Piper PA-60-602P
Service difficulty reports · 18
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 = 'PA60602P' 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 aircraft_model_key = 'PA60602P' 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 2020FA0000028Actuator · failedNOSE GEAR FAILED TO EXTEND AND LOCK. NOSE GEAR FAILED DUE TO A DEFECTIVE NOSE GEAR ACTUATOR (PART NUMBER 450590-001). UPON DISASSEMBLY OF THE ACTIVATOR, IT WAS FOUND THAT THE LOCK WASHER HOLDING THE PISTON TO THE SHAFT HAD DETACHED.SDR 2016FA0000005Window · fracturedWHILE ENROUTE, AT FLIGHT LEVEL 250, THE RT FWD OR COPILOT SIDE WINDOW FRACTURED COMPLETELY AND SUBSEQUENTLY CAUSED A RAPID DECOMPRESSION OF THE CABIN. THE AIRCRAFT HAS A TT OF 6460.5 AS DID THE FAILED WINDOW. THE AIRCRAFT WAS MODIFIED WITH THE OPTION 262, 5.SDR 2008FA0000043Pushrod · corrodedTHE AREA IN WHICH THE CORRODED SECTION OF THE PUSHROD ASSY IS LOCATED IS PRONE TO EXHAUST CONTAMINATION SINCE IT IS DIRECTLY BEHIND THE ENGINE EXHAUST PIPE OUTLETS. AREA NEEDS TO BE KEPT CLEAN OF EXHAUST RESIDUE AND CORROSION PREVENTATIVE APPLIED. OLDER TUBESDR 2006FA0001125Control Unit · malfunctionedAC WAS ACQUIRED IN AN OVERHAULED CONDITION FROM AUTO PILOTS CENTRAL. THIS UNIT WAS AN EXCHANGE UNIT WITH AN OVERHAUL DATE OF APPROX, JUNE 2004. THE KI-256 WAS INSTALLED AND MARRIED TO THE EXISTING FACTORY INSTALLED AUTOPILOT SYS IAW INSTALLATION/ SYS MM. ACSDR 2005FA0001296Valve Guide · burnedDURING ANNUAL INSPECTION, IT WAS DISCOVERED DURING A DIFFERENTIAL COMPRESSION CHECK THAT THE NR 1 CYLINDER ON THIS ENGINE HAD ALMOST NO COMPRESSION. THE CYLINDER WAS REMOVED AND SENT AND WAS DISCOVERED THAT THE EXHAUST VALVE GUIDE WAS BAD. THE GUIDE WAS REPLACSDR 2005FA0001295Valve Guide · burnedDURING ANNUAL INSPECTION, IT WAS DISCOVERED DURING A DIFFERENTIAL COMPRESSION CHECK THAT NR 1CYLINDER ON THIS ENGINE HAD ALMOST NO COMPRESSION. THE CYLINDER WAS REMOVED AND SENT, IT WAS DISCOVERED THAT THE EXHAUST VALVE GUIDE WAS BAD. THE GUIDE WAS REPLACED ALSDR 021081FControl Rod · corrodedRT AILERON PUSH PULL TUBE CORRODED SEVERELY. HOLE WORE THROUGH. LOCATED BEHIND ENGINE. RECOMMEND SPECIAL ATTENTION BE PAID TO THIS AREA DURING INSPECTIONS.SDR CA030214003Bushing · cracked(CAN) DURING INSPECTION OF AN ENGINE IN FOR CRANKCASE REPAIR AND AD 2002-20-51, 4 OUT OF 6 CONNECTING ROD BUSHINGS WERE FOUND CRACKED OR BROKEN. SOME BUSHINGS HAD ROTATED IN THE CONNECTING ROD, PROBABLY AFTER CRACKING.NO HISTORY OF OVERBOOST, OVERSPEED, OR DETSDR 021081Crankcase · crackedON 28 DEC 2002, AEROSTAR N6902T LANDED AT OAJ WITH NR 2 (RT) ENGINE SHUTDOWN AND PROPELLERS FEATHERED. THE PILOT STATED THAT DURING FLIGHT, HE NOTICED A DROP IN OIL PRESSURE AND SHUTDOWN THE ENGINE. PRIOR TO SHUTDOWN, THE PILOT STATED THAT ALL OTHER INDICATISDR AU010368Cylinder · damaged(AUS) RT ENGINE CYLINDERS AND PISTONS DAMAGED BY DETONATION.SDR 20010402CW001Magneto · brokenRT ENGINE, LT MAGNETO POINT CAM FOLLOWER ARM BROKE AFTER 124.9 HOURS USE. MAGNETO OVERHAULED. INSTALLED 6-2-99 AT 2180.1 HOURS. FAILED AND REMOVED AT 2305.0 HOURS.SDR 20010402CW002Manifold · malfunctionedON LT ENGINE START, RED INDICATOR BUTTON RETRACTED, GAGE DROPPED TO ZERO. PNEUMATIC PUMP SUPPLIED PRESSURE BUT ON PRESSURE WAS GETTING TO GYRO FLIGHT INSTRUMENTS, DOOR SEALS, GYRO PRESSURE REGULATOR OR PRESSURE GAGE. RIGHT ENGINE SHOWED NORMAL INDICATOR ANDSDR 20010402CW004Buckle · defectiveON BACK SIDE OF ALL SEAT BELT BUCKLES, LATCH PART, CRACKS AT EACH CORNER OF BELT ATTACH SLOT. PROBABLE CAUSE- MANUFACTURING- JOGGLE TOO SEVERE FOR ALUMINUM BECAUSE CRACKS APPEAR AT EACH JOGGLE.SDR AU000227Pipe · corroded(AUS) LEFT WING FUEL PIPE CORRODED.SDR 98ZZZX636Bellcrank · crackedPILOT NOTICED THE GEAR REQUIRED CYCLING TWICE BEFORE THE UP AND LOCKED LIGHT WOULD ILLUMINATE. INSPECTION AFTER LANDING FOUND BELCRANK THAT ATTACHES TO INBOARD DOOR LOWER PUSH/PULL TUBE WAS CRACKED ALLOWING DOOR TO FALL OPEN.SDR 97ZZZX3789Washer · wornDURING C/W SB 600-131, SUBSTANTIATED BOTH SCAVANGE OIL PUMPS WERE DUE IMMINENT FAILURE. REPLACED PARTS REQUIRED.SDR 95ZZZX1799Cylinder · base nut failedON TAKEOFF, RT ENGINE FIRE LIGHT, LOSS OF POWER. PILOT SHUT DOWN, RETURNED TO AIRPORT. FOUND NR 4 CYLINDER HELD ON BY ONE BASE NUT. EXAMINED CYLINDER/PISTON, FOUND NO DISCREPANCIES. SUSPECT NUTS OVER/UNDERTORQUED.SDR 95ZZZX1174Valve Fitting · crackedEMERGENCY EXIT WINDOW AND CABIN DOOR SEAL LEAKAGE CAUSING CYCLING OF SEAL PRESSURE SWITCH. PILOT WAS SEEING CONSTANT GYRO PRESSURE FLUCTUATIONS ON COCKPIT INSTRUMENT PRESSURE GAUGE AND PREMATURE PRESSURE PUMP FAILURE. CAUSE WAS FOUND TO BE A CRACKED BULKHEAD
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