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 2007UALA04634Wire · arcedLEFT WING O/B SURGE TANK WIRES HAS SIGNS OF ARCING AT TERMINAL BLOCK, HARDWARE RUSTED O/B SIDE OF RIB 31. REPLACED LEVEL SENSOR AND TERMINAL BLOCK. AC OK FOR SERVICESDR AALA20071974Connector · looseMIA INFLIGHT T995/18OCT - RIGHT CENTER FUEL PUMP WOULD NOT TURN OFF. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND LOOSE CONNECTOR FOR RIGHT CENTER FUEL PUMP POUNDS PER SQUARE INCH SWITCH. REPLACED SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR DXTA200702463Circuit Board · malfunctionedAIRCRAFT WILL NOT CROSSFEED IN FLIGHT. HAD NORMAL INDICATIONS OF CROSSFEED BUT NO FUEL TRANSFER FROM LT TO RT. TRANSFER FROM T TO LT HAD BOTH LOW FUEL PRESSURE LIGHTS AND LT BOOST PUMP ILLUMINATED. NO CROSSFEED LIGHT INDICATION. ON THE GROUND STILL NO FLOW INSDR NSVA2007224Connector · dirtyRT FUEL FLOW INDICATOR READS 200 LBS ON TAKEOFF. CLEANED CONNECTOR AND OPS CHECK GOOD.SDR AALA20071505Circuit Breaker · trippedDFW INFLIGHT T2334/12AUG - CREW REPORTED UNABLE TO GET FUEL FLOW FROM CENTER TANK. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND CENTER TANK FUEL PUMP CIRCUIT BREAKER POPPED. RESET CENTER TANK FUEL PUMP CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPSDR HALA0700318Connector · dirtyETOPS SIGNIFICANT SYSTEM - R AFT BOOST PUMP LOW PRESS LGT FAILED TO ILLUM AND EICAS MSG FAILED TO DISPLAY WITH SW OFF. CLEANED CONTACTS AT PRESS SWITCH CONNECTOR. PRESS LIGHT AND EICAS MSG FUNCT NORMAL. OPS CK R AFT BOOST PUMP PER AMM 28-27-00, OPS NORMAL.SDR HALA0700314Connector · dirtyETOPS SIGNIFICANT SYSTEM, R AFT BOOST PUMP LOW PRESS LGT FAILED TO ILLUM AND EICAS MSG FAILED TO DISPLAY WITH SW OFF. CLEANED CONTACTS AT PRESS SWITCH CONNECTOR. PRESS LIGHT AND EICAS MSG FUNCT NORMAL. OPS CK R AFT BOOST PUMP PER AMM 28-27-00, OPS NORMAL.SDR AALA20071374Wire Harness · inoperativeORD INFLIGHT T346/30JUL - FORWARD CENTER FUEL BOOST PUMP CIRCUIT BREAKER TRIPPED AFTER TAKEOFF. UNABLE TO BURN CENTER FUEL. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED FORWARD CENTER FUEL BOOST PUMP AND HARNESS. SYSTEM GROUND CHECKED NORMAL OPERASDR 2007UALA02807Wire · damagedCENTER FQI INOP, NR 2 ENG FUEL FLOW INDICATOR INOP. FOUND CENTER CONDUCTOR WIRE PULLED OUT OF D800 IN COCKPIT. CONNECTOR REPLACED AND CTR TANK DCTU CALIBRATED.SDR DL764070748Wire Harness · damagedRIGHT MAIN AND TOTAL FUEL QTY BLANKED AFTER ENGINE START. MTC IN PROGRESS. TRANSFERRED TO TIMCO OP 6002 AT HMV1, REPLACED RT MAIN FUEL T HARNESS IAW B767 MM 28-41-09. PERFORMED FUEL QUANTITY BITE CH IAW B767 MM 28-41-00-715-001. OPS CHECK GOOD. PERFORMED SDR CA070618004Connector · misinstalled(CAN) ON PATS RT AUXILARY TANK FOUND THE PRESSURE DIFFERENTIAL SWITCH, THE SOCKET OF THE SWITCH AND THE ELECTRICAL HARNESS CONNECTOR HAVING BOTH PINS, THE CONNECTOR SHOULD BE A FEMALE TYPE. THE DIFFERENTIAL SWITCH IS WORKING ONLY ON GROUND DURING FUELING. FOUNSDR 2007UALA01552Connector · damagedRIGHT INBOARD AND OUTBOARD FUEL QTY IND 2 AMBER DASHES ON FUEL PAGE. UNRELIABLE DATA. [06-26-07] FAULT TRACING FOUND FAULTY FUEL BOOST PUMP FUSE CONNECTOR. REPLACED 4044VCA FUSE CONNECTOR.SDR 2007UALA01414Connector · looseRTFL DUE TO LEFT AFT FUEL BOOST PUMP INOPERATIVE. [SUP 06-06-07] LEFT AFT FUEL PUMP ANNUNCIATED EICAS & LOW PRESS ON IN SWITCH. FOUND NR 1 ENG DRIVEN HYD PUMP CONNECTOR LOOSE. SECURED NR 1 ENGINE EDP DEPRESSURIZATION SOLENOID AS REQUIRED.SDR 2007UALA01093Circuit Breaker · burned outFUEL LIGHT TANK NR 1 PUMP LO PRESS IS ON. C/B N23 IS POPPED. [06-12-07] FOUND CB BUSS 1 103XP SPLY PHASE C LOOSE AND BURNED. REPLACED CB AND TERMINAL LUG.SDR CA070329009Wire · chafed(CAN) 5 AMP ANNUNCIATOR INDICATION (CB4) POPPED IN FLIGHT AND THE CREW LOST THE GREEN AND WHITE ANNUNCIATOR LIGHTS. THE CREW ATTEMPTED TO RESET THE 5 AMP CIRCUIT BREAKER, BUT COULD NOT BE RESET. PROBLEM WAS IN FOUND ON WIRE PIN D WIRE NR Q62A20 ON THE RT FUELSDR 2007UALA00909Wire Harness · damagedLEFT FUEL QTY INTERMITTENT. [SUP 4-20-07] AFTER TROUBLESHOOTING DETERMINED THAT LT MAIN FUEL QTY HARNESS NEEDED REPLACING. FINISHED REMOVAL AND INSTALLATION OF LT MAIN FUEL QTY HARNESS PER MM 28-41-05. DUE TO LT WING FUEL QTY HARNESS REPLACEMENT NEED TO OPS SDR 2007UALA00852Pin · shortedCOCKPIT FUEL GAUGES INOPERATIVE. FMC FUEL QUANTITY DOES NOT MATCH. DISPLAYED ERROR NR 4 ON NR 2 TANK COCKPIT FUEL QTY GAUGE. CAUSED BY FOUND PIN 6 ON CONNECTOR D4578P INTERNALLY SHORTED TO PIN 16. REPLACED CONNECTOR D4578P.SDR AALA20070396Relay · inoperativeIAH INFLIGHT T2163/24FEB - AFTER TAKEOFF LEFT TANK CONFIGURATION LIGHT ILLUMINATED. BOTH LEFT FUEL PUMPS BOTH RIGHT BOOST FUEL PUMPS AND RIGHT CENTER FUEL PUMP WAS ON. LEFT CENTER PUMP AS PLACARDED INOPERATIVE AND OFF. COULD NOT MAINTAIN BALANCE USING STANDSDR CALA0700030Connector · burnedNR 1 MAIN FUEL TANK FORWARD BOOST PUMP FOUND INOPERATIVE. PUMP WAS PLACARD INOPERATIVE. MX FOUND PUMP TO BE EXTREMELY HOT DURING TROUBLESHOOTING. CONNECTOR COULD NOT BE REMOVED & WIRING HAD MELTED OFF PUMP. APPROX 6 INCHES OF WIRING HARNESS WAS BURNED & COSDR 2007UALA00014Connector · dirtyON DESCENT THE NR 1 ENGINE SPAR VALVE CLOSED LIGHT IS ILLUMINATED WHILE THE ENGINE IS OPERATING, NO FUEL FLOW CHANGE OR DECREASE. FOUND DIRTY CONNECTOR ON NR 1 ENGINE SPAR VALVE ACTUATOR. CLEANED CONNECTOR. OPERATIONAL CHECKS NORMAL.SDR UPS06848794Connector · brokenINSPECTION TYPE:N/A ON FINAL APPROACH NR 1 ENGINE FLAMED OUT. CROSSFEED LEVERS OPENED, ENGINE RELIT IMMEDIATELY. TAXIING IN NR 1 ENGINE FLAMED OUT AGAIN. (BOOST PUMP OFF) FUEL IN NR 1 MAIN 2000 LBS. FOUND CONNECTOR TO NR 1 MAIN TANK FILL VALVE BROKEN. REPSDR CA061207001Wire · damaged(CAN) THE FUEL TANKS SHOW EVIDENCE OF LOCALIZED DISCOLORATION AND VARIOUS NICKS ON OUTER JACKETS OF FUEL QUANTITY PROBE WIRING. THERE IS ALSO DISCOLORATION ON THE TERMINALS OF THE VARIOUS FUEL PROBES. THIS DAMAGE IS PROBABLY CAUSED BY IMPROPER USE OF THE TYRAPSDR NSVA200600223Wire · brokenRT FUEL PRESSURE LIGHT NOT ILLUMINATING WHEN T-HANDLE IS PULLED AND STANDBY PUMP IS ON. REPAIRED BROKEN WIRE ON DIODE CR3/CR4 IAW BE1900 WDM 76-21-01, OPS CHECK GOOD.SDR 2006UALA01866Wire · damagedRIGHT WING T/E, WS 410, RIGHT MAIN FUEL QUANTITY WIRE BUNDLE FOR CONNECTOR, AFT SHELL CORRODED. FURTHER INSPECTION FOUND THE CORROSION WAS LIMITED TO THE CN1156 -4 CONNECTOR, HOWEVER, WHILE REMOVING THE CONNECTOR BACK SHELL, THE BACKSHELL BROKE APART INTO SESDR CA060906014Connector · shorted(CAN) FLASHING LIGHT OF ENGINE FUEL VALVE NR 2 ON STARTING PROCEDURE. CONNECTOR 1B14P1 SHORTED TOGETHER BETWEEN PINS A AND B AND WATER CONTAMINATION FOUND INSIDE BACK SHELL. INTERNAL LEAKAGE MEASURED ON THE CONNECTOR BETWEEN PINS A AND B CAUSING ON-OFF SIMULTASDR 06FDEA3055Wire · damagedFOUND WIRE BUNDLE DAMAGED IN RT AFT SPAR AREA INBD OF RT MAIN GEAR. WIRE NR" SE201-21-16A, E201-22-16B AND E201-23-16C BURNED THRU ABOUT 1 TO 2 FT INBD OF T-STRIP S3-375. WIRES ARE 3 PHASE WIRES FOR R AFT FUEL PUMP M1-1108. PULLED AND COLLARED AFFECTED C/B.SDR CA061019011Conduit · interference(CAN) DURING GROUND INSPECTION NOTICED FUEL LEAK NEAR FRONT SPAR AREA IN BELLY PANEL. INSPECTION FOUND ELECTRICAL CONDUIT FOR LT FUEL BOOST PUMP, WIRE COVERING INTERFERING WITH FLARE AT BULKHEAD FITTING. THIS ALLOWED FUEL TO PASS INTO THE CONDUIT AND OUT OF BESDR QXEA200601849Connector · dirtySEA FLIGHT 2024 LEFT FUEL TEMPERATURE HIGH. MAINTENANCE CLEANED CONNECTOR. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR CALA0600148Wire Harness · burnedWHILE TROUBLESHOOTING FOR ILLUMINATION OF THE NR 2 FUEL AFT BOOST PUMP LOW PRESSURE LIGHT MAINTENANCE FOUND A BURNED WIRE BUNDLE (W1134) ABOUT SIX INCHES FROM CONNECTOR D74. A NEW WIRE HARNESS ASSEMBLY WAS INSTALLED IAW SWP CHAPTER 20. THE NR 2 FUEL AFT BOOSSDR TSAA0628029Wire · brokenNR 1 ENGINE SHUT DOWN WITHOUT CREW ACTION AFTER NORMAL START, DURING PUSHBACK. FUEL VALVE CLOSED LIGHT ILLUMINATED. REMOVED AND REPLACED THE LT FUEL SHUT OFF VALVE IAW MM 28-22-11, LEAK CHECK OKAY. THIS DID NOT FIX THE PROBLEM. FURTHER INVESTIGATION REVEALSDR 2006UALA00933Connector · burnedLEFT AFT BOOST PUMP CONNECTOR BURNED TO PUMP ASSEMBLY. THE LEAKAGE OBSERVED WAS VERIFIED AND CAUSED BY A LOCALIZED OVERHEATING OF THE CONNECTOR PINS THAT RESULTED IN DAMAGE TO THE SEAL AROUND PIN 2. THE CAUSE FOR THE EXCESSIVE OVERHEATING IN THE CONNECTOR SDR CA060324002Wire Harness · damagedA/C HAS NR 2 AFT FUEL PUMP LOW PRESSURE LIGHT ILLUMINATE ON TAXI. A/C RETURNED TO GATE AND IT WAS DISCOVERED THAT ASSOCIATED CIRCUIT BREAKER WAS TRIPPED. FURTHER INVESTIGATION REVEALED WIRE W1134-3601-18 HAD SHORTED TO GROUND. MOC CONSULTED WITH BOEING ENGISDR 8921Relay · shortedLEFT ENGINE WOULD NOT START. TROUBLESHOT TO SHORTED RELAY ON FUEL RELAY PANEL.SDR 2006UALA00357Wire · exposedTHE NR 1 AFT FUEL BOOST PUMP WIRING WAS FOUND CHAFED THROUGH PLASTIC SHEATHING AND INTO WIRING INSULATION WITH BARE WIRING EXPOSED IN THREE AREAS DURING INSPECTION MANDATED BY AD99-21-15 ON UAL JIC 2S124. REPLACED WIRE ASSEMBLY AS REQUIRED PER AD 99-21-15. CSDR CA060123006Pin · burned(CAN) WHILE DE-FUELING AC FOR ROUTINE MAINT, IT WAS DISCOVERED THAT LT WING WOULD NOT DE-FUEL. MAINT FOUND THAT STBY FUEL PUMP WAS NOT WORKING. TROUBLESHOOTING FOUND CONNECTOR PLUG P221 UNDER CENTER PEDESTAL HAD A BURNED PIN AND CONNECTOR. PLUG AND CONNECTIONSDR AU510001635Wire Harness · deterioratedFUEL BOOST PUMP WIRING HARNESSES PN 27-82015-810 AND PN 27-82015-811 DETERIORATED. FOUND DURING INSPECTION IAW AD/SWA226/51 AND SB226-28-011.SDR AU510001501Wire · damagedNR 2 AFT FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED AND CIRCUIT BREAKER TRIPPED. INVESTIGATION FOUND FUEL PUMP WIRING BADLY BURNT AT EARTH PIG TAIL FERRULE. IT APPEARS THAT WHEN THE WIRING HARNESS WAS MANUFACTURED, ONE OR ALL THREE PHASE POWER WIRES TO THE PUMSDR AU510001471Wire Harness · damaged(AUS) CENTRE WING TANK DAISY CHAIN HARNESS DAMAGED. HARNESS CONTAINED A SUBSTANTIAL GASH ON THE OUTER INSULATION AND INTO THE SHIELD. THE HARNESS HAD ALSO BEEN SHARPLY KINKED AND WEAKENED IN TWO OTHER LOCATIONS. SUSPECT HARNESS DAMAGED DURING PREVIOUS TANK ENTSDR QXEA200501742Connector · unknownEUG FLIGHT NR 2156, NR 1 FUEL FILTER BYPASS, MASTER CAUTION. MAINTENANCE REPLACED NR 1 ENGINE HP AND LOW PRESSURE FUEL FILTERS IAW DHC8-2-- AMM 73-10-00-000-802 AND 73-10-00-400-802, 73-10-00-000-801 AND 73-10-00-400-801. REPLACED CONNECTOR 7700-P1. OPERATISDR ALGA106938Wire Harness · chafedCHAFING AT AREAS WHERE CABLE COMES THROUGH TRANSFER TUBE. ADDED CHAFING PROTECTION TO CABLE ASSY OR ADELING IN ANOTHER MANNER.SDR UPS05445604Wire · burnedWHILE T/S D311541 FOUND WIRE SPLICES BURNED REF WD W1210-014 BYR, W121 0-001 BYR, W1210-014BYR, W1210-024 BYR, W206-022 BYR, AND W1210-024 BYR. NOTE BYR IS BLUE, YELLOW, AND RED WIRE RUNS, SPLICE LOC IS STA 960 LT. REPLACED DAMAGED WIRES AND SPLICES WITH NEWSDR AU510001709Wire · shortedRT INNER FUEL BOOST PUMP PRESSURE SWITCH TO PRINTED CIRCUIT BOARD WIRE SHORT CIRCUITED.SDR CA050909003Wire Harness · failed(CAN) FAULT: FLT DEP.YYZ WITH LT FUEL DENSIOMETER UNDER MEL. FLT CREW CONFIRMS LT IND DID BLANK OUT ON OCCASION DURING THE FLT AND HAD BEEN CALCULATING THE FUEL REMAINING THROUGHOUT THE FLT. AT FL370 AND 50NM FROM TOP OF DESCENT, THE LT ENG FLAMED OUT, ENG RSDR SWAA052281Wire · damagedDIVERSION, EVIDENCE OF ELECTRICAL ODOR IN COCKPIT. FOUND WIRES DAMAGED IN OVERHEAD P-5 PANEL, NR 1 ENGINE FUEL SHUT-OFF VALVE & MLG POSITION SENSOR CIRCUIT BREAKERS POPPED. REPAIRED WIRES PER SWPM. REMOVED AND REPLACED P52 FUEL MODULE & T492 LEFT MLG POSITISDR CA050501001Wire Harness · shortedFUEL QTY IND FOR RT WING TANK INTERMITTENTLY FLICKERED, CHANGED QTY DISPLAYED & OCCASIONALLY ROLLED DOWN TO ZERO POUNDS OF FUEL INDICATED. NO TRUE CONDITION OF FUEL IMBALANCE APPARENT. INVESTIGATION REVEALED THE RED WIRE FOR NR 1 FUEL QTY TRANSMITTER FOR RSDR CA050422003Wire · broken(CAN) SWITCH MONITORS FUEL TEMP AT ENGINE FUEL PUMP & IS FITTED TO TFE731-3 ENGINES INSTALLED ON HAWKER 700 ACFT. ON THIS INSTALL SWITCH WIRES CONNECT TO AIRFRAME SUPPLIED ENGINE HARNESS THROUGH IN-LINE CONNECTORS. THESE CONNECTORS ARE NORMALLY ONLY DISTURBEDSDR CA050408005Relay · corroded(CAN) DURING PHASE INSPECTION, BOTH FUEL PUMP RELAYS (JT AND KT) WERE FOUND WITH CORRODED TERMINAL BLOCKS. ONE WIRE FROM THE RELAY WAS DAMAGED AND ARCHED ON THE CASE OF THE RELAY. THE RELAYS ARE LOCATED UNDER THE WING TO FUSE BELLY FAIRING. THIS AREA IS SUBSDR CA041203001Wire · chafed(CAN) DURING AN INSPECTION ( B CHECK ), FOUND JUST ABOVE THE PRESSURE REFUELLING LINE, LOCATED ON LT WING W/S 196 (ACCESS PANEL 541-5), AN ELECTRIC WIRE, THAT GOES TO THE FUEL DRAIN SOLENOID VALVE, CHAFED. IT DID CAUSE AN ARCING.SDR 2005FA0000290Wire · brokenHEAT ELEMENT INOPERATIVE, DUE TO BROKEN WIRE AT TIP OF VENT TUBE WHERE IT IS GROUNDED. IT IS CAULED BY IMPROPER PROTECTIVE COATING ON THE WIRE. THE COATING WEARS OFF AND OPENS THE WIRE FROM GROUND. (K)SDR 2005FA0000289Wire · inoperativeHEAT ELEMENT INOPERATIVE DUE TO BROKEN WIRE AT TIME VENT TUBE WHERE IS IS GROUNDED. IT IS CAUSED BY IMPROPER PROTECTIVE COATING ON WIRES. IT WEAR OFF AND OPENS THE WIRE FROM GROUND. (K)
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