Piper PA-28RT-201

Service difficulty reports · 66

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 = 'PA28RT201'
  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 96ZZZX4807Cylinder · wornCOMPRESSION CHECK INDICATES ALL 4 CYLINDERS NOT SERVICEABLE DUE TO LOW COMPRESSION AT 110 HOURS TSO. TT: 4,950 HOURS.May 28, 1996 · N377LC · Piper PA28RT201 · Reciprocating Engine Cylinder SectionSDR AU960551Valve · leaking(AUS) LANDING GEAR EMERGENCY EXTENSION VALVE LEAKING DUE TO FAULTY 'O' RING SEALSMar 28, 1996 · Piper PA28RT201 · Landing Gear Retraction/Extension SystemSDR 96ZZZX2429Actuator · arm disengagedGEAR ACTUATOR ARM BECAME DISENGAGED FROM PUSH ROD ARM; THUS, DISABLING EMERGENCY EXTENSION FUNCTION OF MAIN LANDING GEAR.Mar 25, 1996 · N8162S · Piper PA28RT201 · Landing Gear Retraction/Extension SystemSDR AU960244Bolt · incorrect fit(AUS) RH MAIN LANDING GEAR TRUNNION PIN RETAINING BOLT PNO 401335 NOT FITTED OR INCORRECTLY TORQUED FOLLOWING MAINTENANCE - AFTTRUNNION RETAINER PIN PNO 67502-00 DISLODGED - DAMAGE TO WING UPPER SKIN - PERSONNEL/MAINTENANCE ERRORMar 6, 1996 · Piper PA28RT201 · Main Landing Gear Attach SectionSDR AU960165Condenser · faulty(AUS) ALTERNATOR CONDENSER FAULTY - OUTER CASING WAS HOLED DUE TO WEAR CAUSED BY BEING LOOSE IN THE CLAMP BRACKET - PERSONNEL/MAINTENANCE ERRORFeb 5, 1996 · Piper PA28RT201 · DC Generator-AlternatorSDR AU960164Spark Plug · faulty(AUS) SPARK PLUGS (6OFF) FAULTY - CENTRE ELECTRODE WAS BEYOND LIMITS FOR RECONDITIONING - NO1 CYLINDER TOP SPARK PLUG HAD TWO COPPERWASHERS FITTED - NO1 CYLINDER LOWER SPARK PLUG HAD CORE LEAKAGE -ENGINE HAD COMPLETED ONLY 38 HOURS SINCE OVERHAUL -PERSONNEL/MAFeb 5, 1996 · Piper PA28RT201 · Spark Plug/IgniterSDR AU960163Seat · incorrect mod(AUS) PILOTS SEAT HYDRAULIC ADJUSTMENT UNITS FAULTY - SEAT HAS BEEN LOCKED IN A SINGLE POSITION BY FITTING TUBE SPACERS OVER THE PISTON RODS - WITH THE SEAT LOCKED IN A HIGH POSITION THE PILOTS HEAD IS IN CLOSE PROXIMITY TO THE CABIN ROOF - UNAPPROVEDMODIFICAFeb 5, 1996 · Piper PA28RT201 · Flight Compartment EquipmentSDR AU960160Baffle · incorrect fit(AUS) ENGINE FRONT BAFFLE LOWER SIDE SEALING STRIPS INCORRECTLY FITTED - BAFFLE LOWER SIDE MATES WITH LOWER COWL - RAM AIR ENTEREDUNDERSIDE OF ENGINE PREVENTING CORRECT COOLING - PERSONNEL/MAINTENANCE ERRORFeb 5, 1996 · Piper PA28RT201 · Engine Air Baffle SectionSDR AU960158Pipe · incorrect fit(AUS) ENGINE INTAKE FUEL DRAIN LINE INCORRECTLY FITTED - LINE WAS DOUBLED UP INTO A KINK PREVENTING FUEL FROM DRAINING - FUELLEAKED INSIDE COWLING - PERSONNEL/MAINTENANCE ERRORFeb 5, 1996 · Piper PA28RT201 · Engine DrainsSDR AU960146Stud · cracked(AUS) RH MAIN LANDING GEAR SIDE BRACE STUD CRACKED IN AREA UNDER SHOULDER - FOUND DURING INSPECTION IAW AD/PA28/91Jan 31, 1996 · Piper PA28RT201 · Main Landing GearSDR 95ZZZX6807Bearing · bindsTWO PROBLEMS NOTED: SERVICE MANUAL STATES THAT - UNFAVORABLE CONDITION - BEARING ROTATES/WOBBLES. CHAPTER 32-20-05, PAGE 32-25, PARA 2D. SERVICE MANUAL STATES THAT 'BEARING MUST BE FREE TO ROTATE' CHAPTER 32-20-06, PAGE 32-30, PARA 3D. BEARING IS BASIC STEESep 20, 1995 · Piper PA28RT201 · Landing Gear Retraction/Extension SystemSDR 95ZZZX5027Fitting · corrodedTHE AFT WING SPAR ATTACHMENT FITTINGS WERE INSPECTED FOR CORROSION IAW SB NR 977. NO CORROSION WAS FOUND PER SB, HOWEVER, DURING THE REMOVAL OF CORROSION FROM THE INBOARD END OF THE RIGHT FLAP, THE SEALANT BETWEEN FUSELAGE AND THE FITTING WAS KNOCKED OFF REVEAug 23, 1995 · N2142X · Piper PA28RT201 · Wing, Attach FittingsSDR BIER950020Studs · shearedDURING TAKEOFF, PILOT NOTICED VIBRATION/PWR LOSS, AN UNEVENTFUL LANDING WAS MADE. DURING PRELIM INSP, FOUND 5 OF THE 8 CYL HOLD DN STUDS FOR THE NR 4 CYL HAD SHEARED, LEAVING CYL LOOSELY MOUNTED ON ENG. FURTHER INSP REVEALED CRACK IN CASE AROUND AREA OF REARAug 18, 1995 · N8368H · Piper PA28RT201 · Reciprocating Engine Cylinder SectionSDR 95ZZZX2043Anchor Nut · failedDURING THE ANNUAL INSPECTION, RT FWD ATTACH BOLT FOR VERTICAL FIN FOUND LOOSE. BOLT REMOVED AND FND IN SERVICEABLE SHAPE. REPLACED AND ATTEMPTED TO TORQUE TO SPECS. BOLT WOULD NOT TIGHTEN. FURTHER INSP REVEALED ANCHOR NUT SHATTERED. SUBMITTER SUGGESTS THEApr 4, 1995 · N8085Z · Piper PA28RT201 · Vertical Stabilizer, Attach FittingsSDR 95ZZZX1362Bolt · looseDURING A 100-HOUR INSPECTION THE 4 EACH AN5-11A BOLTS THAT MOUNT THE FORWARD MLG TRUNNIONS, PN 67040-14 LEFT, AND PN 67040-15 RIGHT, TO THE MAIN INBOARD WING SPAR, PN 67069-22 LEFT, AND PN 67069-03 RIGHT, WERE FOUND BACKING OUT. AN5-11A BOLTS WERE BACKED OUT Mar 2, 1995 · N2859D · Piper PA28RT201 · Main Landing Gear Attach SectionSDR 95ZZZX999Fitting · corrodedUPON REMOVAL OF WINDSHIELDS FOR REPLACMENT, THE LEFT WINDSHIELD OUTBOARD STRUCTURE FITTING WAS FOUND TO HAVE SEVERE CORROSION FROM A WINDSHIELD LEAK. THE FITTING PART IS STEEL AND RIVETED TO THE ALUMINUM STRUCTURE. SUBMITTER SUGGESTS UPON REMOVAL OF WINDSHIEJan 30, 1995 · N8109D · Piper PA28RT201 · Fuselage Miscellaneous Structure
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