Grumman G-1159

Service difficulty reports · 159

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = 'G1159'
  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.

SDR 95ZZZX1921Brush · wornBLACK STREAKS WERE NOTICED ON THE ENGINE COWLING BY MAINTENANCE PERSONNEL. FOUND THE D. C. GENERATOR TO HAVE PREMATURE BRUSH WEAR, WORN BEYOND LIMITS (NO WEAR MARK REMAINING - 100 PERCENT WORN). RECENT OVERHAUL BY REPAIR STATION. CAUSE OF BRUSH WEAR COULD NMar 16, 1995 · N900DH · Gulstm G1159 · DC Generator-AlternatorSDR 95ZZZX1485Shut-Off Valve · wrong partCREW REPORTED PASSENGER OXYGEN SYSTEM LEAKING. INSPECTED SYSTEM AND FOUND OXYGEN PRESSURE REDUCER/SHUT-OFF VALVE LEAKING. REMOVED VALVE, PN FR-142-A2, SN 91255. ORDERED SAME UNIT AND WAS INFORMED THE PART WAS REALLY A PN FR-141-A2 AND WAS MIS-LABLED AS A FRMar 8, 1995 · N711RL · Gulstm G1159 · Passenger Oxygen SystemSDR 95ZZZX1495Bulkhead · corrodedWHILE REPAIRING CORROSION FOUND DURING INSPECTION OF THE FS 580 BULKHEAD, ALL 3 SKIN DOUBLERS AT FS 580 HAD TO BE REPLACED DUE TO CORROSION DAMAGE. ALL 3 DOUBLERS WERE ORDERED FROM THE MANUFACTURER. THE OUTBOARD AND INBOARD DOUBLERS WERE RECEIVED AND DETERMIMar 3, 1995 · N187PH · Gulstm G1159 · Fuselage Main, BulkheadSDR 95ZZZX1494Doubler · mismanufacturedWHILE REPAIRING CORROSION FOUND DURING INSPECTION OF THE FS 580 BULKHEAD, ALL 3 SKIN DOUBLERS AT FS 580 HAD TO BE REPLACED DUE TO CORROSION DAMAGE. ALL 3 DOUBLERS WERE ORDERED FROM THE MANUFACTURER. THE OUTBOARD AND INBOARD DOUBLERS WERE RECEIVED AND DETERMIMar 3, 1995 · N187PH · Gulstm G1159 · Fuselage Miscellaneous StructureSDR 95ZZZX1521Strap · fracturedENGINE WOULD NOT DEVELOP TAKEOFF THRUST. BLEED VALVE STRAP FOUND FRACTURED. AN EVALUATION (CONDITION REPORT) INDICATES FAILURE DUE TO FLUTTER AND HIGH-CYCLE FATIGUE BROUGHT ABOUT BY EXCESSIVE LOADING OF ONE OR MORE BLEED VALVE SPHERICAL BEARINGS. THIS APPEAFeb 21, 1995 · N58JF · Gulstm G1159 · Compressor Bleed ControlSDR 95ZZZX1010Wheel · crackedWHEEL WAS REPORTED TO HAVE A SLOW LEAK. PERFORMED LEAK CHECK AND FOUND LEAK COMING FROM BOLT HOLE AREA ON THE OUTBOARD WHEEL HALF. DYE-PENETRANT SHOWED NO DEFECT. PERFORMED EDDY CURRENT AND U.T. INSPECTION AND BOTH METHODS SHOWED A DEFECT FROM THE BOLT-BOSSFeb 13, 1995 · Gulstm G1159 · Wheel/Ski/FloatSDR 95ZZZX1034Pre-Cooler · crackedDISCOVERED PRE-COOLER LEAKING WHILE DOING OTHER TROUBLESHOOTING DURING ENGINE RUN-UP. THESE PRE-COOLERS HAVE A HISTORY OF CRACKING WITH AGE AND USE. INSTALLED NEW PRE-COOLER.Feb 10, 1995 · N26WP · Gulstm G1159 · Pneumatic Distribution SystemSDR 95ZZZZ42Bolt · brokenDURING POST FLIGHT INSPECTION, MAINTENANCE FOUND TWO BOLTS BROKEN ON THE RT INBOARD WHEEL. THE FLIGHT CREW INDICATED THAT ALL OPERATIONS HAD BEEN NORMAL. THESE BOLTS HAD 357 LANDING SINCE NDT.Jan 15, 1995 · N220FL · Gulstm G1159 · Wheel/Ski/FloatSDR 95ZZZW114Connector · failedTEB-BDL - EN ROUTE, INTERMITTENT FLASHING OF RT ENGINE FIRE WARNING LIGHT WITH THE BELL OCCURRED. SEVERAL REOCCURANCES DURING FLIGHT FOLLOWED. PROBLEM WAS ALLEVIATED WHEN THROTTLE WAS RETARDED. AFTER LANDING AT BDL WITHOUT INCIDENT, THE ITEM WAS TROUBLESHOTJan 14, 1995 · N666JT · Gulstm G1159 · Fire Detection
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