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.

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.Jan 9, 2020 · N62DG · Piper PA60602P · Landing Gear ActuatorSDR 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.Nov 26, 2015 · N700LD · Piper PA60602P · Flight Compartment WindowsSDR 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 TUBEJan 11, 2008 · N700LG · Piper PA60602P · Reciprocating Engine Power SectionSDR 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. ACNov 1, 2006 · N64715 · Piper PA60602P · Air Conditioning SystemSDR 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 REPLACSep 9, 2005 · N700WG · Piper PA60602P · Reciprocating Engine Cylinder SectionSDR 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 ALSep 9, 2005 · Piper PA60602P · Reciprocating Engine Cylinder SectionSDR 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.Mar 25, 2003 · N6902 · Piper PA60602P · Aileron Control SystemSDR 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 DETFeb 7, 2003 · Piper PA60602P · Reciprocating Engine Power SectionSDR 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 INDICATIJan 9, 2003 · N6902T · Piper PA60602P · Reciprocating Engine Power SectionSDR AU010368Cylinder · damaged(AUS) RT ENGINE CYLINDERS AND PISTONS DAMAGED BY DETONATION.Mar 30, 2001 · Piper PA60602P · Reciprocating Engine Cylinder SectionSDR 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.Feb 5, 2001 · N858CH · Piper PA60602P · Magneto/DistributorSDR 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 ANDDec 14, 2000 · N858CH · Piper PA60602P · Pneumatic Distribution SystemSDR 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.Jun 9, 2000 · N858CH · Piper PA60602P · Flight Compartment EquipmentSDR AU000227Pipe · corroded(AUS) LEFT WING FUEL PIPE CORRODED.Jan 1, 2000 · Piper PA60602P · Aircraft Fuel Distribution SystemSDR 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.Jan 29, 1998 · N6899L · Piper PA60602P · Landing Gear Door Retract SectionSDR 97ZZZX3789Washer · wornDURING C/W SB 600-131, SUBSTANTIATED BOTH SCAVANGE OIL PUMPS WERE DUE IMMINENT FAILURE. REPLACED PARTS REQUIRED.May 15, 1997 · N858CH · Piper PA60602P · Reciprocating Engine Oil SystemSDR 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.Mar 25, 1995 · N6902T · Piper PA60602P · Reciprocating Engine Power SectionSDR 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 BULKHEADFeb 17, 1995 · N6899R · Piper PA60602P · Cabin Pressure Control System
Back to Piper PA-60-602P