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 2013FA0000287Sleeve · splitDURING RT MAIN TANK BOOST PUMPS WIRE BUNDLES INSPECTION FOUND SLEEVES SPLIT AND NOT IN ONE CONTINUOUS PIECE THROUGH THE CONDUIT, FUEL PUMPS WIRE BUNDLES INSPECTED SERVICEABLE. RT MAIN TANK BOOST PUMPS WIRE BUNDLES SLEEVES REPLACED IAW SB 767-28A0053, REV 3.SDR 2013F00116Sleeve · damaged(VHOGN) VISUAL INSPECTION OF THE FUEL TANK BOOST PUMP WIRING IAW SB 767-28A0053, REV 03. DURING THE INSPECTION OF LT MAIN BOOST PUMP WIRING OUTER SLEEVING FOUND SPLIT, AT AREAS WHERE SLEEVING WAS PUSHED FLAT ON FOLD LINES OF SLEEVING WAS NO LONGER ROUND. SDR UALA2013051403343Connector · unsecureUPPER FUEL CROSSFEED SWITCH DOES NOT CYCLE VALVE. SECURED CONNECTOR ON UPPER TRANSFEED VALVE. VALVE CHECKED GOOD.SDR CA130510002Filter · shorted(CAN) DURING A TRAINING FLIGHT, THE NR 1 FORWARD BOOST PUMP FAILED, AND THE PILOT NOTIFIED MAINTENANCE, ABOUT THIS FAULT. IT WAS FOUND THE NR 1 FWD BOOST PUMP NOISE FILTER PN A.3210 HAD SHORTED OUT AND NR 2 PUMP NOISE FILTER CONNECTION WAS ABOUT TO FAIL. THSDR UALA2013050703182Connector · faultyFUEL OVER-FILL RED LIGHT ILLUMINATED ON FUELING PANEL. SURGE TANKS CHECKED EMPTY. FOUND LEFT WING SURGE TANK FLOAT SWITCH S690 GIVING CONSTANT GROUND TO FUELING SHUTOFF RELAY R699. REMOVED CONNECTOR DS690 AND VERIFIED WING WIRING OK IAW WDM 28-21-12.SDR 2013FA0000256Wire Harness · misinstalledRT FUEL QTY NOT DECREASING DURING RUN-UP. GROUND RUN-UP FINDING DATED 25-04, 2013. FOUND LT AND RT FUEL QUANTITY INDICATION SYSTEM CROSSED WITH EACH OTHER UNDERNEATH CENTER PEDESTAL FLOOR AT FS 500. WIRING BUNDLES REROUTED WITH THEIR RELATIVE INDICATORS TO TSDR UALA2013041002413Wire · shortedSTATUS MESSAGE * FUEL SPAR VALVE R *. CIRCUIT BREAKER POP, WILL NOT RESET. MAINT MESSAGE 28-14002. CONNECTOR REMOVED FROM RIGHT ENG SPAR VALVE, CB STILL POPS. REPLACED RELAY K28222, CB STILL POPS. SET RT ENG CUT OFF SWITCH TO RUN, CB STAYS IN REF SSM 28- 22SDR UALA2013040802348Circuit Breaker · trippedLEFT ENGINE WILL NOT START ON PUSHBACK. SPAR VALVE CIRCUIT BREAKER FOUND TRIPPED, CYCLED LEFT ENGINE FUEL SPAR VALVE AND CYCLED VALVE. RESET AND RAN LEFT SPAR VALVE. SPAR VALVE OPS NORMAL AND BREAKER IS OK.SDR UALA2013040502281Circuit Breaker · failedCIRCUIT BREAKER A14 TRIPPED, LOSS OF LT TANK NR 1 FUEL PUMP AND LOSS OF RT TANK NR 1 FUEL PUMP. ELEC PAGE INDICATIONS NORMAL. REPLACED A14 CIRCUIT BREAKER IAW AMM 28-21-00, TRANSFERRED FUEL, OPS CHECKED OKAY.SDR UALA2013032001717Connector · dirtyAFT FUEL CROSSFEED VALVE WILL NOT TEST. VERIFIED VALVE OPERATION OK. CLEANED CONNECTOR, PERFORMED OPERATIONAL TEST IAW AMM, TEST PASSED.SDR U5QA20130228051Connector · looseFUEL INDICATOR AT FL410 STARTED TO DEPLETE RAPIDLY ON RT WING. RT WING WENT TO 0 (ZERO) INDICATION. DECLARED EMERGENCY. MX REPAIRED LOOSE CONNECTION AT RT WING OTBD FUEL PROBE P278, FUNCTIONAL TEST AND OPS CHECK GOOD. NO DEFECTS NOTED.SDR CA130218001Wire · shorted(CAN) RT AFT MAINTANK FUEL PUMP LOW PRESSURE ANNUNCIATOR ILLUMINATED. FOUND SHORTED WIRES ON FUEL PUMP WIRING HARNESS. W1134-3601R-18, 360IY-18, W1134-360IB-18.SDR ASAA2013020893846Connector · looseNR 2 FUEL GAUGE LIGHT FLASHING IN UNDERWING FUEL PANEL. SEATED CONNECTOR ON NR 2 FUEL QUANTITY INDICATOR. REFUEL QUANTITY INDICATION SYS OPS CHECK GOOD. REF MM TASK 28-21, TASK 816.SDR QMLA2013020813023Connector · burnedDURING OTHER MX TO CLEAN AN INTERNAL FUEL BAY IT WAS NOTED THAT THERE WAS A BLACK STREAK GOING BOTH UP FROM AND DOWN FROM THE FUEL QUANTITY WIRE HARNESS CONNECTOR INSIDE THE FUEL BAY OF THE LEFT WING. REMOVED THE CONNECTOR FROM THE BULKHEAD AND FOUND THAT THSDR UALA2013020800772Wire · shortedNR 2 SPAR VALVE LIGHT REMAINS LIT AT ALL TIMES. ENGINE DOES NOT START, NO FUEL FLOW. NO POWER ON ONE SIDE OF ENGINE 2 SPAR VALVE CB ON P6-1 PANEL. AFTER CHANGING CIRCUIT BREAKER WILL NOT STAY IN. SUSPECT VALVE IS ALSO BAD. HUNG NEW SPAR VALVE ACTUATOR, SSDR UALA2013020500704Connector · unsecureCENTER AUXILLARY FUEL OVERRIDE PUMP LOW PRESSURE LIGHT ILLUMINATED. PUMP PREVIOUSLY REPLACED. SEATED CONNECTORS ON P-5 FUEL MANAGEMENT PANEL. FUELED CENTER TANK TO 5000 LBS. TRANSFERRED FUEL TO WING TANKS AND CENTER TANK. LOW PRESSURE LIGHTS GROUND CHECKED SDR ASOA2013021203009Wire · chafedWIRE FOR FUEL QTY PROBE IN PANEL 540BB HAS CHAFE DAMAGE, BECAUSE STANDOFF FOR CLAMP IS NOT LOCATED IN CORRECT POSITION. REPAIRED IAW REO 601R-20-12-111 AND REO 601R-57-21-1862, REV A.SDR UALA2013013000563Wire · brokenEICAS MESSAGE, LT JET TRANSFER VALVE AND OVERHEAD FAULT LIGHT ILLUMINATED FOR APPROX 30 SECONDS TWICE IN CRUISE. FOUND BROKEN WIRE (W450-302B-20) LESS THAN A QUARTER INCH FROM LEFT JETTISON VALVE CONNECTOR (D12180). REPINNED W450-302B-20 AT CONNECTOR D12180.SDR UALA2013011700289Wire · shortedFUEL SPAR VALVE RT STATUS MESSAGE. TROUBLESHOT IAW WDM 28-22-25 AND FOUND RELAY K28222 ON P101 DIST INTEGRATION PANEL WORKING NORMAL. INSPECTED WIRING IAW WDM 28 -22-25 AND FOUND GROUND BETWEEN PIN 34 OF CONNECTOR D1304P ON P101 DISTRIBUTION PANEL AP0461 ANDSDR UALA2012122707413Wire · burnedFOUND BURNT WIRING JUST AFT OF THE BOOST PUMP CONNECTOR. CUT WIRES AT DAMAGED AREA AND RETERMINATED NEW CONNECTOR REF WDM28-22-31 PG2. WIRES DAMAGED 3 INCHES FROM CONNECTOR. ENOUGH SLACK TO RE-TERMINATE. REPAIRED DAMAGED WIRE & REPLACED CONNECTOR. REPLACINSDR 2012F00268Sleeve · crackedDURING VISUAL INSPECTION OF THE FUEL BOOST PUMP WIRING IAW SB 767-28A0053, REV 3. .5 LONG SPLITS WERE FOUND IN THE OUTER TEFLON SLEEVING OF THE LT AFT BOOST PUMP. THERE WAS NO DAMAGE ON THE INNER SLEEVE SO THE OUTER SLEEVE WAS REPLACED.SDR 2012FA0000788Wire · damagedAFTER FINDING A BROKEN WIRE ON THE FUEL LEVEL TRANSMITTER OF ANOTHER ACFT OF THE SAME MAKE AND MODEL, MECHANIC INSPECTED AND FOUND FUEL LEVEL TRANSMITTER WITH BRITTLE WIRE ON THE TRANSMITTER VARIABLE CONTACT MAKING AN NTERMITTENT CONNECTION.SDR UALA2012110906451Connector · dirtyDURING REFUELING FOUND SLOW RATE ON CTR TK. FOUND LEFT CTR REFUEL VLV NOT OPEN MANUALLY OPENED AND CONNECTOR CLEANED THEN FUNCTION AUTO NORMAL AGAIN AUTO REFUEL ACP AND SATISFACTORY.SDR 2012FA0000753Wire · brokenAFTER AN OCCURANCE OF AN OFF AIRPORT LANDING, DUE TO FUEL STARVATION, ON OCT 10,2012, WITH FUEL GUAGE SHOWING 60 GALLONS ON BOARD. THE MECHANIC FOUND A BROKEN WIRE ON THE FUEL LEVEL TRANSMITTER VARIABLE CONTACT. PROBABLE CAUSE COULD BE THE WIRE LOOKED TO BE SDR UALA2012101605913Connector · dirtyNO VALVE IN TRANSIT LIGHT ON FUEL CROSSFEED VALVE TEST. CLEANED CONNECTOR ON V10138. LIGHT CHECKS GOOD.SDR UALA2012092805478Connector · faultyMAIN TANK 1 FUEL QTY FLUX. FOUND A3 CARD FOR CENTER WING SNGLE POINT SENSOR CONTROL GREEN LITE ON CARD FOR CHANNEL A ON AND CHANNEL B OUT. ACCOMPLISHED FIM 28-44 TASK 802 FOR CARD Y5BA3 FAIL. REMOVE REAR SPAR CONNECTOR X1011 FOR IN-TANK WIRING TROUBLESHOOTISDR FDEA201209133327Terminal · burnedTANK 2L AFT PUMP LO LEVEL 1 ALERT IN CRUISE FLIGHT. COMPLIED WITH LEVL 1 QRH CHECKLIST FUEL PUMP TNK 2, LT C/B (G-17) WAS POPPED BY FUEL PUMP. IN ADDITION, THERE WAS A SIGNIFICANT EVIDENCE OF FLAME/SMOKE/HEAT EXPOSURE TO TERMINAL STRIP S3-372 AND SEVERAL INSDR QLMY2012F00205Wire · damagedDURING HEAVY MX, A VISUAL INSPECTION OF THE FUEL TANK BOOST PUMP WIRING IAW SB 767-28A0053, REV 03. DURING THE INSPECTION A .5 INCH LONG SPLIT WAS FOUND IN THE OUTER TEFLON SLEEVE ABOUT 16 INCHES FROM THE REAR OF RT AFT FUEL BOOST PUMP CONNECTOR D1540. THSDR UALA2012090404964Wire · brokenRIGHT WING LEADING EDGE FUEL-DEFUEL ACCESS PANEL, LIGHT WIRING IS BROKEN AT SPLICE AND HAS NON ENVIROMENTAL EXPOSED SPLICE. REPAIRED SPLICE PER BSWPM 20-10-13 AND PERFORMED OPS CHECKED GOOD.SDR FDEA201208283196Wire · failedONE HOUR INTO FLIGHT NOTICED TANK 2 QTY 8000 LBS LESS THAN TANKS 1&3. TROUBLESHOT PER FIM 28-41 AND FOUND NR 2 TANK RT COMPENSATOR PROBE WIRE WAS LOOSE AT RIVET AND WIRE HARNESS HI Z TO SHIELD WAS SHORTED. REPLACED NR 2 TANK RT COMPENSATOR PROBE AND WIRE HARNSDR UALA2012082104675Wire · shortedLEFT ENGINE SPAR VALVE LIGHT ILLUMINATED FOUND SHORT IN WIRE; W3384-1009-18 10" FROM D2142 L SPAR FUEL SHUTOFF VALVE. REMOVED AND REPLACED 50.5 FT RUN FROM D40218P TO D2142. REF WDM 28-22-21WIRE TYPE CODE "GE" OPS CHECKED OKAY.SDR UALA2012082104674Connector · missingLEFT SPAR VALVE CONNECTOR REMOVED. REPLACED SPAR VALVE CONNECTOR, OPS CHECK NORMAL. ACCOMPLISHED VISUAL INSPECTION ON THE INSTALLATION OF SPAR CONNECTOR CHECK RESISTANCE CHECK OKAY PER STD PRACTICE AMM.SDR RYNA201208210033Wire · damagedFLIGHT CREW CALLED MAINTENANCE CONTROL AND REPORTED THAT THE LEFT CENTER BOOST PUMP HAS FAILED RESULTING IN AIR TURNBACK TO CMN. REMOVED AND REPLACED WIRING TO LEFT CENTER FUEL PUMP FROM LEFT LANDING GEAR PLUG D5558J TO D2805 AT PUMP. OPS CHECK NORMAL PER ASDR UALA2012082104652Wire Harness · damagedUNDER WING SERVICE FUEL PANEL HAS NO POWER. FOUND INSULATION DAMAGE TO WIRING HARNESS TO LIGHT ASSY ON FUELING DOOR. WIRING HAS NO BROKEN WIRE STRANDS. REPAIRED INSULATION WITH GUIDELINE TAPE AND SECURED WIRING HARNESS TO PROVIDE CLEARANCE. FUELING ACCOMPLSDR 9JLA2012101904409Wire Harness · intermittentCREW REPORTED THE RT WING FUEL QUANITITY INTERMITTENTLY SHOWS DASHES ON THE INDICATOR. THE RT WING FUEL WIRE HARNESS WAS REMOVED AND A NEW HARNESS WAS INSTALLED. FUNCTIONAL CHECKED SATISFACTORY.SDR 2012F00114Probe · groundedDURING CLIMB OUT, 1/3 RT ROLL WAS REQUIRED TO MAINTAIN LEVEL FLIGHT. THE ACFT RETURNED TO DEPARTURE.SDR QMLA2012052012084Switch · burnedON STARTUP, SMELLED ELECTRICAL BURNING AND NOTICED LOWER FUEL PUMP SWITCH LIGHT TO NOT BE ON AND THE ENGINE FIRE WARNING LIGHT TO BE ON IN THE WARNING CAUTION PANEL. FOUND WARNING BREAKER TO BE TRIPPED AND LOWER FUEL PUMP SWITCH TO BE BURN AND STUCK IN THE ON SDR CA120906012Wire · damaged(CAN) THE FUEL PRESSURE INDICATION WOULD GO TO 1 OR NO BARS INDICATED. THIS REQUIRED A TERMINATION OF ANY PATIENT FLIGHTS AND RETURN TO BASE MULTIPLE TIMES. THE SYSTEM SEEMED TO CHECK OUT PROPERLY WHEN MAINTENANCE SHOWED UP. EVENTUALLY, PN 407-375-007-107 INSDR CA120524008Switch · failed(CAN) UPON TURNING ON AIRCRAFT BATTERIES, SMOKE STARTED TO COME FROM THE CENTER CONSOLE. PASSENGERS WERE EVACUTATED AND POWER WAS TURNED OFF IMMEDIATELY. MAINTENANCE WAS DISPATCHED TO THE ACFT, AND FOUND A FAULTY BOOST PUMP SWITCH INTERNALLY FAILED. ACFT WASSDR CA120516003Wire · damaged(CAN) REPLACED WIRES LEADING TO DENSITOMETER IN LT WING TANK IAW GUIDELINES OF SRPSA 42163 AND MITSUBISHI HARNESS DWG GM598-2510-101, REV "C".SDR CA120326006Connector · damaged(CAN) AIR TURNBACK DUE TO NR 2 FUEL TEMP SPIKED AT 95 DEG. NR 2 FUEL TEMP SWITCH ELECTRICAL CONNECTOR REPLACED AND CHECKED SERVICE ABLE ON ENGINE RUN.SDR UALA2012032001803Connector · unsecureFUELER REPORTS NO PWR TO REFUEL PANEL. DOOR SWITCH 565-1239 20QU CIRCUIT BREAKER 2QU 565-0531 28VDC 4023VC PIN Y. FOUND BAD CONNECTION, SECURED, REF WDM 28-25-01 PG2 AND ASM 24-67-00 SCH1. OPS CK'S GOOD. NO FAULTS NOTED, HAVE POWER TO REFUEL PANEL.SDR NSVA20120318484Wire Harness · defectivePILOT REPORTED WHILE PERFORMING THE CLIMB CHECKLIST NOTICED THAT THE FUEL FLOW INDICATOR WAS READING 0. CREW RAN THE CHECKLIST AND RETURNED BACK TO IAD FOR FURTHER MX. CHANGED THE HARNESS, OPS CK GOOD.SDR UALA2012030501394Connector · dirtyRIGHT CENTER FUEL PUMP PRESSURE LIGHT IS NOT ILLUMINATED WITH ENGINES CUTOFF. REPLACED R ENG SPEED CARD AND RELAY K10399, NO HELP. CLEANED S100011 PRESS SWITCH MATING CONNECTOR AND NORMAL OPERATION RESTORED, OPS CHECKS OKAY.SDR AALA20120301022Pin · backed outJFK - CREW REPORTED RIGHT FUEL TANK AND TOTALIZER BLANKED DURING CLIMB. FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. PLACARD RIGHT FUEL TANK INDICATION AND TOTALIZER PER MEL. FOUND PIN 9 PUSHED BACK ON CONNECTOR D6884. RESET PIN. SYSTEM GROUND CHECK NORMASDR RYNA201202210012Wire Harness · corroded(AIR TURNBACK) EN ROUTE/CLIMBOUT, APPEARS CENTER FUEL TANK NOT SUPPLING FUEL. FOUND AFT/CTR BOOST PUMP C/B OPEN (ALL TESTED GOOD PRE-FLT). COULD NOT VERIFY, FWD/CTR PUMP LEVEL FLIGHT NORMAL. REMOVED AND REPLACED CENTER WING AFT BOOST PUMP HARNESS IAW SWPM 2SDR CALA2012020300071Wire Harness · defectiveRIGHT MAIN FUEL GAUGE DOES NOT SHOW QUANTITY. REPLACED RT MAIN TANK WIRE HARNESS AS PER AMM 28-41-09. FQIS SY SYSTEM CHECKED GOOD. LEAK CHECK GOOD PER FFC RO #5120066. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1434662 SN OFF 06862 HARNESS, FUEL T OFF 64-28SDR CA120203011Wire · loose(CAN) ON A FLIGHT, RT FUEL GAUGE BECAME U/S READING ZERO, THE PILOT LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED A LOOSE WIRE ON THE FUEL SENDER UNIT. THE WIRE WAS REPAIRED AND THE SYS WAS GROUND FUNCTION CHECKED SERVICABLE.SDR UALA2012012400491Connector · dirtyFUEL QTY BITE STATUS WITH RIGHT WING QTY AND BLANK TOTALIZER. REMOVED, CLEANED, AND RESEATED CONNECTOR D2814 AND BUSSING PLUG FOR RT FUEL TANK, OPS CHK GOOD. SEE SCAL NR 9959791. WORK ACCOMPLISHED.SDR RYNA2011123000023Wire Harness · defectiveAIR TURNBACK - CENTER FUEL PUMP CIRCUIT BREAKER POPPED AND CREW WAS UNABLE TO GET FUEL OUT OF THE CENTER TANK. TROUBLESHOT AND FOUND DEFECTIVE FUEL HARNESS. IN TANK WORK IN PROGRESS TO REPLACE HARNESS. SUPPLEMENTAL REPORT TO FOLLOW UPON COMPLETION AND OPER
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