# Service difficulty reports: Piper PA-34-200 A list on [Piper PA-34-200](https://openairdocs.org/model/piper-pa-34-200.md). Newest first. General aviation reporting is voluntary. Page 1 of 5 · 203 reports - [SDR U9FR20200924750](https://openairdocs.org/sdr/U9FR20200924750.md): Latch · malfunctioned · Jun 13, 2020 · N15035 · Piper PA34200 · Cargo/Baggage Doors > BAGGAGE DOOR CAME OFF DURING ROTATION AS PILOT WAS CLIMBING OUT. BAGGAGE DOOR WAS RECOVERED, THE KEY WAS NOT IN THE LOCK. MAINTENANCE WAS NOT ABLE TO DETERMINE THE POSITION OF THE BAGGAGE DOOR LATCH UPON RECOVERY. INSPECTED DOOR AND LATCH MECHANISM, COULD N - [SDR 2020FA0000245](https://openairdocs.org/sdr/2020FA0000245.md): Landing Gear · collapsed · May 6, 2020 · N1369T · Piper PA34200 · Nose/Tail Landing Gear > NOSE GEAR COLLAPSED ON TOUCH AND GO. DOWN LOCK BOLT WAS FOUND BENT BUT BELIEVED TO HAVE BEEN BENT DURING THE COLLAPSE. - [SDR 2020FA0000257](https://openairdocs.org/sdr/2020FA0000257.md): Rod End · broken · May 1, 2020 · N41502 · Piper PA34200 · Power Lever > RIGHT ENGINE THROTTLE RESPONSE INEFFECTIVE. FOUND THROTTLE ROD END FAILED.THREADED BALL POPPED OUT OF SOCKET ON ROD END - [SDR 2017FA0000257](https://openairdocs.org/sdr/2017FA0000257.md): Trunnion · broken · Jun 26, 2017 · N101SA · Piper PA34200 · Wing, Landing Gear Attach Fittings > LEFT MAIN LANDING GEAR REAR TRUNNION BROKE ON LANDING. THIS CAUSED LEFT MAIN GEAR FORWARD TRUNNION TO BREAK AND GEAR TO MOVE UPWARD IN GEAR WELL. - [SDR 2017FA0000254](https://openairdocs.org/sdr/2017FA0000254.md): Trunnion · failed · Jun 19, 2017 · N101SA · Piper PA34200 · Fuselage, Landing Gear Attach Fittings > TRUNNION BROKE ON TOUCHDOWN. OWNER STATED THIRD TRUNNION REPLACED IN LAST THREE YEARS WITH SAME RESULTS. - [SDR 4GPR20170407](https://openairdocs.org/sdr/4GPR20170407.md): Nut Plate · broken · Apr 7, 2017 · N1059 · Piper PA34200 · Fuselage, Landing Gear Attach Fittings > AIRCRAFT HAD A GEAR UNSAFE LIGHT DURING FLIGHT. FOUND RIGHT MAIN GEAR FORWARD TRUNNION ATTACH FITTING HARDWARE LOOSE. FURTHER INSPECTION REVEALED 4 BROKEN NUTPLATES. - [SDR 2017FA0000040](https://openairdocs.org/sdr/2017FA0000040.md): Alternator · shorted · Feb 3, 2017 · N41285 · Piper PA34200 · DC Generator-Alternator > AIRCRAFT EXPERIENCED A FAILURE OF THE LEFT ALTERNATOR IN FLIGHT THAT RESULTED IN SMOKE COMING FROM THE COWL. AIRCRAFT LANDED SAFELY AND UPON INSPECTION FOUND THAT THE ALTERNATOR WOULD NOT TURN WHEN TURNING THE PROPELLER. UPON REMOVAL OF THE ALTERNATOR FROM THE - [SDR 2017FA0000091](https://openairdocs.org/sdr/2017FA0000091.md): Alternator · seized · Jan 15, 2017 · N4128 · Piper PA34200 · AC Inverter > THE ALTERNATOR SEIZED IN FLIGHT CAUSING THE BELT TO BURN AND SMOKE OVER THE PULLEY. - [SDR U9FR20161122003](https://openairdocs.org/sdr/U9FR20161122003.md): Hose · separated · Nov 22, 2016 · N200WS · Piper PA34200 · Hydraulic System, Main > NOSE LANDING GEAR FAILED TO EXTEND IN FLIGHT. PILOT PERFORMED SUCCESSFUL EMERGENCY EXTENSION OF LANDING GEAR WITH UNEVENTFUL LANDING. TROUBLESHOT SYSTEM AND FOUND NLG ACTUATOR HOSE HAD SEPARATED FROM HOSE END FITTING AT ACTUATOR. CORRECTIVE ACTION WAS TO REPLA - [SDR 2016FA0000659](https://openairdocs.org/sdr/2016FA0000659.md): Link · broken · Oct 31, 2016 · N1059U · Piper PA34200 · Landing Gear Retraction/Extension System > AFTER A NORMAL LANDING, THE AIRCRAFT ROLLED 50 FT AND THE NLG COLLAPSED. DURING INSPECTION, FOUND THE NLG DOWNLOCK LINK ASSY BROKEN. - [SDR U9FR20161025002](https://openairdocs.org/sdr/U9FR20161025002.md): Pump · failed · Oct 21, 2016 · N15008 · Piper PA34200 · Hydraulic Pump (Electric/Engine), Main > LANDING GEAR FAILED TO EXTEND IN FLIGHT. PILOT PERFORMED SUCCESSFUL EMERGENCY EXTENSION OF LANDING GEAR WITH UNEVENTFUL LANDING. TROUBLESHOT LANDING GEAR SYSTEM AND FOUND HYDRAULIC PUMP NOT PRODUCING SUFFICIENT PRESSURE TO EXTEND LANDING GEAR. - [SDR U9FS201609190001](https://openairdocs.org/sdr/U9FS201609190001.md): Gear · chafed · Jul 15, 2016 · N852AT · Piper PA34200 · Nose/Tail Landing Gear > PILOT INSTRUCTOR AND STUDENT WERE FLYING THIS ACFT DOING TOUCH AND GOES. ON THE SECOND TOUCH AND GO THE NOSE GEAR WOULD NOT EXTEND. AFTER SEVERAL ATTEMPTS TO EXTEND THE NOSE GEAR BY THE PILOT, HE TRIED TO FREE FALL THE GEAR, BOTH MAINS EXTENDED BUT THE NOSE - [SDR 2015FA0000409](https://openairdocs.org/sdr/2015FA0000409.md): Circuit Breaker · failed · Aug 14, 2015 · N5337T · Piper PA34200 · Landing Gear System Wiring > PILOT REPORTED WHEN HE SELECTED LANDING GEAR UP, THE LANDING GEAR DOWN LIGHTS EXTINGUISHED AND THE LANDING GEAR FAILED TO RETRACT. THE LANDING GEAR HANDLE WAS THEN PLACED IN THE DOWN POSITION, THE LANDING GEAR DOWN LIGHTS REMAINED EXTINGUISHED. THE MANUAL EX - [SDR CA150424001](https://openairdocs.org/sdr/CA150424001.md): Spring · broken · Apr 23, 2015 · Piper PA34200 · Nose/Tail Landing Gear Strut/Axle > (CAN) AFTER TAKEOFF PILOT REPORTED GEAR UNSAFE LIGHT CAME ON AND STAYED ON AFTER SELECTING GEAR UP. PILOT SELECTED GEAR DOWN AND GOT A 3 GREEN LIGHT INDICATION AND LANDED SAFELY. ACFT WAS SNAGGED AND REPORTED TO MAINTENANCE. UPON INSPECTION IT WAS FOUND THA - [SDR CA150204011](https://openairdocs.org/sdr/CA150204011.md): Stud · broken · Jan 26, 2015 · Piper PA34200 · Reciprocating Engine Cylinder Section > (CAN) THREE BROKEN STUDS TOP CYLINDER NR 2. - [SDR CA140820006](https://openairdocs.org/sdr/CA140820006.md): Bracket · unsecure · Aug 7, 2014 · Piper PA34200 · Nose/Tail Landing Gear > (CAN) AFTER TOUCHDOWN, DURING ROLL OUT, THE NOSE GEAR RETRACTED CAUSING BOTH PROPELLERS TO STRIKE THE GROUND. DURING ASSESSMENT INSPECTION, LOWER TUNNEL BRACKET, PN 95554-00 WAS FOUND TO HAVE 4 RIVETS PULLED THROUGH CAUSING THE GEOMETRY TO CHANGE ON DOWN LINK - [SDR ZB0S2014FA0000244](https://openairdocs.org/sdr/ZB0S2014FA0000244.md): Stringer · cracked · Mar 20, 2014 · N15412 · Piper PA34200 · Wing, Longeron/Stringer > DURING ROUTINE ANNUAL INSPECTION, THE FRONT STRINGER, LOWER WING SKIN STIFFENER, WAS FOUND CRACKED UNDER THE LT ENGINE NACELLE USING A FLASHLIGHT & MIRROR VIA THE FRONT WING SECTION ACCESS PANEL JUST INBD OF THE INBD MAIN FUEL TANK. IN ORDER TO FACILITATE A B - [SDR CA130920012](https://openairdocs.org/sdr/CA130920012.md): Squat Switch · defective · Sep 11, 2013 · Piper PA34200 · Landing Gear Position and Warning > (CAN) NOSE GEAR FAILED TO RETACT AFTER TAKEOFF. ACFT PLACED ON JACKS AND INSPECTED. SQUAT SWITCH FOUND DEFECTIVE. SWITCH REPLACED AND GEAR SWING COMPLETED. ACFT RETURNED TO SERVICE. - [SDR CA130220012](https://openairdocs.org/sdr/CA130220012.md): Attach Fitting · corroded · Feb 20, 2013 · Piper PA34200 · Vertical Stabilizer, Attach Fittings > (CAN) EXCESSIVE DISSIMILAR CORROSION FOUND BETWEEN BULKHEAD ASSEMBLY AND STEEL FITTING THAT IS THE FWD ATTACH POINT FOR THE VERTICAL STABILIZER. RIVETS APPEARED TO BE IN PLACE BUT WERE FOUND TO BE NOT HOLDING ANYTHING. DAMAGE WAS FOUND TO BE SAME AS DAMAGE R - [SDR 2012FA0000436](https://openairdocs.org/sdr/2012FA0000436.md): Trunnion · cracked · Jun 26, 2012 · N1039U · Piper PA34200 · Nose/Tail Landing Gear Strut/Axle > ON ANNUAL INSPECTION, FOUND RIGHT PIVOT POINT OF NOSE GEAR TRUNNION CRACKED WHERE TRUNNION IS WELDED TO PIVOT BOLT HOUSING. - [SDR CA120525002](https://openairdocs.org/sdr/CA120525002.md): Spring · broken · May 18, 2012 · Piper PA34200 · Trailing Edge Flaps > (CAN) FLAP RETURN SPRING WAS FOUND BROKEN AT ATTACH POINT DURRING PREFLIGHT INSPECTION. - [SDR CA120518002](https://openairdocs.org/sdr/CA120518002.md): Air Box · cracked · May 17, 2012 · Piper PA34200 · Engine Air Intake System > (CAN) WHILE COMPLETING 100 HR INSPECTION, A CRACK WAS FOUND ON THE RT ENGINE ALTERNATE AIR BOX AT THE FLANGE ATTACHING THE AIR BOX TO THE FUEL SERVO. THE CRACK WAS ON A WELDED FLANGE. THE CRACK WAS VISIBLE FROM THE BOTTOM ONLY. AIR BOX WAS REMOVED AND SENT - [SDR REXA201200063](https://openairdocs.org/sdr/REXA201200063.md): Glowstrip · loose · Apr 24, 2012 · N15156 · Piper PA34200 · Emergency Equipment > PHOTO LUMINESCENT TAPE NEEDS TO BE RE-SECURED IN GALLEY AREA JUST BEHIND MAIN BOARDING DOOR. RE-SECURED EMERGENCY PHOTO LUMINESCENT TAPE BY GALLEY CARTS AS REQUIRED. - [SDR CA120426002](https://openairdocs.org/sdr/CA120426002.md): Rib · cracked · Apr 19, 2012 · Piper PA34200 · Wing Spar > (CAN) ADDITIONAL CRACKS AT THE LOCATION OF RIB REPAIR INSIDE OF GEAR WELL ARE VISIBLE TO NAKED EYE BUT ARE COVERED BY DRAG BRACE PICK UP. THERE ARE HAIRLINE CRACKS IN SPAR AT DRAG BRACE PICK UP POINT WHICH ARE ALSO COVERED BY THE FITTING, MORE EASILY DISTINGU - [SDR CA110930013](https://openairdocs.org/sdr/CA110930013.md): Stringer · corroded · Sep 28, 2011 · Piper PA34200 · Fuselage Main, Longeron/Stringer > (CAN) WHEN REMOVING THE RT INBD FUEL TANK DUE TO A LEAK, CORROSION WAS NOTED ON THE FORWARD STRINGER, DIRECTLY BEHIND THE EXHAUST PIPE. THE CORROSION PRODUCED A HOLE THAT WAS APPROX 1.0" X 0.75". AN APPROVED REPAIR IS BEING CARRIED OUT. - [SDR CA110504008](https://openairdocs.org/sdr/CA110504008.md): Wheel Half · broken · May 2, 2011 · Piper PA34200 · Wheel/Ski/Float > (CAN) DURING TAXI, THE PILOT NOTED A STRONG VIBRATION FROM THE LANDING GEAR. THE PILOT SHUTDOWN THE ACFT ON THE TAXIWAY AND NOTED A PROBLEM WITH THE LT WHEEL, BRAKE. UPON INSPECTION BY AMO, IT WAS FOUND THAT A PIECE OF THE INNER WHEEL HALF HAD BROKEN FREE, AB - [SDR CA101217010](https://openairdocs.org/sdr/CA101217010.md): Tube · cracked · Dec 17, 2010 · Piper PA34200 · Heating System > (CAN) WHILE PERFORMING A PRESSURE DECAY TEST AS REQUIRED BY AD 2004-21-05 AN EXTENSIVE LEAK WAS DISCOVERED IN THE COMBUSTION TUBE. THE COMBUSTION TUBE WOULD NOT HOLD PRESSURE (6 PSIG) FOR MORE THAN A COUPLE OF SECONDS. UPON REMOVAL OF THE FORWARD DUCT A LARGE - [SDR ZB0R201000006](https://openairdocs.org/sdr/ZB0R201000006.md): Controller · frozen · Aug 2, 2010 · N15412 · Piper PA34200 · Propeller Controlling System > (ZB0R) DURING PREFLIGHT RUNUP, PILOT FOUND RT PROPELLER CONTROL TO BE FROZEN - WOULD NOT OPERATE. ACFT REPORTED TO MX. REPLACED RT PROPELLER CONTROL, PN 555-443. OPS CK GOOD - [SDR 2010FA0000483](https://openairdocs.org/sdr/2010FA0000483.md): Attach Bracket · corroded · May 18, 2010 · N737PE · Piper PA34200 · Horizontal Stabilizer, Attach Fittings > FOUND RT STABILATOR ATTACH BRACKET EXFOLIATED. - [SDR CA100805008](https://openairdocs.org/sdr/CA100805008.md): Torque Tube · broken · May 15, 2010 · Piper PA34200 · Rudder Control System > (CAN) TAXING FOR REFUELING PILOT REPORTED LOSS OF LT RUDDER FEEDBACK PRESSURE. AT INSP LT RUDDER CONTROL CABLE ARM WELD WAS FOUND TO BE BROKEN AT TORQUE TUBE. RUDDER BAR (TORQUE TUBE). - [SDR CA100115004](https://openairdocs.org/sdr/CA100115004.md): Rib · cracked · Jan 15, 2010 · Piper PA34200 · Trailing Edge Flaps > (CAN) DURING DISASSEMBLY FOR REPAIR TO THE FLAP ATTACH BRACKET, NOSE RIBS PN 62328-00 AND 62328-01 WERE FOUND TO BE CRACKED AT THE FLAP HINGE BRACKET ATTACH POINT. THIS BRACKET ALSO FORMS THE ATTACHING POINT FOR THE FLAP CONTROL ROD. BOTH LT AND RT FLAPS WE - [SDR CA091008002](https://openairdocs.org/sdr/CA091008002.md): Bolt · sheared · Oct 7, 2009 · Piper PA34200 · Wheel/Ski/Float > (CAN) WHILE TOWING THE ACFT, GROUND CREW NOTICED AN ABNORMAL SOUND COMMING FROM THE LT MAIN WHEEL. UPON INSP BY MX STAFF, THE LT WHEEL WAS FOUND TO HAVE 2 OUT OF 3 WHEEL-HALF BOLTS BROKEN. BOLTS WERE SHEARED AT THE HEAD. WHEEL ASSY WAS REMOVED. GEAR LEG AND A - [SDR CA090504006](https://openairdocs.org/sdr/CA090504006.md): Wire · chafed · Apr 29, 2009 · Piper PA34200 · Landing Gear System Wiring > (CAN) PILOT REPORTED THAT ON APPROACH TO LANDING, THE RT MAIN GEAR "DOWN AND LOCKED" LIGHT WAS UNSERVICEABLE. THE LANDING GEAR WAS CYCLED 3 TIMES BUT THE LIGHT JUST FLICKERED. THE PILOT THEN HAD THE CONTROL TOWER CHECK AND CONFIRM THAT THE GEAR WAS DOWN. A NOR - [SDR AHB2009F00000](https://openairdocs.org/sdr/AHB2009F00000.md): Switch · failed · Apr 20, 2009 · N42866 · Piper PA34200 · Exterior Lighting > THE LT LANDING LIGHT SWITCH SMOKED DURING FLIGHT. REMOVED SWITCH AND REPLACED WITH NEW SWITCH AND TESTED BOTH LANDING LIGHT CIRCUIT BREAKERS. THE PROBABLE CAUSE WAS THE 9107 HOURS ON THE SWITCH. (K) - [SDR CA090223016](https://openairdocs.org/sdr/CA090223016.md): Landing Gear · cracked · Feb 20, 2009 · Piper PA34200 · Nose/Tail Landing Gear > (CAN) CRACK FOUND DURING 400 HOUR ACFT INSP. SMALL CRACK FOUND WHEN INSPECTING NOSE LANDING GEAR. CRACK WAS AT THE ATTACHMENT POINT OF THE PIVOT CHANNEL FOR THE NOSE GEAR STEERING. PART REPLACED WITH OVERHAULED PART. - [SDR CA090223014](https://openairdocs.org/sdr/CA090223014.md): Mount · cracked · Feb 20, 2009 · Piper PA34200 · Engine Mount Section > (CAN) CRACK FOUND DURING A ROUTINE 400 HOUR INSP. REPLACEMENT PART ORDERED AND RECEIVED. CRACKED APPEARED TO BE NEW. TUBING CRACKED AND SEPARATED. CRACK APPEARED ON LWR PORTION OF ENGINE MOUNT WITHIN 1.5 CM OF WELD. - [SDR CA090302002](https://openairdocs.org/sdr/CA090302002.md): Pump · failed · Jan 16, 2009 · Piper PA34200 · Engine Fuel Pump > (CAN) INSTALLED OVERHAULED FUEL PUMP ON ACFT 30/01/08, PUMP FAILED 16/01/09. - [SDR CA090112006](https://openairdocs.org/sdr/CA090112006.md): Stud · broken · Jan 9, 2009 · Piper PA34200 · Reciprocating Engine Cylinder Section > (CAN) ON ROUTINE INSP, NR 4 CYL UPPER CTR HOLD DOWN STUD WAS FOUND SNAPPED OFF. THE CYL WAS REMOVED AND A WASHER WAS FOUND IN BETWEEN CYL AND CRANKCASE. THIS CAUSED CYL TO BE ON SLIGHTLY ANGLED CAUSING STRESS ON THE HOLD DOWN STUDS CAUSING ONE TO BREAK. EN - [SDR CA081113006](https://openairdocs.org/sdr/CA081113006.md): Wheel · cracked · Nov 7, 2008 · Piper PA34200 · Wheel/Ski/Float > (CAN) DURING A TIRE CHANGE, THE AME NOTICED A 4 INCH CRACK ALONG THE WHEEL, WHERE THE TIRE BEAD SITS. THIS TYPE OF FINDING IS RATHER UNUSUAL AT THE AMO. NO HARD OR UNUSUAL LANDINGS WERE REPORTED. THE WHEEL HALF WAS REPLACED, AND THE ACFT RETURNED TO SERVICE. - [SDR 2008FA0000707](https://openairdocs.org/sdr/2008FA0000707.md): Spar Cap · corroded · Oct 26, 2008 · N14258 · Piper PA34200 · Wing, Rib/Bulkhead > DURING ANNUAL INSPECTION, SEVERE INNER GRANULAR CORROSION WAS FOUND IN THE RIGHT WING, MAIN UPPER SPAR CAP AT THE AFT PORTION OF THE T-CAP, IN THE VICINITY OF THE WHEEL WELL IN PARTICULAR THE LOCATION OF WHEEL SPIN OFF. DURING TIME, CAUSED DAMAGE TO THE POINT - [SDR 2008FA0000192](https://openairdocs.org/sdr/2008FA0000192.md): Link Assy · sheared · Feb 18, 2008 · N1031U · Piper PA34200 · Landing Gear Retraction/Extension System > ACFT EXPERIENCED A NLG COLLAPSE UPON LANDING. INSPECTION OF ACFT, NLG DOWNLOCK LINK ASSY FOUND SHEARED NEAR ATTACHMENT TO DOWNLOCK ASSY BODY. IT IS NOT KNOW WHAT CAUSED THIS LINK ASSY TO SHEAR. DETERMINED THAT NOT ALL THE REQUIREMENTS OF AD 2005-13-16 WERE - [SDR EA25200803022](https://openairdocs.org/sdr/EA25200803022.md): Fitting · corroded · Dec 18, 2007 · N1031U · Piper PA34200 · Fuselage Main, Attach Fittings > DURING WINDSHIELD REPLACEMENT, MECHANIC NOTED STEEL FITTINGS AND ATTACHING HARDWARE WERE SUBSTANTIALLY CORRODED. FUNCTION OF FITTINGS IS ATTACHMENT OF FUSELAGE OVERHEAD A PILLAR TO FUSELAGE STRUCTURE PROPER. OTHER THAN SOME RIVETS THROUGH THE SKINS, THESE FITT - [SDR EA25200802753](https://openairdocs.org/sdr/EA25200802753.md): Fitting · corroded · Dec 18, 2007 · N1031U · Piper PA34200 · Fuselage Main, Attach Fittings > DURING WINDSHIELD REPLACEMENT, NOTED STEEL FITTINGS AND ATTACHING HARDWARE WERE SUBSTANTIALLY CORRODED. FUNCTION OF FITTINGS IS ATTACHMENT OF FUSELAGE OVERHEAD (A) PILLAR TO FUSELAGE STRUCTURE PROPER. OTHER THAN SOME RIVETS THROUGH THE SKINS, THESE FITTINGS AR - [SDR ZB0R20070009](https://openairdocs.org/sdr/ZB0R20070009.md): Rod End · separated · Dec 14, 2007 · N15412 · Piper PA34200 · Power Lever > IN CRUISE, PILOT ATTEMPTED TO REDUCE POWER FOR MANEUVERS PRACTICE. LT ENGINE WAS UNRESPONSIVE. INSTRUCTOR IDENTIFIED LT ENGINE THROTTLE PROBLEM, ENGINE RPM WAS STABLE AT NEAR FULL POWER. RETURNED TO HOME BASE. PILOT FEATHERED AND SHUTDOWN LT ENGINE ON APPROACH - [SDR ZB0R20070003](https://openairdocs.org/sdr/ZB0R20070003.md): Actuator · leaking · Oct 15, 2007 · N15412 · Piper PA34200 · Landing Gear Actuator > DURING GEAR MAINTENANCE, FOUND NLG ACTUATOR LEAKING. INSPECTION REVEALED WORN SEALS. REPLACED SEALS BUT STILL LEAKED. FURTHER INSPECTION WITH BORESCOPE IN BODY OF ACTUATOR REVEALED LONGITUDINAL SCORING ON INSIDE WALL OF ACTUATOR BODY. REPLACED ACTUATOR TO CORR - [SDR CA070803012](https://openairdocs.org/sdr/CA070803012.md): Torque Tube · broken · Jul 28, 2007 · Piper PA34200 · Rudder Control System > (CAN) THE LT RUDDER CABLE TORQUE TUBE CONNECTION BROKE OFF FROM THE TUBE. RUDDER CONTROL WAS LIMITED TO THE TRIM. (TC NR 20070803012) - [SDR FAA20070618001](https://openairdocs.org/sdr/FAA20070618001.md): Hub · failed · Jun 18, 2007 · N15156 · Piper PA34200 · Propeller Hub Section > ON JUNE 6,2007 PIPER SENECA N15156 WHILE IN CRUSE ON A TRAINING FLIGHT HAD A CATROSTRIFIC FAILRUE OF THE PROPELLER HUB CAUSING THE LOSS INFLIGHT OF ONE OF THE PROPELLER BLADES. THE FAILURE OF THE HUB WAS OF THE SAME KIND ADDRESSED IN AD2006-18-15 EXCEPT THE FA - [SDR 2007FA0000323](https://openairdocs.org/sdr/2007FA0000323.md): Drag Link · jammed · Mar 1, 2007 · N15338 · Piper PA34200 · Nose/Tail Landing Gear > THE NOSE GEAR LINK ASSEMBLY JAMS INTERMITTENTLY, KEEPING THE FWD AND AFT NOSE GEAR DRAG LINKS FROM LOCKING COMPLETELY. REFER TO SB NR 1123B. (K) - [SDR 2007FA0000144](https://openairdocs.org/sdr/2007FA0000144.md): Switch · frozen · Feb 5, 2007 · N1533E · Piper PA34200 · Landing Gear Retraction/Extension System > UPON LANDING, GEAR EXTENSION, DURING APPROACH TO LANDING, PILOT NOTED AN EXCEPTIONALLY LONG TIME BETWEEN GEAR SWITCH ACTUATION AND INDICATION OF ALL DOWN AND LOCKED. OUTSIDE TEMP +9 F. BELIEVE THAT SWITCH ARM FOR DOWNLOCK HAD FROZEN IN PLACE (UP) AND REQUIR - [SDR CA061227005](https://openairdocs.org/sdr/CA061227005.md): Crankshaft · cracked · Dec 18, 2006 · Piper PA34200 · Reciprocating Engine Power Section > (CAN) LT ENGINE DEVELOPED AN OIL LEAK FROM CRANKSHAFT SEAL. DURING SEAL REPLACEMENT, IT WAS NOTICED THAT THE CRANKSHAFT FLANGE WHERE PROPELLER BOLTS ON, WAS CRACKED FROM ONE LIGHTNING HOLE TO THE OTHER. IT LOOKED AS IF THERE WAS AN INDENTATION ON THE BACK SID Next page: https://openairdocs.org/model/piper-pa-34-200/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 aircraft_model_key = 'PA34200' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/piper-pa-34-200/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.