Pratt & Whitney JT8D-17A
Service difficulty reports · 362
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 engine_model_key = 'JT8D17A' 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 engine_model_key = 'JT8D17A' 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 96ZZZM1487Fuel Pump · malfunctionedEVV - FL 777 - FLIGHT WAS CRUISING AT FL 310 WHEN THE NR 2 ENGINE CAME BACK TO 50 PERCENT POWER OR 2,000 LBS FUEL FLOW. CREW TURNED ON ENGINE HEAT WITH NO EFFECTS ON ENGINE. CREW TURNED ON FUEL HEAT, NR 2 ENGINE WENT PAST NORMAL N1 AND N2 INDICATIONS. CREW SDR USAASB96214Fuel Control · malfunctionedEVV - FL 777 - FLIGHT WAS CRUISING AT FL 310 WHEN THE NR 2 ENGINE CAME BACK TO 50 PERCENT POWER OR 2,000 LBS FUEL FLOW. CREW TURNED ON ENGINE HEAT WITH NO EFFECTS ON ENGINE. CREW TURNED ON FUEL HEAT, NR 2 ENGINE WENT PAST NORMAL N1 AND N2 INDICATIONS. CREW SDR CA961113003Fan · seized(CAN) ON FINAL APPROACH CABIN CREW REPORTED STRONG SMELL OF SMOKE IN AFT PASSENGERS CABIN. GASPER FAN CB PULLED. FAN REPLACED.SDR USAASB96187Seal · leakingBWI - FL 1930 - DURING CLIMB, THE NR 2 ENG LOW OIL PRESS LIGHT ILLUMINATED. THE OIL QTY GAUGE BEGAN DECREASING TO ZERO. CREW SHUT DOWN THE NR 2 ENG. OIL PRESS AT SHUTDOWN WAS 16 PSI. AFTER SHUTDOWN, WINDMILLING OIL PRESS WAS APPROX 15-16 PSI. ENG WAS OPERSDR 96NK197Pt2 Line · cloggedLOG PAGE 028762. FLT ORH/UCA DIVERTED ACY - NR 2 EPR GAUGE READS HIGH AT POWER SETTING ABOVE IDLE WITH ALL OTHER ENGINE PARAMETERS MATCHED. CORRECTIVE ACTION: TROUBLESHOT PER MM CHAPTER 77-11-2. FOUND MUD DEBRIS IN NOSE BULLET LINE. REMOVED DEBRIS AND DIDSDR CA960711006Switch Oil Press · defective(CAN) #2 ENGINE WAS SHUTDOWN IN FLIGHT, AIRCRAFT DIVERTED, DUE TO ENGINE OIL FILTER BYPASS LIGHT ON. OIL BYPASS PRESSURE SWITCH REPLACED. FURTHER TROUBLESHOOTING TO BE CARRIED OUT AS FILTER BYPASS LIGHT DID NOT GO OUT ON ENGINE START UP.SDR 96NK171Fuel Control · out of adjustLOG PAGE 7770. ABORTED TAKEOFF. ON TAKEOFF, LEFT ENGINE DEVELOPED ONLY 1.8 EPR AT 90 PERCENT N1, RIGHT ENGINE DEVELOPED 1.78 EPR AT 88 PERCENT N1, BOTH POWER LEVERS WERE AGAINST THE STOPS. CORRECTIVE ACTION: TRIMMED NR 1 AND NR 2 ENGINES IAW MM 71-00. REFESDR USAASB96036Engine · vibrationFLT NR 885 - GSO - ON INITIAL CLB FLIGHT ATTENDANT NOTICED A VIBRATION THROUGH THE CABIN. AT CRUISE VIBRATION CONTINUES WIHT CAPTAIN ISOLATING PROBLEM TO NR 1 ENGINE. ALL ENGINE READINGS CONTINUED TO BE NORMAL. AIRCRAFT DIVERTED TO GSO. (M)SDR SCNA95273Engine · failedDURING TAKEOFF ROLL, THE NUMBER TWO ENGINE EXPERIENCED A CONTAINED FAILURE AND ENGINE PARTS WERE REPORTED DEPARTING THE AIRCRAFT. THE ENGINE WAS REPLACED. THE FAILED ENGINE IS CURRENTLY UNDER EVALUATION AND SUN COUNTRY IS AWAITING THE RESULTS.SDR 95FDEA01540Turbine · failedABORT ON RUNWAY FOR ENGINE FAILURE ABOUT 80K, #2 ENG MAXIMUM POWER T/O. FOUND NR 2 ENG TURBINE FAILURE. REMOVED NR 2 ENG AS PER WORKCARD 70T0002, INSTALLED NR 2 ENG PER WORKCARD 70T0002. COMPLIED WITH HOOKUPS OPERATIONAL AND LEAK CHECKS PER WORKCARD 70T0002SDR MRKA9570C-1 Fan · bentON APPROACH TO MDW, AIRCRAFT SUSTAINED DAMAGE TO THE NR 1 ENGINE FAN BY A BIRD STRIKE. THE LANDING OCCURED WITHOUT FURTHER INCIDENT. INSPECTED NR 1 ENGINE PER MAINTENANCE MANUAL 72-00. FOUND TWO BLADES BENT BEYOND LIMITS PER 72-33-21, PAGE 801-808, FIGURE 8SDR 95ZZZM736Outlet Duct · crackedNR 1 ENGINE FAILED, NR 9 COMBUSTION CAN INSPECTED. INNER OUTLET DUCT AFT OF NR 9 COMBUSTION CAN CRACKED BEYOND LIMITS OF MM 72-44 PAGE 201 TO 206. REMOVED AND REPLACED NR 1 ENGINE IAW J771-00-01. LEAK AND OPS CHECKS GOOD. ENGINE LAST SHOP VISIT, 10875 HOUR
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