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 AALA20170213008Battery Pack · inoperativeFLIGHT ATTENDANT EMERGENCY FLASHLIGHT BY L4 DOOR AFT STATION IS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW DMC-B767-A-25-64-00. OPS CHECKED GOOD.SDR AALA20170206013Tire · leakingAIRCRAFT WAS NOT GROUNDED. EMERGENCY DECLARED. DURING CLIMB RECEIVED AN EICAS MESSAGE NR 5 MAIN TIRE PRESSURE. PRESSURE GRADUALLY DECREASED TO 0. ITEM DEFERRED. REMOVED AND REPLACED NR 5 WHEEL ASSEMBLY IAW AMM 32-45-01.SDR AALA20170207006Attach Fitting · dirtyAIRCRAFT WAS NOT GROUNDED. L2 DOOR EMERGENCY EVACUATION SLIDE LEVER IS DIFFICULT TO PLACE IN ARMED POSITION. CLEANED DEBRIS FROM GIRT BAR ATTACH FITTING IAW AMM B767-A-52-11-00. OPERATIONAL CHECK GOOD.SDR ANCF2017012401Ring · leakingDURING FLIGHT, AN EICAS FOR THE ENGINE OIL QUANTITY SHOWED LO LEFT ENGINE. SEALING RINGS OF LP TURBINE BEARING HOUSING COVER LT ENGINE REPLACEMENT.SDR AALA20170125006Control Unit · faultyAIRCRAFT WAS NOT GROUNDED. L1 DOOR WIRELESS EMERGENCY LIGHTING SYSTEM CONTROL UNIT BATTERY POWER FAILURE DATA MESSAGE. REMOVED AND REPLACED PRIME CONTROL UNIT IAW DMC-B787-A-33-51-07. OPERATIONAL CHECK GOOD.SDR ASMF20170301004Compressor · inoperativeCAPTAIN REPORTED THAT DURING DESCENT, THE CAC R1 WAS DEFERRED AND THE CAC R2 WAS INOPERATIVE. MAINTENANCE PERSONNEL PERFORMED VISUAL INSPECTION OF CAC R2 AREA IAW DMC B787-A-21-51-19-03A-520A, DETECTING A PUNCTURE HOLE ON CAC CASE BODY, AN AIR DUCT BURST AND PSDR CALA2017012200153Battery · dischargedEMERGENCY FLASHLIGHT AT 2L AFT TEST RED. REPLACED FLASHLIGHT BATTERY AT POSITION 2L AFT. TEST NORMAL.SDR AALA20170123009Smoke Detector · false activationAIRCRAFT WAS NOT GROUNDED. DURING MIDFLIGHT, THE SMOKE DETECTOR IN LAVATORY 3F-1RC EMITTED A WARNING INDICATION. NO SMOKE OR FIRE WAS NOTED. TESTED THE SMOKE DETECTOR IAW AMM DMC-B787-A-26-13-00-00B-320A-A. OPERATIONAL CHECK GOOD.SDR ASMF20170202001Actuator · damagedCAPTAIN REPORTED THAT DURING APPROACH, THE MESSAGE IN EICAS AND STATUS SLAT DRIVE. AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERFORMED THE FIM PROCEDURE IAW DMC-B787-A-27-80-F1-33A-421A-A, DETECTING GEAR ROTATORY ACTUATORS ON SLAT 11, LANYARD SKEW AND BLSDR AALA20170113028Control Unit · failedAIRCRAFT NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHTING ROWS 1 THROUGH 3 BOTH SIDES FAILED TEST. REMOVED AND REPLACED WIRELESS EMERGENCY LIGHTING SYSTEM CONTROL UNIT IAW DMC-B787-A-33-51-07. OPERATIONAL CHECK GOOD.SDR CALA2017010900046Flashlight · inoperativeEMERGENCY FLASHLIGHT AT 2R FWD NOT WORK PROPERLY. TEST INDICATION IS RED TRANSFERRED FOR DEFERRAL. 2R FWD EMERGENCY FLASHLIGHT AS INOP IAW MEL 2564B. PLACARDED INOP. EMERGENCY FLASHLIGHT AT 2R DOOR FWR TEST PFMD IAW DMC-B787-A-25 -6400-04B-320A-A TEST PASSED ASDR ASMF201702004Brake · failedDURING TRANSIT CHECK, AN EICAS AND STATUS BRAKE MESSAGE WAS SHOWN. PERFORMED FIM DMC-B787-A-32-40-F1-U7A-421A-A PROCEDURE, CONFIRMING THE FAILURE THE MLG BRAKE ASSY NUMBER 8 WAS REPLACED IAW DMC-B787-32-45-07-00A-720A /-520A AND THE RIGHT MAIN LANDING GEAR JSDR AALA20170103001Battery · dischargedAIRCRAFT NOT GROUNDED. AIRPLANE HEALTH MONITORING ALERT FOR L1 DOOR EMERGENCY LIGHT SYSTEM PRIME CONTROL UNIT BATTERY POWER FAILURE. REMOVED AND REPLACED L1 DOOR WIRELESS EMERGENCY LIGHTING SYSTEM CONTROL UNIT BATTERY IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.SDR AALA20170104006Battery · dischargedAIRCRAFT NOT GROUNDED. EMERGENCY FLASHLIGHT FORWARD CREW BUNK IS DISCHARGED. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.SDR AALA20161228021Battery Pack · dischargedFLIGHT ATTENDANT FLASHLIGHT AT R3 DOOR HAS A BATTERY WITH A LOW CHARGE. REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECKED GOOD.SDR AALA20161222001Concentrator · faultyFLIGHT ATTENDANT PANEL EMERGENCY EVACUATION SIGNAL SYSTEM IS INOPERATIVE. REMOVED AND REPLACED REMOTE DATA CONCENTRATOR IAW AMM DMC-B787-A-42-21-07-06A-720A-A. OPERATIONAL CHECKED GOOD.SDR CALA2016122101137Light · malfunctionedEMERGENCY LIGHTS DO NOT COME ON WHEN COMMANDED ON IN SEVERAL POSITIONS. PERFORMED RESET AND TS IAW DMC 787-A-33-50-F1-X1A-421A-A ALL EMERGENCY LIGHTS NOW OPS OK.SDR AALA20161221019Battery · inoperativeCAPTAIN`S EMERGENCY FLASHLIGHT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM DMC-B787-A-25-64-00-00B-921A-A. OPERATIONAL CHECKED GOOD.SDR AALA20161220011Transceiver · faultyLOST RADIO COMMUNICATION. EMERGENCY DECLARED, FLIGHT RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED BOTH HIGH FREQUENCY COUPLERS IAW AMM 23-11-03 AND LEFT HIGH FREQUENCY TRANSCEIVER IAW AMM 23-11-05. OPERATIOSDR AALA20161218005Coupler · faultyLOST RADIO COMMUNICATION. EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED BOTH HIGH FREQUENCY COUPLERS IAW AMM 23-11-03 AND LEFT HIGH FREQUENCY TRANSCEIVER IAW AMM 23-11-05. OPERATIONALSDR AALA20161216003Bottle · faultyL1 DOOR EMERGENCY POWER ASSIST SYSTEM PRESSURE BOTTLE ASSEMBLY STATUS MESSAGE. REMOVED AND REPLACED EPAS BOTTLE ASSEMBLY IAW 52-11-22. OPERATIONAL CHECK GOOD.SDR AALA20161216004Brake Assy · faultyMAIN LANDING GEAR BRAKE THREE ACTUATOR MESSAGE DISPLAYED AFTER SHUTDOWN. REMOVED AND REPLACED BRAKE ASSEMBLY IAW AMM 32-45-07. OPERATIONAL CHECKED GOOD.SDR CALA2016121201068Battery Pack · inoperativeR1 DOOR FLASHLIGHT HAD NO PRESS TO TEST INDICATION. R & R THE BATTERY PACK ,OPS CHECKED OK.SDR CALA2016120901037Insert · corrodedINSERTS FOUND CORREDED IN FWD MID AND AFT WET AREA ON FLOOR PANELS , REPLACED CORRODED INSERTS IAW SRM 53-00-50-01A-030A-A PARA 7,SDR AALA20161202013Controller · faultyAIRCRAFT NOT GROUNDED. EICAS MESSAGE/AMBER GENERATED, *BRAKE* SYNOPTIC INDICATION NR 8 BRAKE. FOUND NR 8 BRAKE ACTUATOR HAS A BAD CONNECTOR. REMOVED AND REPLACED RIGHT OUTBOARD ELECTRONIC BRAKE ACTUATOR CONTROLLER IAW AMM 32-41-02. OPERATIONAL CHECK GOOD. SDR AALA20161123014Bracket · dirtyL2 DOOR SLIDE DIFFICULT TO ARM. REMOVED DEBRIS IN GIRT BAR FLOOR BRACKET. OPERATIONAL CHECKED GOOD.SDR AALA20161118007Control Unit · inoperativeL1 DOOR AFT EXIT LOCATOR SIGN IS INOPERATIVE. REMOVED AND REPLACED L1 DOOR WIRELESS CONTROL UNIT IAW AMM 33-51-07. OPERATIONAL CHECK NORMAL.SDR AALA20161117005Battery Pack · inoperativeL1 DOOR FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.SDR AALA20161115011Control Unit · faultyAIRCRAFT WAS NOT GROUNDED. AISLE EMERGENCY LIGHTS ON BOTH SIDES OF ROWS 25 THRU 30 ARE INOPERATIVE. REMOVED AND REPLACED R4 DOOR WIRELESS CONTROL UNIT ASSEMBLY IAW AMM 33-51-07. OPERATIONAL CHECK NORMAL.SDR AALA20161115003Battery · faultyAIRCRAFT WAS NOT GROUNDED. WELS UNIT 4 SHOWS ACTIVE MESSAGE FOR DEGRADED BATTERY. REMOVED AND REPLACED WELS UNIT 4 BATTERY IAW AMM 33-51-07. MESSAGE WENT INACTIVE AND OPERATION CHECK NORMAL.SDR ASMF20161216010Valve · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING START ENGINES, THE LEFT ENGINE AUTO STAR SYSTEM FAILED. MAINTENANCE PERSONNEL PERFORMED REVISION TO AUTO STAR SYSTEM, DETECTING THE EICAS MESSAGE FAIL, MAINTENANCE CODE 28-19217 AND THE CIRCUIT BREAKER C2822803 POPPESDR CALA2016111100874Battery · dischargedEMERGENCY LIGHTS INOP AT DOOR 1L. T/S IAW FIM 33-50-F1-W5A-421A. R&R CONTROL UNIT BATTERY ABOVE DOOR 1L IAW AMM B787-A-33-51-07-02B-520A-A. E- LIGHTS AT DOOR 1L OPS CHECK GOOD.SDR AALA20161114005Circuit Breaker · trippedAIRCRAFT WAS NOT GROUNDED. DURING CRUISE FLIGHT CREW RECEIVED A FUEL IMBALANCE EICAS MESSAGE AND ACCOMPLISHED THE FUEL IMBALANCE CHECKLIST. SUBSEQUENTLY EICAS MESSAGES LEFT FORWARD FUEL PUMP, LEFT AFT FUEL PUMP AND FUEL CROSSFEED WERE RECEIVED AND FUEL CONTINUSDR AALA20161106003Control Unit · inoperativeAIRCRAFT WAS GROUNDED. EMERGENCY EXIT LIGHTS ABOVE SEATS 8D AND 8H ARE INOPERATIVE. REMOVED AND REPLACED WIRELESS CONTROL UNIT NR 18 IAW AMM 33-51-07. OPERATIONAL CHECK NORMAL.SDR CALA2016110400855Strainer · dirtyRIGHT ENG PRESS DOWN TO BETWEEN 49 AND 54 PSI RETURNED TO SFO PER TOMC. ACP INSP NR 2 ENG OIL SYS (SCREENS, MCD & FILTER) NO DEBRIS FOUND ACP AVO0556 FOUND DEBRIS AT STRAINER, CLEANED AND REINSTALLED LEAK CK GOOD. REFER TO 72-DIP FOR FOLLOW-UP ACTION. ACFT SDR AALA20161028006Battery · dischargedAIRCRAFT NOT GROUNDED. WIRELESS EMERGENCY LIGHTING CONTROL UNIT BATTERY INOPERATIVE IN L4 DOOR ZONE. REMOVED AND REPLACED BATTERY IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.SDR ASMF20161216004Seal · leakingDURING OVERNIGHT CHECK AND THE EO 8772004 ISSUED TO REPLACE THE TRANSFER GEARBOX (TGB) ON BOTH ENGINES, MAINTENANCE PERSONNEL DETECTED OIL LEAK IN RIGHT TGB SLEEVE; SO THE RIGHT TGB SLEEVE SEALS WERE REPLACED IAW AMM DMC-B787-A-G72-01-00A-520A-A AND TEST 4 PARSDR ASMF20161216003Warning Light · illuminatedAIRCRAFT RETURNED TO PLATFORM DUE TO AFTER START ENGINES, THE RIGHT ENGINE CONTROL LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED BITE TO CMCF IAW FIM DMC-B787-A-G13-20-F1-52A-421A-A, SHOWING FAILURE CODE 73-11152 AND DURING CHANGE OF THE CONFIGURATION TYPE SDR AALA20161012011Manifold · brokenDURING CRUISE NR 2 ENGINE AUTO SHUT DOWN. ATTEMPTED RESTARTS WERE UNSUCCESSFUL. EMERGENCY DECLARED. LANDING UNEVENTFUL. MAINTENANCE FOUND NR 2 ENGINE FUEL NOZZLE MANIFOLD BROKEN ON OUTER LEFT SIDE. REMOVED AND REPLACED FUEL MANIFOLD IAW AMM 73-11-05. OPERASDR ASMF201611021Control Unit · failedDURING TRANSIT CHECK, THE MESSAGE IN EICAS AND STATUS OF THE STAB L2, CABIN AIR CPRSR L-2, FMC CHANNEL C AND STABILIZER LIGHT TURNED ON WERE SHOWN. MAINTENANCE PERSONNEL FIM 27-40 TASK 801 PROCEDURE AND AMM DMC-B787-A-27-40-F1-01A-421A-A, DMC-B787-A-21-50-F1-SDR ASMF201611012Fairing · crackedDURING RIGHT ENGINE 2 DAY CHECK, A BIRD STRIKE EVIDENCE WAS DETECTED AT RIGHT ENGINE AIR COOLER / OIL COOLER (ACOL). MAINTENANCE PERSONNEL PERFORMED THE BIRD STRIKE CONDITIONAL INSPECTION IAW AMM DMC B787-A-05-51-18-00A-280A-A, DETECTING BENT AND MISSING OF FISDR ASMF201611011Line · leakingDURING TRANSIT CHECK, AFTER TO REPLACE OF RIGHT VARIABLE FREQUENCY STARTER GENERATOR, A HYDRAULIC LEAK WAS DETECTED AT TUBE. MAINTENANCE REPLACED THE TUBE IAW AMM A-24-21-09-00B-520A-A / -720A-A, TESTED CORRECT.SDR ASMF201610020Tube · leakingDURING TRANSIT CHECK, AFTER TO REPLACE OF RIGHT VARIABLE FREQUENCY STARTER GENERATOR (VFSG), A HYDRAULIC LEAK WAS DETECTED AT TUBE OF VFSG. AIRCRAFT WAS SENT TO THE HANGAR, MAINTENANCE PERSONNEL REPLACED THE TUBE OF VFSG IAW AMM DMC B787-A-24-21-09-00B-520A-A SDR ASMF201611008Hinge Fitting · damagedCAPTAIN REPORTED THAT DURING CRUISE, A STRONG NOISE IN THE FWD ENTRY DOOR WAS LISTENED; AT THE GATE THE FLIGHT ATTENDANT DETECTED THAT THE HINGE OF THE DOOR WAS FALL DOWN. MAINTENANCE PERSONNEL PERFORMED A REVISION TO FWD ENTRY DOOR IAW SRM 52-10-00, DETECTINGSDR AALA20160907009Display · faultyCREW REPORTED THE STANDBY ATTITUDE INDICATION FAILED. A RESET WAS ATTEMPTED BUT DID NOT RESOLVE THE ISSUE. EMERGENCY DECLARED. LANDING UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED THE INTEGRATED STANDBY FLIGHT DISPLAY IAW AMM 787-81205-A810-00. OPERATIONAL CSDR CALA2016090600623Thrust Reverser · dirtyEICAS AND STATUS MESSAGE FOR LT ENGINE THRUST REVERSER. AFTER REACTIVATING REVERSERS, OPS TESTED IAW DMC-B787-A-678-31-00-15F-320A-A & MESSAGE CLEARED. MESSAGE WAS CAUSED BY DEBRIS IN REVERSERSDR AALA20160908004Regulator · leakingRECEIVED AN EICAS MESSAGE FOR CREW OXYGEN LOW. THE FLIGHT DESCENDED TO FL 250 INITIALLY, AND THEN DESCENDED TO BELOW FL 180 WHEN THE OXYGEN LEVEL WENT TO ZERO PSI. THE FLIGHT DIVERTED TO ANC AND DECLARED AN EMERGENCY DUE TO OVERWEIGHT CONDITION. THE FLIGHT LANSDR CALA2016083000611Battery Pack · inoperativeFWD CREW REST COMPARTMENT EMERGENCY LIGHTS WILL NOT EXTINGUISH WITH ACFT POWER REMOVED AND EMERGENCY LIGHTS SWITCH OFF. CYCLED SWITCH, NO HELP. REMOVED AND REPLACED BATTERY PACK.SDR AALA20160822008Starter Gen · inoperativeR1 GENERATOR DRIVE LIGHT ILLUMINATED. FOLLOWED QRH, DISCONNECTED DRIVE. AN EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. THE AIRCRAFT GROUNDED. REMOVED AND REPLACED RIGHT ENGINE R1 VARIABLE FREQUENCY STARTER GENERATOR IAW ASDR ASMF201611002Actuator · leakingDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE RIGHT MAIN LANDING GEAR RETRACT ACTUATOR. FOUND TO BE OUT OF LIMITS IAW A-A-29-11-00-00C-364-A. AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL REPLACED THE RIGHT MAIN LANDING GEAR RETRACT AC
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