Boeing 787-8
Service difficulty reports · 1,765
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 = '7878' 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 = '7878' 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 CALA2015092500800Battery · dischargedB787-33-3-0002 L2 DOOR EXIT SIGN EMER LIGHTS NO ILLUMINATION. REPLACED L2 DOOR AREA CEILING PANEL FWD WCU M3351037 & BATTERY. EMER LIGHT OPERATION TEST RESULTED NORMAL IAW AMM 33-51-07.SDR AALA20150922011Warning System · false activationAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CRUISE, RECEIVED VMO GEAR DOWN INDICATION. ACCOMPLISHED DD6 32-30-01 IAW MM 32-00-00-6A 521B-A. RESELECTED NORM FOR OVER SPEED WARNING, NO FURTHER FAULTS. OPERATIONAL CHECKED NORMAL.SDR ASMF201510017Oxygen Bottle · leakingAIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO DURING CRUISE AT 38,000 FEET, THE CREW OXYGEN LOW LIGHT TURNED ON. PERFORMED AN OXYGEN CREW INSPECTION IAW AMM 35-12-85, DETECTING OXYGEN BOTTLE MANOMETER WAS INDICATED 0 PSI. THE OXYGEN BOTTLE WAS REPLACED IASDR AALA20150909019Unknown · leakingDURING TAXI OUT, RECEIVED A FUEL IMBALANCE CAUTION, LT TANK LOW INDICATION. PAXS & FLIGHT ATTENDANTS REPORTED FUEL LEAKING FROM THE RT WING. PUT ACFT IN SAME CONFIGURATION AS REPORTED DURING DISCREPANCY. ACCOMPLISHED FIM 28-10-F1-01A FOR FUEL LEAKAGE WITH NSDR CALA2015090300728Rib · crackedRIGHT WING REAR SPAR AT WS 481.10, AUX D INBD RIB, AFT UPPER RT ANGLE CRACKED WITH APPROX 4" IN LENGTH. RT WING INBD FIXED TE AUX D, RIB CRACKED AREA, CRACK LENGTH 3". REPAIRED IAW ECRA 5750-04814 REV PART 1 INTERIM REPAIR & FORM 44.0008 ATTACHED ITEM 1 - 11SDR CALA2015090300727Connector · unsecureEMERGENCY LIGHT AT DOOR 2L INOPERATIVE DURING TEST. DOOR 2L EMER LIGHT ELEC PLUG SECURED & TESTED NORMAL IAW AMM 33-51-06.SDR CALA2015090300726Connector · unsecureEMERGENCY EXIT LIGHT ABOVE DOOR 2L INOPERATIVE. SECURED PLUG ON LIGHT ASSEMBLY. SYS CHECKED GOOD IAW 33-51-00-0 0C-320A-A.SDR CALA2015090300725Power Supply · inoperativeEMERGENCY LIGHTS ABOVE DOOR 1R NOT TESTING. REPLACED POWER SUPPLY IAW 33-51-07-01A-720A-A.SDR CALA2015090300724Control Unit · defectiveEMERGENCY LIGHTS ABOVE DOOR 4L & LOWER CREW REST AREA INOPERATIVE. REPLACED BATTERY & WCU IAW 33-51-07-01A-720A-A. SYS CHECKED GOOD.SDR ASMF201510012Actuator · failedDURING TRANSIT CHECK, IT WAS DETECTED A HYD LEAK IN THE HORIZONTAL STABILIZER TRIM ACTUATOR. ACFT WAS SENT TO THE HANGAR. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR IAW DMC-B787-A-27-41-07-00B-520A-A, TESTED CORRECT.SDR ASMF201510007Heat Exchanger · failedDURING TRANSIT CHECK, IT WAS DETECTED A FLUID LEAK IN THE AFT GALLEY. THE AFT GALLEY WAS CLEANED. PERFORMED REVISION & CLEANING IAW AMM DMC-B7878-A-12-25-01-02A-258A-A, NO CONFIRMING FLUID LEAK. AS PRECAUTIONARY ACTION, THE AFT GALLEY WAS DEFERRED IAW MEL 2SDR AALA20150821009Actuator · faultyAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB THE RT MLG WOULD NOT RETRACT. R & R RT MLG DRAG BRAKE ACTUATOR IAW DMC-B787-A- 32-32-04-00A-520AA720A-A-1A-C. ACCOMPLISHED RT MLG DRAG BRACE INSTALLATION TEST IAW DMC-B787-A -3SDR CA150917002Actuator · leaking(CAN) DURING WALK AROUND CHECK, FOUND OIL LEAKING FROM STABILIZER COMPARTMENT. FOUND HEAVY LEAK FROM HSTA. HSTA REPLACED IAW DMC-B787-A-27-41-07-00B-520A-A & DMC-B787-A-27-41-07-00B-720A-A.SDR AALA20150727012Radar · failedAIRCRAFT ENCOUNTERED SEVERE HAIL WHICH CRACKED THE COCKPIT LEFT SIDE WINDOW. THE WEATHER RADAR ALSO FAILED. EMERGENCY DECLARED, AND LANDING UNEVENTFUL .SDR CA150729001Oil Cooler · leaking(CAN) DURING MAINTENANCE TESTING FOR TROUBLESHOOTING OF AN AUTO-SHUTDOWN AT THE PREVIOUS FLIGHT, OIL SPRAY REPORTEDLY ORIGINATED FROM THE OIL COOLER AND CAUGHT FIRE. THE FIRE WAS EXTINGUISHED USING EXTERNAL EXTINGUISHERS. NO OBVIOUS DAMAGE WAS REPORTED AT THSDR ASMF201509002Motor · failedDURING TRANSIT CHECK, IT WAS DETECTED MSG IN EICAS & STATUS OF FLIGHT CONTROLS & SPOILERS WERE NOT FOLLOWED THE COMMAND. PERFORMED REVISION AT FLIGHT CONTROLS SYS IAW DMC B787-A-27-61-18-00A-720A-A, DETECTING THE SPOILER ELEC MOTOR UNIT POSITIONS 4, 5, 10 & 1SDR CALA2015072100593Connector · looseROW 33 & BACK BOTH SIDES EMER EXIT LIGHTS ARE ON. REF DMC-B787-A-33-51-07-01A-720A-A. TRIED NEW WCU AT DR 4R & 3L, NO HELP. SOFTWARE, NO HELP. TRIED NEW WCU AT 38D, NO HELP. REF WD DMC-B787-A-33-51-11-10A-051A-D. FOUND CONNECTOR ON 38D SEAT LOOSE. CONNECSDR CA150715004Unknown · malfunctioned(CAN) RECEIVED REPORT FROM ATC, THEY LOST COMMUNICATION FOR 61 MINUTES. THEY TRIED ELCAL & EMER FREQUENCY BUT NO RESPONSE FROM FLIGHT. ATC REQUEST FOLLOW UP & REPORT FROM FLIGHT CREW. RESOLUTION MX TESTED ALL THE RADIOS & FOUND NO FAULT WITH THEIR OPERATIONSDR CA150708003Fan · broken(CAN) METAL CHIP FOUND FROM LT PACK EXHAUST AREA BEFORE DEPARTURE FOUND RAM FAN BLADE BROKEN AND RAM FAN LT STS MSG APPEARED. ALSO FOUND WATER SPRY LINE DE-BONDED FROM DUCT ASSY RESOLUTION LT RAM FAN REPLACED IAW DMD 787-A-21-52-33-00B WATER SPRY LINE RE-BONDSDR ASMF201507019Smoke Detector · malfunctionedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO AFT CARGO FIRE WARNING & MASTER FIRE WARNING LIGHTS TURNED ON & FIRE DETECTION SYS WAS ACTIVATED. DURING MX REVISION, THE DISCHARGE LIGHT WAS FOUND ON & CARGO FIRE EXTINGUISHER BOTTLES WERE FOUND DISCHARGED. PSDR ANCF2015062502Warning System · false activationAFTER ENGS START SPOILERS, MSG ADVISORY SHOWS ON EICAS. SPOILER NR 4. SPOILERS ELEC SYS TEST, AMM B787-A-27-61-00-03B-300B-A WAS PERFORMED SUCCESSFULLY.SDR ANCF2015062501Fuel/Oil Cooler · defectiveENGINE FUEL FILTER RT APPEAR ON EICAS AFTER TAKEOFF. IAW PCM B787 - 81202-A7701-00, DMC A-R79-21-11-00E-720-A-A. THE ENG FUEL & OIL HEAT EXCHANGER WAS REPLACED ON RT ENG & IAW B787-A-R71-00-00-16B-364A-A. FUEL & OIL LEAK TEST WAS DONE & SATISFACTORY.SDR ANCF2015052701Eec · malfunctionedDURING FLIGHT AV0085 ENG LT FAILED PRIOR TO TOP OF DESCENT. THE NNC WAS PERFORMED, RELIGHT WAS ATTEMPTED BUT ENG STAYED FAILED. THE LT ENG ELECTRONIC CONTROL WAS REPLACED. RUN-UP TEST WAS SATISFACTORY.SDR CA150618008Combust Chamber · damaged(CAN) NUMBER 2 ENG WAS ISSUED A CNR ON MAY 5TH, 2015 WITH A 7 DAY COMPLIANCE TO INSPECT IAW SB 72-0239. AN ENG CHANGE WAS PLANNED MAY 12TH TO CARRY OUT INSPECTION OFF WING. THIS WAS DONE TO MINIMIZE THE GROUND TIME FOR THE ACFT. INSPECTION REVEALED EARLY SIGSDR CA150427003Line · leaking(CAN) CREW REPORTED LT HYD SYSTEM FLUID LOSS AND RETURNED. RESOLUTION RT FLAPER ON POWER CONTROL UNIT RETURN LINE, LT HYD SYS, TIGHTENED IAW DMC B787-A-20-11-00-00A-030A-A.SDR ASMF201506001Thrust Reverser · damagedDURING TRANSIT CHECK, IT WAS DETECTED THREE LIGHTNING STRIKES IN LT ENG LOCATED AT 03:00 POSITION. PERSONNEL PERFORMED A LIGHTNING STRIKE CONDITIONAL INSPECTION IAW DMC-B787-A-05-51-19-00C-280B-A, DETECTING TWO DAMAGES ON LT ENG OTBD REVERSER AT 09:00 POSITIOSDR ANCF2015032501Warning System · false activationACCORDING AT 60 KNTS FAULT, FDE ENG EEC MODEL MSG, ADVISORY SHOWS ON EICAS ADVISORY 732 113 71 73-90781 EEC, LT ENG, ALTERNATE CONTROL MODE IS SELECTED. IT WAS PERFORMED FI ALL EEC GND TEST WAS NORMAL.SDR CALA2015032500207Feeder Cable · burnedNUMBER 2 ENG T1 CONNECTOR, RED, ON INBD STARTER GEN HAS SIGNS OF OVERHEAT, FEEDER BLOCK COVER BURNED THROUGH. R & R R1 VARIABLE FREQUENCY STARTER GEN POWER FEEDER CABLE ASSEMBLY IAW AMM 787-24-21-05-01-520 & 720 & 02B-320. ALL ASSOCIATED CHECKS NORMAL. IDT SDR ASMF201503027Bpcu · failedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO SEVERAL MSGS IN EICAS & STATUS. DETECTED FAIL & REPLACED THE LT BPCU IAW DMC-B787-A-24-41-05-004-520A-A & DMC-B787-A-24-41-05-00A-720-A, TESTED CORRECT. THE OVERWEIGHT LANDING CONDITION INSPECTION WAS NOT NECESDR ASMF201503024Structure · damagedDURING TRANSIT CHECK, CAPTAIN REPORTED LIGHTNING STRIKE. ACFT WAS SENT TO THE HANGAR & LIGHTNING STRIKE INSPECTION WAS PERFORMED IAW DMC-B787-A-05-51-19-00C-280B-A. DETECTED DAMAGED AT STATION 1425 BETWEEN STRINGER 11 & 12. NON-ROUTINE CARD A0224971 WAS GENSDR CA150304003Ovrvolt Protect · overheated(CAN) AFTER PUSH BACK, ENGINE START FDE MSG "ELEC GENERATOR CONTROL UNIT L2". WITH MOC ADVISE PILOTS TRIED 2 GENERATOR RESET. ACFT RETURNED TO GATE. OVERVOLTAGE TRANSIENT PROTECTION UNIT INSTALLED IAW B787-A-24-09-08-00A-720A-A. ENGINE RUN CARRIED OUT WITH SDR ASMF201503021Strip · dentedDURING TRANSIT CHECK, DETECTED A DENT OF 0.750” DIAMETER, 0.014” DEPTH AT STATION 1574 ON AFT EDGE PROTECTION METALLIC STRIP OF AFT CARGO COMPARTMENT DOOR COUNTER FRAME. EVALUATED THE DAMAGE & FOUND IT WITHIN LIMITS IAW DMC B787-A-05-51-00A-280A-A & SRM B787-SDR ASMF201503018Acm · malfunctionedDURING TRANSIT CHECK, SMOKE WAS DETECTED IN CREW & PAX CABINS. PERFORMED FAULT ISOLATION PROCEDURE IAW DMC-B787-A-24-10-F5-G4A-421A-A, DETECTING THE MSG CABIN AIR CPRSR R1 STATUS & MSGS 21-41510 & 21-65211. SO THE ACM WAS REPLACED IAW DMC-B787-A-21-52-02-01ASDR ASMF201503017Oxygen Bottle · leakingAIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB AT 26,000 FEET, THE CREW OXYGEN LOW LIGHT TURNED ON. MX PERSONNEL PERFORMED AN OXYGEN CREW INSPECTION IAW MM 35-12-85, DETECTING OXYGEN BOTTLE MANOMETER WAS INDICATED 310 PSI. THE OXYGEN BOTTLE WAS REPLACED IAWSDR CA150212006Oil Cap · missing(CAN) APPROXIMATELY 5 HOURS AFTER DEPARTURE THE CREW REPORTED A CONTINUING REDUCTION IN LEFT ENGINE OIL PRESSURE AND QUANTITY. AFTER DISCUSSION WITH MOC A DIVERSION WAS INITIATED TO COLD BAY, ALASKA (CDB). PANPAN WAS DECLARED WITH ATC. POWER WAS REDUCED ON THESDR CA150202001Trim System · failed(CAN) DURING CRUISE FLIGHT, CREW HAD A TEMPORARY PITCH MODE FAILURE. GPM R2 RESET & TESTED OK. NO FURTHER AUTO PILOT FAULTS.SDR ZI3R2015013000001Fuel Nozzle · burnedRECEIVED AN ENGINE SET OF GENX NOZZLES. UPON RECEIVING INSPECTION IT WAS NOTED THAT THE NOZZLE HAD BURN OUT ON THE SUPPORT.SDR CA141219007Wire Harness · chafed(CAN) ENGINE1 P9 FADEC HARNESS DAMAGED & CHAFING AGAINST LUBE & SCAVENGE PUMP RESOLUTION WIRE HARNESS W09. REPLACED IAW DMC-787-A-G73-22-01-00A-520A & DMC-B787-A-G73-22-01-00A-720A. TESTED OK.SDR CALA2014111901463Unknown · odorBURNT RUBBER SMELL ONLY L4 & R4 BETWEEN JUMP SEAT & REST ROOM. TURN OFF ALL LIGHTS IN THESE AREAS & AFT GALLEY. SMELL DISAPPEARED INSPECTED ALL LIGHTING SYS AT AFT GALLEY & DOOR 4L & R4 AREA, ALSO INSPECTED ABOVE GALLEY CEILING AREA. NO EVIDENCE OF BURNING SDR ZI3R2014111300001Fuel Nozzle · burned outRECEIVED AN ENGINE SET OF NOZZLES. ON RECEIVING INSPECTION IT WAS NOTED THAT TWO NOZZLES HAD BURNED OUT ON THE SUPPORT.SDR CALA2014110701426Elt · no testFORWARD PORTABLE ELT WILL NOT TEST. REPLACED FWD PORTABLE ELT IAW WC 78-2560-1-7800 & MM 25-63-01.SDR ASMF201501009Relay · damagedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING RT ENG START THE RIGHT ENG FUEL VLV RT & ENG SPAR VLV RT LIGHTS TURNED ON. PERFORMED REVISION FIM DMC-B787-A-28-20-F2-25A-421A-A PROCEDURE, SHOWING FAILURE CODE 24-1232 & 28-17303 & MSG RT ENG SOV, DETECTING THE RELSDR ASMF201501007Skin · dentedDURING TRANSIT CHECK, IT WAS DETECTED A LIGHTNING STRIKE IN THE RIGHT LOWER WING SKIN. PERFORMED A LIGHTNING STRIKE INSPECTION IAW AMM DMC-B787-A-05-51-19-00C-280B-A, DETECTING A DENT IN THE STATION 268.70 BETWEEN STRINGER L 13-14, RIB 3-4 WITH DAMAGES OF 2.0SDR ASMF201408001Ram Air Turb · deployedAIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, THE EICAS MESSAGE RAT EXTEND & RAT UNLOCKED LIGHT TURNED ON, WITH THE LANDING GEAR LEVER IN UP POSITION. DURING MAINTENANCE REVISION, THE RAM AIR TURBINE WAS FOUND EXTENDED. ACFT WAS SENT TO THE HANGAR & THE NSDR ASMF201407002Warning System · false activationCAPTAIN REPORTED THAT DURING APPROACH, THE AHM EICAS MSG OF OVERSPEED WAS REACHED WITH MORE 15 KNOTS. PERFORMED FLAP & SLAT DOWN OVERSPEED OR ABOVE 20,000 FEET CONDITION INSPECTION IAW AMM DMC-B787-A-05-51-08-00B-280B-A, PHASE I, NO DAMAGES WERE FOUND.SDR ASMF2014061706012Tube · leakingDURING TRANSIT CHECK, IT WAS DETECTED A FUEL LEAK IN THE RT ENG STRUT SUPPLY TUBE. THE STRUT SUPPLY TUBE WAS REPLACED IAW DMC B787-A-28-22-21-03B-520A-A 720A & THE ENG FUEL FEED MANIFOLD LEAK TEST WAS PERFORMED IAW DMC-B787-A-28-22-21-23B-364A-A & DMC-B787-A-SDR ASMF2014061706011Cowling · dentedDURING TRANSIT CHECK, DETECTED A DENT IN LT ENG INLET COWL NOSE AT 2:30 HRS POSITION OF 3 INCH LENGTH, 0.031 INCHES IN DEPTH, 1 INCH WIDE WITH MISSING MATERIAL & THREE SCRATCHES OF 0.875 INCHES, 2 INCHES & 1.5 INCHES OUT OF LIMITS IAW AMM DMC-B787-A-54-11-01-0SDR ASMF201406001Tube · leakingDURING TRANSIT CHECK, IT WAS DETECTED A FUEL LEAK IN THE RT ENG STRUT SUPPLY TUBE. THE STRUT SUPPLY TUBE WAS REPLACED IAW DMC B787-A-28-22-21-03B-520A-A 720A & THE ENG FUEL FEED MANIFOLD LEAK TEST WAS PERFORMED IAW DMC B-787-A-28-22-21-02B-364A-A, TESTED CORRSDR ASMF201403015Oxygen Bottle · leakingAIRCRAFT RETURNED OF FLIGHT DUE TO DURING CRUISE, THE OXYGEN CYLINDER WITH 0 PSI IN THE CABIN CREW. AT TIJ, PERFORMED AN OXYGEN CREW INSPECTION IAW MM 35-12-85, DETECTING OXYGEN LEAK IN THE BOTTLE & THE MANOMETER WAS INDICATED 0 PSI, SO THE OXYGEN BOTTLE WAS SDR ASMF201403006Oxygen Bottle · leakingAIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT IAD DUE TO A LEAK ON CREW OXYGEN SYS. MX PERFORMED AN OXYGEN CREW INSPECTION IAW MM 35-12-85, DETECTING OXYGEN LEAK IN THE BOTTLE & THE MANOMETER WAS INDICATED 320 PSI. THE OXYGEN BOTTLE WAS REPLACED IAW AMM DMC-B
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