JASC 2820
Service difficulty reports · 3,631
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 95ZZZX2237Tube Assy · corrodedDURING MAJOR INSPECTION, BUILD-UP NOTICED ON INLET AND OUTLET TUBE ASSEMBLIES IN FUEL VALVE BAY. WHEN CLEANED, SEVERE CORROSION FOUND ESPECIALLY UNDER B-NUTS. THESE PARTICULAR TUBES WERE MANUFACTURED WITH STEEL SLEEVES, AND ALUMINUM TUBING AND NUTS.SDR 95ZZZX1686Hose · looseDURING COMPLIANCE OF EN AND CHECKING INTERIOR OF FUEL CELL FOR CLEANLINESS, THE FUEL LINE FROM THE START PUMP TO THE FUEL SHUT OFF VALVE WAS FOUND LOOSE AT THE PUMP. THE UNION WAS LOOSE ALSO. AN ARTICLE IN THE FAA AC 43-16, ALERT NR 201, PAGE 12, PROPAGATED SDR RAIA950343Crossfeed Valve · malfunctionedSTL - FLT 7406 - WITH FUEL CROSS-FEED VALVE IN THE OPEN POSITION AND LEFT BOOST PUMP ON, THERE IS A 150 POUND FUEL IMBALANCE. MAINTENANCE REPLACED FUEL CROSS-FEED VALVE ACTUATOR. SYSTEM TEST GOOD. (X)SDR AWXA9500176Fuel System · malfunctionedPHX - FLT 2172 - LAS-IAH - DURING CRUISE, THE CENTER FUEL TANK SEEMED TO CONSUME FUEL AT AN EXCESSIVE RATE, 3600 LBS TO LESS THAN 900 LBS IN APPROXIMATELY 20 MINUTES. DUE TO A POSSIBLE FUEL LEAK, CREW DIVERTED AIRCRAFT TO PHX AND LANDED WITHOUT FURTHER PROBLESDR C2XA95CL044Flow Valve · malfunctionFLT NR 3468 - ALB-EWR - ON DESCENT INTO EWR THE NR 2 ENGINE FAILED. THIS TOOK PLACE SHORTLY AFTER TERMINATING A FUEL CROSSFEED OPERATION. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED ENGINE FUEL FILTERS AND MSDR COM60435Boost Pump · failedTHE LT FUEL BOOST PUMP IS INOP. REPLACED BOOST PUMP.SDR 96ZZZX1302Fuel Vent Line · corrodedDURING D-CHECK, FUEL VENT LINE AT WS 629 AND WS 601, CHECK THAT REPAIR IS IN C/W E.O. REPAIR. BLENDED OUT PER SRM 51-40-1. MATERIAL LOOSE .002 INCH. INSTALLED REPAIR PER AVITAS ENGINEERING NR 95PMSI.049RO-0 IN BOTH LOCATIONS. TAT: 53,881.4 HRS. TAC: 36,SDR 96ZZZX1301Vent Line · corrodedDURING D-CHECK, VENT TURBINE AT STA 580 HAS IMPROPER REPAIR. INSTALLED PROPER REPAIR PER AVITAS ENGINEERING NR 95PMSI.049 RO-1. TAT: 53,881.4 HRS. TAC: 36,380.SDR DL72W951039Tube · crackedDURING CRUISE, NR 3 FUEL QTY WAS DROPPING AT 2,500 LBS PER HOUR WITHOUT BURNING FROM THAT TANK. VISUALLY CHECKED NR 3 AT CRUISE ALTITUDE AND COULD SEE A STREAM OF FUEL VAPORS OFF THE RIGHT WING. LANDED DFW. FOUND CRACKED FUEL TUBE. REPLACED TUBE AND RETURNESDR USAA950213Module · failedPIT - FLT 852 - FLIGHT EN ROUTE PHL TO MCI WHEN CIRCUIT BREAKER FOR NR 1 FORWARD BOOST PUMP, NR 2 AFT BOOST PUMP, AND CENTER BOOST PUMP POPPED. RESET UNSUCCESSFUL. FLIGHT DIVERTED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED CIRCUSDR 95ZZZX2716Solenoid Valve · leakingBRITTAIN WING TIP TANKS WERE A PIPER FACTORY OPTION WHEN THIS PLANE WAS NEW. THE O-RING IS INTEGRATED WITH A WASHER, SO IT IS SPECIAL. IT IS NOT POSSIBLE TO GET NEW PARTS, SO THE WHOLE SOLENOID WAS REPLACED BY A STC'D FUEL VALVE.SDR 9503329963Coupling · looseFUEL BEGAN VENTING FROM RIGHT WING EN ROUTE MSP-BIL. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND FUEL VENT TUBE COUPLING LOOSE ON OUTBOARD SECTION OF LEFT WING TANK. LEAK AND OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.SDR 95ZZZX1747Fuel Line · chafedAIRCRAFT WAS IN FOR FIRST SERIES OF INSPECTIONS. THE FUEL CROSSOVER FUEL LINE WAS BEING CHAFED BY THE ELEVATOR MAIN CABLES. THE AN833-12D ELBOW LOCATED AT THE RT END OF THE CROSS FLOW TUBE WAS ROTATED IN ITS BRACKET UPWARD. THE TUBE WAS THEN FORMED TO FIT. SDR 95ZZZX2341Transfer Tube · chafedFOUND FUEL LEAKING FROM LT WHEELWELL, MAINTENANCE OPENED UP THE INNER FENDER ASSEMBLY AND FOUND MAIN GEAR UPLOCK SWITCH, WIRE BUNDLE HAD CHAFED THROUGH THE FUEL TRANSFER TUBE ASSEMBLY JUST INBOARD OF THE FUEL CROSS-TRANSFER VALVE. THE LINE WAS REMOVED ADN REPSDR 9501799953Wing · fuel leakFUEL BEGAN LEAKING FROM LEFT WING EN ROUTE HPN-MSP. FUEL WAS VENTING FROM RIGHT TANK AT A RATE OF 800 LBS PER HOUR. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. PERFORMED FUEL TANK BACKFLUSH PROCEDURE PER MAINTENANCE MANUAL. NO TRANSFER PROBLEMS WESDR 96ZZZX191Line · brokeDURING ANNUAL INSPECTION, FUEL LINES FROM TANK TO AIRFRAME WERE SHOWING AGE. WHILE PULLING TANKS, BOTH FUEL LINES SNAPPED. NO CORROSION WAS FOUND ON SPAR OR TANKS. SUBMITTER STATED THESE FUEL LINES HAVE TO BE CHECKED BY MIRROR.SDR 9502829980Fuel · transferingUPON LEVEL OFF AT CRUISE FLIGHT, FUEL WAS TRANSFERRED FROM RIGHT TANK TO CENTER TANK AT RATE OF 50 LBS PER MINUTE. TRANSFER STOPPED WITH APPLICATION OF CENTER TANK PUMPS. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. DISCREPANCY COULD NOT BE DUPLICATESDR COM60417Valve · defectiveGRAVITY FUEL CROSS FLOW VALVE IS INOP. REPLACED CROSS FLOW VALVE.SDR 95ZZZX786Check Valve · defectiveCHECK VALVE LEAKS INTERNALLY AND CAUSES THE AUXILIARY TANK TO GRAVITY FILL OVERNIGHT. TWO VALVES FAILED IN THE LAST 200 HOURS.SDR 95ZZZX836Hose · looseCREWS DESCRIBED AN INTERMITTENT VIBRATION THAT COULD BE FELT THROUGHOUT THE AIRCRAFT DURING FLIGHT. ALSO, A HESITANT START AND A FLUCTUATING TOT INDICATION WAS SQUAWKED. AFTER FLYING OVER 2 HOURS AND BEING LOW IN FUEL, DUPLICATED ALL THREE PROBLEMS. DISCOVESDR COM60395Valve · failedLEFT ENGINE FUEL SHUT OFF VALVE FAIL MESSAGE ON EICAS. REPLACED LT SOV.SDR COM60400Valve · inopRT ENGINE FUEL SHUTOFF VALVE WILL NOT CLOSE WHEN FIRE PUSH SWITCH IS ACTIVATED. REPLACED FUEL SOV.SDR C2XA95CL008Valve · openFLT 3288 - CLE-GSO - AFTER TAKEOFF, AIRCRAFT ROLLED TO THE LEFT. DISCOVERED A 2000 LBS FUEL IMBALANCE, WITH LEFT WING HEAVY. AIRCRAFT AIR RETURNED TO CLE. MAINTENANCE FOUND RIGHT FUEL TANK DEFUEL VALVE SWITCH IN THE OPEN POSITION. CLOSED SWITCH AND TRANSFESDR 95ZZZZ51Fuel Line · damagedFLT 4409 - BNA - PILOT REPORT AT 17,000 FEET DURING CRUISE THE RT ENIGNE SHUT ITSELF DOWN WITH NO WARNINGS. AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. AN INSPECTION OF THE RT FUEL SYSTEM REVEALED THAT THERE WAS NO CONTAMINATION. THE FUEL LINE FROSDR CAL950049Circuit Breaker · trippedFLT NR 1911 - IAH - THE AIRCRAFT WAS RETURNED TO IAH AFTER TAKEOFF DUE TO UNEVEN FUEL BURN FROM FUEL TANKS. THE NR 1 TANK WAS BURNING FASTER THAN OTHERS. FUEL WAS DUMPED TO CONTROL BALANCE. MAINTENANCE FOUND THAT THE NR 1 FUEL TRANSFER VALVE WAS NOT WORKINGSDR COM31011Fuel Hose · leakingFUEL LEAK RT WHEEL WELL AREA. REPLACED FUEL INTERCONNECT TUBE IN RT NACELLE.SDR 95ZZZX598Line · corrodedTHE PROBLEM WAS FOUND DURING AN INSPECTION FOR THE SOURCE OF A HEAVY FUEL SMELL IN THE CABIN. THE LEAK WAS FOUND IN THE FUEL LINE ON THE RIGHT SIDE OF THE CABIN AS IT CAME THROUGH THE WING ROOT. THE CAUSE OF THE LEAK WAS A HOLE THAT HAD CORRODED THROUGH. THSDR 95ZZZX597Line · corrodedTHE PROBLEM WAS FOUND DURING AN INSPECTION TO FIND THE SOURCE OF A HEAVY FUEL SMELL IN THE AIRCRAFT CABIN. THE LEAK WAS FOUND IN THE FUEL LINE ON THE RIGHT SIDE OF THE CABIN AS IT ENTERED INTO THE AIRCRAFT CABIN THROUGH THE WING ROOT. THE CAUSE OF THE LEAK WSDR 95ZZZW437Valve · leakingDURING DEPARTURE (7,000 FEET) ATC CONTROLLER INFORMED CREW FUEL WAS OBSERVED DUMPING FROM THE LEFT WING. FUEL ASSEMETRY LIGHT CAME ON WITH A FUEL INBALANCE AT 700 LBS. AIRCRAFT RETURNED WITHOUT INCIDENT. FUEL STOPPED LEAKING EN ROUTE TO MDW. MAINTENANCE DISDR 95ZZZX1097Line · corrosionDURING AN ANNUAL INSPECTION OF ACFT, LT WING TIP FUEL TANK (FLINT AERO) FUEL LINE TO TRANSFER PUMP FOUND TO HAVE FUEL STAINS IN SEVERAL PLACES & WAS WET TO THE TOUCH. UPON REMOVAL OF FUEL LINE FOR INSP, FOUND SEVERAL PIN HOLES IN AREAS OF THE FUEL STAINS & COSDR COM60364Valve · inopGRAVITY FUEL CROSS FLOW VALVE IS INOP. REPLACED CROSS FLOW VALVE.
Back to JASC 2820