Continental IO-360-D

Service difficulty reports · 33

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 = 'IO360D'
  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 2017FA0000084Pump · failedMECHANICAL ENGINE DRIVEN FUEL PUMP FAILED IMMEDIATELY AFTER ENGINE WAS OVERHAULED. WE HAVE FOUND INTERNAL COMPONENTS OF THIS ITEM FAIL WITHIN A FEW HOURS OF SERVICE.Mar 2, 2017 · N10105 · Cirrus SR20 · Engine Fuel PumpSDR CA150609006Pressure Switch · faulty(CAN) DURING TAKEOFF, THE PILOT SELECTED GEAR UP BUT THE RT MAIN GEAR WOULD NOT RETRACT. THE ELECTRIC HYDRAULIC PUMP SHUTOFF, BUT DID NOT POP THE CIRCUIT BREAKER. GEAR WAS LOWERED USING EMERGENCY HAND PUMP. MAINTENANCE INSPECTION REVEALED THAT THE PRESSURE SMay 26, 2015 · Cessna 337G · Hydraulic Pressure Regulator, AuxiliarySDR CA120420004Cam · cracked(CAN) ON ENGINE SHUTDOWN PILOT NOTICES OIL LEAKING. INSPECTION REVEALED MAGNETO HAD A HOLE NEAR MOUNTING FLANGE. THE MAGNETO WAS REMOVED AND FOUND THAT 1 OF THE FLYWEIGHTS HAD CRACKED BY MOUNTING PIN AND THE FLYWEIGHT HAD EXITED THE MAGNETO THROUGH THE CASE.Apr 15, 2012 · Cessna 337G · Magneto/DistributorSDR 2008FA0000094Hub · crackedRELEVENT INDICATION (CRACKED). (K)Feb 4, 2008 · N373AZ · Cessna M337B · Propeller Hub SectionSDR 2006FA0000966Hub · crackedPROPELLER RECEIVED FOR REPAIR, RED DYE OIL LEAK. PROPELLER WAS DISASSEMBLED AND BLADE RETENSION THREADS EDDY CURRENT INSPECTED. NR2 BLADE RETENTION THREAD, 4 THREADS IN AT APPROXIMATELY 7 O`CLOCK POSITION FOUND CRACKED. HUB REMOVED FROM SERVICE. (K)Sep 18, 2006 · Cessna T41D · Propeller Hub SectionSDR 2006FA0000984Hub · crackedPROPELLER RECEIVED FOR 60 MONTH OVERHAUL. PROPELLER WAS DISASSEMBLED AND BLADE RETENTION THREADS EDDY CURRENT INSPECTED. NR1 BLADE RETENTION THREAD, 4 THREADS IN AT APPROX 7 TO 8 OCLOCK POSITION FOUND CRACKED. HUB REMOVED FROM SERVICE. (K)Sep 18, 2006 · Cessna T41D · Propeller Hub SectionSDR 2005FA0001365Yoke · brokenUPON THE FLAIR ON LANDING AT NORMAL WEIGHTS THE CONTROL YOLK BROKE AT THE OUTSIDE LT RADIUS. THIS CAUSED THE NOSE WHEEL OF THE AC TO DROP AT A GREATER SPEED THAN NORMAL AND SHIMMY WAS EXPERIENCED THE MAIN GEAR HAD JUST TOUCHED DOWN WHEN THE FAILURE OCCURRED. Sep 27, 2005 · N6950X · Cessna 172B · Control Column SectionSDR 2005FA0000365Spar · crackedWHILE REPLACING THE FLAP TRACK ASSY, A CRACK APPROXIMATELY 2 INCHES IN LENGTH AND RUNNING THROUGH THE LOWER RIVET HOLES WAS FOUND UNDER THE LT IB FLAP TRACK. PROBABLE CAUSE WAS A FLAP OVERSPEED DURING FLIGHT. (SO09200502861)Dec 15, 2004 · N7892N · Cessna R172E · Wing SparSDR 2005FA0000367Flap Track · wornWHILE FLAPS WERE BEING RETRACTED, THE LT IB FLAP ATTACH BRACKET CAUGHT ON THE WING COVE PANEL SUPPORT. THIS CAUSED SUBSTANTIAL DAMAGE TO THE COVE PANEL SUPPORT AS WELL AS THE ATTACH BRACKET. CAUSE WAS DETERMINED TO BE WORN FLAP TRACKS. THE FLAP TRACKS AND RNov 29, 2004 · N7892N · Cessna R172E · Trailing Edge FlapsSDR CA040929006Hub · unserviceable(CAN) PROPELLER WAS REMOVED FROM AIRCRAFT FOR 10 YR. CALENDAR O/H. UPON INSPECTION THE HUB WAS FOUND TO BE CORRODED EXTERNALLY BEYOND REPAIR LIMITS. BLADE S/N K32294YS WAS FOUND TO BE CORRODED IN THE BLADE THREADS IN A LOCATION WHERE NO REPAIR IS ALLOWED. THSep 29, 2004 · Maule M5210C · Propeller Hub SectionSDR CA040929007Hub · unserviceable(CAN) PROPELLER WAS REMOVED FOR 10 YR. CALENDAR O/H. UPON INSPECTION THE HUB WAS FOUND TO BE CORRODED BEYOND REPAIRABLE LIMITS. ALSO DURING THIS INSPECTION BLADE M/N76C-0, S/N K32294YS WAS FOUND TO HAVE CORROSION BELOW THE BLADE THREAD PITCH LINE IN AN AREA WHSep 29, 2004 · Maule M5210C · Propeller Hub SectionSDR CA030606010Control Cable · frayed(CAN) INSPECTION OF FLAP CABLES IAW SERVICE DIFFICULTY ALERT NR AL-2003-05, FOUND THREE FRAYED CABLE ENDS, ONE AT OUTBOARD BELLCRANK.Jun 6, 2003 · Cessna 337A · Leading Edge Slat Control SystemSDR AUS20030479Control Cable · frayed(AUS) LH TRAILING EDGE FLAP CONTROL CABLE CONTAINED BROKEN STRANDS IN AREA APPROXIMATELY 25.4MM (1IN) FROM SWAGE AT BELLCRANK END.Mar 9, 2003 · Cessna M337B · Trailing Edge Flap Control SystemSDR AUS20030355Control Cable · frayed(AUS) RT INBOARD FLAP CABLE CONTAINED BROKEN STRANDS LOCATED IN AREA APPROXIMATELY 25.4MM TO 38.1MM (1IN TO 1.5IN) FROM THE INBOARD BELLCRANK TURNBUCKLE.Feb 27, 2003 · Cessna 337B · Trailing Edge Flap Control SystemSDR CA030227004Control Cable · failed(CAN) OPERATOR EXPERIENCED A ASYMMETRIC FLAP CONDITION DURING LANDING CAUSED BY THE FAILURE OF A FLAP CABLE. THE INBOARD RIGHT HAND FLAP CABLE FAILED AT A POINT WHERE THE CABLE STARTS TO BEND AROUND THE INBOARD RIGHT HAND FLAP BELLCRANK. THIS AREA OF THE CABLEFeb 25, 2003 · Cessna 336 · Trailing Edge Flap Control SystemSDR CA020621007Retainer · failed(CAN) PILOT INBOUND FOR LANDING & SELECTED GEAR DOWN. REPORTED THAT GEAR DID NOT EXTEND & GEAR MOTOR CONTINUED RUNNING. BEGAN EMERGENCY EXTENSION OF GEAR WITH HAND PUMP BUT NO PRESSURE BUILDING ON HAND PUMP. SEVERAL PROCEEDURES WERE CARRIED OUT BY PILOT & GRJun 5, 2002 · Cessna 337G · Landing Gear Door ActuatorSDR JK001Oil System · lowDURING CRUISE FLIGHT OIL PRESSURE WAS NOTED TO BE LOW AND FLUCTUATING, ALONG WITH SEVERE VIBRATION. THIS WAS FOLLOWED BY A COMPLETE LOSS OF OIL PRESSURE AND SUBSEQUENT LOSS OF POWER. THE ENGINE EXPERIENCED INTERNAL FAILURE FOR UNKNOWN REASONS RESULTING IN THMay 27, 2002 · N2442 · Reciprocating Engine Oil SystemSDR AUS20010414Rivet · loose(AUS) LT WING STRUT ATTACHMENT RIB TO OUTBOARD TIP RIVETS LOOSE AND MISSING. LEADING EDGE HAD BEEN REPLACED IN 1972.May 4, 2001 · Cessna 337 · Wing Miscellaneous StructureSDR AUS20010415Wheel · corroded(AUS) NOSE AND MAIN WHEEL HALVES (5OFF6) CORRODED WITH BEARINGS SPINNING IN THE WHEEL HALVES. CORROSION ALSO FOUND IN AREA OF THE FELT SEALS.May 4, 2001 · Cessna 337 · Wheel/Ski/FloatSDR AUS20010416Filter · contaminated(AUS) METAL CONTAMINATION OF THE REAR ENGINE OIL FILTER. SUSPECT MAIN BEARING FAILURE.May 4, 2001 · Cessna 337 · Reciprocating Engine Oil SystemSDR AUS20010417Frame · corroded(AUS) RT ROOF SUPPORT FORMER LOWER EDGE CONTAINED INTERGRANNULARCORROSION.May 4, 2001 · Cessna 337 · Fuselage Main, FrameSDR AUS20010418Rivet · damaged(AUS) NOSE LANDING GEAR WHEEL PAN/FIREWALL STRUCTURE RIVETS PULLED. FAILED RIVETS LOCATED IN THE AFT LT TOP CORNER.May 4, 2001 · Cessna 337 · Fuselage Main, StructureSDR AUS20010419Torque Tube · damaged(AUS) RUDDER PEDAL TORQUE TUBE CLAMP SUPPORT STRUCTURE CRACKED ANDWORKING. LOOSE RIVETS AND DAMAGE CAUSED BY BELLCRANK.May 4, 2001 · Cessna 337 · Rudder Control SystemSDR AUS20010420Selector Valve · faulty(AUS) FRONT AND REAR FUEL SELECTORS FAULTY. FUEL CAN'T BE TURNED OFF. SUSPECT FAULTY SEALS.May 4, 2001 · Cessna 337 · Fuel Selector/Shut-Off ValveSDR CA010529023Nut · damaged(CAN) AFTER LANDING PILOT WAS TAXIING FOR SHUTDOWN WHEN HE HEARD A BANKING NOISE AND REAR ENGINE ROUGHNESS. INSPECTION REVEALED A DENT IN VALVE COVER. COVER REMOVED AND FOUND BOTH ROCKER SHAFT HOLD DOWN STUDS SHEARED. IT HAS BEEN NOTED BEFORE ON OTHER AIRCRAFTApr 25, 2001 · Cessna 337G · Reciprocating Engine Cylinder SectionSDR AU000249Piston · damaged(AUS) NR 3 AND NR 4 PISTONS GRABBING IN CYLINDER BORES. FOUR OF SIX CYLINDER BORES UNDERSIZE. SB97-6 AND SIL99-2 NOT COMPLIED WITH.Apr 14, 2000 · Reciprocating Engine Cylinder SectionSDR AU000245Clamp · broken(AUS) FRONT ENGINE RIGHT MAGNETO COIL ATTACHMENT CLAMPS BROKEN. FOUND DURING INSPECTION IAW AD/ELECT/68.Apr 12, 2000 · Cessna 337 · Magneto/DistributorSDR 99ZZZX97Rod · failedINVESTIGATION FOUND NR 5 CONNECTING ROD CAME APART. CAUSE UNDER INVESTIGATION.Jul 13, 1998 · N475DF · Cessna M337B · Reciprocating Engine Power SectionSDR 98ZZZX2465Drive Gear · failedWHILE IN-FLIGHT, OIL PRESSURE AND TACHOMETER DROP TO ZERO, WAS ABLE TO LAND ON PRIVATE GRASS STRIP WITHOUT INCIDENT. DETERMINED THE OIL PUMP DRIVE GEAR HAS FAILED CAUSING FAILURE OF OIL PUMP, TACH DRIVE AND ALTERNATOR GEAR.Jun 25, 1998 · N24FC · Cessna R172E · Reciprocating Engine Rear SectionSDR 99ZZZX92Gear · failedWHILE IN-FLIGHT, OIL PRESSURE AND TACHOMETER DROPPED TO ZERO. WAS ABLE TO LAND ON PRIVATE GRASS STRIP WITHOUT INCIDENT. DETERMINED THE OIL PUMP DRIVE GEAR FAILED CAUSING FAILURE OF OIL PUMP, TACH DRIVE, AND ALTERNATOR GEAR. ON AN EARLIER DATE, FORCED TO MAKJun 25, 1998 · N24FC · Cessna R172E · Reciprocating Engine Oil SystemSDR CA970624005Actuating Pin · worn(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. ACTUATING PIN FOUND WORN. THE PIN WAS REPLACED.Jun 12, 1997 · Maule M5210C · Propeller Hub SectionSDR CA961023003Lock Tab · cracked(CAN) DURING INSPECTION WHILE BENDING THE TAB THAT SECURES THE ROCKER STUD NUT THE TAB CRACKED/BROKE.Nov 15, 1996 · Reciprocating Engine Cylinder SectionSDR CA960606002Split Pin · detached(CAN)ON ANNUAL INSPECTION, ONE SPLIT PIN FOUND IN THE SUCTION OIL SCREEN. OIL PAN REMOVED FOR INTERNAL INSPECTION. #5 CONROD BEARING CAP MISSING ONE COTTER PIN, REPLACED.May 27, 1996 · Maule M5210C · Reciprocating Engine Power Section
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