Cessna T310R

Service difficulty reports · 54

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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 = 'T310R'
  ORDER BY difficulty_date DESC"

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SDR 2026FA0000085Housing · misoverhauledTRIM TAB ACTUATOR HOUSING WAS IMPROPERLY DRILLED SEVERAL TIMES WHEN IT IS REQUIRED TO REUSE THE SAME HOLES WITHOUT ENLARGING AND REPLACE THE HOUSING IF THE HOLES CANNOT BE REUSED. FILLER AND PAINT HAD BEEN APPLIED TO COVER ADDITIONAL HOLES. VERY LITTLE MATERIAFeb 4, 2026 · N98869 · Cessna T310R · Elevator Tab Control SystemSDR 2022FA0000460Cylinder · bypassingDURING A COMPRESSION TEST, THE #3 CYLINDER HAD LOWER COMPRESSION THAN THE MASTER ORIFICE NUMBER. THE LOWER PLUG WAS REMOVED AND IT WAS COVERED IN OIL. BORESCOPE OF THE ENGINE REVEALED OIL IN THE CYLINDER. THE ENGINE HAD BEEN OVERHAULED BY A CRS 152.9 HOURS Jul 25, 2022 · N314BB · Cessna T310R · Powerplant SystemSDR 2022FA0000332Elt · usedTHIS SDR IS IN REGARDS TO AN ACK TECHNOLOGIES INC ELT, MODEL E-04, SERIAL NUMBER: 008372. ELT WAS REMOVED FROM THE AIRCRAFT FOR TESTING (ANNUAL INSPECTION). UPON ARMING THE ELT, A THREE SWEEP TONE WAS HEARD ON 121.5 MHZ. A SLAM TEST WAS PERFORMED, NO TRANSJul 7, 2022 · N1742E · Cessna T310R · Emergency EquipmentSDR 2022FA0000459Crankcase · destroyedAFTER CLIMBING TO 12000 FT FROM KCYS, THE AIRCRAFT TRANSITIONED TO CRUISE TO PREPARE FOR AERIAL SURVEY WORK. SHORTLY THEREAFTER, THE RE HAD A VIBRATION, POWER LOSS, AND STOPPAGE. THE AIRCRAFT WAS LANDING BACK AT KCYS WITHOUT INCIDENT. AFTER THE COWLING WAS RMay 13, 2022 · N314BB · Cessna T310R · Powerplant SystemSDR 2017FA0000550Motor · malfunctionedPILOT ATTEMPTED TO RETRACT GEAR, GEAR MOTOR CIRCUIT BREAKER TRIPPED. PILOT WAS ABLE TO SELECT GEAR DOWN AND PUSHED CIRCUIT BREAKER, GEAR EXTENDED AN LOCKED BEFORE CIRCUIT BREAKER TRIPPED AGAIN. UNEVENTFUL LANDING. TROUBLESHOT THE SYSTEM, FOUND GEAR MOTOR DRAug 3, 2017 · N4948A · Cessna T310R · Landing Gear Retraction/Extension SystemSDR CA141007007Cylinder Head · leaking(CAN) OWNER REPORTED A SMALL OIL LEAK ON BOTH ENGINES. UPON INVESTIGATING IT WAS FOUND THAT EACH ENGINE HAD A CRACKED CYLINDER HEAD. 4 CYLINDERS WERE REPLACED 90 HOURS PRIOR WITH THE SAME PROBLEM. LT CYLINDER NR 6 CRACKED ON INTAKE PORT WHERE YOU COULD SEE Oct 3, 2014 · Cessna T310R · Reciprocating Engine Cylinder SectionSDR CA130725001Cylinder Head · damaged(CAN) FOUND DURING UNSCHEDULED MAINTENANCE A BLUE STREAK ON COWLING. UPON FURTHER INVESTIGATION NR 5 CYLINDER LT ENGINE WAS FOUND TO BE LEAKING FUEL JUST ABOVE INTAKE PORT IN BETWEEN COOLING FINS. SOAP TEST PROVED TO SHOW IT WAS CRACKED FROM SPARK PLUG HOLE OVJul 24, 2013 · Cessna T310R · Reciprocating Engine Cylinder SectionSDR 2013FA0000166Bracket · brokenPILOT HEARD A LOUD BANG ON EXTENSION OF LANDING GEAR, RESULTING IN A GEAR UNSAFE INDICATION. ON LANDING RT MAIN GEAR COLLAPSED. INSPECTION REVEALED BROKEN TORQUE TUBE BRACKET.Mar 13, 2013 · N4941J · Cessna T310R · Main Landing GearSDR CA121130003Cylinder · cracked(CAN) SNAG FROM CUSTOMER WAS GREASE MARKS COMING FROM RIDE SIDE COWLING. WHEN COWLING WAS REMOVED, FOUND FUEL ON INTAKE BOLTS OF NR 5 CYLINDER. WITH A LIGHT, LOOKED DOWN THE FINS TO SEE BLUE STREAKS COMING FROM CYLINDER NEAR UPPER PART OF INTAKE PORT. FURTHNov 28, 2012 · Cessna T310R · Reciprocating Engine Cylinder SectionSDR 2012F00152Beam · perforatedREMOVED LEFT EXHAUST SYS FOR OVERHAUL AT REQUEST OF OPERATOR. FOUND MISSING & CORRODED RIVETS ON FIREWALL. SINGLE PIECE V-BAND CLAMPS WERE DISCOLORED CONSISTENT WITH EXHAUST LEAKAGE. INSPECTED ENGINE BEAMS AS REQUIRED BY AD 2000-01-16. FOUND FIREWALL SEALAAug 16, 2012 · N310SK · Cessna T310R · Nacelle/Pylon, Main FrameSDR 2012F00151Exhaust Pipe · crackedREMOVED RT ENGINE FOR O/H AT REQUEST OF OPERATOR. FOUND EXHAUST OVERBOARD PIPE, CRACKED APPROX 80 PERCENT AROUND THE CIRCUMFERENCE OF THE PIPE. FOUND CORRODED RIVETS IN FIREWALL. A NUMBER OF RIVETS WERE MISSING. THE FIREWALL WAS DARKENED WITH WHITE RESIDUEAug 16, 2012 · N310SK · Cessna T310R · Engine Exhaust SystemSDR 2007FA0000732Relay · failedAIRCRAFT EMERGENCY LANDED WITH COMPLETE ELECTRICAL FAILURE, LG EMERGENCY EXTENDED AND LANDED SAFELY. FOUND BATTERY RELAY FAILURE. UNIT REMOVED 200 AMP FOUND TO BE INCORRECT (PN). SB MEB99-4 ADDRESS THIS PROBLEM, HAD NOT BEEN COMPLIED WITH, CORRECT RELAY 100May 17, 2007 · N16EZ · Cessna T310R · Battery/Charger SystemSDR 2007FA0000105Spar Cap · corrodedLT TOP WING SPAR CAPS AND TOP SKINS SEVERELY CORRODED IN AREA OF FACTORY NACELLE FUEL BLADDERS. LT-PN 5122031-1.Feb 2, 2007 · N465DL · Cessna T310R · Wing SparSDR 2005FA0000770Rod · brokenDURING CRUISE FLT, ENG BEGAN TO VIBRATE SEVERELY AND PILOT SHUTDOWN. TEARDOWN AND INVESTIGATION REVEALED THE NR 2 ROD BROKE 1/2 WAY BETWEEN PISTON AND CRANK. IT IS SUSPECTED THIS ENG ENCOUNTERED LIQUID LOCK AT SOME TIME CAUSING A BENT ROD THAT EVENTUALLY FAIMay 19, 2005 · N6131X · Cessna T310R · Reciprocating Engine Power SectionSDR 2005FA0000427Cylinder Head · separatedDURING TAKEOFF PILOT NOTICED A SHUDDER OR VIBRATION. UPON LANDING ENGINE BEGAN TO RUN ROUGH. MAINTENANCE FOUND LT ENGINE NR 6 CYLINDER HEAD HAD SEPARATED. ENGINE WAS OVERHAULED ON 4-23-2004 AND PUT IN SERVICE ON 5-18-2004. THE ENGINE HAD 475 HOURS SINCE OVERMar 18, 2005 · N96HC · Cessna T310R · Reciprocating Engine Cylinder SectionSDR 2005FA0000235Exhaust Riser · crackedFOUND LT ENGINE OB EXHAUST RISER CRACKED WHILE PERFORMING A 50 HOUR EXHAUST INSPECTION IAW AD 00-01-16. (GL21200500869) (K)Nov 12, 2004 · N3731G · Cessna T310R · Engine Collector/Tailpipe/NozzleSDR CA040723003Wire · failed(CAN) TAKEOFF, LANDING GEAR FAILED TO RETRACT. GEAR CB POPPED IMMEDIATELY ON SELECT UP, CAUSED 3 GREEN (SAFE GEAR) LIGHTS TO GO OUT. THE CB WAS RESET, IMMEDIATELY RE-POPPED. MOMENTARY 3 GREEN INDICATION OF LIGHTS WHEN BREAKER WAS RESET INDICATING GEAR WAS STJul 12, 2004 · Cessna T310R · Landing Gear System WiringSDR 11518Hub · crackedWHEEL REPLACED DUE TO THE FACT WE HAVE FOUND MANY HUBS CRACKED ON THREE PIECE MCCAULEY WHEELS. WE FOUND THE CRACKS AFTER THE WHEEL WAS REMOVED AND COMPLETELY TAKEN APART. RECOMMEND ALL THREE PIECE MCCAULEY WHEELS BE COMPLETELY DISASSEMBLED FOR INSPECTION IMMEDAug 19, 2002 · N500CH · Cessna T310R · Wheel/Ski/FloatSDR 2002FA0000840Window · departedEMERGENCY WINDOW EXIT DEPARTED AIRCRAFT IN FLIGHT, IN RAIN SHOWER. ALL CABLE PINS BENT. VERY DIFFICULT TO SEE WITH INTERIOR INSTALLED.Jun 14, 2002 · N87RJ · Cessna T310R · Emergency ExitsSDR 2002FA0000629Control Cable · brokenALL FOUR CONTROL CABLES HAD STRANDS BROKEN. THE LEFT FORWARD CARRY THRU CONTROL CABLE HAD APPROXIMATELY 70 PERCENT OF ITS STRANDS BROKEN DUE TO CONTACT WITH PULLEY GUARD. THE OTHER PROBLEM IS WHERE CONTROL CABLES COME OUT OF FUSELAGE RUBBING ON PHENOLIC BLOCApr 29, 2002 · N310RH · Cessna T310R · Aileron Control SystemSDR 2001FA0000158Valve · inoperativeDURING INSTALLATION OF AIRCRAFT SURFACE KNOWN ICE KIT FOUND SURFACE DEICE FLOW VALVE #2H59-8 (MFG. BY PARKER HANNIFIN, AIRBORNE) S/N 9AT-83 TO CAUSE UNCOMMANDED DEICE BOOT INFLATIONS. INSTALLED SECOND NEW VALVE S/N 9AT-91 OBTAINED FROM A DIFFERENT DISTRIBUTORMay 22, 2001 · N310KH · Cessna T310R · Airfoil Anti/De-ice SystemSDR 20010418CW006Jam-Nut · crackedGOVERNOR JAM NUT AS INSTALLED BY OVERHAULER RESULTED IN CRACKED STOP WHEN ADJUSTED AND RETIGHTENED. GOVERNOR STOP ARM HAS A FLAT SURFACE AND CURVED SURFACE THROUGH WHICH THE STOP BOLT IS ATTACHED. TRADITIONALLY WE HAVE SEEN THE JAM NUT ON THE FLAT SURFACE. Mar 27, 2001 · N5466J · Cessna T310R · Propeller GovernorSDR 20001011SH006Pump · failedDURING FLIGHT, PILOT NOTICED RIGHT LANDING LIGHT CIRCUIT BREAKER OPEN. AFTER LANDING, INSP FOUND LEFT TIP TANK FUEL TRANSFER PUMP P/N 476411 FAILED ELECTRICALLY. PUMP SHOWED SIGNS OF HEAT AND ARCING ON OUTSIDE OF CASE FROM INTERNAL FAILURE. THIS PUMP IS WIOct 7, 2000 · N310BA · Cessna T310R · Fuel Boost PumpSDR 20000731SH021Blade · scratchedTHE BLADE WAS REJECTED DUE TO SCRATCHES IN THREADS PER MCAULEY SB 150. (X)Jul 13, 2000 · N5466J · Cessna T310R · Propeller Blade SectionSDR 20000731SH020Blade · scratchedTHE BLADE WAS REJECTED DUE TO SCRATCHES IN THREADS PER MCAULEY SB 150. (X)Jul 13, 2000 · N5466J · Cessna T310R · Propeller Blade SectionSDR 20000731SH019Blade · scratchedTHE BLADE WAS REJECTED DUE TO SCRATCHES IN THREADS PER MCAULEY SB 150. (X)Jul 13, 2000 · N5466J · Cessna T310R · Propeller Blade SectionSDR 20000731SH018Blade · scratchedTHE BLADE WAS REJECTED DUE TO SCRATCHES IN THREADS PER MCAULEY SB 150. (X)Jul 13, 2000 · N5466J · Cessna T310R · Propeller Blade SectionSDR 20000731SH017Blade · scratchedTHE BLADE WAS REJECTED DUE TO SCRATCHES IN THREADS PER MCAULEY SB 150. (X)Jul 13, 2000 · N5466J · Cessna T310R · Propeller Blade SectionSDR 20000731SH016Blade · scratchedTHE BLADE WAS REJECTED DUE TO SCRATCHES IN THREADS PER MCAULEY SB 150. (X)Jul 13, 2000 · N5466J · Cessna T310R · Propeller Blade SectionSDR 20000505SH023Valve Guide · wornVERY LOW COMPRESSION NOTED IN THE NR 3 CYL ON RT ENGINE DURING ANNUAL INSP. THE CYL REMOVED AND INSPECTED. THE EXHAUST VALVE GUIDE WAS WORN TO THE POINT WHERE THE VALVE COULD NOT SEAT PROPERLY. CYL REQUIRED BOTH VALVES AND VALVE GUIDES TO BE REPLACED. RE-ASApr 5, 2000 · N310HD · Cessna T310R · Reciprocating Engine Cylinder SectionSDR 2000ZZZX366Inverter · failedDURING FINAL FOR ARTESIA, NM (ATS) PILOT REPORTED SMOKE IN COCKPIT. ON INSPECTION, FOUND ENGINE SWITCH AND PANEL LIGHTS CIRCUIT BREAKER TRIPPED. TROUBLESHOT SYSTEM AND FOUND 28VDC TO 115VAC INVERTER BURNED OUT AND SEALANT DRIPPING. INVERTER WAS REPLACED 8-2Jan 21, 2000 · N828P · Cessna T310R · Flight Compartment LightingSDR 2000ZZZX257Pump · failedOWNER NOTIFIED THAT LEFT LANDING LIGHT/TIP TANK TRANSFER PUMP CIRCUIT BREAKER OPENED. FOUND TIP TANK TRANSFER PUMP FAILED ELECTRICALLY. UNIT SHOWS SIGNS OF ARCING AND OVERHEATING AT POWER WIRE INLET AREA. UNIT HAD BEEN REPLACED 15.7 HOURS PREVIOUSLY. THIS Dec 20, 1999 · N5255C · Cessna T310R · Fuel Boost PumpSDR 2000ZZZX61Stack · mismanufacturedTHIS NEW FAA-PMA PART WAS NOT FORMED PROPERLY AND COULD NOT BE INSTALLED WITHOUT CAUSING UNDUE STRESS ON MATING PARTS. THE PART WAS TAGGED AND RETURNED TO DISTRIBUTOR AND ANOTHER NEW PART ORDERED FOR THE AIRCRAFT. (THE ANGLE OF THE BEND IN THE PIPE WAS NOT CODec 6, 1999 · N376J · Cessna T310R · Engine Collector/Tailpipe/NozzleSDR 2000ZZZX60Slip Joint · crackedPART WAS FOUND CRACKED 330 DEGREES AROUND WELD AND WAS VISIBLE BY OPENING THE OUTBOARD COWLING DOOR.Dec 6, 1999 · N376J · Cessna T310R · Engine Cowling SystemSDR 2000ZZZX59Stack · misinstalledCOUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK. AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQUENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT. THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATERIAL AND IS LOCATED Dec 6, 1999 · N376J · Cessna T310R · Engine Collector/Tailpipe/NozzleSDR 2000ZZZX58Stack · misinstalledCOUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK. AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQUENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT. THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATERIAL AND IS LOCATED Dec 6, 1999 · N376J · Cessna T310R · Engine Collector/Tailpipe/NozzleSDR 2000ZZZX57Header · damagedCOUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK. AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQUENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT. THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATERIAL AND IS LOCATED UDec 6, 1999 · N376J · Cessna T310R · Engine Collector/Tailpipe/NozzleSDR 2000ZZZX56Stack · damagedCOUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK. AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQUENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT. THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATERIAL AND IS LOCATED Dec 6, 1999 · N376J · Cessna T310R · Engine Collector/Tailpipe/NozzleSDR 2000ZZZX55Engine Beam · corrodedENGINE BEAM FOUND SEVERELY CORRODED FROM EXPOSURE TO HOT EXHAUST GASSES DUE TO LEAKING EXHAUST PIPE FLANGES AND CLAMPS. OTHER DAMAGE FOUND INVOLVED THE FIREWALL ACCESS PANEL WHICH COVERS THE FUEL CROSSFEED LINE IN WHICH MOSTLY ALL OF THE ATTACHING SCREW HEADSDec 6, 1999 · N376J · Cessna T310R · Engine Mount SectionSDR 2000ZZZX54Header · damagedCOUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK. AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQUENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT. THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATERIAL, AND IS LOCATEDDec 6, 1999 · N376J · Cessna T310R · Engine Collector/Tailpipe/NozzleSDR 2000ZZZX222Tail Pipe · buckledUPON COMPLETION OF AD 75-23-08-R5 NOTED TAIL PIPE SEVERELY BUCKLED. TOTAL TIME 1,436.0 HOURS. INSTALLED KNISLEY STC SA 00040LB. OPS CHECKED SYSTEM, NO DEFECTS FOUND.Nov 29, 1999 · N5038J · Cessna T310R · Engine Collector/Tailpipe/NozzleSDR 99ZZZX510Dipstick · brokenDIPSTICK BECAME SEPARATED FROM CAP ALLOWING THE DIPSTICK AND SPRING TO DROP INTO DIPSTICK TUBE. THERE ARE FOUR TUBES BUILT INTO THE CAP AND 3 OF THE 4 WERE BROKEN. THE NEW PART NUMBERED DIPSTICK IS MANUFACTURED TO ALLEVIATE THIS FROM HAPPENING AGAIN BY NOT Jan 7, 1999 · N711ED · Cessna T310R · Reciprocating Engine Oil SystemSDR 99ZZZX1026Line · corrodedPILOT REPORTED THE SMELL OF FUEL IN COCKPIT ONCE CABIN COMBUSTION HEATER WAS TURNED ON. PILOT SHUT DOWN HEATER AND LANDED. UPON INSPECTION OF HEATER INSTALLATION IN NOSE COMPARTMENT, FUEL WAS FOUND 'POOLED'. THE FUEL LINE FROM COMBUSTION HEATER FUEL PUMP TO Dec 23, 1998 · N6177X · Cessna T310R · Heating SystemSDR 98ZZZX2615Bolt · failedAIRCRAFT INSPECTED FOR THE CAUSE OF THE RIGHT MAIN LANDING COLLAPSE ON LANDING. FOUND THAT PARTS OF THE BELLCRANK ASSEMBLY (P/N 5041001-12) HAD FAILED. THE BOLT (P/N NAS464P4-26) AT THE UPPER END OF THE BELLCRANK HAD BROKEN AND THE END-FITTING (P/N 0841111-3Dec 28, 1997 · N310RH · Cessna T310R · Landing Gear Retraction/Extension SystemSDR 98ZZZX2614Fitting · failedAIRCRAFT INSPECTED FOR THE CAUSE OF THE RIGHT MAIN LANDING COLLAPSE ON LANDING. FOUND THAT PARTS OF THE BELLCRANK ASSEMBLY (P/N 5041001-12) HAD FAILED. THE BOLT (P/N NAS464P4-26) AT THE UPPER END OF THE BELLCRANK HAD BROKEN AND THE END-FITTING (P/N 0841111-3Dec 28, 1997 · N310RH · Cessna T310R · Landing Gear Retraction/Extension SystemSDR 98ZZZX2613Bellcrank · failedAIRCRAFT INSPECTED FOR THE CAUSE OF THE RIGHT MAIN LANDING COLLAPSE ON LANDING. FOUND THAT PARTS OF THE BELLCRANK ASSEMBLY (P/N 5041001-12) HAD FAILED. THE BOLT (P/N NAS464P4-26) AT THE UPPER END OF THE BELLCRANK HAD BROKEN AND THE END-FITTING (P/N 0841111-3Dec 28, 1997 · N310RH · Cessna T310R · Landing Gear Retraction/Extension SystemSDR 97ZZZX4248Spring · brokenENGINE RUNNING ROUGH. EXHAUST VALVE LEAKING ON COMPRESSION TEST. FOUND OUTER SPRING BROKEN 180 HOURS S.F.R.Sep 17, 1997 · Cessna T310R · Reciprocating Engine Cylinder SectionSDR 97ZZZX2928Header Assy · hole burnedSPECIAL INSPECTION OF EXHAUST SYSTEMS IAW AD 75-23-08-R5 AND CESSNA PILOTS ASSOCIATION LETTER 4-28-97 (URGENT LETTER TO OWNERS OF TURBOCHARGED TWIN CESSNAS). THE HEADER HAD A HOLE BLOWN IN V-BAND CLAMP AREA. THE BAFFLE IN HEADER WAS WARPED FROM HEAT AND CRACJun 12, 1997 · N777V · Cessna T310R · Exhaust TurbochargerSDR 97ZZZX630Trim Arm · misindexedELEVATOR TRIM INDICATOR ARM FREQUENTLY BECOMES MISINDEXED GIVING ERRONEOUS TRIM SETTING INDICATIONS. A PILOT'S KNEE, RESTING AGAINST THE TRIM WHEEL, CAN DISPLACE THE WHEEL ENOUGH TO CAUSE THE TRIM ARM TO MOVE OUT OF THE SPIRAL GROOVE AND INTO ANOTHER GROOVE. Jan 27, 1997 · N4949A · Cessna T310R · Rudder Control SystemSDR 96ZZZX3225Bearing · failedWHILE INSPECTING NOSE LANDING GEAR RODS AND ATTACHMENTS, FOUND NEEDLE BEARINGS SHOWING AND ROD END SITTING HIGHER THAN NORMAL IN THE IDLER BELLCRANK. REMOVED BOLT RETAINING THE PUSH/PULL ROD AND FOUND BEARING RETAINER SHEARED ON THE UPPER SECTION OF BEARING.May 1, 1996 · N6126C · Cessna T310R · Landing Gear Retraction/Extension System
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