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 FDEA201803080630Actuator · intermittentL1 DOOR WILL NOT OPEN ELETRICALLY. ON ARRIVAL, OPS CHECK OF THE L1 DOOR, FOUND NORMAL, NO FAULTS NOTED IAW AMM 52-10-01-2. RESET THE CLUTCH RELEASE ON THE ELECTRICAL ACTUATOR TO LET THE DOOR OPERATE AGAIN. SUSPPECT CLUTCH STUCK INTERMITTENTLY, R & R THE SDR 9WGA5432018030801Bolt · looseLEVEL 2 ALERT, SLAT DISAGREE DURING INITIAL CLIMB WITH THE FLAP & SLAT HANDLE AT FLAPS 20 DEGREES EXTENDED. FOUND A LOOSE BOLT ON SLAT TRACK NR 16. TIGHTENED IAW AMM 27-20-30. PERFORMED RETURN TO SERVICE OF FCC NR 1 & THE NR 1 SLAT SYSTEM IAW AMM 27-20-01. ASDR IPXA2018040328138Skin · dentedINSPECTION TYPE: 2C, RT HORIZONTAL STAB L/E DENTED. REPAIRED L/E SKIN BETWEEN XFS 327.947 AND XFS 333.764 IAW EA 011-5510-01-A7166, REV IR, AND EO MD11-5510-67996-A. MAJORSDR IPXA2018031627525Skin · crackedINSPECTION TYPE: 2C, NR 1 ENGINE AFT LOWER PYLON FAIRING OTBD SKIN CRACKED AT YPN 200. REPAIRED THE PLYLON SKIN IAW SRM 54-55-01, REPAIR 2, AND 54-05-41.SDR FDEA201803060613Switch · inoperativeDURING A POSTFLIGHT CHECK, FOUND RIGHT SIDE EVACUATION SLIDE, REMOTE PRESSURE PRESS-TO-TEST SWITCH INOPERATIVE. R1 DOOR REMOTE PRESSURE INDICATOR ASSEMBLY REMOVED AND REPLACED, OPS TEST CARRIED OUT IAW AMM 25-61-04-4, AND AMM 25-61-04-710-801. FOUND SATISFASDR FDEA201803060612Gcu · inoperativeABOUT 30 MIN INTO FLIGHT, GEN 1 OFF FLASHED ON MOMENTARTLY. ABOUT 20 MIN LATER THE GEN 1 OFF & GEN 2 OFF & GEN 3 OFF FLASHED ON AND OFF CONTINUOUSLY FOR REMAINDER OF FLIGHT. ALL TIE BUSSES OPENED WHEN THE GEN OFF LIGHTS CAME ON. ACCESSED EPCU THRU CFSDR FDEA201803050599Battery · inoperativeDURING PREFIGHT, EMERGENCY LIGHT TEST, A LOW BATTERY ALERT. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY, IAW AMM 33-51-01-4. OPS CHECKED NORMAL.SDR FDEA201803040583Power Supply · inoperativeDURING PREFLIGHT EMERGENCY LIGHT TEST, RECEIVED A LEVEL 1 EMERGENCY LIGHT BATTERY LOW ALERT. REPLACED THE POWER SUPPLY IAW AMM 33-51-01-4, OPS TESTED OK & NO FAULT MESSAGE.SDR FDEA201803040585Structure · damagedLEFT INBOARD FLAP, OUTBOARD ENDCAP DAMAGED. REPAIRED IAW EA 1-5750-T0338672, PT1, INSTALLED A NEW CLOSURE WEB.SDR FDEA201803030572Filter · contaminatedTWO HOURS INTO FLIGHT, CLIMBING FROM FL 340 TO FL 360, RECEIVED A LEVEL 1 FUEL CONTAMINATED ALERT. LASTED APPROXIMATELY 15 SECONDS, CHANGED TO LEVEL 1, THE NR 1 ENGINE FUEL FILTER. LASTED ABOUT 15 SECONDS THEN BACK TO FUEL CONTAMINATED. THEN ALL ALERTS SDR FDEA201803020564Cylinder · failedDURING CLIMBOUT, A LOUD BANG UNDER OUR FEET, RECEIVED A HYD 3 FAIL. IAW CHECKLIST, MANUAL EXTENSION OF LANDING GEAR, ON EXTENSION, NOSE GEAR FELL OUT WITH A LOUD BANG. NOSE GEAR UNSAFE INDICATION. REPLACED NOSE GEAR RETRACT CYLINDER IAW AMM 32-35-02-4.SDR IPXA2018030827231Rudder · corrodedINSPECTION TYPE: 4C, UPPER AFT RUDDER CORRODED UNDER EXTERIOR SKIN. REMOVED AND REPLACED THE RUDDER IAW AMM 27-20-30, P/B 401.SDR IPXA2018030227055Unknown · odor:SMOKE OR FUMES IN THE COCKPIT. PERFORMED A VISUAL INSPECTION, CLEANED THREE PACKS, WATER SEPARATOR, AND CONICAL COALESCER ASSY. OPS AND LEAK CHECKED OK.SDR IPXA2018030527166Skin · damagedRIGHT INBD FLAP HAD A DEEP GOUGE ON THE LOWER SURFACE. INSPECTED THE RT INBD FLAP LOWER SKIN AND FOUND TWO DENTS AND GOUGES. REMOVED 50% OF MATERIAL NT AND 20% OF AFT DENT IAW SRM 57-00-00. REMOVED CRACK DAMAGE WITH 1/4" SPOT FACE.SDR FDEA201802280533Floor Panel · corrodedGALLEY FLOOR, LEFT AFT MOUNT HOLE INSERT HAD SIGNS OF POSSIBLE CORROSION. REMOVED CORROSION IAW EA 1-2530-T0338462, PART 1.SDR IPXA2018030227044Hinge · crackedINSPECTION TYPE: 4C, LT HORIZONTAL STAB T/E ACCESS COVER, LOWER DOOR HINGE IS CRACKED AT XE 178, & XE 180. REPAIRED THE HINGE IAW EA 011-5520-01-A7154, REV I/R, AND EO MD11-5520-67620-A.SDR IPXA2018022826957Seal · brokenCOURIER AREA PBE SEAL BROKEN. REMOVED AND REPLACED THE PBE IAW AMM 35-31-00-001, & 35-31-01- PAGE BLOCK 401.SDR IPXA2018022726928Light · inoperativeR1 EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST LIGHT INOPERATIVE. OPS CHECKED R1 THE SLIDE REMOTE PRESSURE TEST OPS TEST GOOD IAW MM 25-61-15.SDR FDEA201802240483Battery · warning messageDURING A PREFLIGHT EMERGENCY LIGHT TEST, RECEIVED A LEVEL 1 EMERGENCY LIGHT BATTERY 1 LOW. PERFORMED EMERGENCY LIGHT TEST 3 CONSECUTIVE TIMES IAW MM 33-51-01-5. ALL GOOD IAW WRI 30-30/6329. SUSPECT MISC FAILING AND GENERATING SPURIOUS LOW BATTERYSDR IPXA2018022326808Door · inoperativeL1 DOOR INOPERATIVE. IAW EO MD-11 2520-67534-A.SDR FDEA201802220480Seat Track · corrodedMAIN CABIN SEAT TRACK AT R1 DOOR, STA 440 AND RBL 80 SHOWS EVIDENCE OF CORROSION ON THE OUT BOARD FLANGE. REPAIRED THE SEAT TRACK AT STA 440 AND RBL 80 IN REF TO EA 1-5340-T0338688.SDR IPXA2018022226772Fan · failedAIR TURN BACK FOR A STRONG ELECTRICAL ODOR IN THE COCKPIT AFTER TAKEOFF. ON LANDING AT APPX 80 KTS RX LVL 2 AVIONICS EXH FLO OFF. PERFORMED FIM 21-26-01-00, BLOCKS 1, 2, 5, AND 9. AVNX EXHAUST FAN FAILED. SMELL REMOVED FROM A/C. R & R THE EXHAUST FAN IAW MM SDR FDEA201802210462Seat Track · corrodedMAIN CABIN SEAT TRACK HAS CORROSION AT STA 445 AND LBL 28. REMOVED AND REPLACED THE SEAT TRACK, P/N WSP0826-521 FROM STA 445 LBL 27.5 IN REF TO SRM 53-00-52 AND EA 1-5340-T0338764.SDR FDEA201802210461Seat Track · corrodedMAIN CABIN SEAT TRACK AT THE L1 DOOR THRESH HOLD, BS 440 HAS CORROSION. REPAIRED IAW SRM 53-00-52, FIG 101, AND EA 1-5340-T0338800.SDR IPXA2018030227054Panel · crackedINSPECTION TYPE: 3C, LT INBD ELEVATOR L/E FAIRING PANEL LOWER SURFACE AT ATTACH ANGLE WAS FOUND CRACKED, OTBD OF ACTUATOR. ACCOMPLISHED A PERMANENT REPAIR IAW EA. 011-5520-01-A7147, REV IR, AND EO MD11-5520-67625-A. MAJOR.SDR FDEA201802210459Hinge · damagedFOUND MC DOOR HINGES TO HAVE WEAR ON HINGE LUGS AND PITTING BEYOND SRM LIMITS 51-31-01. REPLACED MCD HINGE SECTIONS IAW SRM 51-31-01. REPLACED MCD HINGE SECTIONS AS PER SRM 51-31-01 ALL REPAIRS COMPLIED WITH HINGE SECTIONS PAINTED IAW SRM 51-21-02. ALL INSPESDR IPXA2018022226758Light · damagedDURING AN EMERGENCY LIGHT TEST OF FWD L1 DOOR HANDLE, EMERGENCY LIGHTS WERE FOUND DAMAGED. THE LIGHT ASSY WAS REPLACED IAW AMM 33-52-02-201, REV 90.04. TESTED GOOD.SDR FDEA201802200494Motor · failedHORIZONTAL STAB TRIM RATE 2 CIRCUIT BREAKER FOUND OPEN. CONFIGURED THE ACFT TO OPS CHECK THE STAB TRIM MOTOR IAW MM 27-41-00-5, THE CIRCUIT BREAKER TRIPS DURING OPS CHECK. REMOVED AND REPLACED THE NR 2 HORIZONTAL STAB TRIM MOTOR SOSV IAW AMM 27-43-31-4,SDR FDEA201802200442Warning System · activatedLVL 2 ANTI SKID L FAIL ON APPROACH, COMPLIED WITH QRH. ANTI-SKID CONTROL VALVE INOP. SYSTEM 1 BRAKE 6 DISABLED. ENSURE PENALIES ARE APPLIED. COMPLIED WITH "M" PROCEDURE. BRAKE INOP KIT INSTALLED ON NR 6 BRAKE.SDR FDEA201802200440Power Supply · inoperativeWITH EMER LT SWITCH IN ARM POS AND TEST BUTTON PUSHED, GET EMER LT BAT1 LO ALERT. EMER LT TEST DOES NOT DISPLAY. EMER LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY REF AMM 33-51-01-4. OPS CHECKS GOOD.SDR FDEA201802190433Door Sill · wornSMIS 618 53-10 6121 18FEB18 MEM OPEN U MOD TYPE T MOD NO. 1-5310-T0338478 REV NO. PS P1 FUSELAGE - MAIN DECK CARGO DOOR JAMB WORN HOLES ON MAIN DECK CARGO DOOR FOR COMPLY WITH E..A. 1-5310-T0338478 REV NO. POS. P1 REAMED HOLE ON THE FISDR IPXA2018021926655Skin · dentedFWD CARGO DOOR DENTED AFT OF THE MAIN LOCK - UNLOCK DRIVE. 41 INCHES FROM AFT EDGE OF DOOR AND 27 INCHES FROM BOTTOM. CUT OUT THE DAMAGED SKIN. REPAIRED IAW EO MD11-5230-66816C, SECTION 6 C. MAJOR.SDR IPXA2018021926660Structure · damagedAFT BULK CARGO DOOR LOWER, AFT CORNER DAMAGED.SDR FDEA201802200433Door Frame · wornMAIN DECK CARGO DOOR JAMB WORN HOLES ON MAIN DECK CARGO DOOR FOR COMPLY WITH EA 1-5310-T0338478 REV NO. POS P1. REAMED HOLE ON THE FIRST TWO LUGS ON THE FWD A/C FUSELAGE SIDE HINGE FITTING OVER THE CMM REPAIR LIMITS OF .462. NE DIAMETER OF LUGS BORE IS .470, SDR IPXA2018021926638Lens · missingFOUND THE CABIN RT EMERGENCY LIGHT LENS MISSING ABOVE GALLEY, REPLACED THE LENS & CHECK NORMAL IAW AMM 33-52-04 .SDR IPXA2018021926652Battery Pack · dischargedINSPECTION TYPE: PDC, FOUND DURING PDC EMERGENCY BATTERY POWER SUPPLY, NR 1 LOW. THE BATTERY WAS REPLACED IAW AMM 33-51-01-401, REV 90.04. TESTED SATISFACTORY.SDR FDEA201802180431Anti-Ice Valve · failedLEVEL 1 ENGINE ANTI-ICE OFF ALERT DURING CLIMB OUT, WITH ANTI-ICE NR 2 ENGINE SELECTED. ALSO HAD AN ANTI-ICE DISAGREE ON SELECTOR. REMOVED AND REPLACED THE NR 2 ENGINE ANTI -ICE VALVE IAW AMM 30-22-01-4. ADJUSTMENT AND TESTED GOOD IAW AMM 30-22-00-5-1.SDR FDEA201802180430Anti-Ice Valve · failedHAD A LEVEL 1 ENGINE ANTI-ICE OFF ALERT DURING CLIMB OUT. WITH ANTI-ICE NR 2 ENGINE SELECTED. REMOVED AND REPLACED THE NR 2 ENGINE ANTI -ICE VALVE IAW AMM 30-22-01-4. ADJUSTMENT AND TESTED GOOD IAW AMM 30-22-00-5-1. ENGINE RUN PERFORMED.SDR FDEA201802200431Warning System · activatedHAD LEVEL 1 ENG ANTI-ICE OFF ALERT ON CLIMB OUT WITH A/I ENGINE 2 SELECTED. ALSO HAD A/I DISAGREE ON SELECTOR.SDR IPXA2018021826615Solenoid · inoperativeL1 ELECTRIC ACTUATORS INOPERATIVE. R & R THE DOOR LOCK PIN RELEASES SOLENOID IAW AMM 52-10-06-401 & OPS CHECKED GOOD IAW AMM 52-10-06-501.SDR FDEA201802160629Support · corrodedMAIN CABIN, STRUCTURE AROUND MCD CONTROL PANEL SHOWS EVIDENCE OF CORROSION. REMOVED AND REPLACED MCD CONTROL PANEL (SURROUNDING STRUCTURE), P/N'S: FXABA8355-1, FXABA8363-3 INREF TO DWG ABA8359.SDR FDEA201802160473Seat Track · corrodedMAIN CABIN, SEAT TRACK AT BS 430, RBL 26 SHOWS EVIDENCE OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW DWG SP10530218 AND NR 039.SDR FDEA201802150515Floor Support · corrodedMAIN CABIN FLOOR SUPPORT STRUCTURE IS CORRODED AT STA 425, RBL 55. REMOVED AND REPLACED SUPPORT FX-SP11530074-3 REF DWG SP11530074-3.SDR FDEA201802150493Seat Track · corrodedMAIN CABIN, SEAT TRACK SHOWS EVIDENCE OF CORROSION AT BS 495, RBL 18. REMOVED AND REPLACED THE SEAT TRACK IAW DWG SP11530076.SDR FDEA201802140394Fire Detector · faultyON DOWNWIND INTO KDEN GOT NR 3 TRITONE FIRE BELL, LIGHTS IN FUEL AND FIRE HANDLE FOR 5 SECONDS, SHUT ENGINE DOWN PER QRH. DISCHARGED 1 AGENT TO NR 3 ENGINE, FIRE INDICATION WENT AWAY AFTER RETARDING NR 3 THROTTLE TO IDLE. REMOVED AND REPLACED NR 3 ENG RT UPPERSDR FDEA2018100940385Fire Detector · failedON DOWNWIND INTO KDEN GOT NR 3 TRITONE FIRE BELL, LIGHTS IN FUEL AND FIRE HANDLE FOR 5 SECONDS, SHUT ENGINE DOWN PER QRH. DISCHARGED 1 AGENT TO NR 3 ENGINE, FIRE INDICATION WENT AWAY AFTER RETARDING NR 3 THROTTLE TO IDLE. REMOVED AND REPLACED NR 3 ENG RT UPPERSDR FDEA201802140398Sensor · failedLEVEL 2 SLAT DISAG ALERT ON FINAL APPROACH. FULLY CONFIGURED WITH FLAPS 50 DEG. LANDED WITH SLATS STOWED, FLAPS 28DEG IAW JRH. TROUBLESHOT IAW AMM 27-80-00.. INTERROGATED MCDU-FCCS. FAULTED LT SLAT NR 4 SENSOR. REMOVED AND REPLACED IAW AMM 27-84-03-4. SDR FDEA201802140392Seat Track · crackedMAIN DECK SEAT TRACK AT BS 635, LBL 27.5 FOUND CRACKED. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201802140391Seat Track · corrodedMAIN DECK SEAT TRACK AT BS 770, RBL 75.25 FOUND CORRODED. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1, AND EA 1- 5320-T0338510, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201802140389Skin · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION ON RIGHT WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUTS AND ACCESS DOORS, FOUND ONE CRACK INDICATION, XOS 470 TAI DUCT CUTOUT CORNER NR 2 APPROXIMATELY .20 INCH IN LENGTH, REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, R
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