Pratt & Whitney PW4062
Service difficulty reports · 206
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 = 'PW4062' 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 = 'PW4062' 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 HALA0600918Wire · brokenFOUND EMERGENCY TRACK LIGHTING INOP, CO-PILOTS SIDE.SEATS 1-16 J/H. FOUND BROKEN WIRE FOR EMERGENCY TRACK LIGHTING AT SEAT 12JH, REPAIRED BROKEN WIRE. TRACK LIGHTING FOR SEATS 1-16 J/H. OPS CK NML. OK FOR SERVICE.SDR HALA0600868Connector · disconnectedEMERGENCY TRACK LIGHTS FROM SEAT ROW 2H THROUGH 16H INOP. RECONNECTED CONNECTION AT LIGHT ASSY NEXT TO SEAT 2H ALL EMERGENCY LIGHTS CK GOODSDR HALA0600867Sensor · malfunctionedETOPS SIGNIFICANT SYSTEM - FUEL TEMP DISPLAY INACCURATE. REP FUEL TEMP SENSOR IAW AMM 28-43-01-004-001-001 AND AMM 28-43-01-404-050-001 CKS GOOD.SDR 2005FA0000422Carbon Seal · failedFAILED CARBON SEAL, RESULTING IN LOSS OF OIL, IFSD AND ATB. (NE03200504012)SDR WLDA200445Panel · corrodedITEM: DURING 4-C CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 24.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NRSDR 98ZZZX3682Case · damagedDURING CLIMB FROM MIAMI, THE ENGINE (POS NR 1) EXPERIENCED TWO SURGES WITH EGT EXCEEDING 796 DEGREES CELSIUS FOR 15 SECONDS. AN IN-FLIGHT SHUT DOWN AND AIR TURN BANK EFFECTED. DISASSEMBLY INSPECTION AT PWORC REVEALS 360 DEGREE FAILURE OF THE HPT CASE WALL AP
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