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 FDEA202404300519Brake · damagedNR 1 TIRE REMOVED TO FOM PER AMM 32-41-01-4, REMOVED #1 BRAKE (UNSERVICEABLE) PER AMM 32-43-20-4, FOUND SIGNS OF EXCESSIVE HEAT ON AXLE SLEEVES. REMOVED AXLE SLEEVES PER AMM 32-12-30-4, FOUND DISCOLORATION ON BEARING JOURNALS AND ALSO SOME PITTING ON THE SDR IPXA2024052211513Support Fitting · corrodedFOUND CORROSION ON R/H SIDE SUPPORT FOR O/B FLAP I/B FWD FLAP HINGE ATA 57-55 REMOVE AND REPLACE SUPPORT P/N ARB0029-510 PER MD11 AMM 57-53-01-400-801 AND SRM 51-30 REQUIREMENTS.SDR FDEA202404270518Engine · failedON TO ROLL ENG 2 WOULD NOT MAKE TAKE OFF EPR. RECEIVED RED ENG FAIL LIGHT. REJECTED AT 120 KNOTS. TAKE OFF WEIGHT REQUIRED 62K THRUST LIMITS. AFTER CLEARING RUNWAY, STOPPED UNTIL BRAKE TEMP PEAKED AT 727. TAXIED BACK TO RAMP. ENTERING RAMP TIRE 2 FASDR FDEA202404260298Indicator · failedR1 DOOR PRESSURE TO TEST INOPERATIVE. REMOVED AND REPLACED THE R1 DOOR INDICATOR ASSEMBLY, REMOTE PRESSURE AND OPS CHECKED NORMAL. AC OK FOR SERVICE.SDR IPXA2024042687620Electrical Sys · no testEMERGENCY PWR TEST FAIL REMOVED & REPLACED BOTH MAIN BATTERIES PER AMM 24-34-02 - BATTERY OPS CHECK NORMAL. PERFORMED TEST OF EMERGENCY POWER SYSTEM, TEST INITIALLY PASSED AND THEN BEGAN CONTINUOUSLY RUNNING THE EMERGENCY POWER TEST WITHOUT BEING PROMPTED BY ASDR IPXA2024042552154Light · no testDURING PREFLIGHT EMERGENCY POWER TEST FAIL OPERATIONALLY CHECKED SHIPS BATTERIES, OPS CHECK GOOD, RESET EPCU EMERGENCY POWER TEST GOOD. PER FIM 24-30-03-00SDR FDEA202404230488Lamp · no testR1 SLIDE PRESS TO TEST INOPERATIVE. RELEASED FOR SERVICE PER MEL : 25-61-02. R1 EVAC SLIDE REMOTE PRESS INDICATOR - INOP. PER MEL 25-61-02, VERIFYAND RECORD IN THE AML, EVAC SLIDE SYS PRESS ADEQAUTE ONCE EACH FLIGHT DAY." VERIFIED PRESSURE IS ADEQUATESDR IPXA2024042430017Ceiling Panel · damagedCEILING PANEL IN FRONT OF DOOR AND EMERGENCY LIGHT DAMAGED DURING OPENING OF DOOR DO TO CABLE. FOUND SPRING FOR L1 DOOR SLIDING CEILING BROKEN REMOVED AND REPLACED L1 DOOR SLIDING CEILING PANEL AND SPRING REF MD11 AMM 25-23-23-000 OPS CHECK GOODSDR IPXA2024042330017Ceiling Panel · damagedCEILING PANEL IN FRONT OF DOOR AND EMERGENCY LIGHT DAMAGED DURING OPENING OF DOOR DO TO CABLE. CENTER DAMAGE IS 3 1/2 INCH€™S LENGTH BY 1 1/8 WIDTH FOR THE CENTER FASTER LOCATION. THE RIGHT SIDE WHERE THE FASTENER IS PULLED THROUGH IS 3 INCH€™S LENGTH BY 1 3SDR IPXA2024051808924Attach Angle · brokenFLAP SIDE O/B FLAP I/B HINGE CAGE O/B "S" PANEL ATTACHED ANGLE BROKEN ATA 57-50 ACCOMPLISH EO-90304-REQ1 (VT-SAA EA 011-5753-01-B0201 I/R). ANGLE BRACKET INSTALLATION ON EA : 011-5753-01-B0201 REVISION P1 STEP 5.SDR IPXA2024052395849Hinge Bracket · corrodedFLAP EO - R/H O/B FLAP O/B FWD HINGE #4 LUG BORE HAS CORROSION (114-79) ATA 57 REMOVE AND REPLACE HINGE BRACKET ASSEMBLY P/N ARC0503-504 PER MD11 AMM 57-53-01 REV 96.SDR IPXA2024052395650Hinge Bracket · corrodedFLAP EO - R/H O/B FLAP I/B FWD HINGE #4 LUG BORE HAS CORROSION (114-75) ATA 57 REMOVE AND REPLACE HINGE BRACKET ASSEMBLY, ARC0502-508, PER MD11 AMM 57-53-01/401 REV 96.SDR IPXA2024052389264Hinge · corrodedFLAP EO - L/H O/B FLAP OB FWD HINGE O/B #8 LUG BORE IS WORN (114-53) ATA 57 REPAIR ACCOMPLISHED TO L/H WING O/B FLAP O/B FWD HINGE REF SREO-87943-REQ001 REF LINE#1451.SDR IPXA2024052389256Hinge · corrodedFLAP EO - L/H O/B FLAP O/B FWD HINGE I/B #8 LUG BORE HAS CORROSION (114-51) ATA 57 REPAIR ACCOMPLISHED TO L/H WING O/B FLAP O/B FWD HINGE REF SREO-87943-REQ001 REF LINE#1450.SDR IPXA2024042284630Seat Track · corrodedCORROSION FOUND IN SEAT TRACK WHILE REMOVING LOCK IN POS 1L [REF ORINGAL FAULT T3F18E004BETW] REPAIRED IAW EO-90143. MAJOR REPAIR.SDR IPXA2024041988404Oven · odor**ATB** **EMERGENCY DECLARED** APPROX 30 MIN INTO FLIGHT JUMP SEATERS REPORTED STRONG ELECTRIVAL BURNING SMELL COMING FROM GALLEY AREAS. SMELL BEGAN TO MIGRATE TO COCKPIT DECLARED EMERGENCY ISOLATED JUMPSEAT AREA AND CABIN BUS- DIV. REMOVED AND REPLACED GALLEYSDR IPXA2024041862457Control Unit · failedBLOCK TURN-BACK AT 0829 DUE MECHANICAL. ON APU POWER JUST PRIOR TO ENGINE START ALL ELEC,EXCEPT STANDBY POWER, LOST WITH EXTERNAL POWER RECONNECTED POWER RESTORED, APU POWER AS WELL. REPLACED EPCU IAW MM 24-08-01/401, OPS CHECK NORMAL.SDR IPXA2024051051043Stringer · crackedUPPER CENTER AUXILIARY TANK HAS CRACK LOCATED BETWEEN STA X17 AND X46/STR52. ACCOMPLISHED REPAIR PER EO-90346-REQ1 AND VT-SAA EA 011-5710-01-B0198, REV. I/R.SDR IPXA2024060451189Stringer · crackedUPPER CENTER AUXILIARY TANK HAS CRACK LOCATED BETWEEN STA X17 AND X46/STR49. (015-79) ATA 57. INSTALLED 1EA STRINGER SECTION, 2EA "C" ANGLES REPAIR SPLICE, 2EA "Z" ANGLES REPAIR SPLICE AND 2 EA FITTINGS, AT UPPER CTR AUX TANK, STA X17 AND X46 STR 49 PER REF MDSDR IPXA2024053150485Stringer · cracked[STR] UPPER CENTER AUXILIARY TANK HAS CRACK LOCATED BETWEEN STA X-46 AND X-81/STR44. ACCOMPLISHED REPAIR PER MD-11 SRM 57-10-03-2R-1 REPAIR 1, FIGURE 201 (REVISION 70). AUDIT C/WSDR IPXA2024053150690Stringer · crackedUPPER CENTER AUXILIARY TANK HAS CRACK LOCATED BETWEEN STA X-17 AND X-46/STR47. (015-74) ATA 57. INSTALLED ALL STR. 47 REPAIR PARTS AND REINSTALLED 2 EXISTING SHEAR TIES AT UPPR CENTER AUXILIARY TANK BETWEEN STA. X-30 TO X-57 IAW MD11 SRM 57-10-03-2R-1. ACCOMPSDR IPXA2024052546477Floor Support · corrodedCOURIER FLOOR AREA FWD OF R1 DOOR UNDER LAVATORY HAS CORROSION. INSTALLED FLOOR SUPPORT AT CURIER AREA FWD OF RI DOOR UNDER LAVATORY IAW SRM 51-33-01-51-35-01. REMOVED AND REPLACED FLOOR SUPPOR IAW DWG ABA7341, DWG SP11530074 AND SRM 5100 GUIDELINES.SDR IPXA2024052246418Skin · corrodedMAIN CABIN CTR WING BOX AREA HAS CORROSION ON R/H SIDE BETWEEN STA 1199 - 1219 AND 106 INCH. ACCOMPLISHED REPAIR PER EO-90345-REQ1 AND VT-SAA EA 011-5730-01-B0194, REV I/R.SDR IPXA2024051851130Tank · crackedUPPER CENTER AUXILIARY TANK HAS CRACK LOCATED BETWEEN STA X17 AND X46/STR50. INSTALLED 1EA STRINGER SECTION, 2EA "Z" REPAIR ANGLE SPLICE, 2EA "C" ANGLE REPAIR SPLICE, AND 2EA FITTING, AT UPPER CTR AUX TANK BTW STA X17 AND X46 STR 50 PER REF MD-11 SRM 57-10-03SDR IPXA2024051750844Stringer · crackedUPPER CENTER AUXILIARY TANK HAS CRACK LOCATED BETWEEN STA X17 AND X-17/STR47. (015-75) ATA 57. INSTALLED ALL STR. 47 REPAIR PARTS AND REINSTALLED 2 EXISTING SHEAR TIES AT UPPR CTR AUX TANK BETWEEN STA X3 TO X30 IAW MD11 SRM 57-10-03-2R-1.SDR IPXA2024051850618Stringer · crackedUPPER CENTER AUXILIARY TANK HAS CRACK LOCATED BETWEEN STA X-17 AND X-46/STR50. (015-73) ATA 57. INSTALLED 1 EA STRINGER SECTION, 2 EA "C" ANGLE REPAIR SPLICE, 2 EA "Z" ANGLE REPAIR SPLICE AND 2 EA FITTING, AT UPPER CENTER AUX TANK STA BTW X-17 AND X-46 PER REFSDR IPXA2024051741145Sprocket · wornWORN OUT SPROKET FOR L1 DOOR AFT CLOSURE MECHANISM. REMOVED AND REPLACED 2 EA SPROCKETS ON L1 DOOR AFT CLOSURE MECHANISM DRIVE CHAIN PER. MD-11 DWG ABA7941 REV. S AND ADJUSTED PER. MD-11 AMM 52-11-02-830-801.SDR IPXA2024051049553Skin · crackedWHILE ACCOMPLISHING TASK CARD MXP-7682-JIC FOUND 5 EA CRACKED HOLES ON FUEL LANDING AS MARKED ON PART WITH TAPE. ATA 57-20. INSTALLED 5EA BUSHING REPAIR AT R/H WING FUEL ACCESS PANEL 636AB REF. MD-11 SRM 57-20-02-2R-5 REPAIR 5.SDR IPXA2024051050552Stringer · crackedUPPER CENTER AUXILIARY TANK HAS CRACK LOCATED BETWEEN STA X-17 AND X-46/STR52. ACCOMPLISHED PER EO-90379-REQ1 AND VT-SAA EA 011-5710-01-B0193, REV. I/R.SDR IPXA2024041849724Landing · crackedWHILE ACCOMPLISHING TASK CARD MXP-7633-JIC FOUND 2 EA CRACKED HOLES ON FUEL LANDING AS MARKED ON PART WITH TAPE. ATA. 57-20. INSTALLED 2 EA BUSHING REPAIR AT L/H WING FUEL ACCESS PANEL 536AB REF. MD-11 SRM 57-20-02-2R-5 REPAIR 5.SDR IPXA2024041741145Sprocket · wornAPG - WORN OUT SPROCKET FOR L1 DOOR AFT CLOSURE MECHANISM ATA 52-10.SDR IPXA2024060130995Spar Cap · corrodedLEFT HORIZONTAL STABILIZER LOWER BARREL NUT, 2ND FROM REAR, HAS EXTENSIVE CORROSION IN ITS CAVITY. CAP/PLUG IS BLOWN OUT. ACCOMPLISHED REPAIR PER EO-90520-REQ1 (EA 011-5510-01-B0186, REV. IR).SDR IPXA2024060130410Spar Cap · corrodedCAP/ PLUG IS COMING OUT OF ITS BORO PLUG HOLE, FRONTMOST, UNDERSIDE OF HORIZONTAL STAB/ TAIL TANK, RT SIDE. ACCOMPLISHED REPAIR PER EO-90209-REQ1 AND EA 011-5510-01-B0189, REV. IR.SDR IPXA2024060130520Spar Cap · corrodedHORIZONTAL STABILIZER LOWER BARREL NUT, R/H REARMOST POSITION, HAS EXTENSIVE CORROSION IN ITS CAVITY. CAP/ PLUG IS BLOWN OUT. ACCOMPLISHED REPAIR PER EO-90521-REQ1 (EA 011-5510-01-B0188, REV. IR).SDR IPXA2024060130121Spar Cap · corrodedRIGHT HORIZONTAL STABILIZER LOWER BARREL NUT, 2ND FROM REAR, HAS EXTENSIVE CORROSION IN ITS CAVITY. CAP/ COVER IS BLOWN OUT. REPAIR ACCOMPLISHED PER EO-90521-REQ1 (EA 011-5510-01-B0188, REV. IR).SDR IPXA2024060131048Spar Cap · corrodedCAP/ PLUGS ARE COMING OUT OF THEIR BORO PLUG HOLES, 1ST AND 2ND FROM FRONT, UNDERSIDE OF HORIZONTAL STAB/ TAIL TANK, LT SIDE. MKD AS DB-1Z AND DB-1E. ACCOMPLISHED REPAIR PER EO-90205-REQ1 AND VT-SAA EA 011-5510-01-B0187, REV. IR.SDR IPXA2024060130260Panel · corrodedCAP/ PLUG IS COMING OUT OF ITS BORO PLUG HOLE, 3RD FROM BACK, UNDERSIDE OF HORIZONTAL STAB/ TAIL TANK, RT SIDE. ACCOMPLISHED REPAIR PER EO-90203-REQ1 AND VT-SAA EA 011-5510-01-B0190, REV. IR.SDR IPXA2024041613694Slide · no testL1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYSTEM INOP R&R REMOTE TEST BATTERIES IAW AMM 25-61-04. THIS CLEARS DEFERRAL 25-61-04.SDR FDEA202404150525Control Valve · failedTIRE FAILURE LEVEL 2 MSG SHORTLY AFTER TOUCHDOWN. #3 TIRE AMBER ON CONFIG PAGE. BUFFET AND LOSS OF BRAKING FELT. GROUND REPORTED THAT WE WERE LOSING PARTS AS WE CLEARED THE RUNWAY. CALLED FOR INSPECTION AND TOW IN. REPLACED #3 SYS 3 ANTI SKID CONTRSDR IPXA2024041597990Relay · faultedTHRUST CONTROL MODULE MAKING SPORADIC AUDIBLE NOISES " CLICKING NOISE" T/S REF WDM 78-34-01-1.1, REPLACED FAULTY TERMINAL BLOCK 37BA REF SWPM 20-26-03. #1 REVERSER INTERLOCK OPS OK REF MM 78-30-00.SDR IPXA2024041582975Master Switch · failedF/O SIDE MASTER WARNING SWITCH DOES NOT CANCEL FIRE AURAL WARNING. CAPT SIDE MASTER WARNING SWITCH WORKS NORMAL R/R F/O SIDE MASTER WARNING SWITCH IAW AMM 31-52-01, OPS CK GOODSDR IPXA2024052567973Cap · corrodedLEFT WING XORS 345-433 LWR T.E. AREA TEE CHANNEL HAS MULTIPLE CORROSION AND SINGLE CRACKED. LOCATED, DRILLED AND INSTALLED REPAIR ANGLE AT GUSSET IAW SRM 57-50-02-2R-9. INSTALLED 1 EA TEE CHANNEL, SIX PANEL ACCESS, THREE ANGLES, THREE STIFFENERS, THREE REPAISDR IPXA2024050268880Frame · crackedFWD AVIONIC COMP INSIDE AREA STA 457-475 RH SIDE FUSELAGE FRAME HAS CRACKED. 74-026 ATA CODE 53. ACCOMPLISHED REPAIR REF. EO-90200-REQ1 (VT-SAA EA 011-5310-01-B0191, REV. IR).SDR IPXA2024050377941Support Channel · damagedTWO HOLES BLOWN OUT OF LOWER FWD CARGO BAY CEILING PANEL SUPPORT CHANNEL, BS 989 IN POSITION 4 AREA. ACCOMPLISH REPAIR PER EA 011-5300-01-B0192, REV I/R , AND EO-90199-REQ1, REV 1.SDR FDEA202404110456Sensor · failedUNSAFE RIGHT GEAR UP INDICATION PRIMARY AND SECONDARY ON DEPARTURE PHNL. CYCLED LANDING GEAR PER QRH GEAR PRIMARY AND SECONDARY GEAR INDICATED UP AND LOCKED. PROCEEDED ON ROUTE PER FLIGHT PLAN. REMOVED AND REPLACED RIGHT GEAR UP AND LATCH SENSOR, CRIMPED NSDR IPXA2024041025711Warning Message · illuminatedATB, EMERGENCY DECLARED. MAX THRUST TO ON CLIMB OUT RECEIVED LEVEL 3 ENG 2 A-ICE DUCT APPROVED. MAX THRUST TO ON CLIMB OUT RECEIVED LEVEL 3 ENG 2 A-ICE DUCT REVIEWED.PERFORMED T/S 30-22-00/101 ENG #2 DUCT TST FAIL, VERIFIED RESISTANCE CHECK BTW PIN 10 AND 1SDR FDEA202404100453Battery · inoperativeEMER LT BAT 1 LO DURING PREFLIGHT REPLACED EMERGENCY LIGHT BATTERY. OPS CHECK GOOD. AMM 33-51-01-4.SDR FDEA202404050444Hydraulic Line · leakingAFTER NUMBER 6 BRAKE CHANGE, APPROXIMATELY 2 HOURS INTO FLIGHT, LEVEL 1 HYD 2 OFF DISPLAYED. RAN QRH. ELECTED TO CONTINUE TO DESTINATION. 2.7 HYD FLUID REMAINING IN RESERVOIR 2. ISOLATING #2 SYS HYD LK PER ABOVE REF. APPEARS TO BE CTR W/W AROUND RMP'S. APSDR FDEA2024040400443Light · inoperativeR1 DOOR SLIDE PTT LIGHT INOP.SDR FDEA202404040443Connector · looseR1 DOOR SLIDE PTT LIGHT INOP. FOUND LOOSE CONNECTION AT PTT LIGHT ON R1 DOOR. TIGHTEND CONNECTOR. OPS CHECK GOOD IAW SWPM 20-31-08
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