JASC 2820
Service difficulty reports · 3,630
Reports filed under 2820 · Aircraft Fuel Distribution System, newest first.
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 jasc_code = '2820' 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 jasc_code = '2820' 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 ASAA2015010110131Warning Light · false activationDURING CLIMBOUT YELLOW "IMBAL" ALERT APPEARED FOR NR 1 MAIN TANK. CONFIGURATION : ALL 6 BOOST PUMPS ON WITH T/O FUEL =27,000. NR 1 MAIN TANK INDICATED =800 LESS THAN NR 2 MAIN TANK. ACFT GROUNDED. ACCOMPLISHED FQIS BITES REF FIM 28-41, TASK 801, NO FAULT FSDR CA150119011Line · chafed(CAN) FUEL SUPPLY LINE TO FUEL NOZZLE FIRE SLEEVE BANDING CHAFING AFT FIRE WALL.SDR RJEF20150101001Actuator Valve · faultyAFTER STARTING TAXI THE FUEL RT WING TANK OVERFLOW MSG SHOWED ON ECAM. DUE THAT REASON THE ACFT RETURNED TO THE GATE FOR MX. THE ACFT WAS HELD ON GND & PERFORMED FAULT ANALYSIS AS FOLLOWS. IAW TSM 28-26-00-810-805-A, REPLACED THE RELAY 8QL IAW ESPM 20-53-11SDR RAIA201412280001O-Ring · leakingREPORTED FUEL LEAK, RT WING ROOT WITH STRONG FUEL SMELL IN CABIN AND FLT DECK, RETURN TO BLOCK. MAINTENANCE INSPECTED AND REPLACED O'RING ON RT WING FUEL PANEL 641AB, LEAK CHECK GOOD.SDR CA150213013Control Panel · burned(CAN) OPERATOR CALLED TO REPORT THE REFUEL DEFUEL CONTROL PANEL WAS INOPERATIVE. ORDERED A REPLACEMENT PART & THE DEFECTIVE UNIT WAS RETURN TO THE VENDOR. DURING THE TESTING OF THE ASSEMBLY, VENDOR HAS DISCOVERED BURNT BOARDS 548-337-001 & 548-338-001.SDR 2014FA0000711Line · leakingFUEL LINE, THAT GOES FROM THE FUEL SELECTOR TO THE FUEL BOOST PUMP WAS FOUND LEAKING PROFUSELY. HOSE LOOKED TO BE ORIGINAL EQUIPMENT.SDR IGXR2014FA0000710Line · failedAFTER TAKEOFF, LT ENGINE STOPPED PRODUCING FULL POWER. AIRCRAFT SAFELY RETURNED BACK WITH 1 ENGINE. EXAMINED LT ENGINE AND DISCOVERED CYL NR 6 FUEL LINE DETACHED FROM FUEL MANIFOLD, LINE FAILED AT SOLDER JOINT AT MANIFOLD END. R & R CYLINDER NR 6 FUEL LINE SDR SWIA201440520Line · looseTWO MOTIVE FLOW LINES INSIDE THE FUEL PRESSURE BOX ARE LOOSE. REINFORCED THE FUEL LINES IN FUEL PRESSURE BOX IAW REO.SDR CA141204013Line · chafed(CAN) A FUEL LEAK WAS SNAGGED BY THE RIGHT WHEEL WELL ON C-GSKW. THE AME INVESTIGATED AND FOUND THE RIGID FUEL LINE WHICH RUNS THROUGH THE LANDING GEAR WHEEL WELL TO BE CHAFFED THROUGH. CHAFFING WAS CAUSED BY THE BULKHEAD THAT IT RUNS THROUGH.SDR USAA2014111900010Fuel Control · faultyFLIGHT DIVERTED & AN EMER DECLARED DUE TO CABIN ODOR & A CTR FUEL TANK TRANSFER ISSUE DURING CLIMB. CTR TANK FAULT, FUEL PUMPS IN CTR TANK WILL NOT ACTIVATE IN AUTO OR MANUAL. ACCOMPLISHED TSM 28-21-00-810-829-A, OPERATIONAL CHECKED OK FOR SERVICE IAW AMM 28SDR CA141119005Check Valve · malfunctioned(CAN) AFTER TAKEOFF THE FLIGHT CREW NOTICED FUMES IN THE CABIN, AND QUICKLY DETERMINED THE PRESENCE OF SMOKE. THEY DECIDED TO DECLARE AN EMERGENCY AND RETURN TO THE AIRPORT. THE AIRCRAFT LANDED WITHOUT ISSUE. WHILE INVESTIGATING THE CAUSE IT WAS FOUND THAT A SDR 19PB2014110300164Filter · dirtyDURING CLIMB OUT, NR 1 ENGINE BYPASS FILTER ILLUMINATED BRIEFLY, POWER WAS REDUCED AND LEVELED OFF LIGHT EXTINGUISHED, BEGAN CLIMB AGAIN NR 1 ENGINE BYPASS FILTER BRIEFLY ILLUMINATED AGAIN. ACFT RETURN TO BASE. NR 1 ENGINE BYPASS LIGHT DID NOT ILLUMINATED AGASDR UIEA2014103100542Lanyard · damagedLEFT WING FUEL PUMPS ACCESS PANEL 531AB GND CABLE SHREDDED. R & R LANYARD ON ACCESS COVER 531AB IAW AMM 28-22-03.SDR R61A201410241139Tube · corrodedDURING HEAVY CHECK, THE FUEL VENT TUBE IS DEGRADED. MX R & R FUEL VENT TUBE IAW AMM 20-10-13.SDR 39LA20141023103Control Panel · shortedDURING CRUISE FLIGHT, SMOKE & ELEC FIRE SMELL ROSE NEAR THE CTR OF THE WINDSCREEN. FLIGHT CREW ELECTED TO RETURN TO DEPARTURE AIRPORT & SAFELY LANDED. UPON INSPECTION FOUND FUEL BOOST PUMP CONTROL PANEL TO BE SHORTED. R & R FUEL PANEL.SDR AALA20141022019Bypass Switch · inoperativeDURING CLIMB THE LT ENG FUEL FILTER BYPASS INDICATION CAME ON. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R LT ENG FUEL FILTER & FUEL FILTER BYPASS SWITCH. SYS GND CHECKED NORMAL OPERATION CLOSED.SDR SWAA2014102233266Gasket · leakingAIR TURN BACK, RETURNED DUE TO FUEL SPEWING FROM NR 2 ENG. R & R PANEL 633BB GASKET IAW MM.SDR DXTA2014102005913Drain Valve · leakingTHERE IS A STRONG FUEL ODOR IN THE AFT SERVICE COMPARTMENT. R & R AUTOMATIC DRAIN VALV E70QD. OPS & LEAK CHECKED GOOD. FUEL ODOR NO LONGER PRESENT IN AFT SERVICE COMPARTMENT IAW MM 53-80-09-710-801.SDR WX0A2014101572196Valve · leakingFLIGHT ATTENDANTS & PASSENGERS REPORT STRONG FUEL ODOR IN AFT SECTION OF CABIN. APU WAS RUNNING & LT ENG WAS JUST SHUTDOWN. FOUND REFUEL VLV LEAKING AT O RINGS & HANDLE. R & R VLV & OPERATIONS & LEAK CHECKED GOOD. OPERATED PACKS WITH API & ENG WITH NO FURTSDR CA141010016Line · cracked(CAN) WHILE MAINTENANCE WAS CONDUCTING SCHEDULED ROUTINE MAINTENANCE, THE FUEL DRAIN LINE LOCATED AT THE FUEL DRAIN SOLENOID VALVE LOCATED ON THE WING FORWARD SPAR BETWEEN WING STATION 60 AND 91 WAS DISCOVERED TO BE CRACKED OFF UNDERNEATH THE CLAMP THAT ATTACHSDR 2014FA0000558Fuel Line · leakingFUEL LINE HAS DARK STAIN HALF WAY BETWEEN ATTACHMENT AND FITTING. LINE PITTED UNDER PLASTIC ANTI-CHAFING MATERIAL, FUEL WEEP CAUSING STAIN. FOUND DURING ANNUAL.SDR DJFA20140923001Fuel Line · leakingPILOT REPORTED FUEL LEAKING FROM THE BELLY OF THE AIRCRAFT. MAINTENANCE FOUND THE RIGHT ENGINE MOTIVE FLOW LINE CORRODED AND LEAKING INTO THE CENTER FUSELAGE FAIRING. THE LINE WAS REPLACED, LEAK CHECKS GOOD AND THE AIRCRAFT RETURNED TO SERVICE.SDR SWAA2014091632022Actuator · faultyDIVERSION CROSS FEED VLV CB POPPED. R & R FUEL FEED ACTUATOR IAW MM.SDR CA140915004Screen · crushed(CAN) THE LEFT SCAVENGE EJECTOR MESSAGE CAME ON AT THE TOP OF DESCENT AT FL200. ALL ENGINE PARAMETERS WERE NORMAL. MAINTENANCE REPLACED THE LT SCAVENGE EJECTOR ASSY WHICH CLEARED THE DEFECT. THE REMOVED SCAVENGE EJECTOR WAS DISASSEMBLED AND THE INTERNAL SCRSDR ASOA20140910099Flapper Valve · tornPILOT REPORTED A FUEL LEAK FROM THE RT WING DURING CLIMBOUT, LOST 200 LBS. MAINTENANCE R & R THE RT WING FLAP VALVE WITH LEAK CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA2014090511182Fuel Sys · malfunctioned400 LB IMBALANCE DURING CLIMBOUT, LT TANK, DURING FLIGHT, LEFT TANK IMBALANCE INCREASED TO AROUND 900 LBS WITH PUMPS WORKING, FOLLOWED QRH, DIVERTED. ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. PERFORMED OPS CHECK OF FUEL TRANSFER EJECTOR PUMP IAW AMM 28SDR DXTR2014090201Vent Line · chafedFOUND VENT LINE ASSY TO BE WORN THROUGH AT ELBOW. R & R VENT LINE ASSY IAW SB560-28-16.SDR ASAA2014083009001Actuator · faultedNR 1 ENGINE FUEL SHUTOFF VALVE LIGHT ILLUMINATED BRIGHT BLUE. ACFT GROUNDED. ACCOMPLISHED FIM TASK 28-22, TASK 809. FAULT IS DETERMINED TO BE INTERMITTENT. REPLACED NR 1 ENGINE SPAR VALVE ACTUATOR IAW AMM 28-22-11. OPS CHECKED NORMAL.SDR AALA20140826013Pressure Switch · inoperativeRIGHT CTR FUEL BOOST PUMP LOW PRESS LIGHT ON OVERHEAD & DISPLAYED ON EICAS. EMER DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT CTR FUEL LOW PRESS SWITCH. SYS GND CHECKED NORMAL OPERATION CLOSED.SDR ASOA20140819070Flapper Valve · leakingTHE CREW REPORTED FUEL LEAK FROM RT WING DURING FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE FLAPPER VALE AT RIB NR 7 IN RT WING. OPS CHECKED GOOD.SDR EBV2201408220001Flex Hose · leakingWHEN FUEL PUMPS WERE TURNED ON FUEL CAME PORING OUT FROM ON TOP OF THE WING. FOUND THE FLEXIBLE FUEL LINE THAT LEADS FROM THE TOP OF THE CENTER WING ON THE RT SIDE TO BE SPLIT INTERNALLY. THE FUEL LINE WAS REPLACED AND LEAK CHECKED AGAIN WITH NO LEAKS FOUNDSDR 7EMA20140815003Fuel Line · chafedFUEL LINE FROM RT OTBD FUEL TANK TO RT NACELLE TANK CHAFING WHERE IT PASSES THROUGH LIGHTNING HOLE IN FWD SPAR.SDR 7EMA20140815002Fuel Line · chafedFUEL LINE FROM LT OTBD FUEL TANK TO LT NACELLE TANK CHAFING WHERE IT PASSES THROUGH LIGHTNING HOLE IN FWD SPAR.SDR CALA2014081401114Pressure Switch · faultyAIRCRAFT DIVERTED, LT CTR FUEL PUMP LOW PRESS LIGHT. THE RT CTR FUEL PUMP IS ALREADY ON MEL. DID NOT HAVE ENOUGH FUEL TO GET TO FLL. EMER DECLARED TURNED ON LT CTR PUMP DURING FLIGHT & LOW PRESS LIGHT STAYED ON. CTR TANK HAD 4500 LBS FUEL WITHIN. CHECKED SDR SIMA20140812005Fuel Line · crackedLEFT FUEL SOV PRESS REFERENCE LINE CRACKED. R & R CRACKED LT FUEL SOV PRESS IAW EMB 145 AMM 28-00-01.SDR IPXA2015051389060Valve · stuckFLAME OUT LEVEL 2 LAT FUEL UNBALANCE CHECK LIST ACCOMPLISHED. NR 1 FILL VALVE STUCK OPEN MULTIPLE ATTEMPTS TO CLOSE NR 1 FILL VALVE CYCLED BACK TO AUTO AFTER MANUALLY BALANCING FUEL INADVERTANT ENGINE 2 SHUTDOWN DUE TO F/O TURNED OFF NR 2 TRANSFEED PRIOR TO TSDR 2014FA0000560Tube · failedENROUTE, MANIFOLD PRESSURE DROPPED TO 24". INDUCTION TUBE FROM COMPRESSOR TO THROTTLEBODY FAILED WITH A 2" TO 3" HOLE ONLEFT SIDE BLEW OUT.SDR ASAA2014072708750Fuel Sys · out of balanceFUEL IMBALANCE ALERT, LT SIDE AT FL380. RAN CHECKLIST. DID NOT BALANCE. FUEL LEAK CONFIRMED. SHUT NR 1 ENGINE DOWN AND DIVERTED. F/A REPORTED HEARING LOUD UNUSUAL THUD NOISE LT SIDE AT THE SAME TIME. ACFT GROUNDED. DIVERTED. CROSSFEED VALVE FUNCTIONAL TESDR CA140724001Hose · cracked(CAN) DURING SCHEDULED 100HR INSPECTION, THE LT AFT FUEL VENT HOSE WAS FOUND WITH SURFACE CRACKS, AND MINOR LEAK WHEN PRESSURIZED. HOSE REPLACED AND SYSTEM LEAK CHECKED, NO FAULT FOUND.SDR FDEA201407211895Skin · corrodedCORROSION FOUND AROUND ONE FASTENER HEAD UNDER STUB BEAM AT STATION 960 LT ON CTR WING TANK UPPER SKIN. CORROSION REMOVED & AREA REPAIRED IAW EA F-5710-T0309582.SDR FDEA201407211894Skin · corrodedCORROSION FOUND AROUND TWO FASTENER HEADS UNDER STUB BEAM AT STATION 960 RT ON CTR WING TANK UPPER SKIN. CORROSION REMOVED & AREA REPAIRED IAW EA F-5710-T0309582.SDR R61A201407190886Line · corrodedDURING HEAVY CHECK, UNDER LT WING FUEL PANEL 521BB FUEL VENT TUBE SHOW SIGNS OF DEGRADATION AT CONNECTION POINTS. MAINTENANCE R & R LT WING FUEL PANEL 521BB FUEL VENT TUBE IAW AMM 28-10-13.SDR R61A201407190885Line · corrodedDURING HEAVY CHECK, UNDER LT WING PANEL 521AB FUEL VENT TUBE AT CONNECTION POINTS SHOW SIGNS OF DEGRADATION. MX R & R LT WING PANEL 521AB FUEL VENT TUBE IAW AMM 20-10-13,SDR R61A201407190884Line · corrodedDURING HEAVY CHECK, UNDER LT WING FUEL PANEL 521DB FUEL VENT TUBE AT CONNECTION POINTS SHOW SIGNS OF DEGRADATION. MAINTENANCE R & R LT WING FUEL PANEL 521DB FUEL VENT TUBE IAW AMM 20-10-13. PN 170-06023-401, TUBE ASSY.SDR CA140717016Check Valve · missing(CAN) DURING SCHEDULED MAINTENANCE INSPECTION THE INTERNAL FUEL SCREEN WAS FOUND TO BE MISSING FROM THE CHECK VALVE ASSEMBLY, INVESTIGATING.SDR SWAA2014072130132Panel · faultyON DESCENT THRU 180 AN ELEC OR CHEMICAL SMELL FILLED THE COCKPIT. R & R P5 2 MODULE FUEL PANEL IAW MM.SDR ASAA2014071408556Actuator · warning lightNOTICED LT ENGINE SPAR VALVE ILLUMINATED BRIGHT BLUE AT 5000 FT DURING APPROACH. LIGHT WENT OUT AT 2,000 FT. ACFT GROUNDED. CREW STATED ALL NR 1 ENGINE INDICATIONS WERE NORMAL. ACCOMPLISHED GVI OF NR 1 SPAR VALVE CONNECTOR, NO DEFECTS FOUND. VALVE OPS NOSDR CA140730015Coupling · damaged(CAN) DUE TRO THE FINDINGS ON AIRCRAFT 4127 THE OPERATOR CHOSE TO INSPECT AIRCRAFT MSN 4350, THE OPERATOR FOUND SEVERAL FUEL PIPES & FUEL COMPONENTS IN ENGINE FUEL FEED SYSTEM WITH SIGNS OF CHAFING ON THE FERRULE ENDS OF THESE COMPONENTS. THE OPERATOR HAS ALSOSDR ASAA2014070708475Module · failedRT CTR FUEL PUMP INOPERATIVE. ACFT GROUNDED. TSR ISSUED. ACCOMPLISHED TSR STEPS 1 THROUGH 4 - NO HELP. RT CTR PUMP LOW PRESSURE LIGHT INTERMITTENTLY ON WITH PUMP OPERATING. WHILE TRANSFERRING FUEL FROM CENTER TANK AFTER TSR, FOUND RT CENTER BOOST PUMP LOW PRSDR CA140715003Fitting · leaking(CAN) IT WAS DISCOVERED THAT 3 FUEL FITTINGS (FUEL TRANSFER LINE, FUEL FEED, AND REFUEL LINE) AS INSTALLED PER DESIGN HAVE APPROX. 2 THREAD ENGAGEMENTS INTO THE DOME NUT. IT SHOULD BE ONE TO HALF TREADS PROTRUDING ABOVE THE NUT AS PER REQUIREMENTS. 629 AIRCRAF
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