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 UIEA2016122401053Wire · damagedRIGHT ENGINE ANTI-ICE EICAS MESSAGE. PERFORMED TROUBLESHOOTING IAW FIM 30-21 FT 806 , AND WDM 30-21-11-1. FOUND THREE BROKEN WIRES. PERFORMED REPAIR AND PINNING OF ALL THREE WIRES IAW SWPM 20-10-13. PERFORMED OPS CHECK OF ANTI-ICE AND RT THRUST REVERSER CHSDR ASAA2016122019185Terminal · dirtyR2 FLIGHT DECK WINDOW EXCESSIVELY HOT. ACFT GROUNDED. FOUND R2 SLIDING WINDOW TEMP 170 DEGREE F. TURNED R2 WINDOW HEAT OFF. RELEASED PER MEL 30-11E.. CHECKED WINDOW SENSOR CONNECTOR TERMINALS, CLEAN AND FREE FROM CORROSION. PERFORMED RIGHT SIDE WINDOW HEAT SDR J7SA20161215002Wire · damagedDIVERTED DUE TO SEVERAL ANTI ICE SYSTEM CASS MESSAGES. CREW REQUESTED LOWER ALTITUDE, OUT OF ICING CONDITIONS, AND EXECUTED THE EMERGENCY CHECKLIST. LANDED WITHOUT INCIDENT. PERFORMED OPERATIONAL TEST IAW ADVISORY WIRE AW300-36-0008 REV 2, NO DEFECTS NOTED. OPSDR VQIA2017081000041Connector · damagedRETURNED TO FIELD AT THE REQUEST OF MX CONTROL DUE TO REPEAT LT WINDOW HEAT FAULT REPORT AFTER TAKEOFF. TO DATE THE SPARE WINDOW HEAT SENSOR HAS BEEN ACTIVATED AND THE WINDOW HEAT COMPUTER HAS BE REPLACED. THE LT WINDOW HEAT SYSTEM FAULT RETURNED ON A SUBSEQSDR N6WA2016111701Terminal Block · failedSMOKE IN FLIGHT DECK, 30 MINS PRIOR TO LANDING, FROM TERMINAL BLOCK OF WINDOW HEAT ON FO SIDE WINDSHIELD. DURING TROUBLESHOOTING FOUND FO WINDSHIELD REQURING REMOVAL IAW AMM 56-11-01.SDR VNAA2016102200024Connector · damagedCREW RECEIVED AN ANTI-ICE DUCT WARNING AND A LEFT ENGINE BLEED CAUTION MESSAGE AT 24000 FT. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST AIRPORT, AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, RESEATED PIN 8 ON ELECTRICAL CONNNECTOR P802, AND PSDR UIEA2016090500732Connector · not seatedRT ENGINE ANTI-ICE EICAS MESSAGE IN FLIGHT WITH ENGINE ANTI-ICE ON. RT ENGINE ANTI ICE VALVE LIGHT WAS ON FOUND PRSOV NOT SUPPLYING AIR TO
ANTI-ICE VALVE. RESEATED CONNECTOR ON PRSOV. OPS CHECKED RT ENGINE ANTI-ICE GOOD IAW AMM 30-21-00, OPS CHECKED PRSOV SDR QXEA2016082900559Wire Harness · defectivePROP DE-ICE CAUTION LIGHT ILLUMINATED A FEW SECONDS EVERY TIME NR 1 PROP DE-ICE, GREEN LIGHT ILLUMINATED. RETURNED TO FIELD. LANDING UNEVENTFUL. CLEARED FAULTS AND PERFORMED FUNCTIONAL TEST OF THE PROPELLERS DE-ICING SYS IAW AMM 30-61-00-720-801. FOUND FAUSDR ASAA2016082417793Window · arcedAT FL370 2.5 HOURS INTO FLT, NOTED ELECTRICAL ARCING SOUND FROM CAPTAIN'S FWD WINDSCREEN, TURNED OFF "FWD WINDOW HEAT" ON CAPTAIN'S SIDE AND ARCING SOUND STOPPED. CAME BACK ON INTERMITTENTLY WHEN SWITCHED ON. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 WINSDR 9JLA201610209285Wire · damagedDURING THE INITIAL DESCENT FOR LANDING, THE CREW REPORTED THAT THE STAB/WING HEAT CIRCUIT BREAKER TRIPPED. FOLLOWING THE FLIGHT AIRCRAFT MAINTENANCE CREW TROUBLESHOT AND FOUND WIRE PAR204SA WAS CHAFING EXTERNALLY ON THE P40 RELAY BOX. THE WIRE WAS REPAIRED WSDR Q5QA2016FA0000355Wire · meltedDURING A MFG MINI PROGRESSIVE INSPECTION, THE TECH NOTED THAT THE PILOTS WINDSHIELD WOULD NOT WORK ON THE LOW OR HIGH SETTING. THE HEADLINER WAS REMOVED AND HE DISCOVERED THAT THE POWER AND GROUND WIRES HAD MELTED THEMSELVES TOGETHER AND THE GROUND WIRE WAS BSDR QXEA2016061900403Wire Harness · faultyPROP DE-ICE CAUTION ILLUMINATED ENROUTE, NUMEROUS TIMES, INTERMITTENT. RETURNED TO FIELD, LANDING UNEVENTFUL. REPLACED ON NR 2 ENGINE, THE DE-ICE WIRE HARNESS FOR THE NR 2 AND THE NR 4 BLADES IAW AMM 61-10-06-000/400-805. RETURNED TO SERVICE.SDR HNAA2016060700167Wire · burnedWIRE W102-0268-16 IS BURNED BETWEEN PINS C2 RELAY K0058 AND C1 RELAY K1237 ON NR 3 PITOT. STATIC HEATING SYS. REPLACED WIRE W102-0268-16 BETWEEN PINS C2 RELAY K0058 AND C1 RELAY K1237 IAW WM 30-31-50 AND SWPM 20-21-00. USED PINS, PN M39029/92-536 IAW AD2007-SDR QXEA2016052300345Wire Harness · failedPROP DE-ICE ACTION ILLUMINATED WHENEVER NR 2 PROP WAS HEATING. CAUTION CAME ON ABOUT 1 SECOND AFTER GREEN LIGHT ILLUMINATED AND CAUTION LIGHT GOES OUT ABOUT 1 SECOND BEFORE GREEN LIGHT GOES OUT. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. FOUND C-PHASE OPENSDR QXEA2016050900297Wire Harness · failedPROP DEICE CAUTION LIGHT. SEEMED RELATED TO NR 1 ENGINE ASSOCIATED NR 1 AC GEN CAUTION LIGHT FLICKERING WHILE PROP CAUTION LIGHT ILLUMINATED. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. INTEROGATED CDS, FOUND NR 1 PROP PHASE A OPEN. FOUND NR 4 BLADE DEICESDR HNAA2016050600132Lead · damagedNR1 PROP, A PHASE INOPERATIVE. VERY SMALL LOAD INCREASE BUT WITH NO LIGHT INDICATION. ACFT ALSO ISSUES WITH DEICE BOOTS WERE INTERMITTENT. R & R LEAD FOR NR 3 PROP BLADE. GROUND RAN. ACFT OPS CHECK GOOD.SDR QXEA2016042000272Lead · damagedAT 23,000 FT PROP DEICE CAUTION LIGHT ILLUMINATED. COMPLIED W/E& A CHECKLIST. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. R & R DE-ICE LEAD ON NR 1 PROP, NR 3 BLADE IAW AMM TASK 61-10-06-000/400-806. OPS CHECK, FUNCTIONAL CHECK, GOOD. RETURNED TO SERVICE,SDR AALA201604099005Wire Harness · damagedAIRCRAFT WAS NOT GNDED. WINDOW HEAT ELEC CORD TO CAPTAINS SLIDING WINDOW IS FRAYED & SPARKS WHEN MOVED, UNDER WINDOW ECAM ANTI-ICE LT WINDOW INOPERATIVE. MX REPLACED THE LT SLIDING WINDOW ANTIC-ICE WIRE HARNESS IAW AWM 30-42-03 & 30-42-00-710-001.SDR ASAA2016040816310Circuit Breaker · trippedRIGHT SIDE WINDOW OVERHEAT LIGHT ILLUMINATES WHEN SWITCH IS PLACED ON. WINDOW COOL TO THE TOUCH. ACFT GROUNDED. FOUND WINDOW HEAT POWER RIGHT SIDE C/B OPEN. ACCOMPLISHED C/B RESET AMM 20-60-01, NO DEFECTS FOUND. ACCOMPLISHED GROUND VERIFICATION OF RT SIDE SDR AXSA2016040700001Connector · dirtyWHILE ENROUTE, APPROXIMATELY 15 MINUTES AFTER T/O THE ENGINE AIR INLET DEICE SYS ON ACFT 118WA FAILED. PILOT DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE.SDR HNAA2016030900073Lead · chafedEMERGENCY LIGHTS FLICKERING WITH PROP HEAT SELECTED ON. FOUND CHAFED PROP LEAD AT LEFT, PROP NR 2 BLADE. R & R PROP LEAD. OPS CHECK OK AT THIS TIME.SDR RAIA201602290002Feeder Cable · odorBURNING ODOR NOTICED IN FLIGHT DECK DURING FLIGHT, NO VISIBLE SMOKE ONLY ODOR. R & R F/O'S WINDSHIELD HEAT POSITIVE CABLE IAW AMM 20-00-03 AND PERFORMED OPS CHECK OF F/O'S WINDSHIELD HEAT IAW AMM 30-42-00. OPS NORMAL AT THIS TIME.SDR CA160215007Wire · shorted(CAN) THE PROP DEICE SYSTEM BECAME UNSERVICEABLE IN FLIGHT. THE DEICE WIRE HARNESS WAS FOUND SHORTED AND REPLACED, AND THE BRUSH BLOCK WAS REPLACED AS A PRECAUTION. SATISFACTORY CHECKS WERE THEN CARRIED OUT.SDR VNAA2016020400008Wire Harness · failedCREW REPORTED LT AND RT WING ANTI-ICE CAUTION MESSAGES IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT OTBD TELESCOPIC DUCT WIRING HARNESS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.SDR QXEA2016012600062Lead · damagedAT 12,000 FT MSL AND -1C OAT, SELECTED PROP DEICE ON IN IMC CONDITIONS ABOUT 3 MINUTES LATER, PROP DEICE CAUTION ILLUMINATED. RAN THE E/A CHECKLIST AND CAUTION EXTINGUISHED, BUT REILLUMINATED UPON SECOND CYCLE OF PROPS. THEN WENT OUT ON IT'S OWN AND DID NOT SDR CA160127007Wire · worn(CAN) PROP DEICE CAUTION LIGHT OCCURRED. LEFT CYCLE WAS NOT PRODUCING HEAT ON ONE OR MORE PROP BLADES. MAINTENANCE REPLACED THE LT NR 3 BLADE, AFT WIRES FROM THE BUS BAR TO THE BACK PLATE.SDR ASAA2016011814868Wire Harness · failedLEFT SIDE WINDOW HEAT OVERHEATED. ACFT GROUNDED. REPLACED WINDOW COIL CORD REF AMM 30-41-00, OPS NORMAL.SDR ASAA2016011714816Connector · damagedDURING NR 1 ENGINE ROUTINE INSPECTION DP1103, CONNECTOR FOR THE GROUND WING TAI SOLENIOD FOUND DISCONNECTED. ACFT GROUNDED. R & R WING TAI SOLENOID VALVE WITH NEW, OPS CHECK GOOD IAW AMM 30-11-12/401. R & R MW0311 HARNESS REF AMM 73-21-06-000-802-F00 AND 7SDR QXEA2016011700029Wire Harness · damagedON CLIMBOUT PROP DEICE CAUTION ILLUMINATED INTERMITTENTLY IN CONJUNCTION WITH NR 1 PROPELLER LIGHT. TURNED PROP HEAT OFF, THEN ON IAW EMERGENCY CHECKLIST, CAUTION LIGHT RETURNED, WOULD STAY ILLUMINATED FOR 5-10 SECONDS AT A TIME. HAPPENED ABOUT 10 TIMES TOTASDR ASAA2016011714817Connector · looseNR 1 ENGINE FOUND CONNECTOR DP1103 FOR GROUND WING TAI TEMP SOLENOID VALVE DISCONNECTED AND CHAFING ON ENGINE CASE AT RT CORE, BETWEEN VSV STAGES 2 & 3. ACFT GROUNDED. CONNECTOR DP1103 FOUND SERVICEABLE REF SWPM 20-61-11. RECONNECTED & OPS CK GOOD REF AMM 30SDR P5CA2015123100225Terminal · looseEICAS MESSAGE LT FWD WINDOW. FOUND WINDOW POWER INPUT TERMINAL LUG BOLT, ONE SIZE TOO BIG, CONNECTOR FOUND LOOSE AND ARCING. REPLACED BOLT, OPS CHECK GOOD REF AMM 56-11-01 FOR TERMINAL INSTALLATION.SDR QXEA2015122700663Wire Harness · damagedPROP DE-ICE CAUTION ILLUMINATED WHEN HEATING NR 1 PROP, DIVERTED FLIGHT. LANDING UNEVENTFUL. INTERROGATED CDS AND FOUND TMCU1 FAULT CODE PHASE A AND B. INSPECTED PROP DEICE LEADS AND FOUND NR 4 BLADE AT 1 PROP DEICE LEAD DAMAGED. R & R DEICE LEAD IAW AMM 61SDR CWQA20151224001Wire · brokenDURING CRUISE AT FL430, CREW NOTICED SMOKE COMING FROM THE LOWER PORTION OF LT DIRECT VISION WINDOW. CREW LOCATED SOURCE & TURNED SIDE WINDOW HEAT OFF, THE SMOKE DISSIPATED & SMOKE WAS NO LONGER OBSERVED. CHECK LIST FOLLOWED, EMER DECLARED & UNSCHEDULED LANDSDR ASAA2015122014354Wire · disconnectedWHILE INSPECTING ELEVATOR PITOT STATIC AREA, THRU ACCESS PANEL 323GL, NOTICED WIRES PULLED OUT OF ELEVATOR PITOT HEATER LT SIDE. ACFT GROUNDED. SPLICED & CRIMPED TO PINS THROUGH STANDARD PRACTICES REF AMM TASK 30-31-00-440-801. OPS NORMAL.SDR CA151218005Wire · burned(CAN) FOUND LT WING ANTI-ICE VALVE OPEN WHEN ACFT WAS ON THE GROUND. FAULT WAS FOUND TO BE BURNED WIRING CAUSING THE VALVE TO OPEN AND THE CIRCUIT BREAKER TO OPEN ALONG WITH LT OTBD LANDING LIGHT CIRCUIT BREAKER TO OPEN. DAMAGED WIRING REPLACED AND ALL SYSTEMSDR UIEA2015121600731Bonding Wire · frayedRIGHT WING THERMAL WING ANTI-ICE VLV AT TOP OF PYLON, HAS FRAYED BONDING WIRE. REPLACED RT WING THERMAL WING ANTI-ICE VLV BONDING WIRE IAW SWPM 20-20-10.SDR P5CA2015121400207Receptacle · looseFWD L1 WINDOW INOP, HEAT, PERFORMED FIM TEST 30-41, FTR 803, AMBER CONTROL LIGHT CAME ON. IAW TABLE 102, MEASURED RESIST FROM J4 & J5-10.2 OHM. REMOVED CONTROLLER. NOTED REAR RECEPTACLE LOOSE. SECURED; REINSTALLED IAW AMM 30-41-01, TESTED.SDR HNAA2015120700359Terminal · looseCAPTAINS FORWARD WINDSCREEN HAS SMOKE AT DEICE CONTACTORS. INSPECTED CAPTAIN'S WINDSCREEN HEAT WIRES AT TERMINAL B. FOUND TERMINALS TO BE LOOSE WITH NO ARC DAMAGE. RE-TIGHTENED TERMINALS L1 AND L2. GROUND RAN ACFT WITH CREW. LOADS NORMAL. SYSTEM OPS CHECKESDR ASAA2015112313938Connector · looseON DESCENT, LT SIDE OVERHEAT LIGHT ILLUMINATED. RAN QRH, LIGHT RE-ILLUMINATED. ACFT GROUNDED. PERFORMED FIM TASK 30-41, TASK 801. BITE TEST OK. POWERED DOWN ACFT FOR 5 MINUTES. POWERED ACFT BACK UP. PERFORMED BITE TEST, RESET REF FIM 30-41, TASK 801. SDR CA151123002Lead · broken(CAN) THE PILOT REPORTED LOW CURRENT TO THE LT PROPELLER ELECTRIC DE-ICER SYS. TROUBLESHOOTING FOUND THE BLADE 1 DE-ICER BOOT. LEAD WAS BROKEN. THIS ALSO CAUSED DAMAGE TO THE SPINNER, PN D-5549-P THAT REQUIRED ITS REPLACEMENT.SDR CA151113004Connector · unsecure(CAN) NEW BRUSH BLOCK ASSEMBLIES RECEIVED INCORRECTLY ASSEMBLED. CAUSES THE ATTACHING CONNECTOR TO NOT INSTALL COMPLETELY AND WIRES FROM THE CONNECTOR TO BRUSH ASSEMBLIES TO BE CRIMPED OR DAMAGED.SDR CA151112003Wire · chafed(CAN) WIRES FROM DE-ICE BOOT TO CONNECTOR FOUND CHAFFED ON CONNECTOR MOUNTING BRACKET.SDR CA151121002Wire Harness · burned(CAN) PILOT REPORTED LT PROPELLER HEAT AMPERAGE INDICATING "LOW". UPON FURTHER EXAMINATION/TROUBLESHOOTING, MAINTENANCE DISCOVERED THE PROP HEAT WIRING HARNESS HAD NO PROTECTIVE SHEATHING INSTALLED. WITH NO PROTECTIVE SHEATHING , THE WIRE RUBBED AGAINST THE SSDR ASAA2015103113565Connector · misinstalledCAPT'S WINDOW HEAT CONNECTOR AT L2 WINDOW CLOCKED INCORRECTLY. ACFT GROUNDED. RECLOCKED CAPT'S WINDOW HEAT CONNECTOR AT L2 WINDOW. REF MM TASK 56-12-11-420-006 STEP F, 5. WINDOW HEAT CHECKED GOOD. REF MM TASK 30-41-00-710-801.SDR JIKA2015102001Connector · unsecureEN-ROUTE THE PILOT REPORTED THAT THE LT & RT AIRSPEED INDICATORS WENT TO “0” INDICATION. THE PILOT DECLARED AN EMER WITH ATC. ON DESCENT THE AIRSPEED INDICATORS STARTED INDICATING NORMALLY, THE PILOT CANCELLED THE EMER WITH ATC & LANDED WITHOUT INCIDENT. FOSDR ASAA2015101113459Feeder Cable · failedDURING TAXI, RECEIVED A MASTER CAUTION LIGHT AND A RT SIDE WINDOW OVERHEAT LIGHT. TURNED SWITCH OFF FOR 2 MINUTES, THEN BACK ON AND THE OVERHEAT LIGHT AGAIN ILLUMINATED. ACFT GROUNDED. SHOOK WINDOW CONNECTOR AND DUPLICATED DESCREPANCY. R & R RT SIDE WISDR ASAA2015092513201Connector · looseINTERMITTENT DIM FLASHING OF LT ANTI-ICE COWL VALVE OPEN LIGHT ON CLIMBOUT WITH ENGINE ANT-ICE SWITCH OFF. UPON ENCOUNTERING ICING CONDITIONS, THE SWITCH AND LIGHT OPERATED NORMALLY AND NO FURTHER FLASHING OCCURRED IN EITHER SWITCH ON OR OFF POSITION THE REST SDR ASAA2015072912632Terminal · looseLEFT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. FOLLOW QRH CHECKLIST 3.3 LIGHT RE-ILLUMINATE. SWITCH NOW IN OFF POSITION. ACFT GROUNDED. FOUND TERMINALS ON THE SENSOR AT THE WINDOW TO BE LOOSE ENOUGH TO BREAK CONNECTION. MEASURED RESISTANCE WHILE SHAKING DOWSDR ASAA2015072012519Terminal · discoloredFWD LT WINDOW OVERHEAT LIGHT ILLUMINATED. ACFT GROUNDED. FOUND WINDOW HEAT C/B POPPED P6-11, RESET C/B . C/B STAYED SET REF AMM 20-60-01, WDM 30-41-11, WINDOW OPS CHECK GOOD REF AMM 30-41-00, GROUND VERIFICATION OF WINDOW WAS SUCCESSFUL. INSPECTED AND FOUNDSDR ASAA2015071512476Wire Harness · failedFLIGHT DECK RT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED IN FLIGHT. ACCOMPLISHED QRH LIGHT STAYED OFF UNTILL TAXI IN. DURING TAXI IN OVERHEAT LIGHT ILLUMINATED AGAIN. ACFT GROUNDED. FOUND WIRE HARNESS BAD, IF MOVING HARNESS NEAR CONNECTOR PLUG AT WINDOW COU
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