Alliedsign ALF502R-3A
Service difficulty reports · 38
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 = 'ALF502R3A' 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 = 'ALF502R3A' 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 AUS20031010Windshield · cracked(AUS) RT WINDSCREEN (A) PANEL CRACKED IN OUTER PLY.SDR AUS20030756Computer · faulty(AUS) ANTI-SKID FAULT LIGHT ILLUMINATED DURING TAKEOFF ROLL. THE PROBLEM WAS FIXED BY RERACKING THE ANTI-SKID COMPUTER.SDR AUS20030374Circuit Breaker · failed(AUS) RT OUTER FUEL BOOST PUMP CIRCUIT BREAKER OVERHEATED AND BURNED. HEAT FROM THE BURNED CB DAMAGED THE ADJACENT BRAKE FAN CIRCUIT AND CAUSED FUMES IN THE FLIGHT DECK AND CABIN.SDR AUS20021410Skin · cracked(AUS) FUSELAGE SKIN CRACKED IN AREA BETWEEN STRINGERS NR 12 AND 13 LOCATED IMMEDIATELY AFT OF FRAME 29, BENEATH THE WING ROOT DOUBLER ON THE LT SIDE. FOUND DURING INSPECTION IAW AD/BAE146/70.SDR AUS20021183Manifold · faulty(AUS) ENGINE RT FUEL MANIFOLD LEAKING. NDT INVESTIGATION FOUND A WELD DEFECT AND CORROSION PITTING. DURING TROUBLESHOOTING, ONE OF THE BOLTS SECURING THE AFT COMBUSTOR FUEL DRAIN BROKE OFF REQUIRING THE ENGINE TO BE CHANGED.SDR AUS20020723Indicator · failed(AUS) NR 2 ATTITUDE DIRECTOR INDICATOR TOPPLED IN FLIGHT.SDR AUS20020724Bolt · loose(AUS) RT AIRBRAKE ACTUATOR ATTACHMENT BOLT MIGRATED UPWARDS AND DAMAGED THE RT REAR FUSELAGE AT FRAME 50. INVESTIGATION FOUND THE NUT AND SPLIT PIN MISSING WITH THE WASHER FOUND IN THE AIRBRAKE BAY.SUSPECT SPLIT PIN NOT INSTALLED. PERSONNEL/MAINTENANCE ERROR.SDR AUS20020685Cover · damaged(AUS) REAR (2L) DOOR LOWER HINGE COVER IMPACTED AND BUCKLED CAUSING COVER TO JAM ON THE DOOR WHEN CLOSED. PERSONNEL/MAINTENANCE ERROR.SDR AUS20020677Odor · detected(AUS) NR 1 ENGINE FUMES ENTERING CABIN. LIMITED INFORMATION PROVIDED.SDR AUS20020494Engine · failed(AUS) NR 1 ENGINE FAILED.SDR AUS20020492Wire · unapproved part(AUS) APU FIRE BOTTLE SQUIB WIRE BETWEEN PIN 2 AND EARTH POINT WIRE WAS THE INCORRECT TYPE FOR THE APPLICATION. THE WIRE FITTED WAS A SINGLE CORE SHIELDED WIRE WITH 150 DEGREE BLUE AMP TERMINALS. THE CORRECT WIRE IS 16 GAUGE SINGLE CORE 260 DEGREE WIRE. A SIMISDR AUS20020400Ecu · failed(AUS) FLAPS EXTENDED NORMALLY WITH THE FAULT LIGHT ILLUMINATED. INVESTIGATION FOUND THE FLAP ELECTRONIC CONTROL UNIT FAULTY.SDR AUS20020314Generator · contaminated(AUS) NR 1 INTEGRATED DRIVE GENERATOR CONTAMINATED. OPEN CIRCUIT ON FIELD WINDINGS.SDR AUS20020296Isolation Valve · leaking(AUS) NR 2 HYDRAULIC SYSTEM ISOLATION VALVE LEAKING INTERNALLY.SDR AUS20020280Valve · faulty(AUS) NO3 ENGINE OIL COOLER FUEL SYSTEM VERNATHERM VALVE SUSPECTFAULTY.SDR AUS20020045Computer · faulty(AUS) FLAP SYSTEM INOPERATIVE. NO CAUSE COULD BE FOUND AND INVESTIGATION IS CONTINUING. FLAP COMPUTER PNO 676801007 CHANGED.SDR AUS20011029Indicator · failed(AUS) FIRST OFFICERS ATTITUDE INDICATOR FAILED.SDR AUS20010961Pin · misinstalled(AUS) ENGINE FAN DISC RETAINING NUT LOCK CUP WASHER LOCKING PINS FLUSH WITH SHAFT MAKING LOCKING MECHANISM NON FUNCTIONAL.SDR AUS20010970Pin · misinstalled(AUS) ENGINE FAN DISC RETAINING NUT LOCK CUP WASHER LOCKING PINS FLUSHWITH SHAFT MAKING LOCKING MECHANISM NON FUNCTIONAL. THE FAN HAD BEEN REMOVED TO SERVICE ANOTHER ENGINE.SDR AUS20010835Fastener · corroded(AUS) DURING INSPECTION FOR LOCATION OF CENTRE FUEL TANK LEAK THE FOLLOWING DEFECTS WERE FOUND: 1. FRAME 29 LT HAND UPPER SIDE (AFT WING ATTACHMENTS) FASTENER IN POSITION NR 11 FOUND WITH SHEARED HEAD 2. FRAME 29 RIGHT HAND UPPER SIDE (AFT WING ATTACHMENT) FASSDR AUS20010740Circuit Breaker · faulty(AUS) LT A' SCREEN HEAT CIRCUIT BREAKER FAULTY. INVESTIGATION FOUND THE CIRCUIT BREAKER BURNED OUT ON A' PHASE.SDR AUS20010622Skin · cracked(AUS) FUSELAGE SKIN CRACKED IN AREA LOCATED IMMEDIATELY AFT OF FRAME 29 BENEATH THE WING ROOT DOUBLER. FOUND DURING INSPECTION IAWISB53-144 AND AD/BAE146/70.SDR AUS20010535Spar · corroded(AUS) LT AND RT WING FORWARD AND AFT SPAR LOWER FLANGES CORRODED IN AREA BETWEEN RIB 13 AND RIB 18.SDR AU010321Pipe · loose(AUS) NO3 ENGINE P3 SENSE LINE TO FCU LOOSE. THE AIRCRAFT HAD A NO3 ENGINE AND FCU CHANGED THE PREVIOUS DAY. PERSONNEL/MAINTENANCEERROR.SDR AU010292Pipe · fractured(AUS) ENGINE FUEL PIPE FRACTURED. FUEL LEAKING.SDR AU010258Spar · cracked(AUS) LT AND RT WING FORWARD AND AFT LOWER SPAR CAPS CRACKED IN AREABETWEEN RIBS NR 13 AND NR 18. CORROSION ALSO FOUND ON LOWER SKINS AT RIB BAYS NR 13 TO NR 18.SDR AU000666Engine · failed(AUS) NR 2 ENGINE TGT EXCEEDED 900 DEGREES AND FLAMES CAME FROM THEENGINE. THE ENGINE WAS REMOVED AND SENT FOR INVESTIGATION AND REPAIR.SDR AU000764Indicator · faulty(AUS) ARTIFICIAL HORIZON FAULTY. A TOTAL OF THREE INDICATORS HAVE FAILED IN A FEW WEEKS.SDR AU000494Indicator · fluctuates(AUS) NR 1 ENGINE TGT SYSTEM TERMINAL LOOSE AT FORWARD PYLON BREAK.SDR AU000448Indicator · faulty(AUS) CAPTAINS AIRSPEED INDICATOR (ASI) FAULTY.SDR AU000309Damper · fractured(AUS) RH FORWARD DOOR DAMPER CAN FRACTURED AT FORWARD SECTION. DAMAGE CAUSED TO FUSELAGE FRAME 14. DAMPER CAN IS A PRE-MOD 007714ATYPE.SDR AU000219Pipe · failed(AUS) ENGINE FUEL PIPE FAILED. FUEL LEAK.SDR AU000310Harness · worn(AUS) NR 2 ENGINE TGT HARNESS CHAFING AT PYLON TERMINAL BLOCK B2.SDR AU990792Engine · failed(AUS) ENGINE FAN DECOUPLED FROM LP TURBINE. FULL FLOW CHIP DETECTOR CONTAMINATED AND OIL COLORED BLACK.SDR AU990445Indicator · faulty(AUS) NR 1 ENGINE VIBRATION INDICATOR FAULTY.SDR AU990442Transducer · malfunctioned(AUS) NR 3 ENGINE OIL PRESSURE TRANSDUCER FAULTY.SDR AU960175Gear · separated(AUS) ENGINE ACCESSORY GEARBOX INPUT BEVEL GEAR SEPARATED FROM MOUNTINGFLANGE - BOLTS WERE STILL ATTACHED TO THE GEAR AND BEARING HOUSING - FOUND WHEN ENGINE STRIPPED FOLLOWING OIL PRESSURE LOSS - SUSPECT CAUSED BY INSUFFICIENT BACKLASH BETWEEN THE SPIRAL INPUSDR AU960055Gear · separated(AUS) NO3 ENGINE ACCESSORY GEARBOX INPUT BEVEL GEAR SEPARATED FROM THE MOUNTING FLANGE IN THE CASE - THE SLIMSERTS AND BOLTS WERE STILL ATTACHED TO THE GEAR AND BEARING HOUSING - METAL CONTAMINATION OFENGINE OIL SYSTEM
Back to Alliedsign ALF502R-3A