AiResearch TPE331 series

Service difficulty reports · 394

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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 engine_model_key = 'TPE331'
  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 JIKA2026041701Engine · flamed outON FINAL APPROACH THE NR 2 ENGINE EXPERIENCED A FLAME OUT CONDITION AND THE PILOT WAS ABLE TO LAND THE AIRCRAFT SAFELY WITH ONLY POWER FROM THE #1 ENGINE. A GENERAL VISUAL INSPECTION OF THE FIRST STAGE COMPRESSOR SECTION REVEALED NO DAMAGE. A GENERAL VISUAL INApr 4, 2026 · N672AV · Swrngn SA227AC · Engine (Turbine/Turboprop)SDR JIKA2026012601Hydraulic Line · damagedWHILE PREPARING TO EXTEND THE LANDING GEAR, THE FLIGHT CREW NOTED THAT BOTH HYDRAULIC LOW-PRESSURE LIGHTS WERE ILLUMINATED. QRH PROCEDURES WERE FOLLOWED AND THE LANDING GEAR WAS MANUALLY ACTUATED TO THE DOWN AND LOCKED POSITION. THE LANDING WAS UNEVENTFUL AND Jan 19, 2026 · N241DH · Swrngn SA227AT · Hydraulic System, MainSDR JIKA2026012301Trim System · out of alignmentDURING CLIMB, THE FLIGHT CREW NOTED THAT THE AIRCRAFT ROLLED TO THE LEFT AND REQUIRED FULL INPUT TO LEVEL OFF THE WINGS. THE CREW CALLED IT IN, AND AIR RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT THE SYSTEM, CHECKED ALL FLIGHT CONTROL CABLES FORJan 6, 2026 · N31704 · Beech 1900C · Flight Control SystemSDR JIKA2025123001Hydraulic Line · chafedDURING FLIGHT AFTER SHORTY AFTER LEVEL OFF, THE FLIGHT CREW EXPERIENCE A LOW HYDRAULIC PRESSURE MALFUNCTION AND AIR RETURNED BACK TO BASE. THE EMERGENCY LANDING GEAR HANDLE WAS MANUALLY ACTUATED DUE TO THE FAILURE AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDEDec 24, 2025 · N422MA · Swrngn SA227AC · Hydraulic System, MainSDR KY7A202504220038Engine · unknownAIRCRAFT INTAKE ICING INGESTION DURING TAXI IN. WAITING ON MECHANIC'S FINDINGS, WHICH WILL BE REPORTED AT A LATER DATE.Apr 18, 2024 · N425MA · Swrngn SA226TC · Engine (Turbine/Turboprop)SDR 2023FA0000612Hinge Bracket · crackedA CRACK WAS OBSERVED IN THE LOWER PART OF THE BRACKET HINGE POINT HORIZONTAL, IT WAS DISCOVERED DURING A ROUTINE INSPECTION, THE CRACK SEEMS TO BE PRODUCT OF THE MATERIAL LOSS CAUSED BY RUBBING TOOLS AGAINST THE FILLET, TOOLS ARE USED TO TORQUE THE ADJACENT BOOct 19, 2023 · N3256 · Beech B100 · Horizontal Stabilizer Miscellaneous StructureSDR 2022F00202None · noneLEFT ENGINE FIRE WARNING LIGHT CAME ON IN CRUISE FLIGHT. ALL ENGINE PARAMETERS WERE NORMAL. THE CREW DECLARED AN EMERGENCY AND DIVERTED. THE LEFT ENGINE WAS SHUT DOWN PER EMERGENCY CHECKLIST AND THE AIRCRAFT SUCCESSFULLY LANDED SINGLE ENGINE IN KSHV. NO VISIBLApr 26, 2022 · N852DR · Frchld SA227DC · Fire Protection SystemSDR UATA071320207800Heat Shield · crackedUPON SCHEDULED INSPECTION, FOUND L/H EXHAUST DUCT SHROUD/HEAT SHIELD CRACKED AT THE O/B AFT END. THE CRACK WAS APPROXIMATELY 6" LONG, AND RAN ALONG A ROW OF RIVETS IN A FORWARD DIRECTION.Jul 8, 2020 · N352CA · Casa C212CC · Engine Collector/Tailpipe/NozzleSDR JIKA202006231601Case · leakingON CLIMB OUT, RIGHT ENGINE OIL TEMP GAUGE WENT TO THE RED LINE AND HELD. AFTER A FEW MINUTES THE OIL TEMPERATURE WENT PAST THE RED LINE AND PRESSURE BEGAN TO DROP. PILOT SHUT DOWN THE ENGINE PER AMF PROCEDURES AND INFORMED CANCUN APPROACH, RIGHT ENGINE WAS SHJun 16, 2020 · N241DH · Swrngn SA227AT · Turbine Engine Oil SystemSDR KY7A201912052001Wire · brokenPILOT REPORTED PARTIAL POWER LOSS IN FLIGHT, PILOT ACTIVATED CONTINUOUS IGNITION WHICH RESTORED POWER. AUTO IGNITION DID NOT OPERATE PROPERLY. MX PERFORMED NTS GROUND CHECK IAW TPE331 MM CHAPTER 72-00-00 TROUBLE-SHOT SYSTEM AUTO IGNITION SWITCH NOT EXTINGUISHIDec 2, 2019 · N31171 · Swrngn SA227AC · Ignition System WiringSDR UATA2019112760101Blade · slippedINSPECTION OF THE SLIPPAGE WITNESS STRIPE SHOWED THAT ONE BLADE OF THE PROPELLER SLIPPED ROTATIONALLY IN THE BLADE TO HUB CLAMP, CAUSING THENov 26, 2019 · N352CA · Casa C212CC · Propeller Blade SectionSDR JIKA2019120200501Overheat Sensor · defectiveSHORTLY AFTER TAKEOFF FROM DFW, RIGHT ENGINE OIL TEMP EXCEEDED TOLERANCES OVER HIGH RED LINE. PILOT PERFORMED PRECAUTIONARY ENGINE SHUT DOWN, ATC DECLARED AN EMERGENCY. AIRCRAFT LANDED BACK AT DFW WITH NO INCIDENT. MAINTENANCE REMOVED AND REPLACED OIL TEMPERANov 25, 2019 · N241DH · Frchld SA227CC · Engine Oil Indicating SystemSDR CA190725008Pin · sheared(CAN) NOSE GEAR UPPER SCISSOR LINK SPRING PIN FOUND SHEARED AND SHAFT WAS MIGRATING OUT OF SCISSOR LINK. FLEET CAMPAIGN WAS CONDUCTED AND ONE MORE ROLL PIN WAS FOUND SHEARED. ROLL PINS REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC# 20190725008)Jul 14, 2019 · Swrngn SA227AC · Nose/Tail Landing GearSDR KY7A2019040435001Nozzle · brokenCARRIER RECIEVED REPORT OF BAD SOAP SAMPLE. CARRIER DISASSEMBLED ENGINE GEARARBOX AND FOUND BROKEN OIL NOZZLE ASSEMBLY IN INTERMEDIATE HOUSING AND GEAR ASSEMBLY - ACCESSORY GEAR AND DRIVE IDLER HOUSING ASSEMBLY.Mar 14, 2019 · N820DC · Frchld SA227DC · Turbine Engine Reduction GearSDR JIKA201902201501Engine · making metalMAINTENANCE DISCREPANCY: THE PILOT REPORTED WHILE IN CRUISE FLIGHT THAT THE L\H ENGINE CHIP DETECTOR LIGHT ILLUMINATED. THE PILOT FOLLOWING PROCEDURES PERFORMED AN IN-FLIGHT SHUT DOWN OF THE LEFT ENGINE. THEN THE PILOT DECLARED AND EMERGENCY AND REQUESTED TO RFeb 15, 2019 · N556UP · Swrngn SA227AT · Engine (Turbine/Turboprop)SDR 2020FA0000078Spur Gear · fracturedGEAR PN 896884-1 APPARENTLY FRACTURED AT THE KEYWAY ALLOWING THE MAIN SHAFT DRIVE TO THE FUEL CONTROL DRIVE TRAIN TO BECOME DISENGAGED CAUSING AN UNCOMMANDED ENGINE SHUTDOWN DUE TO LACK OF FUEL.Nov 19, 2018 · N40KC · Mtsbsi MU2* · Fuel Controlling SystemSDR FJTA17124871B-Nut · looseCREW REPORTED AFTER DEPARTURE FROM MDW AT APPROXIMATELY 3000' THE RT ENG OIL LT CAME ON AND OIL PRESS READ ZERO. PERFORMED RH ENG SHUTDOWN AND RETURNED TO MDW. BEFORE LANDING, THE CREW REQUESTED EMERGENCY EQUIPMENT TO BE STANDING BY. AIRCRAFT LANDED WITHOUT Dec 8, 2017 · N487UE · Bag JETSTM3201 · Turbine Engine Oil SystemSDR JIKA2017062201Limiter · intermittentDURING CRUISE, THE RT ENGINE BEGAN TO LOSE POWER. THE RT ENGINE STARTED TO BYPASS FUEL LOWER THAN NORMAL EGT TEMPERATURE. REDUCED POWER AND THE AFFECTED ENGINE QUIT BYPASSING. APPLIED POWER, & RT ENGINE EGT INCREASED AND THE ENGINE BYPASSED AGAIN. FOLLOWED QJun 22, 2017 · N709TR · Swrngn SA227AC · Engine (Turbine/Turboprop)SDR JIKA2017052202Engine · power lossDURING DESCENT, AND WHEN THE ENGINE POWER WAS REDUCED ON THE RIGHT ENGINE, FOUND THE POWER LEVER UNRESPONSIVE. DISCONTINUED THE APPROACH TO TROUBLESHOT THE ISSUE WITH VFR. FOLLOWING THE PROCEDURE FOR ENGINE CONTROL MALFUNCTION CHECK LIST, WAS STILL UNABLE TMay 22, 2017 · N152AF · Swrngn SA227AC · Engine (Turbine/Turboprop)SDR BIGA20160531001Tube · misalignedTHE PILOT NOTED A LT ENG OIL PRESS FLUCTUATION, THEN DURING CLIMB TO 2000 FT, THEN THE LOW OIL PRESS LIGHT CAME ON & TORQUE FLUCTUATION OCCURRED. THE PILOT PERFORMED AN INFLIGHT SHUTDOWN & RETURNED. LANDED WITHOUT INCIDENT. PERSONNEL FOUND THE OIL TUBE, PN May 27, 2016 · N107BH · Casa C212CC · Engine Oil Indicating SystemSDR 2016FA0000220Hinge Bracket · corrodedRT INBD AILERON HINGE BRACKET FOUND TO HAVE EXFOLIATION CORROSION AT AIRFRAME ATTACH POINT, REQUIRING REPLACEMENT OF PART. OTHER CONTROL SURFACE HINGES/ATTACH BRACKETS INSPECTED WITH NO DEFECTS.May 10, 2016 · N217BH · Casa C212CD · Wing, Control Surface Attach FittingsSDR CA150814005Thrust Bearing · damaged(CAN) DURING PRODUCTION ACCEPTANCE TESTING, THE THRUST BEARING, 1415-336 WAS FOUND TO EXHIBIT EXCESSIVE WEAR AFTER 1.5 HR TEST PERIOD. THIS BEARING IS USED IN CONTROLLING THE SPEED IN THE OPERATION OF THE CSSA GOVERNOR, CONSTANT SPEED SINGLE ACTING, CSSA, PROAug 12, 2015 · Propeller GovernorSDR JKGC20150604001Servo · damagedPILOT FELT VIBRATION IN YOKE, MADE PRECAUTIONARY LANDING. RT ELEVATOR SERVO, SERVO CONTROL ROD & ELEVATOR SKINS SUSTAINED DAMAGE.Jun 4, 2015 · N3125N · Dhav DHC3 · Elevator Control SystemSDR 39LA20150501135Escape Hatch · departedDURING TAKEOFF ROLL, THE TOP ESCAPE HATCH DEPARTED THE ACFT. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT & RETURNED TO PARKING.May 1, 2015 · N620AR · Casa C212DF · Emergency ExitsSDR 39LA20150224109Shaft · shearedDURING THE WALK AROUND INSPECTION PRIOR TO FLIGHT, MX OBSERVED THAT THE LT & RT ELEVATORS WERE DEFLECTED IN OPPOSITE DIRECTIONS. FURTHER INVESTIGATION REVEALED THAT THE LT ELEVATOR INTERCONNECT SHAFT HAD SHEARED. THERE WERE REPORTS OF HIGH WIND CONDITIONS INFeb 24, 2015 · N607AR · Casa C212200 · Elevator Control SystemSDR 39LA20150203106Light · malfunctionedAT CRUISE FLIGHT DURING NIGHT VISION GOGGLE TRAINING THERE WAS AN ORDER OF SMOKE IN THE FLIGHT DECK. THE COPILOTS SIDE OF THE OVERHEAD PANEL WAS HOT TO THE TOUCH IN THE VICINITY OF THE LIGHT SWITCHES & RHEOSTATS. FLIGHT DECK LIGHTING WAS EXTINGUISHED & THE OFeb 3, 2015 · N604AR · Casa C212200 · Flight Compartment LightingSDR 39LA20150115105Unknown · smokeDURING CLIMB OUT AT APPROX 10,000 FT MSL THE FLIGHT CREW REPORTED A STRONG SMOKE SMELL IN THE FLIGHT DECK FOLLOWED BY A PLUME OF SMOKE RISING FROM THE FLOOR BENEATH THE FIRST OFFICER`S RUDDER PEDALS. THE FLIGHT CREW ACCOMPLISHED THE EMER CHECKLIST FOR SMOKE EJan 15, 2015 · N620AR · Casa C212DF · Air Distribution SystemSDR CA141104006Indicator · reads high(CAN) COPILOTS ASI READS 85 KTS HIGHER THAN PILOTS ASI. INDICATOR REPLACED AND GROUND CHECKER SERVICEABLE. ACFT RETURN TO SERVICE.Oct 7, 2014 · Swrngn SA227AC · Airspeed/Mach IndicatorSDR 39LA2014060900005Propeller · splitIN CRUISE FLIGHT HEARD A LOUD BANG. SCANNED THE ENG INSTRUMENTS, THE LT TORQUE GAUGE WAS AT 120%, THE LT EGT HAD DROPPED BY APPROXIMATELY 100 DEGREES & THE LT FUEL FLOW HAD DROPPED TO 215 PPH FROM 300PPH. THERE WAS NO OTHER INDICATIONS OF A PROBLEM. PULLEDJun 9, 2014 · N969BW · Casa C212200 · Propeller Blade SectionSDR 8EKA20140327Engine · bird ingestionBIRD STRIKE ON NR 2 ENG. WAITING FOR OFFICIAL REPORT FROM FLT CREW & MAINTENANCE. ENG CHANGE CURRENTLY IN PROCESS. SUPPLEMENTAL INFORMATION WILL BE PROVIDED UPON RECEIPT OF OFFICIAL REPORT & MAINTENANCE LOGS FOR ENG CHANGE MOC FLIGHT.Mar 16, 2014 · N502FS · Casa C212 · Engine (Turbine/Turboprop)SDR 39LA2014022860Connector · damagedDURING CRUISE FLIGHT FROM OASH TO OAIX THE FLIGHT CREW COULD SMELL HOT ELECTRICAL FUMES IN THE FLIGHT DECK. THE QRH WAS COMPLIED WITH, & THE SOURCE OF THE ELECTRICAL SMELL COULD NOT BE DETERMINED. THE FLIGHT WAS COMPLETED WITHOUT FURTHER INCIDENT. FOUND LOOFeb 28, 2014 · N607AR · Casa C212CD · Ice/Rain Protection System WiringSDR 39LA2014022459Unknown · fumesDURING CRUISE FLIGHT FROM OAMS TO OAIX THE FLIGHT CREW EXPERIENCED FUMES IN THE FLIGHT DECK. O2 MASKS WERE DONNED BY THE CREW & THE QRH WAS COMPLIED WITH. THE ELECTRICAL SYSTEMS WERE CHECKED WITH NO DISCREPANCIES NOTED. ENG BLEED VLVS WERE CLOSED & THE FUMEFeb 24, 2014 · N607AR · Casa C212CD · Air Distribution SystemSDR 8EKA20140305001Mount · deformedDURING POST FLIGHT INSPECTION, FOUND ENG ISOLATOR MOUNT PAD TO BE DEFORMED AFTER 13.6 HOURS IN USE. THIS UNIT WAS REPLACED PREVIOUSLY ON 01/06/2013 DUE TO DE-BONDING FROM FUEL & OIL CONTAMINATION.Jan 18, 2014 · N348CA · Casa C212CC · Engine Mount SectionSDR 39LA2013121930Frame · crackedFRAME 27F, STATION 12615 BETWEEN STRINGER 1L & 1R IS CRACKED IN RADIUS BEYOND LIMITS. REPLACED FRAME 27F AT STATION 12615 IAW AIRLIFT EO 2013047-311 PARA 8 41 REV B.Dec 19, 2013 · N620AR · Casa C212DF · Fuselage Main, FrameSDR 39LA2013121931Skin · dentedMULTIPLE DENTS IN FUSELAGE CTR BELLY SKIN AROUND FS 4670. FABRICATED REPAIR DOUBLER & INSTALLED IAW CASA 212-300SRM APPENDIX II, FIG B7 & EO 2013047-311 PARA 8 39 REV B.Dec 19, 2013 · N620AR · Casa C212DF · Fuselage Main, Plate/SkinSDR 39LA2013121932Skin · dentedRIGHT SIDE FUSELAGE SKIN DENTED SEVERAL PLACES BETWEEN FS 3550 - 3950 ABOVE & BELOW STRINGER 7R. R & R RT SIDE FUSELAGE SKIN AT FS 3550 - 3950 ABOVE & BELOW STRINGER 7 RT, FABRICATED NEW REPAIR PARTS IAW DRAWING 13047-2048 REV V MATERIAL SPEC 040 INCHES 2024-TDec 19, 2013 · N620AR · Casa C212DF · Fuselage Main, Plate/SkinSDR 39LA2013121933Skin · dentedLEFT SIDE FUSELAGE SKIN HAS A DENT BETWEEN FS 3950 - 4310, BELOW STRINGER 18L. R & R SKIN AT FS 3550 & FS 3950 BELOW STRINGER 18L IAW EO 2013047-311 PARA 8 19 REV B.Dec 19, 2013 · N620AR · Casa C212DF · Fuselage Main, Plate/SkinSDR 39LA2013121934Skin · dentedDENT ON LOWER SKIN OF LT HORIZONTAL STABILIZER STATION HSS3620. REPAIRED DAMAGED AREA ON LOWER SKIN OF LT HORIZONTAL STABILIZER BY INSTALLING A DOUBLER STATION HSS3620, IAW AAR DRAWING 13047-2043 REV IR.Dec 19, 2013 · N620AR · Casa C212DF · Horizontal Stabilizer, Plate/SkinSDR 39LA2013121935Support Channel · corrodedRIGHT SEAT TRACK SUPPORT CHANNEL BETWEEN FS 2400 & FS 2960 HAS HEAVY CORROSION AROUND ATTACHMENTS. REPLACED SEAT TRACK SUPPORT CHANNEL BETWEEN FS 2400 & 2960 IAW EO 2013047-311 PARA 8 33 REV B.Dec 19, 2013 · N620AR · Casa C212DF · Fuselage, Seat/Cargo Attach FittingsSDR 39LA2013121936Skin · dentedLEFT WING LOWER SKIN DENTED OTBD OF EXISTING REPAIR. R & R REPAIR IAW EO 2013047-311 PARA 8 40 REV B.Dec 19, 2013 · N620AR · Casa C212DF · Wing, Plate/SkinSDR 39LA2013121937Channel · corrodedLEFT WING INBD FLAP TRACK U CHANNEL SHOWS SIGNS OF HEAT EROSION & CORROSION. REPLACED LT WING INBD FLAP TRACK U CHANNEL IAW EO 20130417-311 PARA 8.25 & PARA 8.31 REV B.Dec 19, 2013 · N620AR · Casa C212DF · Trailing Edge FlapsSDR 39LA2013121938Skin · corrodedLEFT WING EXHAUST TRAIL SKIN SHOWS SIGNS OF HEAT EROSION & CORROSION. REPLACED LT WING EXHAUST TRAIL SKIN IAW EO 2013047-311 PARA 8.21 REV B.Dec 19, 2013 · N620AR · Casa C212DF · Wing, Plate/SkinSDR 39LA2013121939Channel · corrodedLEFT WING INBD FLAP TRACK U CHANNEL SHOWS SIGNS OF HEAT EROSION & CORROSION. REPLACED LT WING INBD FLAP TRACK U CHANNEL IAW EO 20130417-311 PARA 8.25 & PARA 8.31 REV B.Dec 19, 2013 · N620AR · Casa C212DF · Trailing Edge FlapsSDR 39LA2013121940Skin · corrodedRIGHT WING EXHAUST TRAIL SKIN SHOWS SIGNS OF HEAT EROSION & CORROSION. REPLACED RT WING EXHAUST TRAIL SKIN IAW EO 2013047-311 PARA 8.22 REV B.Dec 19, 2013 · N620AR · Casa C212DF · Wing, Plate/SkinSDR 39LA2013121941Rib · damagedRIGHT HAND OTBD WING RIB AT WS 9500 FOUND DAMAGED WITH MULTIPLE CRACKS & DENTED FORMERS. R & R RT HAND WING RIB IAW EO2013047-311 PARA 8.42 REV B.Dec 19, 2013 · N620AR · Casa C212DF · Wing, Rib/BulkheadSDR CA131126010Bearing · failed(CAN) PILOT REPORTED CHIP DETECTOR LIGHT ILLUMINATED FOR SEVERAL MINUTES AND THEN EXTINGUISED DURING FLIGHT. FLIGHT CONTINUED NORMALLY. UPON INSPECTION OF THE MAGNETIC CHIP DETECTOR, METAL SLIVERS WERE FOUND. METAL PARTICLES WERE ALSO FOUND IN THE OIL FILTER. Nov 14, 2013 · Swrngn SA227AC · Accessory GearboxesSDR 8EKA20140124001Skin · crackedCRACKS ON & IN THE VICINITY OF THE AFT UPPER DOOR WERE FOUND. ON 22-NOV-13 5 CRACKS WERE REPAIRED IAW THE SRM. THE ACFT WAS FLOWN UNTIL 27-NOV-13 WHEN THE DOM BECAME AWARE OF THE CRACKS, UPON READING THE E-MAIL & THEN PULLED THE ACFT OUT OF SERVICE. THIS E-Nov 5, 2013 · N348CA · Casa C212CC · Cargo/Baggage DoorsSDR 39LA2013072400114Skin · corrodedWHILE PERFORMING GENERAL VISUAL INSPECTION OF WING (TASK 57.02, ITEM 11 OF 1 YEAR INSPECTION UNDER COMPANY CAMP, WO 124890-5), FOUND WING SKIN BEHIND NR 2 ENGINE CORRODED. REPLACED WING T/E SKIN FROM WING STATION 1266 TO WING STATION 3500 WITH 2024-T3, 0.025"Jul 24, 2013 · N606AR · Casa C212CD · Wing, Plate/SkinSDR 2013FA0000248Blade · mismanufacturedDURING INSTALLATION OF BLADES IN ROTOR HUB, IT WAS FOUND THAT 1 BLADE ROOT PLATFORM WAS NOTICEABLY LONGER THAN ALL OTHER BLADES. THIS BLADE ROOT PLATFORM WAS MEASURED TO BE 1.250 WHILE OTHERS WERE 1.237. SUBSEQUENTLY, THIS BLADE WAS R & R WITH ANOTHER.Apr 18, 2013 · Engine Fuel Indicating SystemSDR LHO2013F00000Bellcrank · deformedTHE NOSE GEAR TRAPEZE (BELLCRANK) BECAME DEFORMED, PROBABLY FROM THE GEAR DOOR RETRACT RAMP DURING RETRACTION. THE NOSE UNSAFE LIGHT REMAINED ILLUMINATED AND EXTENTION WAS SELECTED. 3 GREENS AND DOWNLOCK WERE ACHIEVED AND AN UNEVENTFUL LANDING FOLLOWED. BOTMar 29, 2013 · N716SM · Cessna 441 · Nose/Tail Landing Gear
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