JASC 7240
Service difficulty reports · 509
Reports filed under 7240 · Turbine Engine Combustion Section, 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 = '7240' 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 = '7240' 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 95ZZZM21Hot Section · failedFLT 5657 - ON INBOUND FLIGHT TO ICT CREW REPORTED SMOKE IN BLEED AIR SYSTEM. REMOVED POWER SECTION AND FOUND OIL IN GAS GENERATOR, HOT SECTION. REPLACED GAS GENERATOR SECTION. (M)SDR 95ZZZX2939Comb Chamber · hole burnedDURING AN 'N' CHECK INSPECTION, A SMALL .3750 INCH HOLE WAS FOUND IN THE COMBUSTION CHAMBER CASE AT APPROXIMATELY THE 10 O'CLOCK POSITION. (THE OUTER FAN DUCT ALSO BURNED THROUGH). REFERENCE: OPER CONTROL NR AENA131C.SDR 95ZZZX3049Seal Assy · misidentifiedPART RECEIVED FROM STOCK AND WAS FOUND TO BE IMPROPERLY IDENTIFIED. PART IS A CL 5, BUT IS IDENTIFIED AS A CL 7.SDR 95ZZZX2171Combustion Liner · crackedDURING INSPECTION, FOUND 2 SPOTS BURNED THROUGH AND CRACKED AT 6:30 AND 2:00, 1 INCH FORWARD OF SKIRT LOUVERS.SDR CKSA95013Defuser Case · crackedMSLP-KMIA - NR 1 ENGINE SHUTDOWN AT 1742Z DUE TO FIRE WARNING. INSPECTED AND FOUND NO EVIDENCE OF FIRE. REMOVED AND REPLACED NR 1 ENGINE IAW DC-8 MIP-1, CHAPTER 9 DO TO DIFFUSER CASE CRACK. OPS AND LEAKS CHECK GOOD IAW AIA DC-8 MIP-1 CHAPTER 10. (W)SDR 95ZZZM222Vane Ring · failedON CLIMB-OUT AT 16,000 FEET, A LOUD BANG WAS HEARD. AFTER THE LOUD BANG, THE LEFT ENGINE TEMPERATURE STARTED TO RISE AND THE ENGINE STARTED LOOSING POWER. THE ENGINE WAS THEN SHUTDOWN AND THE AIRCRAFT RETURNED FOR AN EMERGENCY LANDING WITHOUT FURTHER INCIDENSDR BDHA9500001Plenum · crackedRAP - FLT 435 - DURING A ROUTINE RT ENGINE INSPECTION, MAINTENANCE FOUND A CRACK AROUND THE P3 AIR SUPPORT BOSS ON THE ENGINE PLENUM. ENGINE REMOVED AND PLENUM REPLACED, COMPLETED ENGINE RUNS AND ACFT RELEASED FOR SERVICE. (W)SDR ABXA9500111Drain Boss · crackedDURING COMPLIANCE OF AD 87-11-07, PRATT AND WHITNEY SB 5676, FOUND PS4 AND LOWER AFT DRAIN BOSS ON OUTER CASE OF COMBUSTION CHAMBER HAD CRACK INDICATIONS. REPLACED NR 1 ENGINE IAW ABX WORKCARD RTJ 7001.SDR ABXA9500110Drain Boss · crackedDURING COMPLIANCE OF AD 87-11-07, PRATT AND WHITNEY ASB 5676, FOUND CRACK INDICATION ON FORWARD LOWER COMBUSTION CHAMBER OUTER CASE DRAIN BOSS. REPLACED ENGINE IAW ABX WORKCARD RJT 7001.
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