAL POWER PANEL REFERENCE DRAWING AAN7220 AND AMM 20-50-0SDR FDEA201908302043Skin · crackedON REMOVAL OF THE BANJO ACCESS, FOUND THE LEFT VERTICAL STABILIZER SKIN AT REAR CENTER SPAR CRACKED. REPAIRED THE SKIN PANELS. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201908302042Skin · crackedON INSPECTION, FOUND RIGHT VERTICAL STABILIZER SKIN CRACKED. REPAIRED IAW EA 1-5530-T0349100 P2, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR IPXA2019083046152Control Unit · faultedINTERMITTANT FIRE DETECTOR 2 FAULT LEVEL ONE ALERT IN FLIGHT. REPLACED THE NR 2 FIRE DETECTION CONTROL UNIT. OPS CHECKED GOOD IAW AMM 26-11-02.SDR IPXA2019083046145Actuator · leakingATB DUE TO HYDRAULIC 2 FAIL AFTER TAKE OFF, LEVEL ONE HYD 2 OFF ALERT. LEVELING OFF AT 23000 FT, HYDRAULIC QUANTITY WAS DROPPING AT APPROXIMATELY 1.2 GAL ILLEGIBLE LEVEL 2 HYD 2 FAIL ALERT. ACFT TAKEN OOS.NR 5L SPOILER ACTUATOR LEAKING SEVERELY.SDR 9WGA2019082911907Structure · corrodedCORROSION AROUND LOCK FASTENERS BS 1229 TOP OF FUEL TANK LBL 40 TO RBL 40. NON-ROUTINE 1556.SDR 9WGA20190829106Floorbeam · corrodedMAIN CARGO FLOOR BEAM CORROSION STA. 495 BL 48R. NON-ROUTINE 1554.SDR 9WGA201908291905Panel · corrodedNR 2 ENGINE PYLON L/H SIDE PANEL 457AL MULTIPLE FASTENERS ON TOP OF COMPARTMENT LEFT AND RIGHT SIDE HAVE CORROSION AROUND FASTENERS.SDR FDEA201908282037Indicator · failedR1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYSTEM, INOPERATIVE. R & R THE REMOTE PRESSURE INDICATOR ASSEMBLY FOR R1 DOOR, OPS CHECK GOOD IAW AMM 25-61-04-4.SDR FDEA201908282152Seat Track · wornMAIN DECK SEAT TRACK STA1261-1301 RBL=75.25 HAS () AREAS WORN. REPLACE NOTED MAIN DECK SEAT TRACK IAW SRM 53-00-52 REPAIR-1 FIG-201.SDR FDEA201908282034Web · crackedFOUND THE CENTER LANDING GEAR COMPARTMENT LEFT WEB, FOUND THE WEB CRACKED. REPAIRED PER EA 1-5310-T0349128 PART 1, THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201908282033Spar · crackedON REMOVAL FOR TH BANJO ACCESS, FOUND LEFT VERTICAL STABILIZER AT REAR CENTER SPAR PLANE AJC 7308 AT INTERNAL WEB BOX CRACKED. REPAIRED IAW SRM 55-30-02-2R, REPAIR 7 FIGURE 203, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR IPXA2019083086109Solenoid · failedL1 DOOR SOLENOID CLICKING EXCESSIVELY. REPLACED THE L1 FWD PASSENGER DOOR LOCK PIN RELEASE SOLENOID IAW AMM 52-10-06. OPS TEST NORMAL.SDR FDEA2019083082038Brake · damagedFOUND NR 5 BRAKE DAMAGED R&R THE NR 5 BRAKE IAW AMM 32-43-20-4.SDR FDEA2019082872021Longeron · crackedDURING NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING REPAIR ( REFERENCE SRNM : N00930) FOUND LONGERON 48 RIGHT CRACKED AFTER EXSITING CRACK TRIM OUT AT STATION 582. LANDING GEAR RIGHT HAND TRUNNION FITTING AT STATION 582 CRACKED LONGERON 48 RIGHT REMOVEDSDR FDEA2019082872022Bulkhead Web · crackedBS 594.875 AFT PRESSURE BULKHEAD CRACKED. COMPLY WITH EA 1-5310-T0348395 REV . THE PRESSURE BULKHEAD WEB WAS REPAIRED IAW EA 1-5310-T0348395 P1.SDR FDEA201908262020Access Panel · corrodedINTERNAL CORROSION ON DRAIN ACCESS PANEL DOUBLER R/R DOUBLE AND REPAIRED SHEAR TIE REF J.PF. (SEE NR0030). REMOVED AND REPLACED CRACKED INTERCOATAL REF NR00029 JPF. 475227 09-06-20119.SDR FDEA2019082862020Access Panel · corrodedINTERNAL CORROSION ON DRAIN ACCESS PANEL DOUBLERSDR FDEA2019101732675Stringer · crackedLEFT WING - LOWER SURFACE - FORWARD PANEL LAND IS CRACKED AFT OF #9 SLAT TRACK (MARKED). CORRECTIVE ACTION: INSTALLED REPAIR DOUBLER PER MD11 SRM 57-40-03-2R & SRM 51-31- 01.SDR FDEA201908232003Skin · dentedTO CARRY OUT REPAIR ON EXTERIOR FUSELAGE SKIN AT CENTER CARGO DOOR CUTOUT AFT LOWER CORNER STA 1781, L 43R AS PER EA 1- 5330 -T0336398 E P2 REPAIR CARRIED OUT ON EXTERIOR FUSELAGE SKIN AT CENTER CARGO DOOR CUTOUT AFT LOWER CORNER STA 1781 LONGERON 43 RIGHTSDR FDEA201908232004Switch · failedR1 PRESSURE TEST LIGHT INOP. R&R'ED R1 DOOR "PRESS TO TEST" LIGHT SWITCH IAW REF: AMM 25-61-04-4. OPS CH'D GOOD.SDR IPXA2019082324592Door · unknownR-1 DOOR WILL NOT CLOSE PROPERLY. R-1 DOOR SLIDING ILLUMINATION. REPLACED LIGHT ASSY PER MM 33-22-01. OPS CK GOOD. OK TO CONT SERV.SDR FDEA201908212337Spar Cap · cracked#2 PYLON RT UPPER SPAR CAP FWD EDGE AT THE OUTER RADIUS HAS A .100 IN CRACK PROPAGATING AFT AT YID 408.600. REPAIRED #2 PLYON UPPER SPAR CAP AVB7506 PER EA 1-5450-T0349293 (MANUFACTURING JOINT FATIGUE CRACK IN RT UPER SPAR) MAJOR REPAIR.SDR FDEA201908211995Line · failedAFTER LANDING GOT "HYD 2 FAIL" PER CREW DEBRIEF LOSS OF FLUID OCCURED WHEN REVERSER WAS DEPLOYED PRESSURE REMAIND GOOD UNTIL ENGINE SHUT DOWN. BLOCK IN HYDRAULIC QTY INDICATING .6 GALLONS. FOUND HYDRAULIC STOW LINE AT THE HCU FAILED AT THE B NUT BRAZEDSDR FDEA201908211990Skin · delaminatedEMPENNAGE - LEFT HAND IN BOARD ELEVATOR TOP SURFACE AT STATION XE=160.5 FOUND DELAM. EMPENNAGE - LEFT HAND IN BOARD ELEVATOR TOP SURFACE REPAIRED AND SMOOTHEN AS PER SRM 55-20-80-2R, REPAIR 2, PARAGRAPH 2A, FIGURE 201 AND THE E.A #1-5520-T0348878 PART 1.SDR IPXA2019082105842Battery Pack · inoperativeL1 DOOR REMOTE PRESSURE PRESS TO TEST LIGHT INOP. RELAMPED & REPLACED SYSTEM BATTERIES IAW MM 25-61-04-000-801. SYSTEMS CKS GOOD.SDR FDEA2019082101959Hinge · wornFWD CARGO DOOR, DOOR SIDE, HINGE SEGMENT IS WORN REMOVED REPLACED HINGE SEGMENT PER DWG. ADA0253 AND SRM 51-33-01SDR FDEA2019082101958Hinge · wornFWD CARGO DOOR, DOOR SIDE HAS A WORN HINGE. P/N ADA0253-509 REMOVED AND REPLACED HINGE SEGMENT PER DWG. ADA0253 AND SRM 51-33-01SDR FDEA2019082101957Hinge · wornFWD CARGO DOOR HINGE , DOOR SIDE IS WORN P/N ADA0253-505 REMOVED AND REPLACE DOOR HINGE SEGMENT PER DWG. ADA0253 ANDSRM 51-33-01.SDR FDEA2019082191934Longeron · corrodedLOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 45 LEFT FOUND WITH CORROSION AT STATION 1531 . LOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 45 LEFT WITH CORROSION AT STATION 1531 REPAIR CARRIED AS PER EA#1-5310-T0349099 PART 1. TITLE: FUSELAGE-SDR FDEA2019082191946Support Fitting · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 5 SUPPORT FITTING ECCENTRC HOLE BORE FOUND CORROSION. SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED AND FOUND EXCEEDED LIMITS IAW SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED IAW SRM 57-50-0SDR FDEA2019082191945Support Fitting · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRC HOLE BORE FOUND CORRODED. UPPORT FITTING ECCENTRIC HOLE BORE REWORKED AND FOUND EXCEEDED LIMITS IAW SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED IAW SRM 57-5SDR FDEA2019082191944Support Fitting · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRC HOLE BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED IAW SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND EA 1-
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