JASC 2897
Service difficulty reports · 656
Reports filed under 2897 · Fuel System Wiring, 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 = '2897' 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 = '2897' 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 UIEA2018101302256Wire · brokenAUTOMATIC FUNCTION OF LEFT FWD PUMP INOP. FOUND WIRE 09G-16 BROKEN AT CONNECTOR D5800P, PIN 10. RE-PINNED AND INSTALLED IN CONNECTOR IAW SWPM 20-63-00, SPM 20-60-03. OPS TEST GOOD IAW AMM 28-25-01.SDR UIEA2018101002226Connector · dirtyRIGHT ENGINE SPAR VALVE SLOW TO CYCLE ON START. CLEANED SPAR VALVE CONNECTOR, OP'S CHECK NORMAL IAW AMM 28-22-01.SDR UIEA2018100802199Connector · contaminatedCTR L FUEL PUMP MSG DISPLAYED AFTER ENG START, LEFT C PUMP DISPLAYED PRESSURE LIGHT. PERFORMED VOLTAGE CHECK AT LT CENTER FUEL PUMP AT PINS 2,4,6, 115VOLTS AC PERFORMED VOLTAGE CHECK AT LT FUEL OVRD PUMP CONT RELAY AT PINS A2,B,C2 115 VOLTS AC NOTED, THEN ALSOSDR RU3A201808130036Pressure Switch · dirtyRIGHT TRANSFER LIGHT CAME ON IN FLIGHT WITH 800 LBS FUEL PER SIDE. SWITCHED TRANSFER PUMP TO OVERIDE AND TRANSFER FAIL LIGHT REMAINED ON. THE TRANSFER PUMP PRESSURE SWITCH WAS REMOVED, CLEANED AND REINSTALLED. THE SYSTEM OPERATING NORMALLY. NO FURTHER ACTION SDR AALA2018061329022Wire · brokenCENTER FUEL TANK PUMP 1 WAS INOPERATIVE. THE PUMP DOES NOT AUTO SHUT OFF, ALWAYS STAYS CROSSED AND AMBER IN AUTO MODE, MANUAL WORKED GOOD. FOUND WIRE 3154-1358 BROKEN IN 2M BUNDLE. REPAIRED THE WIRE IAW ESPM 20-53-21. OPS CHECKED GOOD IAW AMM 28-21-00-71SDR MUIA201806011001Connector · contaminatedREJECTED TAKEOFF, DUE TO THE FUEL RESERVOIR LOW LIGHT ILLUMINATING DURING THE TAKEOFF ROLL. FOUND AND CLEARED MOISTURE FROM ANNUNCIATOR PANEL CONNECTOR WITH INDICATION GOING AWAY AND NOT RETURNING DURING A REPO FLIGHT.SDR UIEA201806011010Circuit Breaker · trippedEICAS MESSAGE FOR THE CENTER LT FUEL PUMP. COMPLIED WITH QRH, TURNED THE PUMP OFF. MESSAGE CLEARED. FOUND C369 CIRCUIT BREAKER TRIPPED AT THE P6. RESET THE CIRCUIT BREAKER IAW AMM 20-60-01. ACCOMPLISHED FIM 28-22 TASK 812. LEFT CENTER FUEL PUMP OPS CHECKESDR AALA2018052299002Wire · chafedNR 1 ENGINE FIRE LOOP B, FAULTED, COMBINED WITH OIL ODOR THROUGHOUT THE ACFT. EMERGENCY DECLARED LANDED WITHOUT INCIDENT. AIRCRAFT WAS GROUNDED. IAW TSM 26-12-00-810-936-A22, ACCOMPLISHED WIRE CHECKS FROM FDU 1 TO THE NR 1 ENG, MANIPULATED WIRING AT ALL LOCSDR SOKF20180430004Contactor · damagedTHE AIRCRAFT RETURN TO DEPARTURE DUE TO AN ECAM WARNING FOR THE CENTER TANK PUMP 1, LOW PRESSURE AND CENTER TANK PUMP 2, LOW PRESSURE PREVIOUSLY. REPLACED THE CONTACTOR GFI FOR THE CENTER TANK PUMP 2 SUPPLY 70QA IAW ESPM 50-46-50, INSTALLATION SATISFACTORY CSDR 7C7A2018042400401Wire Harness · chafedLEFT WING FSL-13 FAILED A FUNCTIONAL CHECK, WS 225 & 243. WIRE FOUND CHAFED IN THE CONDUIT. REPLACED WITH NEW INDICATOR HARNESS IAW AMM.SDR HALA2018041900179Connector · dirtyRT FUEL QTY INDICATOR STATUS MESSAGE INTERMITTENT, ILLUMINATED FOR THE LAST 2 HOURS OF FLIGHT. LOST THE RT INDICATION TOTALIZER. PERFORMED THE FUEL QTY BITE PROCEDURE IAW FIM 28-41-TREE 847. NO FAULTS NOTED. CLEANED SPARK CONNECTOR. NO DEFECTS NOTE. SUMPSDR UIEA2018041900742Relay · failedRIGHT AFT FUEL PUMP AFT RELAY K 189 FAILED. REPLACED THE RELAY IAW AMM 28-22-00.SDR AALA201804099013Gfi · faultyFUEL CENTER TANK PUMP NR 2 LOW PRESSURE, FAULTY. AIRCRAFT WAS GROUNDED. ACCOMPLISHED A FUNCTIONAL CHECK OF THE CENTER TANK PUMP 2 IAW TSM 28-21-00. NO FAULTS NOTED. TROUBLESHOT FAULTY GFI (70QA) WILL NOT TEST. REPLACED GFI IAW AMM 28-18-00.SDR UIEA2018031600418Wire Harness · defectiveL FWD FUEL PUMP EICAS MSG IN FLIGHT. REMOVED AND REPLACED LT FWD BOOST PUMP WIRE HARNESS FROM D1550 TO D4600P WIRE W460-301B, 301R, 301X, 001 REF SWPM20-10-00, 20-61-00 OPS GOOD REF AMM 28-22-00 C/W CDCCL AND SFAR 88.SDR ASAA2018031223879Wire · shortedNR 1 FUEL TANK AFT PUMP LOW PRESSURE LIGHT ILLUMINATED WITH 5900 LBS INDICATED. ACFT GROUNDED. R18 GFI RELAY TRIPPED. ACCOMPLISHED FIM 28-22 / 803. FOUND WIRE W1136-3601B-16 SHORTED AT CONNECTOR D70 BACKSHELL. REMOVED THE DAMAGE, PINNED WIRING AND REPLACESDR UIEA2018022600279Connector · failedLEFT FWD BOOST PUMP CIRCUIT BREAKER TRIPPED. REMOVED AND REPLACED CONNECTOR D1550 IAW SWPM 20-61-11. OPS CHECKED NORMAL.SDR UIEA2018022400270Connector · dirtyEICAS MESSAGE FOR THE CENTER RT FUEL PUMP CAME ON IN CRUISE, WITH 7000 LBS FUEL IN CENTER TANK. PUMP CIRCUIT BREAKER TRIPPED. PERFORMED FIM 28-22, FT 812, NO FAULTS NOTED. RESISTANCE CHECKED GOOD CLEANED CONNECTOR RAN CENTER RT FUEL PUMP, OPS GOOD.SDR ASAA2018021323542Connector · failedDURING FLIGHT, THE NR 1 FUEL TANK, AFT FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED. ACFT GROUNDED. FOUND THE LT AFT FUEL PUMP CIRCUIT BREAKER TRIPPED. LEFT AFT PUMP INOPERATIVE. REMOVED AND REPLACED THE PUMP CONNECTOR D70 IAW SWPM 20-61-11. REPLACED THE WIRSDR UIEA2018020800194Connector · damagedWITH FUEL IN CENTER TANK AND AFTER SELECTING CENTER PUMPS ON, THE LEFT CENTER PUMP DID NOT LOD SHED , RIGHT INDICATED NORMAL OPERATION. REPLACED THE CONNECTOR AT LT OVERRIDE PRESSURE SWITCH IAW SWPM 20-61-11. REMOVED AND REPLACED THE LEFT OVERRIDE PRESSURESDR ASAA2018020323390Wire · chafedNR 1 MAIN TANK, AFT LOW PRESSURE ILLUMINATED DURING CRUISE WITH 8500 LBS OF FUEL IN THE NR 1 MAIN TANK. ACFT GROUNDED. ACCOMPLISHED WIRING CHECKS IAW TSR 701389 AND FOUND W1136-3601B-16 CHAFED CAUSING ARCING BY D70 CONNECTOR ON THE NR 1 TANK AFT BOOST PUMP. SDR UIEA2018012300104Circuit Breaker · trippedFOUND THE LT AFT FUEL PUMP CIRCUIT BREAKER TRIPPED. PERFORMED CIRCUIT BREAKER RESET AND PERFORMED OPS CHECK IAW AMM 28-22-00, OPS CHECKED GOOD.SDR UIEA2018011500066Connector · corrodedRIGHT CENTER FUEL PUMP NO LOW PRESSURE LIGHT INDICATION OR ASSOCIATED EICAS WITH TANK EMPTY. CLEANED CORROSION FROM CONNECTOR S-424. OPS CHECKED IAW AMM 28-42-00. NO DEFECTS NOTED.SDR COEA2018011301805Connector · dirtyABORTED TAKEOFF DUE TO A FUEL CCAS LIGHT ILLUMINATED BETWEEN 80-90 KTS. MAINTENANCE TROUBLESHOT AND SUMPED THE FUEL TANKS, CHECKED AND CLEANED ALL FUEL PROBE CONNECTORS IN FLAP WELL. CHECKED GOOD.SDR DALA2018010200021Connector · corrodedCORROSION ON ELECTRICAL CONNECTORS ON FUEL QUANTITY CONTROL PANEL AT RIGHT HAND WING. REPLACED CONNECTOR J2 AND CLEANED CONNECTOR J1. OPERATION CHECKS GOOD.SDR HALA2017122200312Circuit Breaker · malfunctionedON SHUTDOWN, FUEL CENTER TRANSFER FAULT AMBER XX ON RT TRANSFER PUMP. RESET CENTER RIGHT TRANSFER CIRCUIT BREAKER. OPS CHECKED NORMAL. OK FOR SERVICE.SDR A6WA201745479Wire · damaged4199 4225 APU AUTO SHUTDOWN. IMMEDIATELY AFTER SHUTDOWN A STRONG SMELL OF FUEL IN CABIN AND COCKPIT. F/O OBS FUEL DRIPPING AND SMOKE COMING OUT APU DOOR. NO FIRE WARNING PRESENT. INTERROGATED APU ECU FOUND CODES 154,155 AND LRU FUEL SOLENOID.FLAGGED. FOUND FSDR UIEA2017112702311Connector · crackedLT REAR SPAR FOUND APU FUEL SOV ELECTRICAL CONNECTOR CRACKED. CONNECTOR REMOVED AND REPLACED IAW WDM 28-25-21 REV 13 AND SWPM 20-61-00 REV 65. OPS TESTED GOOD IAW AMM 28-25-00 REV 122.SDR UIEA2017120502364Connector · damagedP37 PANEL ELECTRICAL CONNECTOR (D05052P) FOUND TERM 8 PIN LOCK BROKEN. REMOVED AND REPLACED IAW SWPM 20-61-11 REV 66 FOUND SATISFACTORY.SDR UIEA2017092201775Wire · brokenNR 1 ENGINE READS 13.6 FUEL FLOW ON EICAS. REPAIRED A BROKEN WIRE W744-302 B-24 AND PERFORMED AN ENGINE RUN, FUEL FLOW INDICATION NORMAL IAW SWPM 20-30-12 AND AMM 71-00-00-501.SDR UIEA2017082701552Connector · dirtyRIGHT AFT FUEL PUMP TRIPS THE CIRCUIT BREAKER DURING CRUISE. INSPECTED RT AFT BOOST PUMP CONNECTOR. OK. CLEANED CONNECTOR IAW SWPM 20-10-10. PERFORM OPEN CHECK IAW AMM 28-22-00-215-154 AND GROUND CHECKED OK.SDR UIEA2017071901239Bonding Jumper · frayedLEFT ENGINE SPAR VALVE BONDING JUMPER FRAYED. THE BONDING JUMPER WAS REMOVED AND REPLACED IAW AMM 20-11-00, REV 121.SDR UIEA2017071901240Connector · crackedRIGHT WING REAR SPAR VALVE CONNECTOR (D1572) CRACKED. THE CONNECTOR WAS REMOVED AND REPLACED IAW SOPM 20-61-11, REV 64. OPS TEST PERFORMED IAW AMM 28-22-01, REV 121.SDR SWAA2017072615300Connector · dirtyFUEL TRANSFER FEED VALVE WILL NOT OPEN. BLUE LIGHT NEVER DIMS. CLEANED THE CONNECTER IAW AMM.SDR AALA20170718006Wire · brokenTOTAL LOSS OF FUEL INDICATION SYSTEM AFTER TAKEOFF. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED DEPARTURE WITHOUT FURTHER INCIDENT. PILOT STATED THAT PANEL WAS FLICKERING WHEN THEY HIT TURBULENCE AND WHEN THEY HIT BUMPS ON THE GROUND. BOTH THE FLIGHT DECKSDR 2017FA0000306Wire Harness · openLEFT FUEL QUANTITY, 200 POUNDS LOWER THAN ACTUAL WHEN FUEL QUANTITY OVER 600 POUNDS. AT LOWER QUANTITIES READS SOMEWHAT ACCURATE. FOUND ALL PROBES AND INDICATOR OPERATING SATISFACTORY. OPEN LEFT WING PANELS AND FOUND WIRING TO THE TWO WET WING PROBES INTERMSDR 2017FA0000316Wire Harness · openWHEN AIRCRAFT IS FULL OF FUEL, AIRCRAFT HAS A DIFFERENTIAL QUANTITY INDICATION OF 200 POUNDS. THE INDICATOR GOES FROM 100 TO ZERO POUNDS IN FLIGHT. TESTED SYSTEM AND FOUND INSULATION AND CAPACITY CHECK OK. OPENING UP INTEGRAL WING PANELS TO GAIN ACCESS TO PSDR YENA201706280544Contactor · damagedDIVERTED DUE TO NR 2 CENTER TANK PUMP, NR 2 FAULT. R & R CONTACTOR FOR THE CENTER TANK NR 2 PUMP IAW ESPM 20-46-50. OPS TESTED GOOD IAW AMM 28-21-51-710-052-A.SDR UIEA2017060800954Bonding · dirtyOVERRIDE, JETTISON PUMP AT LT WING HIGH BONDING RESISTANCE. BONDING CLEANED &TREATED, CHECKED AND FOUND OK IAW MM 20-41-00.SDR UIEA2017060800955Bonding · dirtyENGINE FUEL SHUTOFF VALVE ACTUATOR AT LT WING TANK, BONDING HIGH RESISTANCE. THE BONDING WAS REMOVED CLEANED REINSTALLED CHECKED AND FOUND OK IAW MM 20-41-00SDR UIEA2017060500937Bonding · dirtyOVERRIDE, JETTISON PUMPS AT RT WING TANK HAS RESISTANCE AT BONDINGS. THE BONDING WAS CLEANED AND REINSTALLED. CHECKED FOR OPERATION AND FOUND OK IAW MM 20-41-00.SDR UIEA2017060500936Bonding · failedFWD AND AFT ENGINE FUEL CROSSFEED HINGE BONDING RESISTANCE. FUEL CROSSFEED BONDING CLEANED, REINSTALLED CHECKED FOR OPERATION & FOUND OK PER MM 20-41-00</P>)SDR UIEA2017051900820Wire · chafedLEFT AFT FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED. PERFORMED TROUBLESHOOTING IAW FIM 28-22. FAULT TREE 819 AND FIG 114 FOUND. REPAIRED CHAFED WIRE WITH BACK SHELL AT AFT LEFT BOOST PUMP CONNECTOR D1542 IAW SWPM 20-10-11.SDR A6WA2017042844945Switch · failedACRID ODOR IN COCKPIT, (FAINT ELECTRICAL PLASTIC ODOR) APPROX. 10 MIN INTO FLIGHT, NOT NOTICEABLE OUTSIDE COCKPIT, NO ABNORMAL EICAS MESSAGES. DURING TROUBLESHOOTING, FOUND GROUND FAN INTERNAL WIRING HAD FRAYED AND MISSING SHIELDING ON INTERNAL WIRING. R & RSDR UIEA2017041700602Connector · dirtyLEFT ENGINE FUEL FLOW INDICATOR FROZEN ON DESCENT, FL 390 DOWN TO 340, INDICATOR FROZEN AT 4.4, FL 180 ON DOWN. CLEANED AND SEATED THE FUEL FLOW CONNECTOR. OPS CHECKED NORMAL IAW AMM 73-31-01.SDR UIEA2017040400517Connector · corrodedD5930J ELECTRICAL CONNECTOR FOUND CORRODED. THE CONNECTOR WAS REMOVED & REPLACED IAW SWPM 20-61-00, REV 64, AND FOUND GOOD.SDR UIEA2017040400512Bonding Jumper · dirtyLEFT OTBD MAIN FUEL TANK FUELING SHUTOFF VALVE BONDING RESISTANCE CHECK, FOUND OUT OF TOLERANCE. THE BONDING JUMPER WAS REMOVED, CLEANED & INSTALLED IAW AMM 20-11-00, REV 120. A ELECTRICAL BONDING RESISTANCE CHECK PERFORMED IAW AMM 28-22-11, REV 120, AND FOUNSDR UIEA2017040400511Bonding Jumper · dirtyLEFT INBD MAIN FUEL TANK FUELING SHUTOFF VALVE BONDING RESISTANCE CHECK FOUND OUT OF TOLERANCE. THE BONDING JUMPER WAS REMOVED, CLEANED & INSTALLED IAW AMM 20-11-00, REV 120. BONDING RESISTANCE CHECK CARRIED OUT IAW AMM 28-22-11, REV 120 AND FOUND SATISFACTSDR UIEA2017040400510Bonding Jumper · dirtyAPU DC FUEL PUMP MOTOR HOUSING AND REAR SPAR BONDING RESISTANCE CHECK FOUND OUT OF LIMITS. THE APU DC PUMP BONDING JUMPER WAS REMOVED, CLEANED, AND INSTALLED IAW AMM 20-11-00, REV 120, AND BONDING RESISTANCE CHECKED IAW AMM 28-25-01, REV 120. FOUND SATISFACTSDR AALA201704069007Wire · damagedFUEL LT TANK PUMP 1 LOW PRESSURE. FOUND A DAMAGED WIRE FOR THE LT NR 1 FUEL PUMP. REMOVED AND REPLACED THE WIRE.SDR DALA2017030601827Receptacle · corrodedTHE LEFT WING SPAR ENGINE FUEL SHUTOFF VALVE ACTUATOR RECEPTICLE HAS CORROSION. REMOVED AND REPLACED THE LEFT ENGINE FUEL SHUTOFF VALVE ACTUATOR IAW 28-22-11. PERFORMED DUAL PATH WIRING CHECK AND LT ENGINE FUEL SHUTOFF VALVE ACTUATOR OPERATIONAL TEST IAW 2
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