# Service difficulty reports: Continental IO-360-D A list on [Continental IO-360-D](https://openairdocs.org/engine/continental-io-360-d.md). Newest first. General aviation reporting is voluntary. - [SDR 2017FA0000084](https://openairdocs.org/sdr/2017FA0000084.md): Pump · failed · Mar 2, 2017 · N10105 · Cirrus SR20 · Engine Fuel Pump > MECHANICAL 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. - [SDR CA150609006](https://openairdocs.org/sdr/CA150609006.md): Pressure Switch · faulty · May 26, 2015 · Cessna 337G · Hydraulic Pressure Regulator, Auxiliary > (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 S - [SDR CA120420004](https://openairdocs.org/sdr/CA120420004.md): Cam · cracked · Apr 15, 2012 · Cessna 337G · Magneto/Distributor > (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. - [SDR 2008FA0000094](https://openairdocs.org/sdr/2008FA0000094.md): Hub · cracked · Feb 4, 2008 · N373AZ · Cessna M337B · Propeller Hub Section > RELEVENT INDICATION (CRACKED). (K) - [SDR 2006FA0000966](https://openairdocs.org/sdr/2006FA0000966.md): Hub · cracked · Sep 18, 2006 · Cessna T41D · Propeller Hub Section > PROPELLER 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) - [SDR 2006FA0000984](https://openairdocs.org/sdr/2006FA0000984.md): Hub · cracked · Sep 18, 2006 · Cessna T41D · Propeller Hub Section > PROPELLER 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) - [SDR 2005FA0001365](https://openairdocs.org/sdr/2005FA0001365.md): Yoke · broken · Sep 27, 2005 · N6950X · Cessna 172B · Control Column Section > UPON 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. - [SDR 2005FA0000365](https://openairdocs.org/sdr/2005FA0000365.md): Spar · cracked · Dec 15, 2004 · N7892N · Cessna R172E · Wing Spar > WHILE 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) - [SDR 2005FA0000367](https://openairdocs.org/sdr/2005FA0000367.md): Flap Track · worn · Nov 29, 2004 · N7892N · Cessna R172E · Trailing Edge Flaps > WHILE 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 R - [SDR CA040929006](https://openairdocs.org/sdr/CA040929006.md): Hub · unserviceable · Sep 29, 2004 · Maule M5210C · Propeller Hub Section > (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. TH - [SDR CA040929007](https://openairdocs.org/sdr/CA040929007.md): Hub · unserviceable · Sep 29, 2004 · Maule M5210C · Propeller Hub Section > (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 WH - [SDR CA030606010](https://openairdocs.org/sdr/CA030606010.md): Control Cable · frayed · Jun 6, 2003 · Cessna 337A · Leading Edge Slat Control System > (CAN) INSPECTION OF FLAP CABLES IAW SERVICE DIFFICULTY ALERT NR AL-2003-05, FOUND THREE FRAYED CABLE ENDS, ONE AT OUTBOARD BELLCRANK. - [SDR AUS20030479](https://openairdocs.org/sdr/AUS20030479.md): Control Cable · frayed · Mar 9, 2003 · Cessna M337B · Trailing Edge Flap Control System > (AUS) LH TRAILING EDGE FLAP CONTROL CABLE CONTAINED BROKEN STRANDS IN AREA APPROXIMATELY 25.4MM (1IN) FROM SWAGE AT BELLCRANK END. - [SDR AUS20030355](https://openairdocs.org/sdr/AUS20030355.md): Control Cable · frayed · Feb 27, 2003 · Cessna 337B · Trailing Edge Flap Control System > (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. - [SDR CA030227004](https://openairdocs.org/sdr/CA030227004.md): Control Cable · failed · Feb 25, 2003 · Cessna 336 · Trailing Edge Flap Control System > (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 CABLE - [SDR CA020621007](https://openairdocs.org/sdr/CA020621007.md): Retainer · failed · Jun 5, 2002 · Cessna 337G · Landing Gear Door Actuator > (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 & GR - [SDR JK001](https://openairdocs.org/sdr/JK001.md): Oil System · low · May 27, 2002 · N2442 · Reciprocating Engine Oil System > DURING 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 TH - [SDR AUS20010414](https://openairdocs.org/sdr/AUS20010414.md): Rivet · loose · May 4, 2001 · Cessna 337 · Wing Miscellaneous Structure > (AUS) LT WING STRUT ATTACHMENT RIB TO OUTBOARD TIP RIVETS LOOSE AND MISSING. LEADING EDGE HAD BEEN REPLACED IN 1972. - [SDR AUS20010415](https://openairdocs.org/sdr/AUS20010415.md): Wheel · corroded · May 4, 2001 · Cessna 337 · Wheel/Ski/Float > (AUS) NOSE AND MAIN WHEEL HALVES (5OFF6) CORRODED WITH BEARINGS SPINNING IN THE WHEEL HALVES. CORROSION ALSO FOUND IN AREA OF THE FELT SEALS. - [SDR AUS20010416](https://openairdocs.org/sdr/AUS20010416.md): Filter · contaminated · May 4, 2001 · Cessna 337 · Reciprocating Engine Oil System > (AUS) METAL CONTAMINATION OF THE REAR ENGINE OIL FILTER. SUSPECT MAIN BEARING FAILURE. - [SDR AUS20010417](https://openairdocs.org/sdr/AUS20010417.md): Frame · corroded · May 4, 2001 · Cessna 337 · Fuselage Main, Frame > (AUS) RT ROOF SUPPORT FORMER LOWER EDGE CONTAINED INTERGRANNULARCORROSION. - [SDR AUS20010418](https://openairdocs.org/sdr/AUS20010418.md): Rivet · damaged · May 4, 2001 · Cessna 337 · Fuselage Main, Structure > (AUS) NOSE LANDING GEAR WHEEL PAN/FIREWALL STRUCTURE RIVETS PULLED. FAILED RIVETS LOCATED IN THE AFT LT TOP CORNER. - [SDR AUS20010419](https://openairdocs.org/sdr/AUS20010419.md): Torque Tube · damaged · May 4, 2001 · Cessna 337 · Rudder Control System > (AUS) RUDDER PEDAL TORQUE TUBE CLAMP SUPPORT STRUCTURE CRACKED ANDWORKING. LOOSE RIVETS AND DAMAGE CAUSED BY BELLCRANK. - [SDR AUS20010420](https://openairdocs.org/sdr/AUS20010420.md): Selector Valve · faulty · May 4, 2001 · Cessna 337 · Fuel Selector/Shut-Off Valve > (AUS) FRONT AND REAR FUEL SELECTORS FAULTY. FUEL CAN'T BE TURNED OFF. SUSPECT FAULTY SEALS. - [SDR CA010529023](https://openairdocs.org/sdr/CA010529023.md): Nut · damaged · Apr 25, 2001 · Cessna 337G · Reciprocating Engine Cylinder Section > (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 AIRCRAFT - [SDR AU000249](https://openairdocs.org/sdr/AU000249.md): Piston · damaged · Apr 14, 2000 · Reciprocating Engine Cylinder Section > (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. - [SDR AU000245](https://openairdocs.org/sdr/AU000245.md): Clamp · broken · Apr 12, 2000 · Cessna 337 · Magneto/Distributor > (AUS) FRONT ENGINE RIGHT MAGNETO COIL ATTACHMENT CLAMPS BROKEN. FOUND DURING INSPECTION IAW AD/ELECT/68. - [SDR 99ZZZX97](https://openairdocs.org/sdr/99ZZZX97.md): Rod · failed · Jul 13, 1998 · N475DF · Cessna M337B · Reciprocating Engine Power Section > INVESTIGATION FOUND NR 5 CONNECTING ROD CAME APART. CAUSE UNDER INVESTIGATION. - [SDR 98ZZZX2465](https://openairdocs.org/sdr/98ZZZX2465.md): Drive Gear · failed · Jun 25, 1998 · N24FC · Cessna R172E · Reciprocating Engine Rear Section > WHILE 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. - [SDR 99ZZZX92](https://openairdocs.org/sdr/99ZZZX92.md): Gear · failed · Jun 25, 1998 · N24FC · Cessna R172E · Reciprocating Engine Oil System > WHILE 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 MAK - [SDR CA970624005](https://openairdocs.org/sdr/CA970624005.md): Actuating Pin · worn · Jun 12, 1997 · Maule M5210C · Propeller Hub Section > (CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. ACTUATING PIN FOUND WORN. THE PIN WAS REPLACED. - [SDR CA961023003](https://openairdocs.org/sdr/CA961023003.md): Lock Tab · cracked · Nov 15, 1996 · Reciprocating Engine Cylinder Section > (CAN) DURING INSPECTION WHILE BENDING THE TAB THAT SECURES THE ROCKER STUD NUT THE TAB CRACKED/BROKE. - [SDR CA960606002](https://openairdocs.org/sdr/CA960606002.md): Split Pin · detached · May 27, 1996 · Maule M5210C · Reciprocating Engine Power Section > (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. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/engine/continental-io-360-d/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.