JASC 3097
Service difficulty reports · 858
Reports filed under 3097 · Ice/Rain Protection 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 = '3097' 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 = '3097' 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 UIEA2018020500181Connector · dirtyLT ENGINE ANTI ICE EICAS ILLUMINATED DURING ENGINE RUN. REMOVED AND CLEANED THE ANTI ICE CONNECTOR, CHECKED PINS J1,J2 & J3 IAW FIM 30-21 TR 803, RAN ENGINE OPS CHECKED GOOD.SDR HNAA2018020100019Brush Block · damagedEMERGENCY LIGHT AND BACK EXIT SIGN FLICKERING IN FLIGHT. INSPECTED BRUSHBLOCK WIRING AND CONNECTORS. NO DEFECTS NOTED. REMOVED AND REPLACED THE NR 1 & 2 ENGINE BRUSHBLOCKS IAW MM 61-10-11. OPS CHECKED GOOD IAW PDT -8. RAN MANUAL. NO FLICKER OF EMERGENCY LIGSDR HNAA2018011900011Connector · not seatedLEFT OTBD TAIL DEICE BOOT WOULD NOT INFLATE IN FAST, LOW, AUTO OR MANUAL MODES. FOUND THE DE-ICE BOOT DISTRIBUTOR ASSOCIATED WITH THE LT OTBD HORIZONTAL TAIL BOOT CONNECTOR PLUG NOT SEATED. SEATED THE CONNECTOR. OPS CHECKED SEVERAL TIMES. OKAY FOR SERVICE.SDR C77A20171219001Wire Harness · failedWING ANTI-ICE LEAK ON CLIMB OUT. FLIGHT UNABLE TO PROCEED TO DESTINATION DUE TO WEATHER CONDITIONS. EMERGENCY DECLARED. MAINTENANCE REMOVED THE NR 4 SLAT ACCESS PANEL IAW AMM 27-83-07 SUBTASK 010-003-A FOR TROUBLESHOOTING. REMOVED AND REPLACED THE LT NR 4 SDR 2017FA0000650Wire · shortedUPON INSPECTION OF RH COCKPIT AREA FOUND SPLICE SP1474 AND SP4273 BURNT AND FUSED TOGETHER. ALSO FOUND WIRES W201-11086-16 AND W201-11087-16 BURNT AND DAMAGED FOR THE STANDBY PITOT STATIC SYSTEM.SDR HNAA2017121800391Wire · brokenDURING DESCENT. AFTER ENTERING ICE CONDITION, STAB ANTI ICE FAILED, WING ANTI ICE FAIL AND ICE CONDITION. ANTI ICE INOPERATIVE. REMOVED, CLEANED AND SWAPPED NR 1 AND NR 2 FAN AIR CONTROL THERMOSTATS. R & R IAW AMM 36-11-06-000-802A. OPS AND LEAK CHECKED SDR UIEA2017120502365Connector · damagedFOUND CONNECTOR D5656P PIN 38 UNABLE TO LOCK., REMOVED AND REPLACED IAW SWPM 20-61-11 REV 66 FOUND SATISFACTORY.SDR DALA2017120408418Connector · failedIMMEDIATLEY AFTER ENGINE SHUTDOWN,COPILOTS FORWARD WINDSHIELD HEATING ELECTRICAL CONNECTOR HAD A LOUD POP AND EMMITTED SPARKS. FOUND SENSOR SPRING IN CONTACT WITH WIRING.RETERMINATED WIRES AND INSTALLED NEW SENSOR PER MD90 AMM 30-41.WINDOW HEAT CKS GOOD. (LP# SDR ASAA2017112122659Wire Harness · faultedR2 WINDOW OVERHEAT LIGHT ILLUMINATED. ACFT GROUNDED. REPLACED THE SIDE WINDOW COIL HARNESS IAW WDM 30-41-11, P3, S2, AND AMM 30-41-21-760-801. OPS TESTED SATISFACTORY IAW AMM 30-41-00-710-801.SDR ASAA2017112022658Wire · faultedRIGHT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED WHCU BITE IAW FIM 30-41 TASK 801, FOUND WINDOW SENSOR FAULTS ON PREVIOUS FLIGHT LEGS. PERFORMED FIM 30-41 TASK 811, SENSOR RESISTANCE READINGS IN LIMITS AND WINDOW FILM RESISTANCE READ 59SDR SWAA2017112017870Element · arcedR1 FORWARD WINDOW HEAT ELEMENT ARCED. R & R THE WINDOW IAW AMM.SDR DALA2017111608172Wire Harness · damagedDIVERTED DUE TO FUMES IN THE COCKPIT AND CABIN. REPLACED THE CONNECTOR D01906 ON R2 WINDOW WIRE HARNESS IAW SWPM 20-16. REPLACED WINDOW HEAT CONTROLLER M191 IAW AMM 30-41. REMOVED THE R2 WINDOW IAW AMM 56-11. INSTALLED AND ADJUSTED THE R2 WINDOW IAW AMM 56-1SDR ASAA2017110522518Wire Harness · faultyFOLLOW-UP TO HISTORY OF P18-3 A6 ANTI-ICE & RAIN ENG 1, ENG & WING CONTROL CB TRIPPING GROUNDED - YES. PERFORMED REQUESTED RING-OUTS OF THE NR 1 ENGINE WIRING BETWEEN GND WTAI SOLENOID VALVE AND P5-11 PANEL. NO DEFECTS NOTED. AIRCRAFT RETURNED TO NORMAL CONFIGSDR ASAA2017102622323Wire Harness · deterioratedRT ENGINE NOSE COWL ANTI-ICE THERMAL VALVE HAS A DETERIORATED HARNESS. GROUNDED - YES. REMOVED AND REPLACED #2 ENG TAI VALVE , LEAK OPS CHECK GOOD REFB737-800 AMM 30-21-11-400-801.SDR ASAA2017102322305Terminal · damagedLEFT WINDOW OVERHEAT LIGHT ILLUMINATED AND CIRCUIT BREAKER TRIPPED. ACFT GROUNDED. CONFIRMED TERMINAL LUG AT CIRCUIT BREAKER C392 TO BE DAMAGED FROM HEAT. REPLACED THE TERMINAL LUG. RESET THE CIRCUIT BREAKER AND OPS TEST PASSED. BITE CHECK OF WINDOW HEATSDR UIEA2017101201958Terminal · arcedVERY STRONG ODOR OF ELECTRICAL FUMES AFTER TAKEOFF, TURNED OFF RIGHT FORWARD WINDOW HEAT , ODOR DISSIPATED IMMEDIATELY. FOUND THE LOWER RIGHT TERMINAL LOOSE AND ARCING, CLEANED THE TERMINAL AND REINSTALLED. OPS CHECKED GOOD IAW AMM 56-11-00.SDR ASAA2017100822131Pitot Tube · shortedAFTER ENGINES STARTED THE LT ELEVATOR PITOT LIGHT ILLUMINATED. ACFT GROUNDED. IAW WDM 30-31-11 FOUND THE LT ELEVATOR PITOT HEATER OPEN D644 PIN 40 TO GND OPEN. REPLACED LT ELEVATOR PITOT TUBE IAW AMM 27-31-94-000-801 & -400-801. OPS NORMAL. LEAK CHECKED GOODSDR ASAA2017100622130Circuit Breaker · openPROBE HEAT AUTO CIRCUIT BREAKER FOUND IN OPEN POSITION. ACFT GROUNDED. INSPECTED BEHIND P18-3, CAPTAIN`S PITOT TUBE AND P5-9 MODULE. NO DEFECTS NOTED. RESET THE CIRCUIT BREAKER IAW AMM 20-60-01. NO PREVIOUS HISTORY. OPS CHECKED NORMAL IAW AMM 30-31-00-730-801SDR QXEA2017092100579Connector · dirtyENG ADPT HEAT 1 CAUTION LIGHT ILLUMINATED IN FLIGHT DURING ICING CONDITIONS. REMOVED FROM SERVICE. FOUND CB "INTK LIP HTR ENG 1" POPPED. INSPECTED NR 1 ENGINE INTAKE HEATER CONNECTOR, NO DEFECTS NOTED. CLEANED CONNECTOR AND RE-INSTALLED. CLOSED CB IAW GPM 9.2.SDR UIEA2017092701891Wire · disconnectedRIGHT ENGINE STATUS MESSAGE, ENG TAI VALVE DOES NOT SHOW DURING RUNUP WHEN ANTI-ICE SWITCH IN ON POSITION. FOUND A WIRE DISCONNECTED W066-56W-24 OF PLUG D5406P. THE WIRE WAS RECONNECTED IAW W/D 30-12-11.SDR DALA2017081106139Wire · burnedWITH ANTI-FOG SWITCH ON, GET AN ELECTRICAL ODOR IN COCKPIT. NO CIRCUIT BREAKERS OPEN, TURN SWITCH OFF, ODOR DISAPPEARS. TROUBLESHOT AND FOUND THE SLIDING F/O WINDOW ANTI-FOG WIRING SPLICES NOT MAKING GOOD CONTACT AND BURNING. REPAIRED THE WIRING IAW SWPM 20.SDR ASOA201708094048Contactor · overheatedTHE CREW REPORTED HEAVY ELECTRICAL SMOKE ODOR COMING FROM BEHIND CAPTAINS SEAT AND WITNESSED ACTUAL SMOKE CLOSE TO THE FLOOR. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO BUF WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAF AND FOUSDR UIEA2017072801340Feeder Cable · damagedFOUND MAINTENANCE EICAS MESSAGES FOR THE NR 2 WINDOW HEAT. REPLACED THE NR 2 WINDOW HEAT WIRE CABLE IAW SWPM 20-10-11, REV 65, AND CARRIED OUT WINDOW OPERATIONAL TEST IAW AMM 56-11-02, REV 121.SDR ASAA2017071021330Circuit Breaker · openCIRCUIT BREAKER FOUND OPEN WHEN LEFT SIDE WINDOW HEAT SWITCH TURNED ON. ACFT GROUNDED. NO HISTORY OF FAULT LAST 120 DAYS. INSPECTED THE LT WINDOW & ELECTRICAL CONNECTIONS, NO DEFECTS NOTED. INSPECTED THE LT SIDE WINDOW HEAT POWER CIRCUIT BREAKER ON P6-12 PASDR UIEA2017070701117Wire · openLEFT WINDOW HEAT EICAS MESSAGE. PERFORMED CONTINUITY CHECK FROM D4294J TO D1922, FOUND OPEN WIRE, BSD SPLICE ON WIRE W624-209R-24. IAW WDM 30-41-12. SPLICED THE WIRE IAW SWPM 20-30-12. PERFORMED OPS CHECK OF L2 WINDOW HEAT IAW AMM 30-41-00, OPS CHECKED GOOD.SDR ASAA2017070521300Wire · out of limitsLEFT SIDE WINDOW HEAT OVERHEAT LIGHT ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED LEFT SIDE WHCU BITE IAW FIM 30-41, TASK 801. FAULT HISTORY LAST THREE REGISTERS SHOW SENSOR FAULTS. IAW FIM 30-41, TASK 811, & AMM 30-41-11. MEASURED LEFT SIDE TEMP SENSOR FROM SDR ASAA2017061521108Contact · dirtyRIGHT SIDE NR 2 WINDOW OVERHEAT LIGHT ILLUMINATED DURING DESCENT, CYCLED OFF FOR 2 MINUTES, TURNED BACK ON OK. ACFT GROUNDED. PERFORMED FIM 30-41, TASK 801, WINDOW HEAT CONTROL UNIT BITE PROCEDURE. NO CURRENT FAULT NOTED. OPS NORMAL. CHECKED WINDOW ALREADYSDR JGVR20170614004Wire · failedWINDSHIELD HEAT ELECTRICAL CABLE AND INSULATION BURNED INTERIOR COVERINGS ABOVE THE MAIN ENTRY DOOR. PROBLEM CAUSED BY WRONG WIRE SPLICE INSTALLED IN THE POWER CABLE.SDR ASAA2017051020730Lead · malfunctionedLEFT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED AT FL 330. FOLLOWED QRH PROCEDURES. WHEN WINDOW HEAT SWITCH RETURNED TO THE ON POSITION, OVERHEAT LIGHT REAPPEARED. ACFT GROUNDED. PRESSURIZED AIRCRAFT IAW AMM 05-51-91 AND TESTED LT SIDE WINDOW HEAT FOR 15 MINUSDR P5CA2017050400103Cover · missingDURING INSPECTION FOUND COCKPIT WINDOWS NR 1 AND 2 HEATER TERMINAL LUG COVER MISSING. THE COVER WAS REPLACED IAW SWPM 20-61-11, REV 64.SDR SIMA20170507001Lead · unknownCLIMBING IN THE 30,000'S FLIGHT LEVELS, RECIEVED W/S 2 HEAT FAIL MESSAGE. COMPLIED WITH CHECKLIST. MSO HAD RELAY CLICKING NOISES BEHIND FO SEAT. MOVED WINDSHIELD HEATING LEADS TO SPARE IAW AMM 30-42-04. OPERATIONAL TEST IAW AMM 30-42-00. OPERATIONS TESTED GOOSDR DALA2017050103519Wire · arcedON DESCENT INTO ATL TURNED ON W/S ANTI-FOG SWITCH. RECEIVED A QUICK FLASH IN COCKPIT, POPPING SOUND, EFIS FLICKERED MOMENTARILY. HAD ELECTRICAL BURNING SMELL FOR ABOUT 10 SECONDS, NO SMOKE, DISSIPATED QUICKLY. EVERYTHING NORMAL AFTER INCIDENT. PERFORMED 2120-2SDR QXEA2017042400322Wire Harness · arcedINFLIGHT, OBSERVED STRONG ARCING FROM WIRE BUNDLE TO CAPTAIN'S WINDSHIELD HEAT CONNECTOR BLOCK. TURNED WINDSHIELD HEAT OFF- ARCING STOPPED. REMOVED LT WINDSHIELD REFERENCE AMM TASK 56-10-01-000-801 AND INSTALLED SERVICEABLE LT WINDSHIELD FROM STOCK REFERENCE ASDR DXTA2017041506396Terminal Block · overheatedWHILE CLIMBING THROUGH FL 280 AROUND 20 MINUTES INTO FLT, A STRONG ELECTRICAL ODOR WAS NOTICED IN COCKPIT. VISUALLY FAINT SMOKE COULD BE SEEN IN ALL OF COCKPIT AREA AS WELL. NO ODOR OF SMOKE IN GALLEY OR CABIN. WINDSHIELD HEAT WAS ON AND NORMAL. SMOKE CAMESDR DALA2017041703115Terminal Block · burnedRETURNED TO DEPARTURE DUE TO AN ACRID ODOR IN THE FLIGHT DECK REPORTED TO BE FROM THE F/O'S WINDSHIELD. MAINTENANCE FOUND TERMINAL BLOCK R5-38 AND THE F/O'S WINDSHIELD BURNED AT CONNECTION P WHICH IS THE GROUND SIDE FOR WINDOW ANTI-ICE. THE TERMINAL BLOCK, SDR COEA2017041204923Lead · damagedCREW RECEIVED A NR 1 PROP ANTI ICE FAULT. ELECTED TO RETURN TO DEPARTURE DUE TO ICING CONDITIONS EXPECTED. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 PROP HEATER LEAD. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SSDR AU3R2017041233286Connector · burnedDURING CRUISE FLIGHT, ALL ANTI-ICE CIRCUIT BREAKERS TRIPPED. CREW SMELLED SMOKE. PROCEDED TO MAKE A NORMAL LANDING. OPENED THE FORWARD NOSE PANELS AND FOUND CONNECTOR E462, JUST FORWARD OF PRESSURE BULKHEAD, COMPLETELY BURNED AND MELTED ON BOTH HALVES AND SDR AALA201704039027Wire · damagedCAPTAIN SAW AN ARC EMANATE FROM HIS WINDSHIELD AFTER WINDOW HEAT WAS OPERATIVE FOR SEVERAL MINUTES. MEL PROCEDURE WAS APPLIED AND THE FLIGHT CONTINUED TO DSM WITHOUT FURTHER INCIDENT. MAINTENANCE REPAIRED WIRES TO TERMINAL ENDS OF CAPTAIN'S ANTI-FOG THERMAL SWSDR ASAA2017032820289Circuit Breaker · pulledL1 WINDOW HEAT LIGHT INDICATED AN OVERHEAT WHEN SWITCH IS PLACED ON. ACFT GROUNDED. FOUND THE LEFT FWD WINDOW HEAT POWER CIRCUIT BREAKER OUT ON P6-11 PANEL. INSPECTED THE CIRCUIT BREAKER & ASSOCIATED WIRING BEHIND PANEL. INSPECTED WINDOW & CONNECTIONS. NO DSDR QXEA2017031600125Wire Harness · failedPROPELLER DEICE CAUTION, ILLUMINATION ON NR 2 PROPELLER HEAT. CAUTION EXTINGUISHED ONCE NR 2 PROP HEAT LIGHT EXTINGUISHES. DIVERTED. LANDING UNEVENTFUL. REPLACED THE NR 2 PROPELLER, NR 4 BLADE DEICE WIRE HARNESS & FUNCTIONAL TESTED IAW AMM TASK 61-10-06-000-8SDR ASAA2017030720076Wire Harness · shortedTAXI OUT WITH SELECTOR OF ANTI-ICE NR 1 ENGINE DID NOT LIGHT, NR 2 DID LIGHT. EGT SOGS RISE. CHECKED LIGHTS BUT PANEL DOESN'T HAVE POWER. CIRCUIT BREAKER TRIPPED. ANTI-ICE WING PANEL ALSO LACKS POWER. ACFT GROUNDED. FOUND ENGINE AND WING ANTI-ICE PANEL HAD SSDR ASAA2017022719961Wire · failedOVERHEAT WINDOW HEAT ILLUMINATED R2 SIDE AT APPROXIMATELY 5000FT DURING APPROACH. COMPLETED QRH AND DID NOT EXTINGUISH. ACFT GROUNDED. ACCOMPLISHED R2 SIDE WHCU BITE IAW FIM 30-41 TASK 811. SENSOR FAULT ILLUMINATED IN CURRENT AND LAST 10 LEGS OF HISTORY. RSDR ASAA2017022619948Wire · failedAT CRUISE R2 WINDSHIELD OVERHEAT LIGHT ILLUMINATED, PERFORMED QRH CHECKLIST, LIGHT REMAINED OUT. ACFT GROUNDED. NUMEROUS FAULT FOR SENSOR ON WHCU BITE. RESISTANCE CHECKED FOR WINDOW COLD & EXTENDED HEAT APPLIED SHOW SAME VALUE WITHIN LIMITS, IAW AMM 30-41-21SDR UIEA2017022300239Connector · damagedRIGHT ENGINE ANTI-ICE CAUTION MESSAGE RECEIVED DURING INITIAL CLIMB. COMPLIED WITH QRH AND FOUND A LOOSE CONNECTOR AND CORRODED PIN, CLEANED AND LUBED. REINSTALLED THE CONNECTOR. RAN ENGINE AND OPS CHECKED GOOD IAW AMM 30-21-00.SDR ASAA2017022019883Lead · failedLEFT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED, RESET WITH QRH PROCEDURE. ACFT GROUNDED. PERFORMED BITE IAW FIM 30-41 TASK 801. FOUND SENSOR FAILURE. REPLACED COIL CHORD ASSEMBLY, NO FAULTS FOUND.SDR RU3A20170210003Connector · dirtyRIGHT ENGINE COWL ANTI-ICE FAIL LIGHT ILLUMINATED DURING FLIGHT, PROBLEM WAS CORRECTED AFTER CLEANING OF ELECTRICAL CONNECTORS.SDR QXEA2017020800046Wire Harness · failedDESCENDING OUT OF FL 180 WE EXPERIENCED DUAL A/C GEN CAUTION LIGHTS AND CAUTION LIGHTS OF ALL A/C CONSUMERS. RAN E&A CHECKLIST RESET PROCEDURE AND EXTINGUISHED ALL CAUTION LIGHTS. NO OTHER ABNORMALITIES OBSERVED. LANDING UNEVENTFUL. FOUND NR 1 ENGINE NR 2 PROPSDR DALA2017012600695Wire · arcedDIVERTED DUE TO A STRAKE ICE FAULT ON EOAP DURING FLIGHT, WITH ICING CONDITIONS FORECASTED. MAINTENANCE REMOVED AND REPLACED THE RIGHT STRAKE WITH NO HELP. MAINTENANCE FOUND AND CONFIRMED THE RIGHT STRAKE CONNECTOR INSIDE THE FUSELAGE, BEHIND RIGHT RADIO RASDR ASAA2017010819277Wire · damagedLEFT SIDE WINDOW OVERHEAT LIGHT CAME ON AFTER RUNNING QRH. LANDED BEFORE 25 MINUTES EXPIRED. ACFT GROUNDED. ACCOMPLISHED WINDOW HEAT SYSTEM, OPERATIONAL TEST IAW AMM 30-41-00-710-801. LEFT SIDE WINDOW SWITCH MOVED TO ON, ON LIGHT WOULD NOT ILLUMINATE AFTER 30SDR GLBA2017010300628Wire · loosePILOT REPORTED THAT THEY HAD AN ELECTRICAL SMOKE SMELL IS OBSERVED WHEN THE RIGHT SIDE WINDSHIELD HEAT IS ACTIVATED. MAINTENANCE FOUND THE POWER WIRE ON RT WINDSHIELD HEAT TERMINAL NOT FULLY SECURED, REMOVED WIRE AND CLEANED TERMINAL AND RESECURED IAW MM 56-10
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