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 FDEA201906281453Floorbeam · damagedCTR CARGO PIT FLOORBEAM UPPER AFT FLANGE DAMAGED AT STA. 1701 APPROX. X=30.000. REPAIRED PER E.A. 1-5310-T0347878. INSTALLED SPLICE/REPAIR TO FLOORBEAM AT STA 1701 LOWER CARGO FLOOR.SDR IPXA2019070143937Track · crackedINSPECTION TYPE:3C FWD. AVIONICS ACCESS DOOR RT TRACK IS CRACKED. REMOVED AND REPLACED TRACK IAW SRM 51-31-01 & 51-33-01. (MINOR)SDR FDEA201906281423Charger · malfunctionedLVL 1 " BATT CHARGER IONP" ON TAXI, FOUND BATT CHARGER CONNECTOR ON BATT CHARGER DIS-CONNECTED FROM BATT CHARGER...PERFORMED BATTERY CHARGER ADJ/TEST AND NOT FAULTS NOTED ALSO HAD APU RUNNING WITH LOAD APPLIED HAD NORMAL BATTERY CHARGING LIGHT COME ON ANDSDR FDEA201906281422Warning Message · illuminatedLVL 1 "BAT DISCHARGING" ALERT FL 380. DIVERTED.SDR FDEA201906271416Skin · corrodedRIGHT WING UPPER SURFACE TRAILING EDGE WAS FOUND CORRODED AT XORS 1080 TO 1093. REPAIRED IAW ENGINEERING AUTHORIZATION 1-5730-T0347862, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100. CORROSION REWORKED AREA MEASURE AT RIGHT HAND WING AT XORS SDR FDEA201906271417Former · crackedRIGHT WING FIXED LEADING EDGE FORMER AT XOS 673 WAS FOUND CRACKED. THE FORMER WAS REMOVED IAW SRM 51-31-01-OG AND FABRICATED A NEW FORMER IAW DRAWING ARB 2924, REVISION B. INSTALLED THE NEW FORMER IAW SRM 51-33-01-OG. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201906271415Access Panel · crackedDURING HIGH FREQUENCY EDDY CURRENT SURFACE SCAN ON LEFT WING CORNER NR 11 FUEL ACCESS DOOR, FORWARD INBOARD CORNER, FOUND ONE CRACK, LENGTH APPROXIMATELY 1 INCH. REPAIRED THE LEFT WING ACCESS PANEL IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 18. THE REPAIR CLSDR IPXA2019062843835Battery · lowINSPECTION TYPE:N/A EMERGENCY BATT LIGHT BATT LOW. DEFERRED PER MEL 33-50-4 DMP CW PLACARD INSTALLED. **SUPPLEMENTAL SDR** DMP REVERSED. REMOVE AND REPLACED EMERGENCY POWER BATTERY SUPPLY IAW AMM 33-51-01. OPS CHECKS GOOD. THIS CLEARS MEL M675066. IPC 33SDR FDEA2019062761413Support Fitting · corrodedRIGHT WING, OUTBOARD FLAP VANE NR 4 SUPPORT FITTING ECCENTRIC HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMITS IAW SRM 57-50-02-2R, REPAIR 5, FIGURE 201. OVERSIZED BUSHING FABRICATED IAW SRM 57-50-02-2R, REPAIR 5 , FIGURE 201, AND EA 1-5750-T0347861,SDR FDEA2019062761412Support Fitting · corrodedRIGHT WING, OUTBOARD FLAP VANE NR 1 SUPPORT FITTING, ECCENTRIC HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMITS IAW SRM 57-50-02-2R, REPAIR 5, FIGURE 201. OVERSIZED BUSHING FABRICATED IAW SRM 57-50-02-2R, REPAIR 5, FIGURE 201, AND EA 1-5750-T0347861, SDR IPXA2019062874792Sign · failedL1 DOOR EMERGENCY SIGN FAILS TO MOVE TO CLOSED POSITION WITH DOOR CLOSED. ALIGNED THE ACTUATOR LINK ARM ON L1 DOOR OPS IAW AMM 52-10-01-700-801. OPS NORMAL.SDR IPXA2019062874787Skin · corrodedINSPECTION TYPE:3CCENTER WING TANK UPPER SKIN HAS CORROSION S-14 AND S-15 XCW 81.ACCOMPLISHED BLEND OUT REPAIR ON CENTER WING TANK UPPER SKIN BETWEEN STGR 14 AND STGR 15 XCW 81 PER VT SAA EA#011-5730-01-A7791 I/R AND UPS EO MD11-5730-72891-A.SDR IPXA2019062874784Skin · corrodedINSPECTION TYPE:3CCENTER WING TANK UPPER SKIN CORRODED BETWEEN S-14 AND S-15 XCW -46.5.ACCOMPLISHED BLENDOUT REPAIR ON CENTER WING TANK UPPER SKIN BETWEEN STGR 14 AND STGR 15 STA XCW -46.5 PER VT SAA EA# 011-5730-021-A7790 I/R AND UPS EO MD11-5730-72879-A.SDR IPXA2019062874788Skin · corrodedINSPECTION TYPE:3CCENTER WING TANK UPPER SKIN HAS CORROSION BETWEEN S-14 AND S-15 XCW 5 TO XCW 9.ACCOMPLISHED BLEND OUT REPAIR ON CENTER WING TANK UPPER SKIN BETWEEN STGR 14 AND STGR 15 XCW 5 TO XCW 9 PER VT SAA EA# 011-5730-01-A7792 I/R AND UPS EO MD11-5730-7SDR IPXA2019071144337Hinge · brokenINSPECTION TYPE:4C EXTENDED TAILCONE RT SIDE AT STA. CANT.Y=2165.6, X=36.5, AND Z=61.53. REPAIRED EXTENDED TAILCONE AT SAID LOCATION IAW EA 011-5310-01-A7832 REV. I/R AND EO MD11-5310-73209-A. (MINOR)SDR IPXA2019070444063Longeron Splice · crackedINSPECTION TYPE:4C MAIN CABIN LONGERON 2L SPLICE FITTING IS CRACKED AT STA. 5-123. REMOVED AND REPLACED CRACKED MAIN CABIN LONGERON 2L SPLICE FITTING IAW SRM 51-33-01. (MINOR)SDR IPXA2019070344032Intercostal · crackedINSPECTION TYPE:4C TAILCONE RT MIDDLE GUIDE PIN INTERCOSTAL IS CRACKED. REMOVED AND REPLACED CRACKED TAILCONE RT MIDDLE GUIDE PIN INTERCOSTAL IAW SRM 51-35-01. (MINOR)SDR IPXA2019070244023Intercostal · crackedINSPECTION TYPE:4C TAILCONE LT MIDDLE GUIDE PIN INTERCOSTAL IS CRACKED. REMOVED AND REPLACED CRACKED TAILCONE LT MIDDLE GUIDE PIN INTERCOSTAL IAW SRM 51-35-01. (MINOR)SDR IPXA2019062643761Battery Pack · no testEMERGENCY LIGHT BATTERY 1 LOW MESSAGE WHEN TESTING THE EMERGENCY LIGHT SYSTEM. R&R BATTERY PACK IAW MM 33-51-01. OPS CHECKS GOOD.SDR IPXA2019062854734Line · brokenAIR TURNBACK AFTER TAKE OFF. RECEIVED LEVEL 2 ALERT HYD 3 FAIL. DURING INSPECTION, FOUND THE LT LANDING GEAR HYD TRIM CYLINDER PRESSURE PIPE BROKEN. TEMP REPAIR OF HYD RIGID PIPES WITH FLEXIBLE WAS APPROVED BY ENGINEERING IAW AMM 20-10-01-300-805, THREE FLESDR IPXA2019071044289Rivet · looseINSPECTION TYPE:4C #2 ENG. INLET ASSY HAS 1 LOOSE RIVET AT 8:30 POS. REPAIRED #2 ENG. INLET ASSY IAW EA 011-7110-01-A7829 REV. I/R AND EO MD11-7110-73153-A. (MINOR)SDR IPXA2019070544117Doubler · damagedINSPECTION TYPE:4C TAILCONE RT UPPER PRODUCTION DOUBLER IS DAMAGED. REPAIRED DAMAGED TAILCONE RT UPPER PRODUCTION DOUBLER AT STA. 2165 & X=-36.5 IAW EO MD11-5350-66790-A APPENDIX A. (MINOR)SDR IPXA2019070544116Doubler · damagedINSPECTION TYPE:4C TAILCONE LT UPPER PRODUCTION DOUBLER IS DAMAGED. REPAIRED DAMAGED TAILCONE LT UPPER PRODUCTION DOUBLER AT STA 2165 & X=36.5 IAW EO MD11-5350-66790-A APPENDIX A. (MINOR)SDR IPXA2019070444072Door Frame · crackedINSPECTION TYPE:4C LT AFT CLG DOOR FRAME IS CRACKED. REMOVED AND REPLACED CRACKED LT AFT CLG DOOR IAW AMM 32-17-04-400-801. (MINOR)SDR IPXA2019062543735Unknown · malfunctionedINSPECTION TYPE:NA DIVERSION -- AFTER T/O FLAP/SLAT RETRACTION LEVEL 2 AIL DEFLECT DISAG AC FT VERY DIFFICULT TO CONTROL REQUIRING ALMOST FULL RT AILERON AT TIMES QRH CHECK LIST NO HELP DECLARED EMERGENCY AND DIVERTED TO KCVG. DEFERRED PER MEL 27-13-2-0-1 DMPSDR IPXA2019062643715Battery Pack · dischargedDURING EMERGENCY LIGHTS TEST, OBSERVED LEVEL 1 EMERGENCY LIGHT BATTERY 1 LOW ILLUMINATED. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY. OPS CHECK GOOD IAW AMM 33-51-01.SDR IPXA2019071044301Hinge Bracket · brokenINSPECTION TYPE:4C RT WING O/B FLAP I/B HINGE BRACKET ABOVE LOWER HINGE POINT IS BROKEN. REMOVED, FABRICATED AND REPLACED BRACKET IAW DWG. ARC0504 AND SRM 51-33-01. (MINOR)SDR IPXA2019070744174Doubler · crackedINSPECTION TYPE:4C LT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XIS=276.5 TO XIS=282.4. REPAIRED CRACKED LT WING FIXED L/E BEADED DOUBLER BETWEEN STA. XIS=276.5 TO XIS=282.4 IAW SRM 57-40-05 REPAIR 15 FIG. 205. (MAJOR)SDR IPXA2019062643710Switch · malfunctionedL1 MAIN ENTRY DOOR SLIDE INDICATION, R&R GIRT BAR SWITCH REF AMM 52 11 02 OPS TEST GOOD REF AMM 52 70 00 (501) 700 801 (D) THIS CLEARS M674321SDR IPXA2019062643695Bottle · low pressurePNEUMATIC SYSTEM DOOR L1 BLEW PRESSURE ZERO. DEFERRED L1 DOOR IAW MEL 52-10-3-1-2-1SERVICED L1 DOOR PNEUMATIC STORAGE SYS PER MM 12-25-04.SDR FDEA2019062421402Pump · failedAFTER TAKEOFF HYD 2 FAILURE. LOSS OF ALL FLUID. RCM CHECKLIST AND RETURNED FOR LANDING. CHECKED THE HYD LEAK FROM #2 ENG R HYD PUMP. REMOVED AND REPLACED THE 2R EDP PER AMM 29-11-20-4-1. LEAK CHECKED NORMAL .BUT THE L AND R PUMP ALWAY DISPLAY LOW HYD PRESDR FDEA2019062421401Check Valve · leakingAPPROX. 1 HOUR INTO FLIGHT LEVEL 1 HYD EIU 3 OFF ALERT. HYD QTY 3.2. HYD QTY CONTINUED TO DECREASE TO 2.5 LEVEL 1 HYD 3 OFF. QTY THEN HELD SEADY AT 2.5. AT SLAT EXNTENSION, QTY IMMEDIATLY DROPPED AND RECIEVED LEVEL 2 HYD FAIL ALERT. QTY WENT TO NEARSDR IPXA201906243612Battery · inoperativeDURING EMERGENCY LIGHTING TEST EXIT BATTERY 1 LOW MESSAGE SHOWS. R&R NR 1 EMERGENCY LIGHTING BATTERY IAW MM 33-51-01-401 OPS CHECKED NORMAL.SDR IPXA2019071044300Skin · dentedINSPECTION TYPE:4C #1 ENG. O/B T/R TRANSLATING SLEEVE UPPER FWD. CORNER SKIN IS DENTED. REPAIRED #1 ENG. O/B T/R SLEEVE IAW EA 011-7930-01-A7933 REV. I/R AND EO MD11-7830-73171-A. (MINOR)SDR FDEA201906211398Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT LUG HOLE BORE (HOLE #3) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRISDR FDEA201906211397Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT LUG HOLE BORE (HOLE #3) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATESDR FDEA201906211396Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (B AND A HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-SDR FDEA201906211395Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-5SDR FDEA201906211394Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57- 52-03SDR FDEA201906211393Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52- 03. SDR IPXA2019062143579Cable · disconnectedL1 ENTRY DOOR FWD SIDE CABLE DAMAGED. DRIVE WHEEL DISCONNECTED FROM DRIVE SPLINE. R & R BOTTOM FWD L1 CABLE PER AMM 52-11-03 OPS CHECK NORMAL.SDR IPXA2019070244022Stiffener · crackedINSPECTION TYPE:4C LT MLG W/W O/B AFT SIDE VERTICAL STIFFENER IS CRACKED. REMOVED AND REPLACED CRACKED LT MLG W/W O/B AFT SIDE VERTICAL STIFFENER IAW SRM 51-33-01 & 51-35-01. (MINOR)SDR IPXA2019070244020Stiffener · crackedINSPECTION TYPE:4C RT MLG W/W O/B AFT SIDE VERTICAL STIFFENER IS CRACKED. REMOVED AND REPLACED CRACKED RT MLG W/W O/B AFT SIDE VERTICAL STIFFENER IAW SRM 51-33-01 & 51-35-01. (MINOR)SDR IPXA2019062143577Switch · malfunctionedLEFT DOOR DISARMED LIGHT CAME ON AFTER LANDING, EVEN THOUGH THE DOOR WAS ARMED. R & R GIRT BAR SWITCH IAW AMM 52-11-02. OPS TESTED GOOD. IAW AMM 52-70-00 (501) 700-801 (D).SDR IPXA2019071144318Skin · dentedINSPECTION TYPE:4C LT SIDE SKIN DENT AND GOUGED AT STA 330 REQUIRES PERMANENT REPAIR. REPAIRED DENTED & GOUGED LT FUSELAGE SKIN AT STA. 330 ABOVE Z=-2.900 IAW EA 011-5330-01-A7835 REV. IR AND EO MD11-5330-73199-A. (MAJOR)SDR IPXA2019071144315Receptacle · gougedINSPECTION TYPE:4C#1 ENGINE EXHAUST NOZZLE O/B CORE COWL AFT LATCH PIN RECEPTACLE IS GOUGED. REPAIRED GOUGED #1 ENGINE EXHAUST NOZZLE O/B CORE COWL AFT LATCH PIN RECEPTACLE IAW EA 011-7810-01-A7834 REV. IR AND EO MD11-7810-73170-A. (MINOR)SDR FDEA201906201389Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE SURFACE FOUND CORROSION CORROSION AT RIGHT 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 FDEA201906201388Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE SURFACE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. SDR FDEA201906201387Hinge Bracket · 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 MD-11 CMM 57SDR FDEA201906201386Hinge Bracket · 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 MD-11 CMM 57- 4
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