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 N6WA2026100902Elec Connector · damagedLEFT PITOT HEAT CAUTION MESSAGE AFTER T/O. REMOVED AND REPLACED LH PITOT PROBE HEATER CONNECTOR IAW ESPM 20-33-00 OPS CHECK GOOD SEALANT NEEDS VERIFIED CURED.SDR IPXA2026090366928Circuit Breaker · trippedAIR TURN BACK, WHILE ENROUTE, EICAS MSG GND EQUIPMENT COOLING RAN QRH AND PUT GND EQUIPMENT IN ALT. PROBE HEAT EICAS MSG. RT FWD FUEL PUMP AND L AFT FUEL PUMP EICAS MSGS. STATUS MSG EQPT COOLING FAN. RESET CB 310 AND RAN ALL SYSTEMS COMING OF AC BUS L SECTIOSDR AALA202607174116Elec Connector · looseAIRCRAFT WAS GROUNDED: ON LIFTOFF MULTIPLE FLIGHT DECK WARNING AND CAUTION LIGHTS ILLUMINATED. LOST COMM 1, NAV 1, UNABLE TO EXTINGUISH ANY LIGHTS ILLUMINATED. DECESION MADE TO RETURN TO PHL, EMERGENCY DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCSDR N6WA2026051507Wire · brokenR WING A/I CAUTION MESSAGE. FOUND BROKEN WIRE AT RH OB WING ANTI ICE TEMP SENSOR. RESCURED WIRE IAW CRJ-AMM-30-12-00. OP CHECKS GOOD.SDR DALA2026040302146Circuit Breaker · failedDIV - TO RDU DUE TO CAPTAIN'S PITOT HEAT INOP (ANTI ICE CAPT PITOT ECAM WARNING) AND FLYING INTO ICING CONDITIONS. REPLACED C/BS 3DA1 AND 2DA1. FOUND 3DA1 LOCK NUT LOOSE, AND WIRE STRAIN FROM BACK SHELL ON PITOT PROBE CONNECTOR (9DA1-A). LGCIU-1 REPLACED AS SDR IPXA2026030531783Terminal · out of toleranceR FWD WINDOW EICAS POSTED ON TAXI IN AFTER LANDING AS PER FIM 30-41 FT 804 NOTE, APU HISTORY REVIEWED IN MTX AND NO START DISCREPANCIES NOTED IN PAST 60 DAYS. T/S PER FIM 30-41- FT 803, FOUND WINDOW POWER TERMINAL RESISTANCES TO BE OUT OF TOLERANCE. J1-J5 11.2SDR HNAA2026021000115Wire · burnedPITOT 3 INOP WITH BOTH ENGINES RUNNING FACT 10FEB26 21:50 AGS R&R WIRE FROM PIN 2 AT A3 PITOT TUBE TO PIN C3 AT RELAY K0058 USING STANDART MAINTENANCE PRACTICES. INSTALLED NEW PITOT TUBE IAW AMM 34-13-02. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.
.SDR DALA2026011800404Wire Harness · shortedDURING PUSHBACK SAW ARCING COMING FROM WIRE GOING TO LEFT WINDOW. FOUND WIRE CHAFFED, DEACTIVATED WHC NR 1 PER AMM 30-42-00- 0404-001-A. AND APPLIED MEL 30-42-01 MCO & PLAC INSTALLED M PROC C/W DISP APPROVED. NR 1 WHC INOPERATIVE. FOUND VENDOR FURNISHED HARNSDR DXTA2026010906458Distribution Box · faultyIN FLIGHT WE GOT A CYAN R PROBE MON FAIL MESSAGE, WHICH THEN TRIGGERED THREE AMBER CAS MESSAGES: R AOA HEAT FAIL, PITOT 2 HT FAIL AND STBY PITOT HT FAIL. THIS ALL BEGAN WHEN THE HBMU 2 CIRCUIT BREAKER TRIPPED ON THE EMS-CDU. T/S SYSTEM, REMOVED SUSPECTED HBSDR COEA2026010601759Lead · faultedFLIGHT 8658, ENROUTE: SMF - CEC AIR TURNBACK, RECURRING AMBER PROP HEAT L CAS MESSAGE MIDWAY TO CEC DURING ICING CONDITIONS. AIRCRAFT RETURNED TO SMF. NO EMERGENCY WAS DECLARED. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LT NR 3 PROP LEAD. SDR HYIA20251212002Elec Connector · burnedPILOT REPORTED PITOT HEAT INOP. UPON INSPECTION THE PITOT SWITCH & SWITCH CONNECTION WERE FOUND TO BE BURNT. BOTH WERE REPLACED WITH NO ADDITIONAL DEFECTS NOTED.SDR HYIA20251212003Elec Connector · burnedPILOT REPORTED PITOT HEAT INOP. UPON INSPECTION THE PITOT SWITCH & SWITCH CONNECTION WERE FOUND TO BE BURNT. BOTH WERE REPLACED WITH NO ADDITIONAL DEFECTS NOTED.SDR HYIA20251107003Elec Connector · burnedPILOT REPORTED PITOT HEAT NOT WORKING. MAINTENANCE INSPECTED AND FOUND THE LEFT PIOTO HEAT SWITCH CONNECTOR MELTED. REPLACED WITH NEW SWITCH WITH NO FURTHER DEFECTS NOTED.SDR IPXA2025101589962Elec Connector · faultedRIGHT SIDE WINDOW EICAS DID NOT RESET. REPLACED POWER PLUG TERMINALS FOR J8 PER SWPM 20-30-12. WINDOW HEAT OPS CHECK GOOD PER AMM 30-41-00. THIS CLEARS THIS MEL. PLACARD REMOVED. DMP REVERSED. TERMINALS INSTALLED & TORQUED PER AMM 56-11-02. VERIFIED INSTALL OFSDR IPXA2025100489962Connector · shortedRIGHT SIDE WINDOW EICAS DID NOT RESET. REVERSED DMP.PER FIM 30-41 TREE 803,PERFORMED WHCU BIT/VERIFY TEST, FOUND WINDOW 2 AMBER LIGHT COME ON. PER TABLE 101 AND WDM 30-41-11, CHECK D2916A PIN 11, D1906 PIN C GOOD CIRCUIT, D1906 PIN D SHORT TO GROUND. PERFORMSDR DALA2025092306946Wire Harness · shortedANTI ICE L WINDOW SHORT CICUITED 3 TIMES CONSECUTIVELY REACHING CRUISE CB X14 PULLED PER MCC. R/R L SLIDING WINDOW HARNESS PER A320 AMM 56-12. OPS TEST OK PER A320 AMM 30-42. (LP: 6564526)SDR N6WA2025082701Terminal Block · looseSMOKE IN FLIGHT DECK FROM F/O'S WINDSHIELD. INSPECTED AND FOUND RH WINDSHIELD TERMINAL BLOCK IS LOOSE AND CAUSED THE SMOKE. NO DAMAGE TO THE WINDSHIELD EXCEPT THE TERMINAL BLOCK FOR THE WINDSHIELD HEAT. DEACTIVATED AND DEFERRED RH WINDSHIELD HEAT ON OCN 7009SDR IXXA20250820047Elec Connector · corrodedRETURN TO BLOCK DUE TO PROBE HEAT EICAS MESSAGE ACCOMPAINED BY A BURNING SMELL. AIRCRAFT WAS GROUNDED FOR INSPECTION AND MAINTENANCE. MAINTENANCE FOUND AND REPAIRED SHORTED WIRE W688-301B-20 IN ACCORDANCE WITH WDM 27-62-11 AND B767 SWPM 20-30-12. REMOVED AND RSDR SWIA2025040329Terminal Block · smokeSMOKE IN COCKPIT FROM CP SIDE WINDSHIELD HEAT. QRH RESOLVED ISSUE. (FLIGHT 5025 - FILED CLOSED)TROUBLESHOT COCKPIT SMOKE EVENT PER FIM 21-21-00 AND FOUND WHILE INSPECTING L/H WINDSHIELD WITH HEAT ON, FOUND LIGHT SMOKE COMING OUT BETWEEN L/H WINDSHIELD HEAT POWSDR VNAA2025021911102Wire Harness · damagedL WING A/I CAUTION MSG. DURING CLIMB OUT OF CLT. / REMOVED AND REPLACED LH OUTBOARD TELESCOPIC HARNESS IAW CRJ 900 AMM 30-11-10-000/400-802. OPS CHECK GOOD. NO FURTHER FAULTS FOUND AT THIS TIME.SDR VNAA20250108024Elec Connector · failedCIRCUIT BREAKER CBP-2 G5 KEEPS POPPING WHEN PILOT/CO-PILOT WINDSHIELD WIPER KNOBS ARE TURNED TO THE INT, SLOW, AND FAST SETTINGS. TROUBLESHOOTED THE CO-PILOT WINDSHIELD WIPER SYSTEM, BY TESTING WIRE CONTINUITY AND CHECKING IF VOLTAGE WAS BEING APPLIED TO THESDR DALA2024121011567Windshield · arced(LOG 6599544) CA L1 WINDOW ARC'ED CF 390 AND SPIDER WEBBED ACROSS THE WINDOW. CA FWD OVERHEAT AMBER LIGHT THEN ILLUMINATED. R&R L1 WINDOW REF B737 AMM 56-11-11. H12 WINDOW INSTALLED, TERMINAL TAP MATCHES TAP 2. ALL CKS GOOD. ALSO REPLACED HEAT CONTROLLER ON LOSDR JJBA20241227055Wire · burnedUPON REMOVAL OF STANDBY PITOT PROBE, WE FOUND EVIDENCE OF OVERHEATING ON WIRING AND CONNECTOR P0089. THE WIRE W102-0270-16 REMOVED FROM P0089 AND RELAY K0058 AND REPLACED.SDR CALA2024112901358Circuit Board · faultyREF L/P 3013410 - MSG 30-24051 WIPS HEATER MAT SLAT 5 ZONE A SHO WN FAULT IN FLIGHT AND AFTER 30 WING ICE PROTECTION SYSTEM GROUN D TEST ACCOMPLISHED MESSAGES CLEARED. DUE HISTORY AND AIR DIVERS ION TOMC REQUEST CONTINUE WITH FIM DMC-B787-A-30-10-F1-49A-421A SDR AALA202410116015Circuit Card · faultedAIRCRAFT WAS GROUNDED: WING ANTI ICE STATUS MESSAGE. AIRCRAFT RETURNED TO DFW, LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED WIPS ZONE CONTROL CARD 9 IAW MM 30-11-03.SDR SCNA20240903308Wire · pinchedDURING PREFLIGHT HEARD AN ELECTRICAL POP AND SAW ELECTRICAL FLASH SOMEWHERE NEAR MASTER CAUTION AND VISOR, AFTERWARDS SMELLED ELECTRICAL BURNING FOR A MOMENT. DURING INSPECTION BEHIND CAPTAIN GLARESHIELD COVER, FOUND LH FWD WINDOW HEAT WIRE PINCHED WITH EXPOSSDR UIEA2024082400844Wire · unsecureWINDOW OVERHEAT CAUTION MSG(<P>FOUND VERY LOOSE WIRE ON #1 WINDOW. TIGHTENED WIRE FASTNER PER AMM 56-11-11. BITE CHECK AND OPS CHECK SATISFACTORY. NO FURTHER DEFECTS NOTED.</P>)SDR DALA2024072407435Buss Bar · damagedAT CRUISE F340 NOTICE FO'S SIDE WINDOW WAS HOT TO TOUCH DELAMINATING AND ACTIVELY BUBBLING ON BOTTOM CENTER OF WINDOW. SLIGHT PLASTIC SMELL NOTED A LITTLE LATER PULLED W14 PER QRH. C/A: INSP RT WINDOW PER A320 AMM 56-12-11-200-001-A. WINDOW HAS BURN MAKRS AND SDR SWAA2024071512477Connector · damaged#2 ENGINE COWL ANTI ICE ILLUMINATED AT APPROX 9000 MSL<BR>RAN QRH AND REDUCED THRUST ON ENGINE LIGHT STAYED ILLUMINATED EVEN AT IDLE<[01] REMOVED AND REPLACED #2 ENG TAI VALVE IAW AMM 30-21-11. DURING INSTALL; TAI VALVE CONNECTOR WAS DAMAGED DUE TO CONNECTOR DSDR DALA2024053105715Terminal · arcedSHIP 0673 -SMKE- BEFORE DEPARTURE L1 WINDOW HEAT TERMINAL CONNECTION ARCED AND SMOKED. CORRECTIVE ACTION: REPLACED WINDOW HEAT HARNESS. (5958138)SDR CALA2024052201561Circuit Board · failedMAINTENANCE MEMO SHOWS ON CMCF ANTI-ICE WING ANTI-ICE WING, MAINTENANCE MESSAGE 30-20072 - FAULT ISOLATION REFERENCE: DMC-B787-A-30-10-F1-16A-421A-A. WIPS ZONE CONTROL CARD 12 FAILED. WING ICE PROTECTION CONTROLLER CARD 12 - REMOVAL AND INSTALL REFERENCE: DMSDR NACA2024050900001Connector · crackedLH WING TAI PRESSURE SWITCH CONNECTOR D2388 CRACKED. REPLACED L WING TAI PRESSURE SWITCH CONNECTOR D238 IAW SWPM 20-61-11, TESTED PER 30-41-04 OPS CHECK GOOD.SDR DALA2024042504700Wire Harness · faultedSHIP 3756 -DIV- TO SLC DUE TO A NUMBER 2-ENGINE COWL VALVE OPEN LIGHT ILLUMINATING. CORRECTIVE ACTION: MAINTENANCE PERFORMED OPS TEST OF ANTI ICE VALVE AND SWITCH PANEL. OPS OK REPLACED HARNESS PER B 737 AMM 71-51.SDR AALA202404190455Circuit Card · faultyAIRCRAFT WAS GROUNDED: WINDOW HEAT R FWD INOP.PILOT RETURNED TO ORD. MAINTENANCE TS AND FOUND MM 30-32442 IN FAULT HISTORY. ACCOMPLISHED FIM B787-A-30-40-F1-A9A-421A-A AND REPLACED SLOT 8 P300M1 AC2 CARD.SDR CALA2024012400222Connector · unknownLOW SPEED REJECT FOR AIR CONDITIONING UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED FOR WITH VENDOR ID V939095 MAC RELATED WORK ORDER 000000003095479 AND PRTR ANTI-ICE AND MASTER CAUTION ILLUMISDR VNAA2024010911101Unknown · unknownANTI-DUCT WARNING AND ANTI-ICE CAUTION MSG IN FLIGHT / INTERROGATED MAC FOUND EVENT LOC HISTORY AT SS14. REMOVED CONNECTOR MT168P2 IAW CRJ700 AMM 36-21-09-000-801. FOUND OLD STYLE INSERT. R&R CERAMIC INSERT IAW CRJ700 ESPM 20-26-00. RECONNECTED MT168P2 IAW CRJSDR 2023FA0000616Connector · failedPILOT DEPARTED THE MORNING OR MARCH 31 2023 AND SHORTLY INTO HIS FLIGHT, REPORTED AN ELECTRICAL BURNING SMELL. TURN BACK WAS PREFORMED AND FLIGHT RETURNED TO AIRPORT WHERE MAINTENANCE WAS READILY AVALLABLE. AFTER INVESTIGATION FOUND THO ELECTRICAL CONNECTORSDR AALA202309181386Circuit Card · failedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO EICAS MESSAGE Ï¿½ANTI ICE WINGÏ¿½. AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED WING ANTI-ICE ZONE CONTROL CARD #3 PER AMM 30-11-03.SDR ASAA2023071344051Wire · faultyLEFT SIDE WINDOW OVERHEAT. GROUNDED - YES. REMOVED & REPLACED L2 WINDOW CORD REF MM 30-41-00. OPS CHECK GOOD. 2 C/B PULLED & RESET. NO 30 DAY HISTORY. GROUND VERFICATION SUCCESSFUL. SEAMC JARED NOTIFED.SDR ASAA2023013081709Wire Harness · damagedAFTER OPENING #1 T/R'S AND COWLS, FOUND CONNECTOR FOR GROUND WING THERMAL ANTI-ICE SOLENOID VALVE MISSING. GROUNDED - YES. AFTER SEARCH, FOUND CANNON PLUG WEDGED BEHIND NEARBY ACTUATOR. IT HAS DAMAGE ON CONNECTOR AND CABLE SHIELDING IS FRAYED. VERIFIED CONNECTSDR 6CBA2023012623026Lead · faultedDURING A ROUTINE FLIGHT FROM KBOX TO KCYUL, THE FLIGHT CREW NOTED A PROP DE-ICE FAIL CAS IN FLIGHT. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO KCYUL. THE AIRCRAFT CONTINUED TO LAND WITHOUT INCIDENT. REPLACED THE LEAD TO THE PROP DE ICE SYS.SDR REXA2023012600158Terminal Block · burnedAT 3500 MSL COCKPIT CREW NOTED METALLIC BURNING SMELL AND SMOKE FROM LOWER LEFT CORNER OF CAPTAINS WINDSHIELD NEAR VENT/POWER ELEMENT. CLEANED AND RESECURED LOOSE WIRES TO THE TERMINAL BLOCK REF AMM 56-11-01. PERFORMED OPS CHECK OF THE WINDOW TEMP CONTROLLER SDR CALA2023011300107Connector · disconnectedANTI-ICE WING CAUTION SYSTEM CANNOT PROVIDE ICE PROTECTION TO TWO OR MORE ZONE PAIRS O N THE WING OR LOSS OF COMMUNICATION FROM THE WIPCU TO DCA. TEST PASSED MULTIPLE TIMES. PLUG, UPON INSPECTION OF HEATING MATS FOUND CONNECTOR BEHIND REINSTALLED ACCESS PANELSDR CALA2023010900056Circuit Breaker · trippedTAT PROBE EICAS MSG AFTER LIFT OFF. RAN QRH AND RETURED TO EWR. FLIGHT CREW STATES L TAT PROBE C/B TRIPPED WITH ASSOCIATED EICAS MSG. RESET C/B AND PERFORMED TAT PROBE HEAT SYSTEM OPERATIONAL TEST REF AMM 30-33-00-715-710. TEST PASSED SEVERAL TIMES WITH NO FAUSDR ASAA2022122941310Wire · faultedAFTER ROTATION, THE MASTER CAUTION AND L SIDE (L20) WINDOW OVERHEAT ILLUMINATED. WE RAN THE QRH AND THE CAUTION EXTINGUISHED. 30 SECS LATER, CAUTION ILLUMINATED AGAIN & TURNED OFF ASSOCIATED WINDOW HEAT SWITCH AS DIRECTED BY QRH & CONTINUED THE FLIGHT. GROUNDESDR ASAA2022122841290Circuit Breaker · trippedL SIDE WINDOW HEAT "OVERHEAT" ILLUMINATED. GROUNDED - YES. PER B737-9 IFIM 30-41-00-810-827 WHCU LEFT SIDE HAD NO POWER. CIRCUIT BREAKER WAS OUT. RESET CIRCUIT BREAKER. PERFORMED WHCU BITE. NO FAULTS. PERFORMED WINDOW HEAT TEST. TEST GOOD.SDR ASAA2022122721242Wire Harness · faultedUPON TURNING ENGINE ANTI ICE ON FOR ENGINE #1 NO BLUE LIGHTS SEQUENCED. TAI INDICATION WAS PRESENT ABOVE # 1 ENG N1 DISPLAY. FOUND P18-3 A7 ENGINE 1; ENGINE & WING CONTROL CB HAD POPPED - RESET CB FOR ICING CONDITIONS WE ENCOUNTERED. GROUNDED - YES. PERFORMED SDR QXEA2022120900333Wire Harness · openPROP DEICE CAUTION ILLUMINATED AGAIN AS WE TOOK THE RUNWAY FOR DEPARTURE. OCCURED DURING THE #1 PROP. TAKEOFF ABORTED AND RETURNED TO THE GATE. REMOVED FROM SERVICE. INTERROGATED CDS. FOUND OPEN PHASE B AND OPEN PHASE C UNDER TMCU1. DURING ELECTRICAL CONTINUITSDR QXEA2022112900329Circuit Breaker · malfunctionedENG ADPT HEAT 2 CAUTION LIGHT ILLUMINATED IN CRUISE. INTK LIP HTR ENG 2 CIRCUIT BREAKER POPPED. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REF W/O 326282 N/R-00001 FOR WORK PERFORMED AND REPLACEMENT OF THE #2 ENGINE INTAKE LIP HEATER CIRCUIT BREAKER. SDR ASAA2022112440930Lead · disconnectedFO SIDE WINDOW OVERHEAT ILLUMINATED AT CRUISE. RAN QRH, BUT UNABLE TO CORRECT THE WINDOW OVERHEAT. GROUNDED - YES. FOUND FO #2 WINDOW HEAT CORD DISCONNECTED. RECONNECTED WINDOW HEAT CORD IAW B737-900 AMM 56-12-11. PERFORMED WINDOW HEAT OPS CHECK IAW AMM 30-41-
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