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.

SDR AU000450Housing · eroded(AUS) MAIN FORWARD FUEL TANK LEFT BOOST PUMP FAILED. INVESTIGATION FOUND PIECES OF METAL SEPARATED FROM THE HOUSING INLET STRUTS JAMMING THE CHECK VALVE PARTIALLY OPEN.May 20, 2000 · Boeing 767277SDR USAABB00067Pump · failedCLT - FLT 855 - EN ROUTE TO JAX, WITH THE RIGHT FORWARD FUEL BOOST PUMP ON MEL, CREW RECEIVED INDICATIONS OF LOW PRESSURE ON THE LEFT FORWARD BOOST PUMP. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT FORWARD BOOSTMay 9, 2000 · N645US · Boeing 767201SDR DLL19000965Stator · failedL1011 FUEL BOOST PUMP APPEARS TO HAVE BURNED UP THE STATOR WINDING. NEW STATOR (P/N 770917 NHA 112-508-06), AND (S/N 1741).Apr 29, 2000 · N768DL · Lkheed 10113853SDR AU000411Pump · faulty(AUS) LEFT FUEL TRANSFER PUMP FAILED. INVESTIGATION FOUND THAT THE PUMP POSITIVE WIRE HAD BURNED OFF AT THE HOUSING. LEFT LANDING LIGHT CIRCUIT BREAKER TRIPPED.Apr 27, 2000 · Cessna 310RSDR 2000UALA00219Drain Valve · leakingFUEL INCREASE OF 1200 POUNDS IN CENTER TANK ON CLIMBOUT. NOTE: CORRECTED TRANSFER WEIGHT FROM 12000 LBS TO 1200 LBS DUE TO TYPOGRAPHICAL ERROR IN INITIAL REPORT. *S/D* THE APPARENT FUEL TRANSFER WAS FOUND TO BE CAUSED BY FAILURE OF THE FUELING MANIFOLD DRApr 25, 2000 · N611UA · Boeing 767222SDR AALA20000686Cover · leakingDFW - FLT 1913 - BEFORE FLIGHT, FUEL LEAK NOTED ON LEFT WING BOOST PUMP COVER. RESEALED BOOST PUMP COVER. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)Apr 24, 2000 · N7540A · Doug DC982SDR AU000412Pump · faulty(AUS) RIGHT FUEL TRANSFER PUMP FAILED. INVESTIGATION FOUND THAT THE PUMP POSITIVE WIRE HAD BURNED OFF AT THE HOUSING. RIGHT LANDING LIGHT CIRCUIT BREAKER TRIPPED.Apr 19, 2000 · Cessna 310RSDR 20000907SH034Transfer Pump · failedSUBMITTER STATED THIS IS ONLY ONE OF MANY INCIDENTS. THESE PUMPS ARE REPEATEDLY FAILING AROUND 300 OR LESS HOURS. INSTALLED ON 11-15-99. FAILED ON 4-17-00. (X)Apr 17, 2000 · N3208Q · Cessna 401SDR 20000426SH022Pump · failedAFT BOOST PUMP INOPERATIVE. INSPECTED AIRFRAME FUEL FILTER AND FOUND FILTER WAS COATED WITH A BLACK CARBON LIKE MATERIAL THAT WAS SUSPECTED TO BE RESIDUE FROM THE MAGNETS SURROUNDING THE BOOST PUMP CORE. (X)Mar 22, 2000 · N198H · Bell 206BSDR 00FDEA00166Pump · failedRIGHT FWD BOOST PUMP LOW PRESSURE LIGHT ILLUM (APPROX 5500 FUEL IN NR 2 TANK). SAME TIME DETECT ELECTRICAL ODOR. *S/D* REMOVED AND REPLACED WATER SEPARATOR CONDENSER BAGS PER MM 21-5-051-4. REMOVED AND REPLACED PUMP PER 28-22-021-4. AC OK FOR SERVICE.Mar 22, 2000 · N209FE · Boeing 7272S2FSDR 20000329SH048Pump · inoperativeTHE CREW REPORTED THE ELECTRIC BOOST PUMP INOPERABLE. THE PUMP WAS REPLACED. THIS PUMP ROUTINELY FAILS IN THIS FLEET OF 172R AIRCRAFT, AND IN MOST CASES, PRODUCES METAL THAT CONTAMINATED THE FUEL INJECTION COMPONENTS. (X)Mar 16, 2000 · N416ER · Cessna 172RSDR CA000323026Pump · contaminated(CAN) NR 2 INBOARD QUANTITY LOW LIGHT ON WITH MORE THAN 700 POUNDS. AFTER SEVERAL BOOST PUMP REPLACEMENTS A BOLT WAS DISCOVERED IN BOOST PUMP CHECK VALVE. THE BOLT HAD DAMAGED THE CHECK VALVE. ORIGIN OF BOLT WAS UNKNOWN.Mar 8, 2000 · Lkheed 1011385115SDR AU000410Pump · faulty(AUS) LEFT FUEL TRANSFER PUMP FAILED. INVESTIGATION FOUND THAT THE PUMP POSITIVE WIRE HAD BURNED OFF AT THE HOUSING. LEFT LANDING LIGHT CIRCUIT BREAKER TRIPPED. (X)Mar 6, 2000 · Cessna 310RSDR CA000306010Armature · misoverhauled(CAN) PUMP WAS SENT FOR OVERHAUL. INTERNAL INSPECTION REVEALED THAT THE ARMATURE HAD BEEN MODIFIED BY REDUCING THE ARMATURE SHAFT SIZE AND SUBSTITUTING THE ORIGINAL BEARING WITH A COMMERCIAL BEARING THAT HAD THE SAME OUTSIDE DIAMETER, BUT A SMALLER INSIDE DIAMar 6, 2000 · Dhav DHC6300SDR CA000306009Armature · misoverhauled(CAN) PUMP WAS SENT FOR OVERHAUL. INTERNAL INSPECTION REVEALED THAT THE ARMATURE HAD BEEN MODIFIED BY REDUCING THE ARMATURE SHAFT SIZE AND SUBSTITUTING THE ORIGINAL BEARING WITH A COMMERCIAL BEARING THAT HAD THE SAME OUTSIDE DIAMETER, BUT A SMALLER INSIDE DIAMar 6, 2000 · Dhav DHC6SDR CA000306008Armature · misoverhauled(CAN) PUMP WAS SENT FOR OVERHAUL. INTERNAL INSPECTION REVEALED THAT THE ARMATURE HAD BEEN MODIFIED BY REDUCING THE ARMATURE SHAFT SIZE AND SUBSTITUTING THE ORIGINAL BEARING WITH A COMMERCIAL BEARING THAT HAD THE SAME OUTSIDE DIAMETER, BUT A SMALLER INSIDE DIAMar 6, 2000 · Dhav DHC6200SDR 20000523SH011Rotor · will not testUPON INCOMING FUNCTIONAL TEST OF THE UNIT, THE UNIT COULD NOT ACHIEVE THE REQUIRED PRESSURES OR FLOW RATES PER THE OHM. ON FURTHER INSPECTION, THE ROTOR WAS DETERMINED TO BE THE CAUSE OF TEST FAILURE. (X)Mar 2, 2000 · Airbus A320212SDR HEEA066546Switch · failedPRESSURE SWITCH NOT WORKING PROPERLY. LIGHT STAYS OFF.Feb 28, 2000 · N4999 · Bell 407SDR AU000183Pump · failed(AUS) LEFT MAIN FUEL TANK TRANSFER PUMP FAILED. INSPECTION FOUND BURNT CONNECTOR.Feb 17, 2000 · Cessna 310RSDR AU000156Pump · burned out(AUS) RIGHT MAIN FUEL TANK TRANSFER PUMP CONNECTOR BURNT AND BLACKENED.Feb 17, 2000 · Cessna 310RSDR 20000907SH020Switch · shortedNR 4 FUEL BOOST PUMP SWITCH SHORTED OUT WHEN PLACED IN THE LOW BOOST POSITION DURING ENGINE START. SWITCH INTERNALLY SHORTED DIRECT TO GROUND. SWITCH REPLACED. SYSTEM THOROUGHLY INSPECTED. OPS CHECKED NORMAL. (X)Feb 15, 2000 · N151 · Doug DC6BSDR 20000407SH009Switch · failedNR 4 FUEL BOOST PUMP SWITCH SHORTED OUT WHEN PLACED IN THE LOW BOOST POSITION DURING ENGINE START. SWITCH INTERNALLY SHORTED DIRECT TO GROUND. SWITCH REPLACED. SYSTEM THOROUGHLY INSPECTED. OPS CHECKED NORMAL. (X)Feb 15, 2000 · N151 · Doug DC6BSDR AU000106Pump · failed(AUS) RIGHT FUEL BOOST PUMP BLADE RETAINING RING BROKEN. PUMP HAD ONLY JUST BEEN FITTED FOLLOWING OVERHAUL AND HAD ONLY OPERATED FOR APPROXIMATELY FIFTEEN MINUTES.Feb 11, 2000 · Piper PA31350SDR HEEA065922Switch · failedLIGHT WILL NOT ILLUMINATE IN OFF POSITION.Feb 4, 2000 · N722PH · Bell 407SDR 20000523SH016Rotor · will not testUPON INCOMING FUNCTIONAL TEST OF THE UNIT, THE UNIT COULD NOT ACHIEVE THE REQUIRED PRESSURES OR FLOW RATES PER THE OHM. ON FURTHER INSPECTION, THE ROTOR WAS DETERMINED TO BE THE CAUSE OF TEST FAILURE. (X)Feb 3, 2000 · Airbus A320212SDR 20000523SH014Rotor · will not testUPON INCOMING FUNCTIONAL TEST OF THE UNIT, THE UNIT COULD NOT ACHIEVE THE REQUIRED PRESSURES OR FLOW RATES PER THE OHM. ON FURTHER INSPECTION, THE ROTOR WAS DETERMINED TO BE THE CAUSE OF TEST FAILURE. (X)Feb 3, 2000 · Airbus A320212SDR 20000523SH013Rotor · will not testUPON INCOMING FUNCTIONAL TEST OF THE UNIT, THE UNIT COULD NOT ACHIEVE THE REQUIRED PRESSURES OR FLOW RATES PER THE OHM. ON FURTHER INSPECTION, THE ROTOR WAS DETERMINED TO BE THE CAUSE OF TEST FAILURE. (X)Feb 3, 2000 · Airbus A320212SDR 20000523SH012Rotor · will not testUPON INCOMING FUNCTIONAL TEST OF THE UNIT, THE UNIT COULD NOT ACHIEVE THE REQUIRED PRESSURES OR FLOW RATES PER THE OHM. ON FURTHER INSPECTION, THE ROTOR WAS DETERMINED TO BE THE CAUSE OF TEST FAILURE. (X)Feb 3, 2000 · Airbus A320212SDR 20000523SH010Rotor · will not testUPON INCOMING FUNCTIONAL TEST OF THE UNIT, THE UNIT COULD NOT ACHIEVE THE REQUIRED PRESSURES OR FLOW RATES PER THE OHM. ON FURTHER INSPECTION, THE ROTOR WAS DETERMINED TO BE THE CAUSE OF TEST FAILURE. (X)Feb 3, 2000 · Airbus A320212SDR 20000523SH008Rotor · will not testUPON INCOMING FUNCTIONAL TEST OF THE UNIT, THE UNIT COULD NOT ACHIEVE THE REQUIRED PRESSURES OR FLOW RATES PER THE OHM. ON FURTHER INSPECTION, THE ROTOR WAS DETERMINED TO BE THE CAUSE OF TEST FAILURE. (X)Feb 3, 2000 · Airbus A320212SDR USAASB00032Pump · failedCLT - FLT 2876 - EN ROUTE FROM MIA TO IAD, FUEL GAUGES BECAME UNRELIABLE. LEFT FUEL QTY INDICATOR STUCK AT 10.5 AND THE CENTER TANK RIGHT FUEL PUMP WOULD NOT PRESSURIZE. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. Feb 3, 2000 · N251AU · Boeing 737201SDR CA000209001Terminal Block · shorted(CAN) THE CREW REPORTED THAT THE NR 1 AUX FUEL PUMP WAS NOT OPERATING. MAINTENANCE DETERMINED THE FAULT TO BE AN INTERNAL BREAKDOWN IN THE TB-1-2821 TERMINAL BLOCK.Jan 31, 2000 · Dhav DHC8102SDR HEEA065974Pump · inoperativeFUEL PUMP INOPERATIVE.Jan 10, 2000 · N60951 · Snias AS350B2SDR HEEA065606Switch · inoperativePRESSURE SWITCH INOPERATIVE.Jan 6, 2000 · N8595X · Bell 407SDR SCNA99159Circuit Breaker · failedAIR RETURN DUE TO ALL CIRCUIT BREAKERS FOR TANK NUMBER TWO FUEL BOOST PUMPS POPPED. FOUND NUMBER TWO FWD RT CIRCUIT BREAKER PHASE B AFT RT CIRCUIT BREAKER PHASE A AND AFT LEFT CIRCUIT BREAKERS PHASE A INTERMITTENTLY OPENING. REMOVED AND REPLACED CIRCUIT BREADec 29, 1999 · N294SC · Boeing 7272M7SDR 99ZZZX4677Boost Pump · failedHORIZON HELICOPTERS HAD NOTICED FUEL CONTAMINATION AFTER A BOOST PUMP FAILURE ON 4 OCCASIONS. THE FILTER IS FULL OF BLACK CARBON. SUBMITTER BELIEVES THE BOOST PUMP INTERNAL BREAKDOWN IS THE SOURCE OF CONTAMINATION AND HAS SAMPLE PUMP AND FILTER AT FACILITY FDec 28, 1999 · N198H · Bell 206B3SDR 2000ZZZX257Pump · failedOWNER NOTIFIED THAT LEFT LANDING LIGHT/TIP TANK TRANSFER PUMP CIRCUIT BREAKER OPENED. FOUND TIP TANK TRANSFER PUMP FAILED ELECTRICALLY. UNIT SHOWS SIGNS OF ARCING AND OVERHEATING AT POWER WIRE INLET AREA. UNIT HAD BEEN REPLACED 15.7 HOURS PREVIOUSLY. THIS Dec 20, 1999 · N5255C · Cessna T310RSDR MWEA99909Pump · failedCENTER FORWARD FUEL BOOST PUMP POPPED CIRCUIT BREAKERS. MTC REMOVED AND REPLACED FORWARD CENTER BOOST PUMP.Dec 19, 1999 · N809ME · Doug DC982SDR HEED065791Switch · failedMUST CYCLE BOOST PUMP SWITCH SEVERAL TIMES TO GET CAUTION LIGHT WHEN BOOST PUMP (RIGHT) IS TURNED OFF. REPLACED UNIT.Dec 17, 1999 · N3193E · Bell 407SDR HEEA065469Pressure Switch · malfunctionedRIGHT TRANSFER LIGHT WILL NOT COME ON.Dec 17, 1999 · N723PH · Bell 407SDR HEEA065450Switch · malfunctionedLOW LEVEL LIGHT CAME ON WITH FUEL ON BOARD.Dec 17, 1999 · N612PH · Bell 407SDR HEEA065448Pressure Switch · inoperativePRESSURE SWITCH INOPERATIVE.Dec 17, 1999 · N612PH · Bell 407SDR HEEA065443Switch · stuckPRESSURE SWITCH STICKS IN OPEN POSITION.Dec 17, 1999 · N490PH · Bell 407SDR 99ZZZX4638Pump · failedTHE PILOT REPORTED ZERO FUEL PRESSURE WHEN THE BOOST PUMP WAS TURNED ON. INVESTIGATION REVEALED IT HAD FAILED IN THE PUMP SECTION. THE METAL PARTICLES HAD MIGRATED THROUGHOUT THE FUEL SYSTEM REQUIRING THE INSPECTION, CLEANING, AND REPLACEMENT OF COMPONENTS ADec 13, 1999 · N424ER · Cessna 172RSDR 99ZZZX4633Pump · failedON TAKEOFF ROLL, HEARD ELECTRIC FUEL PUMP SURGING. ABORTED TAKEOFF. SUMPED STRAINER TWICE AND FOUND BRASS FLAKES BOTH TIMES. LEFT THE BRASS FLAKES IN THE STRAINER FOR MAINTENANCE TO VERIFY.Dec 13, 1999 · N403ER · Cessna 172RSDR HEEA065359Switch · failedPRESSURE SWITCH NOT FUNCTIONING.Dec 9, 1999 · N405PH · Bell 407SDR HEEA065358Switch · malfunctionedPRESSURE SWITCH NOT EXTINGUISHING CAUTION LIGHT.Dec 9, 1999 · N405PH · Bell 407SDR 99ZZZX4657Pump · failedTHE ELECTRIC FUEL PUMP FAILED AND CAUSED THE CIRCUIT PROTECTION DEVICE TO TRIP. SUBMITTER STATED THIS IS A COMMON PROBLEM ON THIS FLEET OF 172R AIRCRAFT.Dec 8, 1999 · N405ER · Cessna 172RSDR 99ZZZX4656Pump · failedTHE ELECTRIC FUEL PUMP FAILED AND CAUSED THE CIRCUIT PROTECTION DEVICE TO TRIP. SUBMITTER STATED THIS IS A COMMON PROBLEM ON THIS FLEET OF 172R AIRCRAFT.Dec 8, 1999 · N407ER · Cessna 172RSDR 99ZZZX4655Pump · failedTHE ELECTRIC FUEL PUMP FAILED AND CAUSED THE CIRCUIT PROTECTION DEVICE TO TRIP. SUBMITTER STATED THIS A COMMON PROBLEM ON THIS FLEET OF 172R AIRCRAFT.Dec 8, 1999 · N421ER · Cessna 172R
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