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 FDEA201409122604Door · bindingL1 DOOR WOULD NOT CLOSE. CYCLED DOOR CLOSED HALF WAY MANUALLY & THEN OPERATES NORMAL. CYCLED DOOR THROUGH FULL TRAVEL ELECTRICALLY IAW AMM 52-11-02-2 OPENING & CLOSING FWD PAX DOOR MX PRACTICES, ALL OPERATIONS CHECKED NORMAL.SDR KO0R201409080007Door Frame · corrodedFORWARD LOWER CORNER OF THE LOWER AFT CARGO DOOR CUTOUT IS CORRODED AT BS 1637 AT LONGERON, 43R.SDR FDEA201409072503Control Panel · malfunctionedAUTOPILOT NR 1 & 2, AUTO THROTTLES WOULD NOT ENGAGE. NO FLIGHT FAULTS LOGGED FOR THE FCC1 OR FCC2. CHECKING THE FCC1 & FCC2 PREVIOUS FAULTS. BOTH FCC SHOW LEG 1 NO FAULTS, OR FLY INTO IND. LEG 2 FAULTS WERE ELEV FAULT, WHICH EWR RESOLVED. THEN NEXT FAULT SDR FDEA201409062485Ring · defectiveDURING CLIMB OUT RECEIVED ENG 2 FADEC MAINT ALERT. FOLLOWED QRH CHECKED WITH GOC & RETURNED TO ZGGG. REMOVED AND REPLACED NR 2 ENGINE INLET TRANSITION RING PER AMM 71-11-03-4-2. PERFORMED THE ENGINE IDLE TEST PER AMM71-02-06-5-2, NO FAULT NOTED. PERFORMED SDR FDEA201409062501Battery Pack · inoperativeDURING EMERGENCY LIGHT TEST, RECEIVED AN EMERGENCY LIGHT BATTERY 1 LOW. TROUBLESHOOTING IS REQUIRED PRIOR TO INSTALLING PARTS. R & R EMERGENCY BATTERY IAW AMM 33-51-01-4 & FUNCTIONED IAW AMM 33-51-01-5. ALL TESTS PASSED. R & R EMERGENCY LIGHTS BATTERY IASDR FDEA201409052469Battery · dischargedON EMER LIGHT TEST GOT EMER LT BAT 1 LO MEL 33-50-04, EMER LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PER AMM CHP33-51-01-4 AND FUNCTIONED PER AMM CHP33-51-01-5. ALL TESTS PASSED.SDR FDEA201409052479Landing Gear · defectiveUPON DEPARTURE CTR GEAR WOULD NOT RETRACT. RAN QRH CTR GEAR REMAINED. RETURNED TO PHNL. REMOVED AND REPLACED CENTERLINE LANDING GEAR ASSY PER WORK CARD 32T1004, LEAK AND OPS CHECK GOOD.SDR IPXA2014091584295Mount · gougedINSPECTION 3C, R1 DOOR FWD AND AFT ESCAPE SLIDE MOUNT BRACKETS GOUGED. ACCOMPLISHED PERMANENT REPAIR TO FWD AND AFT R1 DOOR ESCAPE SLIDE MOUNTS IAW EA 011-5200-01-A5528, REV I/R AND EO 5320-55517-A.SDR KO0R201409040006Skin · corrodedLEFT WING UPPER SKIN PANEL SURFACE IS CORRODED FROM XORS 715 TO 742 AFT SPAR AREA.SDR KO0R201409040003Skin · corrodedLEFT WING UPPER SKIN PANEL SURFACE IS CORRODED FROM XORS 756.5 TO 768.5 T/E AREA.SDR IPXA2014091584282Rib · crackedINSPECTION 3C, RT WING NR 1 SLAT INTERNAL INBD RIB CRACKED. R & R RT WING NR 1 SLAT IAW AMM 27-80-20-400-801.SDR WRNA201409040023Pitot Line · contaminatedTHE CREW REPORTED THAT DURING TAKEOFF, THERE WAS AN AIRSPEED DIFFERENCE AFTER 80KTS. THE F/O AIRSPEED INDICATOR DROPPED TO 55 KTS WHILE THE CAPTAIN’S AIRSPEED INDICATOR READ 95 KTS. REJECTED TAKEOFF AT 95 KIAS AND TAXIED BACK TO THE RAMP WITHOUT ANY FURTHER SDR IPXA2014090284134Floor Panel · damagedFLOOR PANEL SPONGY. FABRICATED NEW FLOOR PANEL IAW SRM 53-00-50 REPAIR 1 & 3 AND DWG WSP0825.SDR FDEA201408302361Door Frame · crackedLEFT MLG DOOR UPPER FRAME CTR HINGE ATTACHMENT FOUND CRACKED AT APPROXIMATE STATION Y=1438.375. AREA REPAIRED AS PER EA 1-3210-T0310973A PART 1 TITLE: "LANDING GEAR - MAIN GEAR AND DOORS - MLG LT DOOR HINGE FRAME FOUND CRACKED" WORK INSTRUCTIONS. REPAIR CLASDR FDEA201408282345Pressure System · defectiveR1 DOOR EMER SLIDE REMOTE PRESS TO TEST BUTTON INOPERATIVE. R&R REMOTE PRESSURE ASSY PER M/M 25-61-04-4, 25-61-04-5 .SDR FDEA201408272323Longeron · crackedCABIN AT LT STATION 1257 LONGERON 27 FOUND CRACKED. CABIN AT LEFT HAND STATION 1257 CRACKED LONGERON 27 REMOVED AND REPLACED AS PER SRM 51-31-01 FROM STATION 1256 TO STATION 1305 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100SDR FDEA201408272321Skin · crackedRIGHT WING HAS EVIDENCE OF POSSIBLE CRACK IN ACFT SKIN AT SLAT TRACK NR 14. REMOVED DAMAGE, FABRICATED REPAIR, INSTALLED REPAIR IAW SRM 51-40-02.SDR FDEA201408272320Skin · crackedLEFT WING HAS EVIDENCE OF POSSIBLE CRACK IN ACFT SKIN AT SLAT TRACK NR 14. COMPLETED REPAIR IAW SRM 57-40-02.SDR IPXA2014091284260Doubler · crackedINSPECTION 1C, LT WING FIXED L/E BEADED DOUBLER CRACKED IN THREE PLACES BETWEEN XOS 633.491 AND 648.2994 OTBD OF REFUELING PANEL. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG 203.SDR IPXA2014090584184Doubler · crackedINSPECTION 1C, RT WING FIXED L/E BEADED DOUBLER CRACKED AT XOS 760. REPAIRED IAW SRM 57-40-02, FIG 203, REPAIR 15.SDR IPXA2014082784096Warning Message · false activationAFTER TAKEOFF, A LEVEL 3 FLAPS DISAGREE. CONFIG PG SHOWED FLAPS 15, FOLLOWED QRH FLAPS EXTENDED NORMALLY. PERFORMED FCC RETURN TO SERVICE TESTS AND FOUND NO FAULTS IAW FIM 22-00-00-101. FLAPS OPS CHECKS NORMAL IAW MM 27-50-00-710.SDR FDEA201408252305Frame · dentedCABIN LT STATION 1641, LONGERON 11 - 12 FRAME FOUND DENTED. FRAME REPAIRED AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REPETITIVE INSPECTION REQUIRED - INITIAL INSPECTION AT 14,500 FLIGHT CYCLES AND REPETITIVE INSPECTION 9,500 FLIGHT CYCLES TO BE CARRIED OUT SDR IPXA201409084200Intercostal · crackedINSPECTION 3C, EMPENAGE INTERCOSTAL CRACKED AT LOWER PYLON CARRY THRU REAR CENTER, SPAR TO REAR SPAR BETWEEN STA Z=200 TO Z=224 AND Y=2164. ACCOMPLISHED PERMANENT REPAIR TO EMPENAGE LOWER PYLON CARRY THRU INTERCOSTAL BETWEEN STA Z=200 TO Z=224 AND Y=2164 IAW SDR FDEA201408252309Hydraulic Line · failedUPON TOUCHDOWN WITH FLAPS 35 & MEDIUM BRAKES SELECTED, EXPERIENCED COMPLETE LOSS OF NR 2 HYD SYS FLUID RESERVOIR WAS ZERO & PUMPS OFF. ALL THESE HAPPENED BETWEEN TOUCHDOWN & TAXI SPEED. NR 2 LT FAN COWL OPENED, FOUND PRESS LINE GOING INTO THE HYD CONTROL UNISDR IPXA2014091584281Skin · damagedINSPECTION TYPE:3, CLEFT WING L/E UPPER SKIN HAS CHAFE DAMAGE OTBD OF NR 8 SLAT STA XOS 1185 TO 1191.8. ACCOMPLISHED PERMANENT REPAIR ON LT WING LEADING EDGE UPPER SKIN STA XOS 1185 TO 1191.8 IAW VT-SAA, EA 011-5730-01-A5571, REV I/R AND EO 5730-55521-A.SDR FDEA201408242301Web · crackedCABIN R3 MAIN ENTRY DOOR AFT LOWER JAMB STATION 1310, LONGERON 26 - 27 WEB FOUND CRACKED. WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100SDR FDEA201408242300Web · crackedCABIN L3 MAIN ENTRY DOOR AFT LOWER JAMB STATION 1310, LONGERON 26 - 27 WEB FOUND CRACKED. WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100SDR FDEA201408242299Web · crackedCABIN R3 MAIN ENTRY DOOR FWD LOWER JAMB STATION 1254, LONGERON 26 - 27 WEB FOUND CRACKED. WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100SDR FDEA201408242298Web · crackedCABIN L3 MAIN ENTRY DOOR FWD LOWER JAMB STATION 1254, LONGERON 26 - 27 WEB FOUND CRACKED. WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100SDR IPXA2014082984089Fan · failedWITH AVIONICS AIR FLOW OFF, CREW REPORTED SMOKE IN THE COCKPIT. EMERGENCY DECLARED. DIVERTED. FOUND NR 1 AV RACK FAN AT FAULT IAW AMM 21-26-03-00. R & R NR 1 AND NR 2 AV RACK FAN IAW AMM21-26-02-201. TEST EDIAW AMM 21-26-02-201, TASK 700-801. BOTH 1 AND 2SDR WRNA201408280021Rccb · faultedTHE CREW REPORTED THAT PRIOR TO TOP OF DESCENT THAT A LEVEL 2 ALERT FOR GEN BUSS 3 FAULT WAS DISPLAYED IN THE EAD. FOLLOWED THE QRH PROCEDURES, DEPLOYED THE ADG AND NO FUEL DUMP WAS PERFORMED. LANDED WITHOUT FURTHER INCIDENT OR DELAY. PERFORMED FIM 24-20-17,SDR 9WGA2014082501Wire · burnedLEFT PUMP OFF ALERT. TROUBLESHOOTING REVEALED SEVERAL BURNED AREAS OF WIRING HARNESS ABOVE TAIL FUEL TANK.SDR FDEA201408232294Skin · crackedLEFT WING LOWER FIXED LE SKIN XORS 799 ON SLAT TRACK CUT OUT FOUND CRACK. CRACKED AREA AT LEFT HAND WING LOWER FIXED LEADING EDGE SKIN AT STATION XOS 799 AREA REPAIRED AS PER SRM 57-40-02. REPAIR 7 FIGURE 201 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100SDR FDEA201408232296Power Supply · inoperativeINTERMITTENT LEVEL ONE EMER LIGHT BATTERY 1 LOW ALERT AFTER LANDING. SAME ALERT WHEN TESTING EMER LIGHTS. R&R POWER SUPPLY EMERGENCY EXIT LIGHT ASSEMBLY PER AMM 33-51-01-4 AND FUNCTIONAL CHECK SATISFACTORY. OK FOR SERVICE.SDR IPXA2014082784076Autopilot Sys · malfunctionedAUTOPILOT WOULD MAKE ERRATIC PITCH CHANGES DOWN IN CLIMB UP AND IN LEVEL FLIGHT. RETURNED TO DEPARTURE. PERFORMED RTS TEST ON FCC 2IAW AMM 22-00-00-700-801. TEST PASSED.SDR IPXA201409084197Attach Fitting · crackedINSPECTION 3C, LEFT WING LOWER WINGLET FORWARD ATTACHMENT FITTING IS CRACKED. R & R FORWARD ATTACH FITTING IAW EO 5720-2720-27680-C.SDR IPXA2014090384149Doubler · crackedINSPECTION 3C, LT WING L/E BEADED DOUBLER CRACKED AT XOS 765. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIGURE 203.SDR IPXA2014090384147Doubler · crackedINSPECTION 3C, LT WING L/E BEADED DOUBLER CRACKED AT XOS 756. REPAIRED IAW SRM 57-40-02, REPAIR 15 FIG 203.SDR IPXA2014091584293Support Fitting · corrodedINSPECTION 3C, LIGHT SURFACE CORROSION ON RT MLG RETRACT CYLINDER SUPPORT FITTING LOWER FOOT FAYING SURFACE. REPAIRED RT MLG RETRACT CYLINDER SUPPORT FITTING IAW EA 011-5730- 01-A5572, REV B AND EO 5740-55458-C.SDR IPXA2014091584292Support Fitting · corrodedINSPECTION 3, FLIGHT SURFACE CORROSION ON RT MLG RETRACT CYLINDER SUPPORT FITTING UPPER FOOT FAYING SURFACE. REPAIRED RT MLG RETRACT CYLINDER SUPPORT FITTING IAW VTSAA EA 011-5730-01-A5572, REV B AND EO 5740-55458-C.SDR IPXA2014091584269Attach Fitting · damagedINSPECTION 3C, RT MLG LOWER FORWARD BOLT HOLE BUSHING FOR RETRACT CYLINDER ATTACH FITTING DAMAGED ACCOMPLISHED BUSHING REPAIR ON RT MLG LOWER FORWARD BOLT HOLE FOR RETRACT CYLINDER ATTACH FITTING IAW EA 011-5720-01-A5576, REV I/R AND EO 5740-55475-A.SDR IPXA2014091584268Attach Fitting · damagedINSPECTION 3C, RT MLG UPPER AFT BOLT HOLE BUSHING FOR RETRACT ATTACH FITTING DAMAGED ACCOMPLISHED BUSHING REPAIR ON RT MLG UPPER AFT BOLT HOLE FOR RETRACT ATTACH FITTING IAW EA 011-5720-01-A5576 AND EO 5740-55475-A.SDR IPXA2014091584267Attach Fitting · damagedINSPECTION 3C, RT MLG LOWER AFT BOLT HOLE BUSHING FOR RETRACT CYLINDER ATTACH FITTING DAMAGED ACCOMPLISHED BUSHING REPAIR ON RT MLG LOWER AFT BOLT HOLE BUSHING FOR RETRACT CYLINDER ATTACH FITTING IAW EA 011-5720-01-A5576, REV I/R AND EO 5740-55475-A.SDR IPXA2014091584266Trunnion · damagedINSPECTION 3C, RT MLG TRUNNION UPPER FORWARD BOLT HOLE BUSHING FOR RETRACT CYLINDER ATTACH FITTING DAMAGED. ACCOMPLISHED BUSHING REPAIR ON RT MLG TRUNNION IAW EA 011-5720-01-A5576, REV I/R AND EO 5740-55475-A.SDR IPXA2014091184256Trunnion · corrodedINSPECTION 3CR, MLG TRUNNION FITTING INBD FACE CORRODED AROUND UPPER ATTACH BOLT HOLES FOR RETRACT CYLINDER FITTING. REPAIRED RT MLG TRUNNION FITTING IAW EA 011-5720-01-A5565 REV IR AND EO 5340-55499-A.SDR IPXA2014091184255Trunnion · corrodedINSPECTION 3C, RT MLG TRUNNION FITTING INBD FACE CORRODED AROUND LOWER ATTACH BOLT HOLES FOR RETRACT CYLINDER FITTING. REPAIRED IAW EA 011-5720-01-A5565, REV IR AND EO 5340-55499-A.SDR IPXA2014091184253Rib · crackedINSPECTION 3C, NR 3 ENGINE INBD CORE COWL AFT RIB CRACKED. REPAIRED IAW CV14-4901 AND EO 7110-55425-A.SDR IPXA2014090384146Doubler · crackedINSPECTION 3C, RT WING L/E BEADED DOUBLER CRACKED AT XOS 753 - 763. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIGURE 203.SDR IPXA2014090384145Doubler · crackedINSPECTION 3C, RT WING L/E BEADED DOUBLER CRACKED XOS 728 - 734. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG 203.SDR IPXA2014090384144Doubler · crackedINSPECTION 3C, RT WING L/E BEADED DOUBLER CRACKED AT XOS 653- 657. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG 203.
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