JASC 2822
Service difficulty reports · 2,745
Reports filed under 2822 · Fuel Boost Pump, 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 = '2822' 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 = '2822' 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 VJ32002F00019Pump · leakingINSPECTION OF THE FUEL PUMP FOUND OIL LEAKING FROM THE DRAIN PORT OF FUEL PUMP. IN FLIGHT THE ENGINE WAS ROUGH AT TIME. PUMP WAS REMOVED AND A NEW PUMP INSTALLED IAW MM. DEFECTIVE PUMP SENT IN FOR WARRANTY.SDR HEEA078365Pressure Switch · failedBOOST PUMP CAUTION LIGHT WILL NOT COME ON.SDR AUS20020301Pump · rusted(AUS) FUEL BOOST PUMP SOLENOID RUSTY CAUSING THE PUMP TO INTERMITTENTLY SWITCH TO HIGH' WHEN SELECTED TO LOW'.SDR 441MWire Harness · chafedFOUND CHAFED WIRE THAT HAD BEEN ARCING ON THE BOX THAT SURROUNDS THE BOOST PUMPS TO KEEP THE FUEL IN THE FUEL HOPPER. ABOUT SIX INCHES FROM WHERE THE BOOST PUMP, CONNECTOR PLUG ENTERS THE INBOARD RIB OF THE WET WING AREA, A WIRE (THE RED WIRE) HAD BEEN CHAFINGSDR 2002FA0000389Pump · inaccurateUNABLE TO ADJUST FUEL PUMP PRESSURE. PRESSURE IS TO HIGH AT LOW RPM AND THE ADJUSTMENT SCREW BACK ALL THE WAY OUT. PUMP REMOVED AND SENT IN FOR WARRANTY.SDR CA020408004Pump · failed(CAN) IN FLIGHT, FUEL PRESSURE FLUCTUATED AND WENT TO ZERO ON LT FUEL PUMP, CIRCUIT BREAKER POPPED.SDR 2002FA0000328Pump · failedFUEL PUMP WOULD NOT PRODUCE FUEL FLOW OR PRESSURE. ENGINE WOULD NOT IDLE BELOW 1000 RPM AND WOULD NOT PRODUCE POWER.SDR AALA20020203O-Ring · leakingRDU - FLT 1858 - EN ROUTE PBI-LGA, FUEL LEAK COMING FROM BOOST PUMP COVER DURING FLIGHT. DIVERTED AND LANDED RDU WITHOUT INCIDENT. REPLACED AND SECURED O-RING AT LEFT WING FUEL PROBE FIRST OUTBOARD FROM HEATER BLANKET. SYSTEM GROUND CHECKED NORMAL OPERATIONSDR HEEA078109Cartridge · inoperativeBOOST PUMP CARTRIDGE IS INOPERATIVE.SDR HEEA078082Cartridge · inoperativeFUEL PUMP CARTRIDGE IS INOPERATIVE.SDR HEEA078071Pressure Switch · inoperativeFUEL SYSTEM PRESSURE SWITCH IS INOPERATIVE.SDR LS1R088297Pump · inoperativeFUEL PUMP FAILED CHECK/ INOPERATIVE.SDR CA020211008Attach Fitting · cracked(CAN) DURING THE NDT INSPECTION OF THE FUEL BOOST PUMP SCREW HOLES 3 CRACKS WERE FOUND. REPAIR IN ACCORDANCE WITH REO 601R-57-21-164.SDR HEEA077788Cartridge · faultyFAULTY CARTRIGE CAUSING FUEL BOOST PUMP TO NOT RUN.SDR 2002FA0000147Pump · shortedFUEL PUMP CIRCUIT BREAKER POPS. RESET BREAKER POPS AGAIN WHEN PUMP SWITCH IS TURNED ON.SDR 2002FA0000170Pump · inoperativeENGINE QUIT DURING STALL PRACTICE. ENGINE WOULD START BUT NOT RUN. LANDED IN FIELD. FUEL PRESSURE TOO LOW. FACTORY REP INSTALLED SETUP GAGES AND ADJUSTED TO PROPER SPECS. ENGINE RAN GOOD AFTER PROPER ADJUSTMENT.SDR SWAA020190Pump · failedNR 2 FUEL TANK FWD FUEL BOOST PUMP LOW PRESS LIGHT ILLUMINATED. REMOVED AND REPLACED NR 2 FUEL TANK FWD BOOST PUMP AND LOW PRESS SWITCH PER MM.SDR LS1R088291Pump · inoperativeBOOST PUMP IS INOPERATIVE.SDR AALA20020063Pump · defectiveORD-ATL - FLT 419 - AFTER LEVELING OFF AT CRUISE ALTITUDE, FUEL NOT FEEDING FROM CENTER TANK. INLET FUEL LOW PRESSURE LIGHTS CAME ON WITH CENTER PUMPS ONLY ON. AIRCRAFT LANDED ORD WITHOUT INCIDENT. REPLACED FORWARD AND AFT FUEL PUMPS. SYSTEM GROUND CHECKEDSDR GTIA030020Pump · inoperativeORD - FLT 1225 - AFT CENTER BOOST PUMP INOPERATIVE. LOW PRESSURE LIGHT ILLUMINATES WTH AFT CENTER PUMP ONLY RUNNING. PULLED AND RESET CIRCUIT BREAKER. LIGHT GOES OUT FOR 25 SECONDS THE ILLUMINATES. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M)SDR HEEA077632Pressure Switch · malfunctionedLIGHT WILL NOT COME ON.SDR HEEA077626Pressure Switch · failedRIGHT FUEL BOOST PUMP LIGHT DOES NOT COME ON WHEN CIRCUIT BREAKER SWITCH IS TURNED OFF.SDR HEEA077614Cartridge · inoperativeFUEL PUMP CARTRIDGE INOPERATIVE.SDR HEEA077600Pressure Switch · failedPRESSURE SWITCH FAILED.SDR HEEA077583Pressure Switch · failedBOOST PUMP LIGHT WILL NOT COME ON WHEN PUMP OFF.SDR HALA0100315Pump · damagedETOPS SIGNIFICANT SYSTEM, PER EO 28-01-03-71, LEFT AFT FUEL BOOST PUMP CONDUIT OUTER SLEEVE HAS A HOLE APPROX 44 INCHES FROM TERMINAL END. REPLACED LEFT AFT BOOST PUMP CONDUIT OUTER SLEEVE PER EO 28-01-0371 REV A. (M)SDR HALA0100314Pump · damagedHNL - ETOPS SIGNIFICENT SYSTEM, PER EO 28-01-03-71 LT AUX TANK BOOST PUMP CONDUIT OUTER SLEEVE HAS A HOLE APPROX 14 INCHES FROM TERMINAL END. REPLACED LEFT OVERRIDE AUX PUMP CONDUIT OUTER SLEEVE PER EO 28-01-03-71 REV A. (M)SDR EKI2002F00000Pump · inoperativeMFG OVERHAULED SUBMERSABLE FUEL PUMP FOR RIGHT MAIN FUEL TANK QUIT WORKING AFTER 91.6 HOURS 3 MONTHS.SDR AWXA200100590Pump · failedCMH - DIVERTED FLIGHT - FLT 683 -C- EN ROUTE FROM PHX TO EWR DURING CLIMB THE FLIGHT DECK CREW OBSERVED ECAM MESSAGE CTR TK PUMP 1 LO PRESS, FOLLOWED BY PUMP 2 LO PRESS. THE CREW CONTACTED MAINTENANCE CONTROL AND WERE INSTRUCTED TO TRY MANUAL MODE, BUT STILL SDR 2001FA0000499Pump · failedPILOTS REPORTED THAT IN CRUISE FLIGHT LEFT LOW FUEL PRESSURE ANNUNCIATOR ILLUMINATED AND LEFT FUEL PUMP CIRCUIT BREAKER POPPED A FEW SECONDS LATER. AFTER LANDING, MAINTENANCE CREW REENGAGED CIRCUIT BREAKER, AND PUMP RAN, BUT WAS EXTREMELY NOISY. THERE WERE NSDR ACE1031011Pump · leakingA FAILED NR 2 ENGINE LOW PRESSURE FUEL BOOST PUMP WAS IDENTIFIED WHILE THE AIRCRAFT WAS IN THE HANGAR FOR OTHER MAINTENANCE. THE FAILURE WAS IDENTIFIED BY FUEL DRIPPING OUT OF THE NR 2 ENGINE GANG DRAIN DUE TO PREVIOUS COMPLIANCE WITH MFG MANDATORY SB 71-3307SDR HEEA076983Cartridge · failedLT BOOST PUMP FUEL PRESSURE DROPPED TO ZERO, LT BOOST PUMP LIGHT ILLUMINATED. REPLACED WITH SERVICEABLE PART.SDR LS1R076726Pump · malfunctionedBOOST PUMP PRODUCING LOW PRESSURE AND LOUD NOISE.SDR LS1R076724Pump · failedBOOST PUMP WILL NOT TURN ON.SDR HEEA076862Pump · wornPUMP SHAFT SPLINE WEAR.SDR HEEA076511Cartridge · inoperativeFUEL CARTRIDGE INOPERATIVE.SDR HEEA076386Cartridge · inoperativeINOPERATIVE. REPLACED WITH SERVICEABLE BOOST PUMP CARTRIDGE.SDR CA011011009Pump · failed(CAN) PUMP NOT WORKING MOTOR UNSERVICEABLE. REPLACED PUMP ASSEMBLY.SDR DL757011471Pump · failedAPPROXIMATELY 25 MINUTES INTO FLIGHT WITH 5,100 LBS IN CENTER FUEL TANK, RIGHT CENTER LOW PRESSURE LIGHT ILLUMINATED. TWO MINUTES LATER LEFT CENTER LOW PRESSURE LIGHT ILLUMINATED. ACCOMPLISHED POM, TURNED OFF PUMPS. INSPECTED INLET LINES AND PRESSURE LINES.SDR HEEA075488Pump · malfunctionedPUMP PRODUCES NO PRESSURE.SDR LS1R074939Pump · inoperativePART WILL NOT OPERATE.SDR DVP2001F00000Seal · failedDURING DESCENT, PILOT HAD TO OPERATE ELECTRIC FUEL BOOST PUMP IN ORDER TO MAINTAIN ENGINE POWER. ON LANDING, FUEL WAS FOUND TO BE LEAKING FROM SEAL DRAIN LINE OF ENGINE DRIVEN FUEL PUMP. FUEL STAINS WERE EVIDENT ALONG ENGINE SIDE OF NOSE GEAR BAY AND ONTO LOSDR CA010725010Pump · unserviceable(CAN) BOOST PUMP FAILED CAUSING FUEL IMBALANCE. AIRCRAFT LANDED AND PUMP REPLACED.SDR AUS20010752Pump · misinstalled(AUS) TRANSFER PUMP CONNECTORS INCORRECTLY WIRED. THE PUMPS HAD WIRINGSWAPPED AT PIN 2 AND PIN 3. THE WIRES WERE RECONNECTED IN THE BELIEF THAT THE WIRING CONFIGURATION WAS INCORRECT. THE AIRCRAFTHAD BEEN SUPPLIED WITH THE WIRING IN A NON-STANDARD FORMAT. INVESDR AUS20010753Pump · misinstalled(AUS) HORIZONTAL STABILISER FUEL TANK RT TRANSFER / JETTISON PUMP WIRINGCONNECTIONS AT PIN 2 AND PIN 3 REVERSED AT PUMP CONNECTOR PLUGDM7863. WIRING WAS CORRECT AS PER WIRING DIAGRAM BUT INCORRECT AS PER BSB 747-28-2217 FIG10. INVESTIGATION FOUND THAT SOME AIRSDR CA010815002Pump · failed(CAN) 1. EXTENGUISHED. NR 1 115 VAC TR BUS INOP. AIRCRAFT LANDED WITHOUT INCIDENT. MAIN FUEL TANK, AFT FUEL BOOST PUMP UNSERVICEABLE. BOOST PUMP CHANGED IAW MM 28-22-41. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT.SDR CA020405018Pump · inoperative(CAN) FORWARD BOOST PUMP INOPERATIVE.SDR WVBA2001039Pump · failedDURING PRE-INSPECTION RUN UP, IT WAS OBSERVED THAT THE FUEL PRESSURE WAS 34 PSI AT 1500 RPM. THE PUMP WAS ADJUSTED UP .5000 TURN AND WAS STILL 34 PSI (LOW RED LINE) FROM IDLE TO 1900 RPM. PUMP WAS REMOVED FROM SERVICE.SDR WVBA2001038Pump · failedPILOT REPORTED DECREASE IN FUEL PRESSURE AT CRUISE POWER SETTINGS. PUMP WAS REMOVED AND REPLACED.SDR WVBA2001037Pump · failedPILOT REPORTED FUEL PRESSURE 50 PSI AT CRUISE POWER SETTINGS. PUMP WOULD NOT ADJUST WITHIN PARAMETERS. NO MID ADJUSTMENT. PUMP WAS REMOVED AND REPLACED.
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