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 ASAA2020022863306Connector · looseLEFT COWL VALVE FAILED OPEN. GROUNDED - YES. PERFORMED GVI ON LEFT ENGINE COWL ANTI ICE VALVE, FOUND CANON PLUG LOOSE, REINSTALLED, PERFORMED COWL VALVE BITE PROCEDURES REF B737-800 FIM 30-21 TASK 803, OPS CHECK GOOD.SDR UIEA2020020410161Terminal Block · arcedAT 15000 IN A CLIMB, THE CREW NOTICED AN ACRID/NOXIOUS FUME IN THE COCKPIT. THE CREW RETURNED TO IAH ON OXYGEN AND RAN "THE SMOKE FIRE OR FUMES" QRH CHECKLIST. ON RUNWAY EXIT, THE EVACUATION CHECKLIST WAS RUN. LANDING WEIGHT 243,000 LBS, BELOW 272,000 LBS MLW.SDR QXEA2020012800058Wire Harness · damagedON CLIMB OUT PROP DE-ICE CAUTION ILLUMINATED. DURING RUNNING OF PROP DE-ICE CHECKLIST, CAUTION LIGHT EXTINGUISHED AND RE ILLUMINATED. FINISHED CHECKLIST AND CAUTION ILLUMINATED AGAIN. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INTERROGATED CDSDR A6WA2020012847131Connector · disconnectedWING OVERHEAT WARNING MSG ON CLIMBOUT. CW QRH MSG CLEARED WITH WING A TIICE OFF WITHIN 40 SECONDS. RETURNED TO MKE. LANDING WEIGHT UNDER 44 000 LBS, BTMSMAX 3,3,2,3 MC ACARS REPORTS THIS IS THE RH WING AIRCRAFSDR 2020FA0000121Terminal · damagedTHE SUPPLY CABLE AND POSITIVE TERMINAL ON THE LT WINDSHIELD DEICING POWER SUPPLY, L1001DG, PN16N24334 HAD BEEN SEVERELY HEAT DAMAGED. THE THREE DEICING POWER SUPPLIES WERE REPLACED FOR AN UPGRADE ON 23 MARCH 2017. REMOVE AND REPLACED DAMAGED POWER SUPPLY. RSDR QXEA2020010300003Wire Harness · defectivePROP DEICE CAUTION ILLUMINATED DURING CYCLING OF #2 PROP DEICE. #1 PROP DEICE OPERATED NORMALLY. CHECKLIST RUN. NO HELP. DIVERTED. ACCOMPLISHED UNEVENTFUL LANDING. REMOVED FROM SERVICE. REPLACED # 2 PROP #6 DEICE HARNESS. OPS CHECK GOOD. RETURNED TO SERVICE.SDR P6UR2020010298001Circuit Breaker · burnedDURING ACCOMPLISHMENT SCREEN HEAT CIRCUIT BREAKERS INSPECTION (F6 INSPECTION) OVERHEATING/MELTING OF THE CIRCUIT BREAKER BODY WAS DETECTED.SDR ASAA2020010231721Wire · out of positionRIGHT SIDE WINDOW HEAT OVERHEAT ILLUMINATED IN FLIGHT PER QRH PROCEDURES SELECTED OFF FOR 5 MINUTES, THEN ON. LIGHT DID NOT RE-ILLUMINATE. GROUNDED - YES. SWITCHED WIRE FROM PRIMARY SENSOR TERMINAL TO SPARE TERMINAL FOR R2 WINDOW IAW FIM 30-41 TASK 811. BITE CSDR AALA202001029001Wire Harness · burnedAIRCRAFT WAS GROUNDED: PILOT REPORTS LEFT SIDE WINDOW OVERHEAT ILLUMINATED ON APPROACH. MAINTENANCE REPORTS UPON TROUBLESHOOTING FOUND WIRE WO420-2005B FIMD41440J AND TB4201Y BURNT, WIRE WO420-5504 FROM D01046A AND D04203 BURNT, WIRE W0420-1002 FROM D400685 TOSDR AALA2019122659002Wire · damagedAIRCRAFT WAS GROUNDED: CAPT SLIDING WINDOW HEAT WIRE ATTACH POINT LOWER RT. SIDE STARTED SMOKING IN FLIGHT WINDOW HEAT OFF SMOKE STOPPED. MAINTENANCE FOUND CAPT SLIDING WINDOW LOW RT POWER TERM & SCREW BURNT. INSTALLED NEW TERMINAL END AND REPAIRED WIRE W2004SDR DALA2019111986763Wire Harness · damagedSHIP 1808 -DIV- TO JFK DUE TO LT FWD WINDOW HEAT INOP. UNABLE TO CONTINUE DUE TO WEATHER EN ROUTE. CORRECTIVE ACTION: REPAIRED LT FWD WINDOW HEAT WIRING HARNESS. REPLACED LT WINDOW HEAT CONTROLLER.SDR AALA2019111439008Wire Harness · burnedAIRCRAFT WAS GROUNDED: PILOT REPORTS ANTI-ICE WING EICAS ILLUMINATED IN DESCENT ALONG WITH THE WING ANTI ICE SYS STATUS MESSAGE. MAINTENANCE TROUBLESHOT TO FAULTY WING ICE PROTECTION TRANSLATING WIRE BUNDLE FOR #8 SLAT, FOUND SIGNS OF BURNT PINS. REMOVED AND RSDR ENHA20191111618Wire · damagedPILOT LOG PAGE DISCREPANCY: "USE OF WINDSHIELD HEAT CAUSED ELECTRICAL SPARKS TO COME FROM L/H CIRCUIT BREAKER PANEL"SDR CALA2019110901936Wire · damagedLEFT ELEV PITOT LIGHT ON. TROUBLESHOT LH ELEV PITOT REF FIM 30-31-00-810-805, FOUND OPEN CONTINUITY REF STEP F. 2 AT PIN 40 OF CONNECTOR D644. PITOT PROBE REQS REPLACEMENT. REF FIM 30-31-00-810-805 STEP F2(B) FOUND PIN SEPERATED FROM PIN ON WIRE W7102-2001B-20SDR HNAA2019103000333Wire · burnedPDIS 686 30-31 2088311 29OCT19 TRI CLOSE
PITOT 3 INOP MESSAGE.
FACT 29OCT19 03:29 TRI
REPAIRED BURNT WIRE IAW IAW SWPM 20-21-00. INSTALLED
NEW #3 PITOT-STATIC TUBE IAW AMM 34-13-02. LEAK CHE
CK GOODSDR DALA2019102406129Wire · burnedON A/C WAKE UP ,CB POPPED + ANTI-FOG TURNED ON. C/B LEFT OUT, FOUND FLASH SOOT BY PREVIOUS REPAIR ON CAPT,S SLIDING WINDOW HEAT WIRING MARKED WIP 507047. COLLARED C/B. CAPT CLEARVIEW WINDOW DEFOG WIRE X3 FOUND BURNT + BROKEN AT UPPER AFT CORNER OF WINDOW. B717SDR DALA2019102106014Wire · sparksSPARKS FROM CAPTAINS WINDSHIELD, DID NOT TOUCH. NO TURBULENCE. RANDOM SPARKS. ON CAPT'S WINDSHIELD FOUND HEAT SINK WIRE TERMINAL CONTACTING HEAT SINK RETAINER SPRING. ADJUSTED FOR CLEARANCE. ALL CKS GOOD. (LP6193492)SDR UIEA2019101765736Connector · not reportedF/O'S SLIDING WINDOW HEAT INOPERATIVE. ACCOMPLISHED M PROCEDURE PER DDG. REMOVED AND REPLACED R2 WINDSHIELD CONNECTOR J8 IAW SWPM 20-30-12. OPS CHECKED GOOD.SDR ASOA2019101424056Connector · burnedCUU - THE CREW REPORTED A BURNT SMELL IN THE COCKPIT, FAINT WITH NO SMOKE OBSERVED. MAINTENANCE REMOVED AND REPLACED A BURNT CONNECTOR FOR THE NUMBER TYWO WINDSHIELD HEAT CONTROLLER, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURNSDR JIKA201910110901Circuit Breaker · burnedAMF FLT 1367 - ON DECENT INTO KLAS PILOT NOTICED A BURNING SMELL / ODOR COMING FROM THE RH ESSENTIAL CIRCUIT BREAKER PANEL. CREW CONTINUED WITH SAFEST COURSE OF ACTION AND LANDED IN KLAS WITHOUT ISSUES. INSPECTED RH ESSENTIAL BUS AND FOUND R DUCT ANTI-ICE CISDR QXEA2019091600355Wire Harness · damagedENGINE ADPT HEAT 2 CAUTION ILLUMINATED. (CB TRIPPED), REMOVED FROM SERVICE. FOUND DAMAGED WIRES SHORTING TO GROUND ON #2 ENGINE INTAKE LIP HEATER. REPLACED HARNESS. GROUND RAN ENGINE AND OPS CHECKED INTAKE ANTI-ICING SYSTEM PER AMM TASK 30-21-00-710-801. NO FASDR UIEA2019091205484Wire · brokenLEFT SIDE WINDOW HEAT INOP. TRANSFERRED TO MDDR # 117627 AS PER MEL 30-40-01-02 CAT C LP 1076367: REPAIRED BROKEN WIRE AT L2 WINDOW C/P IAW SWPM 20-10-11. OPS CHECK NORMAL. MDDR 117627 CLEARED. PLACARD REMOVED AND MCC NOTIFIED.SDR UIEA2019082805310Wire · disconnectedRT FWD WINDOW HEAT EICAS MESSAGE AND INOP LIGHT ON OVERHEAD PANEL CAME ON AFTER LANDING. DURING TROUBLESHOOTING, FOUND 2 SHIELDED WIRES FROM TERMINAL BOARD T234, FA2 AND FC2 NOT CONNECTED FOR WIRES W624-203B AND W624-202R. RESOLDERED IAW SWPM 20-10-15. PERFORSDR SIMA201908276001Circuit Breaker · shortedCIRCUIT BREAKER BEHIND CAPTAIN SEAT B2 (HEAT PITOT 1) WHEN PULLED ELECTRIC BURN SMELL.-C/A-FOUND K0054 RELAY PITOT CURRENT SENSOR TO HAVE A ELECTRIC BURN SMELL. REMOVED AND REPLACED PITOT CURRENT SENSOR K0054 IAW EMB 145 AMM 30-31-01. PERFORMED OPERATIONAL CHESDR UIEA2019082705304Wire · shortedEICAS MESSAGE FOR RT FWD WINDOW. RAN QRH 3.15. PERFORMED FIM 30-41 FT 802. CHECKED SENSOR 1 SENSOR 2 OHMS GOOD. CHECKED WINDOW HEAT ELEMENT RESISTANCE AT 10.2 OHMS GOOD, FOUND SHORT TO GROUND ON WIRE W624-202B-24 W624-203B-24, W624-215B-24. ITEM 3. ITEM 3SDR DALA2019082604949Connector · sparksDURING FLT, CENTER WINDSHIELD WINDOW HEAT CONNECTION SPARKED AND MADE LOUD POPPING SOUND. REMOVED AND REPLACED CENTER WINDSHIELD IAW MD88 AMM 56-10-01C. LEAK CK GOOD. WINDOW HEAT CKS GOOD PER MD88 AMM 30-41. WINDOW, COCKPIT OFF 09-5611-9-0013 S/N 31037 ON 09-5SDR ASAA2019082633476Connector · loose#2 ENGINE, CORE LOCATION, GROUND WING THERMAL ANTI ICING SOLENOID VALVE CONNECTOR DP1103 IS LOOSE. GROUNDED - YES. REMOVED AND REPLACED THERMAL ANTI ICING SOLENOID REF B737-900 AMM 30-11-12-400-801 OPS CK GOOD.SDR IPXA2019081645689Connector · damagedLEVEL 2 TAIL A-ICE DISAG DURING CLIMBOUT (IN ICING CONDITIONS) COMPLIED WITH QRH DEPARTED ICING CONDITIONS AND LIGHT EXTINGUISHED DUE TO ICING AT DESTINATION MALFUNCTION RESULTED IN DIVERSION. REPLACED TAIL WING ANTI ICE VLV IAW AMM 30 12 01 400 801 P/N ON/OFSDR ASAA2019081203370Wire · misinstalledR2 WINDOW HEAT OVERHEAT LIGHT ILLUM ON SHORT FINAL AT NIGHT. GROUNDED - YES. WHCU FAULTS WINDOW SENSOR. SENSOR RESISTANCE NORMAL, WIRING FROM WINDOW TO WHCU NORMAL. FOUND HEAT LEAD ON TRANSFORMER TERM 2, SHOULD BE ON TERM 1 FOR H16 REF B737-800 WDM 30-41-11. RSDR DALA2019080604589Terminal · shortedTAXING INTO RAMP, BIG SPARK OUT OF CAPT WINDSHIELD ANTI-ICE CONNECTOR. FOUND WIRE TERMINAL IN CONTACT WITH SPRING ON WINDOW TEMP SENSOR. ADJUSTED WIRE TERMINAL FOR CLEARANCE. CKS OK. (LP5490390)SDR CA191115005Wire · damaged(CAN) FROM PILOT REPORT - DURING FLARE ON LANDING, ELEVATORS JAMMED AND THE AIRCRAFT WAS NOT ABLE TO BE PITCHED UPWARDS OF 2-3 DEGREES. AIRCRAFT TOUCHED DOWN AT LOW PITCH ATTITUDE. NO CREW CO-ORDINATION PROCEDURE INITIATED BY CAPTAIN (OPERATING RIGHT HAND SEATSDR IPXA2019080245252Connector · inoperativeAIR TURN BACK DUE TO ANTI ICE ISSUES AND FORECAST ICING EN ROUTE. REPLACED THE CONNECTORS AND WIRES FOR THE NR 1 ENGINE. REPLACED THE NR 3 ENGINE WIRES, CW 3020 3020 73496 A.SDR DALA2019072904449Connector · arcedACRID SLIGHT ELECTRICAL SMELL FROM CAPTS EFIS SELECTOR PANEL BELOW CLEAR VIEW WINDOW. REMOVED AND INSP CAPTS EFIS SELECT PNL, CAPTS ACP AND CAPTS GRIMES LIGHT. NO TROUBLE FOUND. REMOVED LT WINDSHIELD ELEC CONN R5-13 AND FOUND TERMINAL 'P' HAD ARC CAUSING ELEC SDR DALA2019072604440Wire Harness · defective(LOG 5952208) DURING FLIGHT THE LEFT SLIDING WINDOW HEAT INOPERATIVE AND ELECTRICAL SMELL FROM COILED POWER CORD THAT ATTACHES TO CAPTAINS SLIDING WINDOW. R/R LT SIDE WINDOW HARNESS D10572 PER AMM 30-41. ALL CHKS NML.SDR CA190722013Relay · faulty(CAN) REPEATED STANDBY PITOT HEAT CAUTION IN FLIGHT, PITOT TUBE AND TMU WERE REPLACED BUT THE DEFECT RETURNED, MTC`S TROUBLESHOOTING INDICATE THAT TAPPING THE RELAY RECTIFIED THE FAULT. THE RELAY WERE PREVIOUSLY REPLACED 9 DAYS AGO. THE 3000-K5 RELAY WERE REPLSDR ASAA2019071530083Wire Harness · failedL-2 WINDOW OVERHEAT LT CAME ON DURING CLIMB-OUT RESET PER CHECKLIST. LIGHT CAME ON AGAIN. GROUNDED - YES. DUE TO HISTORY REMOVED AND REPLACED L2 WINDOW CORD REF AMM 30-41-00. ALT DEACT REVERSED. VERIFIED L2 WINDOW IS CORRECTLY TAPPED REF W/D 30-41-12. PERFORMESDR CA190710004Wire Harness · failed(CAN) WING A/ICE FAULT CAUTION DURING ROLLOUT ASSOCIATED WITH C/B TRIPPED INDICATION FOUND OUTBOARD SLAT HARNESS, LEFT OUTBOARD WING SHORTED. LH OUTBOARD SLAT HARNESS REPLACED IAW AMP J24-09-06-40AAA-720A-A TEST PFD SATIS IAW AMP BD500A-J30-12-00-01AAA-320SDR ASAA2019062089760Wire Harness · disconnectedR2 WINDOW HEAT OVERHEAT LIGHT. GROUNDED - YES. FOUND RH SIDE WINDOW HEAT HARNESS DISCONNECTED. CONNECTED HARNESS AND ACCOMPLISHED WINDOW HEAT CONTROL UNIT SYSTEM - TEST, NO DEFECTS NOTED, REF B737-900 AMM 30-41-11.SDR CA190531006Wire Harness · unknown(CAN) WING ANTI-ICE FAIL MESSAGE POSTED ALL REMAINING WIRING CHECKS COMPLETED AND NO FAULTS FOUND HARNESS AND SENSOR REPLACED AS A PRECAUTION, C08141004-103, PRESSURE TRANSDUCER, (2 QTY) CPWLC7025-011 ANTI-ICE WING HARNESSES CPYLC7032-013 ANTI-ICE WING HARNSDR CA190529002Pin · loose(CAN) WING ANTI-ICE FAIL MESSAGE POSTED IN FLIGHT. CHECKING ALL GROUNDS, FOUND NO GROUND AT GS2610-L1, NO GROUND AT PIN B. (TC# 20190529002)SDR ASAA2019051329333Connector · contaminatedENROUTE RT COWL VALVE OPEN BLUE LIGHT FLICKERING WITH ENG ANTI ICE SWITCH OFF. WHEN ENG ANTI ICE SWITCH SELECTED ON BRIGHT BLUE COWL OPEN LIGHT ILLUMINATED. LIGHT BRIGHT BLUE IN DESCENT REGARDLESS OF SWITCH POSITION. GROUNDED - YES. PERFORMED FIM 30-21 TASK 80SDR CA190506009Wire Harness · damaged(CAN) FLIGHT CREW REPORTED A DUAL AC GENERATOR FAILURE WITH THE PROP DE-ICE ON WHEN CLIMBING THROUGH 17000` . CREW WERE ABLE TO RESET THE GENERATORS BUT THEY WENT OFF LINE AGAIN WHEN THE PROP RPM WAS SET TO 900. CREW ELECTED TO RETURN TO THE DEPARTURE AIRPORT SDR UIEA2019042974052Connector · miswiredL2 WINDOW HEAT INOP(<P><SPAN>PERFORMED FIM 30-41-00 TASK 804, FOUND PINS 6 & 4 MISS-WIRED AT WINDOW CONNECTOR PER WDM 30-41-00. RE-PINNED PINS 6 & 4. WINDOW HEAT L/H #2 AND #3 OPS CHECK NORMAL. PLACARDS REMOVED.</SPAN></P>)SDR CA190425016Wire Harness · faulted(CAN) L WING A/I FAULT WIRING MEASURED BETWEEN L OUTBD ANTI ICE PRESSURE SENSOR MT 126 AND CONNECTOR P5027. FOUND OPEN CIRCUIT BETWEEN MT126 PIN A, AND P5027 PIN 1. REFERENCE IAW ASDP BD-500-A-J30-12-00-01AAA-054A-A HARNESS CPWLC725-011 REPLACED IAW BD50SDR DALA2019042282570Safety Wire · out of positionHEARD AND OBSERVED SPARKS & SMOKE COMING FROM THE SIDEWALL AREA, JUST AT THE BASE OF THE F/O CHART HOLDER. SHUT OFF WINDOW HEAT ON RT SIDE. SMOKE & SPARKS STOPPED. IAW WDM 30-41-12. FOUND SAFETY WIRE ARCING NEAR TERMINALS 1 AND 2 ON TB5038. REMOVED THE SAFSDR UIEA2019041973900Connector · brokenRH SIDE WINDOW HEAT INOP. FOUND BROKEN CONTACT AT RT SIDE WINDOW HEAT, PLACED P/N CW02-2010 TERM C KIT02-2010 PER TABLE 5 IAW SWPM 20-64-16. REMOVED AND REPLACED R2 WINDOW CONNECTOR D1906 J-B IAW WDM 30-41-11 AND SWPM 20-30-12. OPS CHECK GOOD IAW AMM 30-41-0SDR UIEA2019041203861Connector · dirtyL2 WINDOW HEAT INOP. FOUND LOOSE CONNECTION AT C/P D5872P. CLEANED AND SECURED REF WDM 30-41-02. PERFORMED OPS TEST IAW AMM 30-41-00-715-001, OPS TEST GOOD.SDR DALA2019040702265Wire · exposedFO SHOCKED BY WINDOW HEAT WIRE CONNECTORS. FOUND EXPOSED WIRE ON ONE QUICK DISCONNECT CONNECTOR ON FO'S ANTIFOG SLIDING WINDOW. REPAIRED CONNECTO PER SPWM CH 20 AND MD88 WDM 30-44 OPS CKS NML. (LP4694336)SDR HNAA2019040400088Contactor · faulted656 30-41 1919182 01APR19 PHL CLOSE
WINDSHIELD HEAT 1 INOP EICAS MSG
27626 00 RNR
HISTORY: 31MAR (3X)
FACT 01APR19 06:46 ALB
TROUBLESHOT WS HEAT 1 INOP MSG PER EMB145 FIM TASKSDR ASAA2019040188835Connector · damaged#2 ENGINE, CONNECTOR DP1103 AT GROUND WING THERMAL ANTI-ICE SOLENOID VALVE IS LOOSE. GROUNDED - YES. RESECURED #2 ENGINE CONNECTOR DP1103 BACKSHELL REF B737 SWPM 20-60-09.
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