JASC 7297
Service difficulty reports · 275
Reports filed under 7297 · Turbine Engine 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 = '7297' 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 = '7297' 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 HEEA080088Wire Harness · damagedENGINE YELLOW ELECTRICAL HARNESS PRODUCING MGT FLUCTUATION ON GAUGE IN COCKPIT. TO BE SENT TO VENDOR.SDR MALA020351Wire Harness · faultyDURING FLIGHT 3320, HAD A UNCOMMANDED AUTO COARSEN EVENT. EVENT OCCURRED DURING APPROACH TO CRW, AT 1,000 FT AGL. RT ENGINE AUTO COARSEN, ENGINE CONTINUED TO RUN, LANDED NORMALLY. MAINTENANCE BORESCOPED RT ENGINE, NO DEFECTS NOTED. REMOVED AND REPLACED RT SDR HEEA078875Wire Harness · brokenBREAK IN CABLE CAUSING FADEC NG1 FAULT AND NG1 CONTINUITY FAULT. BREAK IS APPROXIMATELY 3 INCHES FROM ECU CONNECTOR PLUG.SDR SWIA200210829Wire Harness · faultyLEVEL AT 27,000 FEET, AFTER COWL ANTI-ICE WAS TURNED ON AND ASSOCIATED THRUST REDUCTION WAS MADE, THE RIGHT ENGINE N1 FLUCTUATED UNCOMMANDED 89.0 TO 95 PERCENT. ALSO ON DESCENT, WITH THRUST LEVER REDUCTION, RIGHT N1 FROM 81 TO 83 PERCENT. NOTICED SOME N2 FLUSDR BMAC020003Wire · brokenRT EGT FLUCTUATED BETWEEN 450 AND 650, TORQUE DROPPED TO 40. EGT THEN FELL TO 100 C. TORQUE FELL TO 30 WITH CORRESPONDING LOSS OF POWER. SHUT DOWN RT ENGINE IN FLT. REPAIRED EGT WIRE AT ENGINE DISCONNECT. RAN ENGINE IAW J-31 MM 76-13-00 EGT AND TQ INDICATSDR 2002UALA00570Wire · shortedNUMEROUS ECAM FAULT MESSAGES FROM THE NUMBER TWO ENGINE. FOUND NUMEROUS WIRES SHORTED IN THE RIGHT ENGINE OUTBOARD PYLON AREA. AREA WAS CHECKED FOR DAMAGE AND NEW WIRES INSTALLED AS REQUIRED.SDR HEEA078513Harness · failedFADEC FAIL AND FADEC FAULT LIGHTS KEEP COMING ON. REPLACED WITH SERVICEABLE HARNESS. TO BE SENT TO BELL HELICOPTER TEXTRON FOR CREDIT.SDR HEEA078512Harness · failedFADEC FAILURE DUE TO SHORT BETWEEN PINS U & V OF HMU CONNECTOR. REPLACED WITH SERVICEABLE HARNESS.SDR CA020315012Connector · contaminated(CAN) IN CRUISE FROM MANCHESTER NR 2 ENGINE PARAMETERS FLUCTUATED & TGT PEGGED VERY HIGH, THE THROTTLE RETARDED, SAME FLUX, ENGINE PUT ON N1 MODE, PARAMETERS STABILIZED EXCEPT FOR TGT. THROTTLE ADVANCED & ALL PARAMETERS STARTED TO FLUCTUATE AGAIN&TGT FLUCTUATSDR AUS20020206Wire Harness · worn(AUS) ENGINE BAY WIRING LOOMS WORN THROUGH IN NUMEROUS PLACES.SDR SWIA200210600Wire Harness · malfunctionedLEFT EEC FAILED ON TAKEOFF. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT ENGINE UPPER WIRE HARNESS IAW POWER PLANT BUILDUP MANUAL 71-00-00. OPS CHECKED IAW MM 71-00-00. ALL PARAMETERS GOOD. P/N ON 31159-11-01, S/N OFF AA9663.SDR MEX2002015Wire Harness · damagedFLT 239 - GDL-MEX - CREW REPORTED THAT DURING THE ENGINE STARTING, THE ENGINE 1 WAS NOT STABILIZED, THE RPM'S REMAINED AT 42 PERCENT AND MAINTENANCE AREA REPORTED THE PRESENCE OF FLAME IN SUCH ENGINE. AT CHECKING IT WAS FOUND A DAMAGE IN THE WIRE BUNDLE NEAR SDR SWIA200210599Wire Harness · malfunctionedCLIMBING OUT OF GJT THROUGH 16,000 EXPERIENCED A TORQUE DROP FLUCTUATION ON LEFT ENGINE TO 30 PERCENT. EXPERIENCED CONTINUED TORQUE FLUCTUATIONS IN CLIMB THROUGH 19,000. RESET LEFT ENGINE EEC WITH NO CHANGE. RETURNED FOR PRECAUTIONARY LANDING WITH CONTINUEDSDR CA011207007Wire · chafed(CAN) SHIELDED WIRES FOUND CHAFED TO CENTER CONDUCTORS. THESE WIRES ARE LOCATED ON TOP PORTION E.E.C. ENGINE DISCONNECT. 4 OF THE WIRES HAVE ARCED & CAUSED LOSS OF ENGINE IDG & THRUST REVERSER OPERATION.SDR HEEA076271Engine · malfunctionedENGINE HAS HIGH T-5 HARNESS OHMS OUT LESS THAN 100 OHMS.SDR VE32001F00000Module · failedMO2 AND MO3 WERE REPLACED ON ENG. GRND RUNS WERE PERFORMED. VIBR TESTS AT FRONT AND RR PNTS WERE NML. OIL PRESS TESTS WERE NML. OIL FLOW AT RR BRG WAS MEAS AT 180 ML. NO FUEL OR OIL LKS NOTED ON ANY OF GRND RUNS. AT APPROX. 1000 FT AGL, AND ENG CHIP LISDR HEEA076328Harness · failedSHORT BETWEEN PIN D & C OF TORQUE TRANSMITTER CONNECTOR. TO BE SENT TO VENDOR FOR CREDIT.SDR HEEA076327Harness · failedFADEC DEGRADE LIGHT. TO BE SENT TO VENDOR FOR CREDIT.SDR HEEA076326Harness · failedCONSTANT FADEC DEGRADE LIGHT. TO BE SENT TO VENDOR FOR CREDIT.SDR HEEA076325Harness · failedFADEC DEGRADE LIGHT ILLUMINATED ON SHUTDOWN.SDR 2001UALA02079Harness · defectiveAUTO THROTTLE DISCONNECTED ON DESCENT WITH LEFT ENGINE CONTROL ROLL EICAS MSG. RE-ENGAGED AUTO THROTTLE AND DISCONNECTED AGAIN. INTERMITTENT HARNESS PROBLEM BETWEEN THE PERMANENT MAGNET ALTERNATOR (PMA) AND THE ELECTRONIC ENGINE CONTROL (EEC) CAUSED THE EEC ASDR DL76L010542Wire · brokenRIGHT ENGINE HPSOV ON TAKEOFF ROLL, RETURN TO CVG. . REPAIRED BROKEN WIRE ON D4208P RAN ENGINE LEAK AND OPS CHECKS GOOD.SDR CA980713030Wire · chafed(CAN) SHORTLY AFTER TAKEOFF, THE LEFT CHIP DETECTOR ANNUNCIATOR LIGHT CAME ON. AIRCRAFT RETURNED TO BASE. CHIP DETECTOR WIRE FOUND RUBBING AGAINST THE ENGINE NEAR THE RIGHT HAND MOUNT.SDR CA980325008Wire · cracked(CAN) FOUND AT ENGINE SHOP VISIT. OUTER COMBUSTION COWL WIRE HAS WORN THROUGH A PORTION OF THE COWL AND TRANSLATED FORWARD CONTACTING FUEL NOZZLE STEM. SIGNIFICANT DAMAGE OF NOZZLES IN POSITIONS 1, 2, 3 AND4. SB 72-240 ISSUED AUG 9TH 1991 AND REV.1 ISSUED DEC SDR C2XA97IA354Harness · failedIAH - AIRCRAFT HAD THE NR 2 ENGINE AUTO SHUT-DOWN. MAINTENANCE REMOVED AND REPLACED THE RIGHT A-SYSTEM ENGINE HARNESS. THE B-SYSTEM HARNESS AS WELL AS THE ENGINE TRIM HARNESSES WERE CHANGED AS A PRECAUTIONARY MEASURE. THE AIRCRAFT OPERATIONALLY CHECKED GOOD
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