# Service difficulty reports: Continental TSIO-360 series

A list on [Continental TSIO-360 series](https://openairdocs.org/engine/continental-tsio-360-series.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 77 reports

- [SDR 2024FA0000960](https://openairdocs.org/sdr/2024FA0000960.md): Skin · cracked · Dec 13, 2024 · N9022K · Piper PA28R201T · Wing, Plate/Skin
  > RH WING WALK BUCKLES AND IS CRACKED.
- [SDR 2017FA0000030](https://openairdocs.org/sdr/2017FA0000030.md): Clamp · broken · May 1, 2016 · N321QC · Mooney M20K · Exhaust Turbocharger
  > V BAND CLAMP HOLDING TURBOCHARGER ONTO EXHAUST BROKE AT THE SPOT WELD.
- [SDR 2013FA0000249](https://openairdocs.org/sdr/2013FA0000249.md): Filter · failed · Apr 16, 2013 · N38776 · Piper PA28R201T · Standard Practices/Structures
  > FOUND SEAM IN FILTER ELEMENT SEPARATED. NO TEARING OF THE MATERIAL WAS EVIDENT.
- [SDR 2013FA0000040](https://openairdocs.org/sdr/2013FA0000040.md): Switch · failed · Dec 31, 2012 · N231PQ · Mooney M20K · Landing Gear Retraction/Extension System
  > LANDING GEAR FAILED TO RETRACT ON TAKEOFF.
- [SDR 2012FA0000131](https://openairdocs.org/sdr/2012FA0000131.md): Trunnion · cracked · Feb 23, 2012 · N8076K · Piper PA34200T · Fuselage, Landing Gear Attach Fittings
  > DURING A VISUAL INSPECTION OF THE MLG, RT AFT TRUNNION MOUNTING PLATE PT WAS FOUND TO BE CRACKED ON THE STIFFENERS THAT FORM PART OF THE UPPER MOUNTING ARMS.
- [SDR 2011FA0000717](https://openairdocs.org/sdr/2011FA0000717.md): Magneto · failed · Jul 7, 2011 · N231E · Mooney M20K · Magneto/Distributor
  > DURING A POST ACFT ACCIDENT ENGINE TEARDOWN IT WAS NOTED THAT THE RT MAGNETO FIRED ERRATICALLY BELOW 1400 RPM. FURTHER INVESTIGATION REVEALED THAT THE DISTRIBUTOR GEAR WAS LOOSE AND THE ROTOR GEAR WAS LOOSE. PILOT REPORTED LOSS OF POWER ON TAKEOFF.
- [SDR 2011FA0000364](https://openairdocs.org/sdr/2011FA0000364.md): Air Filter · debonded · Jun 13, 2011 · N626DM · Piper PA34200T · Engine Air Intake System
  > DURING ANNUAL INSP, INPECTOR NOTED ONE BRACKET AIR FILTER ELEMENT, PN BA3 TO HAVE SEPARATED AT SEAM. INSPECTOR NOTES HAVING FOUND SEVERAL OTHER FILTERS FAILED IN THE SAME WAY.
- [SDR 2010FA0001236](https://openairdocs.org/sdr/2010FA0001236.md): Elt · malfunctioned · Dec 9, 2010 · N2190K · Piper PA34200T · Emergency Locator Beacon
  > (BIER) ELT REMOVED FOR INSP AND TESTING IAW CFR PART 91.207D. DURING BENCH TESTING OF ME-406 ELT, THE ELT WOULD NOT TURN OFF OR RESET. INTERNAL BATTERY HAD TO BE UNPLUGGED TO PREVENT ELT FROM REPEATED TRANSMITTION. ELT PN 453-6603, SN 14668 WAS SENT FOR NEED
- [SDR 2010FA0000955](https://openairdocs.org/sdr/2010FA0000955.md): Truss · failed · Aug 12, 2010 · N231DT · Mooney M20K · Nose/Tail Landing Gear
  > PILOT STATES THAT HE HAD MADE SEVERAL LANDINGS DURNG THE DAY BUT ON THE FINAL ONE AS THE NOSE WHEEL TOUCHED DOWN IT STARTED TO "WOBBLE BRIEFLY" AND THEN COLLAPSED FOLLOWED BY THE MAIL LANDING GEAR. DURING THE INCIDENT INVESTIGATION IT WAS FOUND THAT THE NOSE
- [SDR 2010FA0000993](https://openairdocs.org/sdr/2010FA0000993.md): Cover · bent · Jun 14, 2010 · N47629 · Piper PA28R201T · Aircraft Fuel Filter/Strainer
  > DURING THE CLIMB OUT, AT APPROX 4200 AGL, ONE SIDE OF THE WIRE BAIL ON THE FIREWALL MOUNTED GASCOLATOR CAME OUT OF THE FUEL STRAINER COVER. THIS ALLOWED ENGINE DRIVEN PUMP TO SUCK AIR INTO THE SYS WHICH RESULTED IN A LOSS OF FUEL PRESSURE TO THE POINT THE ENG
- [SDR 2010FA0000076](https://openairdocs.org/sdr/2010FA0000076.md): Rod · failed · Jan 27, 2010 · N252VV · Mooney M20K · Landing Gear Steering System
  > STEERING LINKAGE ROD BROKE AT THE NLG TRUSS ASSY.
- [SDR 2009FA0000807](https://openairdocs.org/sdr/2009FA0000807.md): Shaft · sheared · Aug 29, 2009 · N2443M · Piper PA28R201T · Reciprocating Engine Oil System
  > INFLIGHT FAILURE OF ENGINE, DUE TO OIL PUMP DRIVE GEAR SHAFT SHEARING. PILOT WAS IN CRUISE. ALTITUDE APPROXIMATELY 4000 FT MSL, UNSCHEDULED LANDING AT AIRPORT.
- [SDR 2009FA0000936](https://openairdocs.org/sdr/2009FA0000936.md): Autopilot Sys · inoperative · Aug 7, 2009 · N8086Q · Piper PA34200T · Autopilot System
  > UNIT WAS INITIALLY REMOVED FROM ACFT IN MARCH OF 2009 BECAUSE AUTOPILOT WOULD NOT OPERATE PROPERLY. TO VERIFY AUTOPILOT OUTPUTS FROM ATTITUDE GYRO WERE WORKING GYRO REMOVED FROM ACFT AND A BENCH TEST PERFORMED. BENCH TEST REVEALED THAT IT WOULD NOT ERECT AT
- [SDR ATJ2009F00000](https://openairdocs.org/sdr/ATJ2009F00000.md): Trunnion · broken · Jul 28, 2009 · N1494X · Piper PA34200T · Fuselage, Landing Gear Attach Fittings
  > LT MAIN LANDING GEAR WOULD NOT COME DOWN AND LOCIN IN FLIGHT. EMERGENCY PROCEDURES USED TO EXTEND GEAR. AFTER LANDING ACFT WAS MOVED BY GROUND PERSONELL AND LT GEAR COLLAPSED. FWD LT GEAR FITTING WAS FOUND TO BE PARTIALLY MISSING. SB HAD BEEN COMPLIED WITH
- [SDR FFKA137](https://openairdocs.org/sdr/FFKA137.md): Pump · unserviceable · Apr 29, 2009 · N3570M · Piper PA34200T · Engine Fuel Pump
  > PILOT REPORTED A POWER LOSS AND VIBRATION COMING FROM THE RIGHT ENGINE. AFTER TURNING ON THE AUXILIARY FUEL BOOST PUMP ENGINE RETURNED TO NORMAL, PILOT ELECTED TO LAND. POST INVESTIGATION FOUND THE ENGINE DRIVEN FUEL PUMP WORKED FINE ON THE GROUND, MAINTENAN
- [SDR 2009FA0000240](https://openairdocs.org/sdr/2009FA0000240.md): Oil Filter · loose · Mar 23, 2009 · N7CX · Cessna P337H · Turbine Engine Oil System
  > PILOT REPORTED LOW OIL PRESSURE DURING TAKEOFF PHASE OF FLIGHT FOLLOWED BY NO OIL PRESSURE INDICATION SHORTLY AFTER. PILOT THOUGHT THE LOW OIL PRESSURE WAS AN INDICATION PROBLEM. UPON INSPECTION AND FUNCTIONAL CHECK OF PRESSURE GAUGE, THE INDICATOR WAS RULED O
- [SDR 2008FA0000840](https://openairdocs.org/sdr/2008FA0000840.md): Ground Stud · misinstalled · Nov 24, 2008 · N305P · Mooney M20K · Electrical Power System
  > AIRFRAME GROUND PLUG IN HAS NEVER BEEN CONNECTED TO AIRFRAME GROUND. BASE OF RECEPTACLE WAS INSULATED FROM AIRFRAME GROUND BY PRIMER ON METAL ANGLE. WE FOUND COMPLETE ISOLATION FROM GROUND POINT TO FUEL FILLER OPENING, NO GROUND ON OUR FUELING OPERATIONS FOR P
- [SDR 2008FA0000509](https://openairdocs.org/sdr/2008FA0000509.md): Arm · worn · Jul 22, 2008 · N2190K · Piper PA34200T · Landing Gear Steering System
  > NLG MOUNT ASSY ATTACHMENT POINT FOR STEERING ARM ASSY HAS EXCESSIVE WEAR AT LWR MOUNT HOLE, SRM DOES NOT SPECIFY AT FIX OR ALLOWABLE LIMIT FOR PN 95551-23. DISCREPANCY FOUND DURING INSP IAW SB 1123A & B AND ANNUAL INSPECTION IAW SRM INSPECTION GUIDE. SB 1123
- [SDR 2007FA0001074](https://openairdocs.org/sdr/2007FA0001074.md): Control System · seized · Nov 30, 2007 · N557C · Piper PA34220T · Rudder Control System
  > WITH FULL RT RUDDER TRIM, RT RUDDER FOR HARD CLIMBING RT TURN, RUDDER FROZE WITH FULL RT DEFLECTION. RUDDER CABLE TURNBUCKLE IN TAIL SECTION WAS (CAUGHT) UNDER BULKHEAD TOP EDGE CAUSING RUDDER TO FREEZE IN FULL RT DEFLECTION - DESPITE SIGNIFICANT LT RUDDER PR
- [SDR 2008FA0000251](https://openairdocs.org/sdr/2008FA0000251.md): Fitting · separated · Nov 14, 2007 · N467TC · Piper PA34200T · Fuselage, Landing Gear Attach Fittings
  > SB 1123B TABLE 1, ITEM 14 STATES TO INSPECT TUNNEL BRACKET 95554-000 AND FITTING 95555-000 FOR CONDITION AND ATTACHMENT. ACCORDING TO FIGURE 1A, THE CONDITION INDICATED NO PROBLEMS, HOWEVER FITTING 95555-000 WAS SEPARATED FROM BRACKET 95554-000. ALL 4 AN426
- [SDR 2007FA0000941](https://openairdocs.org/sdr/2007FA0000941.md): Roll Servo · loose · Oct 9, 2007 · N697SP · Mooney M20K · Flight Control System
  > MOTOR ASSY COMING LOOSE ON SERVO MOUNT. LOOSE HARDWARE, LOOSE MOTOR. RECOMMEND SERVO TO BE INSPECTED FOR PROPER SERVO ASSY (THAT MOTOR AND HARDWARE ARE NOT LOOSE). (K)
- [SDR 2007F00054](https://openairdocs.org/sdr/2007F00054.md): Spring · disconnected · Sep 11, 2007 · N464WA · Piper PA34200T · Passenger/Crew Doors
  > TENSION SPRING ON UPPER CABIN DOOR LATCH BECAME DISCONNECTED. CAUSED THE UPPER DOOR LATCH NOT TO LATCH/SEAL, ALLOWED RAIN TO ENTER.
- [SDR 2006FA0000582](https://openairdocs.org/sdr/2006FA0000582.md): Bolt · loose · May 22, 2006 · N7609C · Piper PA34200T · Main Landing Gear Attach Section
  > NOSE GEAR RETRACTED ON LANDING. FOUND BOLT PN 401-421 (AN6-41A) LOOSE WHERE NOSE GEAR MOUNT BOLTS TO BULKHEAD AT STA 49.5. THIS RELEAVED DOWNLOCK LINK OVER CENTER POSITION. BOLTS SHOULD BE CHECKED EACH 500 HRS. (K)
- [SDR 2006FA0000717](https://openairdocs.org/sdr/2006FA0000717.md): Rib · cracked · Mar 11, 2006 · N8164D · Piper PA34220T · Wing, Rib/Bulkhead
  > DURING COMPLIANCE WITH SB, LT AND RT RIBS FOUND CRACKED AS SUSPECTED. INSTALLED REPAIR KITS. LT DRAG BRACE PIVOT, PN 39479002, ALSO FOUND CORRODED AND CRACKED. THIS IS NOT PART OF SB INSPECTION. (K)
- [SDR 43881](https://openairdocs.org/sdr/43881.md): Fuel Line · chafed · Dec 13, 2005 · N1130D · Piper PA34220T · Engine Fuel Distribution
  > THE FUEL INJECTOR LINE FROM THE FLOW DIVIDER TO THE NR3 CYLINDER ON THE RT ENGINE WAS ROUTED UNDER A COWL LATCH FOR THE COWLING NOSE BOWL WHICH CAUSED SEVER CHAFING IN A LOCALIZED AREA. THIS WAS ORIGINAL FACTORY ROUTING. NO FAILURE OCCURRED, PART WAS REPLACE
- [SDR 2006FA0000565](https://openairdocs.org/sdr/2006FA0000565.md): Bulkhead · cracked · Oct 5, 2005 · N344HP · Piper PA34220T · Propeller Spinner Section
  > THIS AC WAS NEW IN 3/3/2002. LT AND RT SPINNER BULKHEADS HAVE HAD TO BE REPLACED TWICE. FIRST SET OF SPINNER BULKHEADS WERE REPLACED 12/28/2004, WITH 563.3 HOURS ON THEM. PROPS WERE BALANCED TO PREVENT FURTHER PROBLEMS. SECOND SET OF SPINNER BULKHEADS WERE
- [SDR 2005F00104](https://openairdocs.org/sdr/2005F00104.md): Wheel · loose · Sep 14, 2005 · N435 · Cessna T337G · Wheel/Ski/Float
  > WHEEL ASSEMBLY RETURNED FOR LOOSE TIE BOLTS OF 18 INSTALLED 14 WERE FOUND LOOSE 2 MISSING. MFG HAS NOW RELEASE SERVICE LETTER F6137-32--843 IN HOPES THIS WILL RESOLVE.
- [SDR GNB2005F00004](https://openairdocs.org/sdr/GNB2005F00004.md): Valve · warped · Jun 8, 2005 · N494BC · Cessna 402C · Exhaust Turbocharger
  > WARPED VALUE. (K)
- [SDR 2005FA0001015](https://openairdocs.org/sdr/2005FA0001015.md): Logic Card · malfunctioned · May 17, 2005 · N7333L · Piper PA34200T · Indicating/Recording System
  > SCC CARD INSTALLED AS PART OF THE EFIS-SV SYSTEM IAW STC NR SA02203AK WOULD NOT ALLOW THE MOVING MAP PAGE TO APPEAR ON THE IDU DURING START UP. (ALO5200502600) (K)
- [SDR 2005FA0000658](https://openairdocs.org/sdr/2005FA0000658.md): Spring · broken · Apr 20, 2005 · N994BD · Piper PA34220T · Landing Gear Retraction/Extension System
  > OPERATOR DID NOT GET RT MAIN GEAR DOWN INDICATION AFTER EXTENDING LANDING GEAR USING EMERGENCY EXTENSION. AIRCRAFT LANDED WITHOUT INCIDENT. RT MAIN GEAR OVER-CENTER SPRING ATTACH PLATE WAS FOUND BROKEN. WITH THE HYDRAULIC PUMP DISABLED FOR THE GEAR EXTENSION
- [SDR 2005FA0000355](https://openairdocs.org/sdr/2005FA0000355.md): Torque Tube · elongated · Mar 4, 2005 · N39655 · Piper PA34200T · Rudder Tab Control System
  > DURING INSPECTION, TECH DISCOVERED PLAY IN RUDDER TORQUE TUBE FITTING. TECH INSTALLED SERVICE KIT 764-100V. AD AND SB ADDRESSES INSP AN REPLACEMENT OF THE STEEL TORQUE TUBE FITTING WITH A STEEL REPLACEMENT PART. THIS AC HAD THE STEEL TORQUE TUBE FITTING INS
- [SDR 2005FA0000342](https://openairdocs.org/sdr/2005FA0000342.md): Powerpack · failed · Feb 9, 2005 · N4358X · Piper PA34200T · Hydraulic System, Main
  > AC DEPARTED, DIVERTED, PILOT THOUGHT THAT HIS LANDING GEAR WAS NOT FULLY IN THE UP AND LOCK POSITION (UNKNOWN IF GEAR UNSAFE LIGHT WAS ON). PILOT SELECTED GEAR DOWN, NOTHING HAPPENED, PULLED EMERGENCY GEAR EXTENSION AND LANDED WITH NO FURTHER INCIDENT. MAINT
- [SDR 2005FA0000178](https://openairdocs.org/sdr/2005FA0000178.md): Combustion Liner · cracked · Jan 31, 2005 · N13AG · Piper PA34200T · Heating System
  > WHILE PERFORMING AD 04-21-05, THE HEATER FAILED THE PRESSURE DECAY TEST. REMOVED UNIT AND FOUND CRACKS IN END OF COMBUSTION LINER. UNIT WAS REMOVED AND REPLACED WITH OVERHAULED UNIT. UNIT INSTALLED MAY 1998, AND CONTAINED NEW STYLE CERAMIC LINER.
- [SDR 2005FA0000143](https://openairdocs.org/sdr/2005FA0000143.md): Bolt · misinstalled · Jan 26, 2005 · N249PM · Piper PA34200T · Shimmy Damper
  > DURING RAMP INSPECTION, INSPECTOR NOTICED BOLT ATTACHING NOSE GEAR CENTERING DEVICE WAS INSTALLED INCORRECTLY, HEAD OF BOLT AT TOP OF HARDWARE STACK. AD 92-13-05 AND SB 893 REQUIRE BOLT TO BE INSTALLED WITH HEAD DOWN AND A CAUTIONARY PLACARD TO BE AFFIXED. P
- [SDR 2004FA0000737](https://openairdocs.org/sdr/2004FA0000737.md): Battery Cable · overheated · Aug 16, 2004 · N467TC · Piper PA34200T · Electrical Power System Wiring
  > LT ENGINE HARD STARTING. EXCESSIVE AMPERAGE DRAW THROUGH BATTERY CABLES CAUSING HOT CABLES AND SUBSEQUENT BATTERY FIRE. REPLACED BATTERY POSITIVE AND NEGATIVE CABLES, RT AND LT STARTER CABLES, ENGINE (STARTER) TO GROUND CABLES, MASTER SOLENOID TO TERMINAL CA
- [SDR HJL2004F00000](https://openairdocs.org/sdr/HJL2004F00000.md): Spring · broken · Jul 12, 2004 · N252YE · Mooney M20K · Landing Gear Actuator
  > LANDING GEAR ACTUATOR, PN R5329M24-1, OR MFG AC PN 880037-507, WOULD NOT FUNCTION MANUALLY OR ELECTRICALLY. ACTUATOR WAS SENT FOR INSPECTION. AFTER VERIFYING THAT ACTUATOR WOULD NOT FUNCTION, THE ACTUATOR WAS OPENED, INSPECTED, AND THE TORSION SPRING WAS FOU
- [SDR FFK2004F00005](https://openairdocs.org/sdr/FFK2004F00005.md): Pump · faulty · Jul 8, 2004 · N86BW · Piper PA34200T · Engine Fuel Pump
  > PILOT REPORTED THAT THE LT ENGINE SURGED ON TAKE OFF. AFTER INVESTIGATING LT ENGINE, FOUND THAT THE ENGINE DRIVE FUEL PUMP FUEL FLOW WOULD DROP OFF AT HIGH RPMS. SUSPECT BAD FUEL PUMP, REPLACED AS NEEDED.
- [SDR 2004FA0000774](https://openairdocs.org/sdr/2004FA0000774.md): Housing · broken · Jun 29, 2004 · N2190K · Piper PA34200T · Turbine Engine Oil System
  > DURING SEARCH FOR OIL LEAK ONTO ALTERNATOR FOUND. OIL SCAVENGE PUMP HOUSING HAD BROKEN MOUNT LUG. REPLACED WITH NEW PART. CAUSE OF FAILURE BELIEVED TO BE WEAK CONSTRUCTION. AIRCRAFT FREON COMPRESSOR MOUNTS HERE. AIRCRAFT HAS HAD DYNAMIC PROP BALANCES. SE
- [SDR BNG2004F00000](https://openairdocs.org/sdr/BNG2004F00000.md): Link · cracked · Apr 20, 2004 · N47681 · Piper PA28R201T · Nose/Tail Landing Gear
  > NOSE GEAR LINK PN 76426-03, CRACKED TOP RT SIDE.
- [SDR 2004FA0000521](https://openairdocs.org/sdr/2004FA0000521.md): Switch · failed · Apr 15, 2004 · N103JH · Piper PA34200T · Engine Start Valves/Controls
  > WATER FROM WASHING THE AIRCRAFT WENT DOWN LEFT SIDE WINDOW INTO SWITCH PANEL CAUSING MASTER SWITCH TO ACTIVATE MASTER SOLENOID (WHEN IN OFF POSITION). THE WATER FROM WASHING ALSO CAUSED LT ENGINE STARTER SWITCH TO ACTIVATE STARTER SPINNING PROPELLER (WHEN IN
- [SDR 2004FA0000522](https://openairdocs.org/sdr/2004FA0000522.md): Master Switch · failed · Apr 15, 2004 · N103JH · Piper PA34200T · Electrical Power System
  > WATER FROM WASHING THE AIRCRAFT WENT DOWN LEFT SIDE WINDOW INTO SWITCH PANEL CAUSING MASTER SWITCH TO ACTIVATE MASTER SOLENOID (WHEN IN OFF POSITION). THE WATER FROM WASHING ALSO CAUSED LT ENGINE STARTER SWITCH TO ACTIVATE STARTER SPINNING PROPELLER (WHEN IN
- [SDR 2004FA0000396](https://openairdocs.org/sdr/2004FA0000396.md): Relay · inoperative · Apr 13, 2004 · N312AJ · Piper PA34220T · Exterior Lighting
  > DURING A RAIN STORM FLIGHT PERSONNEL REPORTED TO RAMP 66 MAINTENANCE DEPT THAT AC. WINGS AND TAIL STROBE LIGHTS CAME ON. MAINT MECH CHECKED BATTERY SWITCH. SWITCH WAS TURNED OFF. DURING TROUBLESHOOT AFT COMPARTMENT FLOORING WAS REMOVED BEHIND PASSENGER SEA
- [SDR LER2004F00000](https://openairdocs.org/sdr/LER2004F00000.md): Tube · fractured · Mar 9, 2004 · N4023U · Piper PA34200T · Fuel Storage
  > FUEL LINE FRACTURED CAUSING FUEL STARVATION AND ENGINE FAILURE.
- [SDR AKG2004F00005](https://openairdocs.org/sdr/AKG2004F00005.md): Cylinder · failed · Mar 2, 2004 · N102RM · Piper PA34200T · Reciprocating Engine Cylinder Section
  > THE NR 6 CYLINDER WAS FOUND CRACKED AROUND THE INSIDE OF THE STEEL PART ABOUT 1.5 INCHES FROM THE TOP WHERE IT SCREWED INTOTHE HEAD. THE CRACK IS ALMOST COMPLETELY AROUND THE CYLINDER. THIS CYLINDER IS A REPAIRED SERVICEABLE FROM ENGINE COMPONENTS WITH THE C
- [SDR 2004FA0000568](https://openairdocs.org/sdr/2004FA0000568.md): Fitting · corroded · Feb 26, 2004 · N157BJ · Piper PA34200T · Fuselage Main, Structure
  > BOTH LOWER AFT WINDSHIELD FRAME STEEL FITTING VERY CORRODED. WINDSHIELD LEAK AND INSULATION HOLDING MOISTURE ON FITTING. NEED TO BE INSPECTED MORE OFTEN AND CLEANED AND TREATED.
- [SDR 2004FA0000569](https://openairdocs.org/sdr/2004FA0000569.md): Fitting · corroded · Feb 26, 2004 · N157BJ · Piper PA34200T · Fuselage Main, Attach Fittings
  > BOTH LOWER AFT WINDSHIELD FRAME STEEL FITTING VERY CORRODED. WINDSHIELD LEAK AND INSULATION HOLDING MOISTURE ON FITTING. NEED TO BE INSPECTED MORE OFTEN AND CLEANED AND TREATED.
- [SDR WYNBRANDT](https://openairdocs.org/sdr/WYNBRANDT.md): Fluid · solidified · Feb 2, 2004 · N963PM · Mooney M20K · Landing Gear Brake System
  > DURING A ROUTINE OIL CHANGE IT WAS NOTED THAT THE AIRCRAFT TOOK VERY HIGH RPM TO TAXI. THE BRAKE FLUID IN THE WHEEL CYLINDER HAD TURNED THE CONSISTENCY OF HONEY. THE FLUID WAS PURGED BY BLEEDING USING PEDALS PRESSURE TO MOVE FLUID OUT. THE BRAKE BLEEDERS HAD T
- [SDR 2004FA0000172](https://openairdocs.org/sdr/2004FA0000172.md): Fuel Cap · loose · Jan 12, 2004 · N4142R · Piper PA34220T · Fuel Storage
  > PILOT ENCOUNTERED LOSS OF POWER ON LT ENGINE AND MADE AN UNSCHEDULED LANDING. WATER WAS FOUND IN LT TANK AND LT FUEL LINES. WATER WAS SUMPED OUT, ENG TEST RUN, AC RETURNED TO HOMEBASE. LT SIDE CAP WAS FOUND TO BE LOUSY FIT, PROBABLY ALLOWED WATER TO ENTER
- [SDR 2004FA0000526](https://openairdocs.org/sdr/2004FA0000526.md): Bulkhead · cracked · Dec 24, 2003 · N12699 · Piper PA34220T · Propeller Spinner Section
  > DURING ANNUAL INSPECTION, FOUND THE LT PROP SPINNER BULKHEAD CRACKED IN SEVERAL PLACES. THE CRACKS ARE LOCATED AT JUST ABOUT EVERY BOLT HOLE FOR ATTACHING THE BULKHEAD TO THE PROP BULKHEAD HAD TO BE REPLACED.
- [SDR 2003FA0001238](https://openairdocs.org/sdr/2003FA0001238.md): Pushrod Tube · corroded · Dec 1, 2003 · N231PF · Mooney M20K · Aileron Control System
  > FOUND BOTH AILERON OB PUSH ROD TUBES RUSTING INTERNALLY. IF RUST IS NOTICED ON EXTERIOR OF TUBE, IT IS ALREADY AT POINT OF FAILURE. TT 5140 HRS RECOMMEND REPLACING BOTH AILERON PUSH ROD TUBE ASSEMBLIES ON ANY AC WHICH HAVE NOT BEEN REPLACED IN PAST FIVE YEA

Next page: https://openairdocs.org/engine/continental-tsio-360-series/reports.md?page=2

## 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 = 'TSIO360'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/continental-tsio-360-series/reports

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