Partenavia P68B
Service difficulty reports · 80
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 = 'P68B' 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 = 'P68B' 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 AU510002124Door · separatedRT SIDE EMERGENCY EXIT POPPED OUT ON TAKEOFF. INVESTIGATION COULD FIND NO FAULTS. SUSPECT CAUSED BY PREVIOUS PASSENGER INTERFERENCE WITH LOCKING LEVER.SDR AU510001994Fitting · corrodedTORQUE TUBE ATTACHMENT FITTING CORRODED. LIMITED INFORMATION PROVIDED.SDR AUS20040321Support Angle · cracked(AUS) WING SPAR STRAP SUPPORT FORWARD AND AFT ANGLES CRACKED ALONG RIVET LINE.SDR AUS20040276Injector · faulty(AUS) RT ENGINE FUEL INJECTOR FLOW ERRATIC.SDR AUS20040267Injector · contaminated(AUS) RT ENGINE FUEL INJECTORS CONTAMINATED BY SMALL FERROUS (RUST) PARTICLES.SDR AUS20040118Nozzle · blocked(AUS) NR 4 CYLINDER FUEL INJECTOR NOZZLE BLOCKED.SDR AUS20040133Spar Cap · cracked(AUS) REAR WING SPAR BOTTOM SPAR CAP CRACKED IN AREA OF LT SIDE WING ATTACHMENT. CRACK LENGTH 6MM (0.236IN). FOUND DURING EDDY CURRENT INSPECTION.SDR AUS20040067Hose · distorted(AUS) VACUUM HOSE KINKED. DISTORTION WAS LOCATED ON FRAME F AT THE TOP FRONT LT DOOR FRAME AND WAS CAUSED BY THE BEND RADIUS BEING TOO SMALL AFTER PASSING OVER THE FRAME. PERSONNEL/MAINTENANCE ERROR.SDR AUS20031334Doubler · corroded(AUS) WING SPAR DOUBLERS PN 68-1.4009-3 AND PN 68-1.4009-4 CONTAINED A SMALL AMOUNT OF CORROSION. DOUBLERS ARE LOCATED IN AREA BEHIND ENGINES AND ENGINE FIREWALLS.SDR AUS20031333Fitting · cracked(AUS) ENGINE MOUNT FITTINGS PN 68-1.2025-1 AND PN 68-1.2025-2 CRACKED AROUND RIVET HOLES.SDR AUS20031107Generator · failed(AUS) LT AND RT GENERATORS FAILED.SDR AUS20021303Spar Cap · cracked(AUS) LH WING SPAR CAP CRACKED. PREVIOUS CRACK HAD BEEN REPAIRED USINGSTAINLESS STEEL LAMINATIONS. DURING EDDY CURRENT INSPECTION IAW AD/P68/43 AMDT1 IT WAS FOUND THAT THE CRACK HAD GROWN FROM 10MM (0.39IN) TO 21MM (0.826IN) ON THE VERTICAL FACE.SDR AUS20020860Bracket · cracked(AUS) TOP RUDDER HINGE BRACKET CRACKED.SDR AUS20020778Cylinder · misinstalled(AUS) RT ENGINE NR 2 CYLINDER INLET VALVE PUSHROD BROKEN. SHROUD TUBE SEVERELY DISTORTED. METAL IN OIL FILTER. INVESTIGATION FOUND THE FOLLOWING DEFECTS: NR 1 CYLINDER HAD ONE INLET AND ONE EXHAUST ROCKER ARM INSTALLED BUT THE INLET WAS INSTALLED IN THE EXHAUSDR AUS20020350Key · unapproved part(AUS) STABILATOR KEYS (2OFF) WERE UNAPPROVED HANDMADE PARTS. UNAPPROVED PART. PERSONNEL/MAINTENANCE ERROR.SDR AUS20020349Bolt · misinstalled(AUS) STABILATOR FORWARD CONTROL ROD BOLT INSTALLED IN INCORRECT DIRECTION.SDR AUS20011281Brake · missing(AUS) AIRCRAFT NOSE SPAT AND PITOT TUBE DAMAGE WHEN AIRCRAFT RAN INTO THE SIDE OF THE HANGAR WHILE BEING TAXIED FOR REFUELLING. INVESTIGATION FOUND THAT THE PILOT WAS SITTING IN THE RH SEAT AND THAT THE BRAKES HAD BEEN REMOVED FROM THE RH SIDE POSITION. THE RESDR AUS20010960Bracket · corroded(AUS) LH WING LEADING EDGE TOP FORWARD ATTACHMENT BRACKET CORRODED.SDR AUS20010430Flange · cracked(AUS) AFT WING SPAR WEB FLANGE CRACKED ON THE LH SIDE IN THE AREA OUTBOARD OF THE ATTACHMENT FITTING. FOUND DURING INSPECTION IAW AD/P68/22, AD/P68/45 AND SB 65.SDR AU001049Spar · cracked(AUS) LEFT AND RIGHT WING REAR SPAR WEBS CRACKED AT RELIEF HOLE FOR NR 3 FLAP HINGE BRACKET. (X)SDR AU000774Pipe · worn(AUS) ENGINE OIL PRESSURE LINE LOCATED BEHIND INSTRUMENT PANEL WORN BY OPILOT ASHTRAY. OIL LEAKING. (X)SDR AU000543Rivet · misaligned(AUS) LEFT OUTBOARD ENGINE NACELLE COWL RIVET MISALIGNED TO SPAR CAP RIVETS BY APPROXIMATELY 3.175 MM (0.125 INCH). FOUND DURING INSPECTION IAW AD/P68/46. (X)SDR AU000357Link · corroded(AUS) LEFT AND RIGHT INBOARD FLAP HANGERS CORRODED IN AREA OF BONDING WIRE ATTACHMENT. FOUND DURING INSPECTION IAW AD/P68/40.SDR AU000087Rivet · misaligned(AUS) LEFT AND RIGHT WING INBOARD ENGINE COWL RIVETS MISALIGNED. THE RIVETS DID NOT IMPINGE ON THE SPAR. FOUND DURING INSPECTION IAWAD/P68/46.SDR AU000111Mount · cracked(AUS) LEFT AND RIGHT ENGINE MOUNTS CRACKED AND CORRODED.SDR AU990726Control Cable · worn(AUS) RIGHT FORWARD RUDDER CABLE EXCESSIVELY WORN IN THE AREA OF THE FORWARD PULLEY LOCATED AT FRAME NR 3.SDR AU990722Fitting · cracked(AUS) LEFT ENGINE MOUNT UPPER INBOARD ATTACHMENT FITTING CRACKED IN THE VERTICAL FLANGE.SDR AU990678Rod End · wrong part(AUS) LEFT ENGINE MIXTURE CONTROL TO FCU CONTROL ROD ROD END AND ATTACHING HARDWARE SUSPECT UNAPPROVED PARTS.SDR AU990516Bracket · corroded(AUS) RT WING FLAP BRACKET CORRODED.SDR AU990569Engine · overserviced(AUS) SMOKE IN COCKPIT. INVESTIGATION FOUND A SMALL QUANTITY OF OIL AROUND THE MUFFLER SHROUD. SUSPECT OIL HAD BEEN SPILT DURING ENGINE OIL TOP UP.SDR AU990027Angle · cracked(AUS) FORWARD WING SPAR RIGHT AFT SPAR CAP ANGLE FOUND TO BE CRACKED IN THE AREA OUTBOARD OF THE RIGHT WING ATTACHMENT. FOUND DURING INSPECTION IAW AD/P68/45 (SB/65). PART TC: 6,062.SDR AU990002Control Cable · failed(AUS) PILOT REPORTED RUDDER CABLE SLIPPAGE. INVESTIGATION FOUND THAT THE RT RUDDER (FORWARD) CABLE HAD FAILED AT THE FORWARD MOST PULLEY. THE LT CABLE WAS THEN INSPECTED AND WAS FOUND WITH BROKEN STRANDS. 2,394.SDR AU981040Angle · cracked(AUS) SPAR CAP ANGLE CRACKED BEYOND THE STOP DRILL HOLE. PART TC: 7,384.SDR AU980847Mount · cracked(AUS) RIGHT LOWER ENGINE MOUNT TUBE CRACKED.SDR AU981187Valve · worn(AUS) LEFT ENGINE FUEL SELECTOR VALVE WOULD NOT COMPLETELY OPEN. PART TC: 7,649.SDR AU980317Hose · deteriorated(AUS) PITOT/STATIC SYSTEM HOSE DETERIORATED. SILICON HOSE APPEARS TO BE BREAKING DOWN AND EXUDING AN OILY FILM WHICH IS PARTIALLY BLOCKING THE STATIC AIR DISTRIBUTOR MANIFOLD.SDR AU980318Skin · corroded(AUS) RT ENGINE LOWER NACELLE SKIN SEVERELY CORRODED INTERNALLY. SKIN IS LOCATED ABOVE THE EXHAUST GAS STREAM. PART OF THE NACELLE LATERAL BEAM WAS ALSO CORRODED.SDR AU980225Battery · leaking(AUS) ELT BATTERY ACID SPILLAGE. ACID ATE THROUGH THE BATTERY CASE AND BATTERY MOUNTING PLATE.SDR AU980182Pump · failed(AUS) ENGINE FUEL PUMP DRIVE LEVER FAILED ACROSS PIVOT PIN HOLES. LEVER SECTION WITHIN THE PUMP HAS SECONDARY CRACKING AND IS SLIGHTLY BOWED OUTWARDS. BROKEN PORTION OF LEVER FOUND IN THE ENGINE SUMP.SDR AU980653Pipe · loose(AUS) RT FUEL SELECTOR PIPE TO TANK LOOSE.SDR AU980215Fitting · loose(AUS) RT ENGINE SURGED AND FAILED. LT ENGINE SURGED AND THEN FAILED DURING TAXI FOLLOWING LANDING. INVESTIGATION FOUND THAT THE RT FUEL SELECTOR FITTING WAS LOOSE ALLOWING AIR TO ENTER THE FUEL SYSTEM CAUSING THE RT ENGINE TO STOP. NO POSITIVE CAUSE WAS IDESDR AU971570Bracket · cracked(AUS) ENGINE MOUNT TO WING ATTACHMENT BRACKETS (3OFF) WERE FOUND CRACKED:1. LH LOWER INBOARD PNO 68-1.2027,2. RH UPPER INBOARD PNO 68-1.2025-1 AND 3. RH UPPER OUTBOARD PNO 68-1.2025-3. FOUND IAW AD/P68/28A3, SECTION 3.SDR AU971623Bulkhead · cracked(AUS) FRONT BULKHEAD CRACKED THROUGH TWO BOLT HOLES. FOUND FOLLOWING REMOVAL OF THE UPPER NOSE LEG MOUNT PLATE DUE TO TOWING DAMAGE. DAMAGE CAUSED BY INCORRECT GROUND HANDLING.SDR AU971410Control Cable · frayed(AUS) RH FLAP CABLE STRANDS BROKEN. FOUND DURING INSPECTION IAW AD/P68/44 (PARTENAVIA SB 75 REV3).SDR AU971409Control Cable · frayed(AUS) RH FORWARD ELEVATOR CABLE STRANDS BROKEN. FOUND DURING INSPECTION IAW AD/P68/44 (PARTENAVIA SB 75 REV3).SDR AU971408Control Cable · frayed(AUS) RH AILERON BALANCE CABLE STRANDS BROKEN. FOUND DURING INSPECTIONIAW AD/P68/44 (PARTENAVIA SB 75 REV3).SDR AU971407Control Cable · frayed(AUS) LH AILERON BALANCE CABLE STRANDS BROKEN. FOUND DURING INSPECTIONIAW AD/P68/44 (PARTENAVIA SB 75 REV3).SDR AU971406Control Cable · frayed(AUS) RH AILERON OUTBOARD CONTROL CABLE STRANDS BROKEN. FOUND DURINGINSPECTION IAW AD/P68/44 (PARTENAVIA SB 75 REV3).SDR AU971403Control Cable · frayed(AUS) LH OUTBOARD AILERON CABLE STRANDS BROKEN. FOUND DURING INSPECTION IAW AD/P68/44 (PARTENAVIA SB 75 REV3).SDR AU970948Capacitor · burnt(AUS) MAGNETO CAPACITOR AND POINTS BURNT - FOUND DURING INSPECTION IAWAD/ELECT/46 AMDT 6
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