Beech C90A

Service difficulty reports · 461

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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 = 'C90A'
  ORDER BY difficulty_date DESC"

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SDR CA100108001Intake Duct · cracked(CAN) INTAKE DUCT SKIN CRACKED AT TWO LOCATIONS, LOCATIONS ARE, LEADING EDGE FASTENER ROW, FASTENER HOLES AT 3:00 AND 9:00 O’CLOCK. (TC NR 20100108001)Dec 22, 2009 · Beech C90A · Engine Cowling SystemSDR CA091214003Control System · failed(CAN) ACFT REACHED CRUISING ALTITUDE OF FL270, PILOT NOTICED RT ENGINE OIL TEMP INDICATION REACHING RED LINE, AND OIL PRESSURE STARTING TO DECREASE. PILOT REDUCED POWER ON RT ENG AND FEATHERED AFFECTED ENG, HE THEN RETURNED TO BASE AND HAD AN UNEVENTFUL LANDINDec 11, 2009 · Beech C90A · Engine Oil CoolerSDR CA090904011Petcock · openACFT WAS DEPARTING FOR A LOCAL TRAINING FLIGHT. STUDENT OCCUPIED THE LT SEAT AND WAS PILOT FLYING, INSTRUCTOR WAS PILOT NOT FLYING ON RT SIDE. ON INITIAL CLIMB INSTRUCTOR NOTED THAT STUDENT HAD MISSED CROSSWIND TURN ALTITUDE AND ADVISED SAME. STUDENT CALLED Sep 4, 2009 · Beech C90A · Pitot/Static SystemSDR CA090904010Oil Cap · unsecureDURING TRAINING FLIGHT AT APPROX 1 HOUR INTO FLIGHT, FLYING PILOT NOTICED A LWR THAN NORMAL ENG OIL PRESSURE ON LT ENGINE. EMERGENCY CHECKLIST WAS CARRIED OUT AND COMPLETED. LT ENG OIL PRESSURE WARNING LIGHT THEN ILLUMINATED MOMENTARILY (FLICKERED). ENG SHUSep 3, 2009 · Beech C90A · Turbine Engine Oil SystemSDR 2009FA0000929Torque Knee · wrong partLWR TORQUE KNEE STOP LUG IS MACHINED TOO SHORT ALLOWING OVER EXTENSION OF THE LWR LANDING GEAR STRUT. THIS ALLOWS THE BRAKE ASSY AND TIRE TO CONTACT AND DAMAGE THE LWR NACELLE SKIN DURING GEAR RETRACTION AND EXTENSION. THE MFG DATED CODE STAMPED ON THE TORQUJul 27, 2009 · N299RP · Beech C90A · Main Landing Gear Strut/Axle/TruckSDR E07A446ASSwitch · intermittentRT MLG DID NOT INDICATE DOWN AND LOCKED WITH GREEN LIGHT. EMERGENCY HAND PUMP WAS USED TO NO AVAIL. ON FINAL APPROACH ( 400 FEET AGL) GREEN LIGHT CAME ON AND INDICATED DOWN AND LOCKED ACFT WAS LANDED WITHOUT PROBLEMS. SWITCH OPERATION WAS NORMAL. COULD NOJul 16, 2009 · N446AS · Beech C90A · Landing Gear Position and WarningSDR CA090602009Pin · worn(CAN) ON A SCHEDULED PHASE 4 INSP, A RUBBING SOUND WAS NOTED COMING FROM BENEATH CABIN FLOOR JUST AFT OF THE CABIN ENTRANCE WHEN THE ELEVATOR CONTROLS WERE MOVED. AME NOTING THE SOUND, GAINED ACCESS TO INVESTIGATE IN THIS AREA. IT WAS DISCOVERED THAT A CABLE GJun 1, 2009 · Beech C90A · Elevator Control SystemSDR CA090526005Oil Filter · damaged(CAN) DURING OPS NR1 INSP, ENG OIL FILTERS WERE REMOVED AND INSPECTED. THERE WAS NO EVIDENCE OF CONTAMINATION ON THE FILTER ELEMENT, HOWEVER, WHEN THE SECONDARY FILTER WAS INSPECTED IT WAS FOUND WITH AN OPEN END. THE SECONDARY FILTER IS CONICAL SHAPED WITH THEMay 25, 2009 · Beech C90A · Turbine Engine Oil SystemSDR 2009FA0000445Door · missingRT INBD HINGED COWLING DOOR (PN 109-910027-31) DEPARTED AIRCRAFT. SPINE ASSY (PN 109-910060-1) HINGE ATTACHMENT DAMAGED. NO OTHER DAMAGE TO ACFT NOTED. DOOR AND SPINE ASSY REPLACED WITH SERVICEABLE PARTS. (K)Apr 9, 2009 · N550SW · Beech C90A · Nacelle/Pylon, Main FrameSDR CA090206007Casting · crackedDURING 72 MONTH INSPECTION IT WAS FOUND THAT THE LOWER CASTING WAS CRACKED AT THE LOWER TORQUE KNEE CONTACT POINT.Feb 6, 2009 · Beech C90A · Main Landing Gear Strut/Axle/TruckSDR DYV2009F00000Downlock Switch · intermittentBEFORE LANDING, WHEN GEAR WAS SELECTED DOWN, THE RT GREEN DOWN LIGHT FAILED TO ILLUMINATE. THE GEAR UNSAFE LIGHT AND HORN DID NOT INDICATE AN UNLOCKED GEAR. AFTER A FLYBY AND A VISUAL LOOK BY GROUND PERSONNEL, THE FAILED GEAR LIGHT CAME ON AND A LANDING WAS Jan 29, 2009 · N1083S · Beech C90A · Landing Gear Position and WarningSDR CA080905007Tab · bent(CAN) EMERGENCY EXIT DOOR LATCH APPEARS AS THOUGH THE LATCH TAB HAD BEEN BENT SO THAT IT COULD BE INSTALLED IN THIS MANNER. IN THIS MODE, THE LATCH CAN ALWAYS (EVEN WHEN PRESSURIZED) BE OPENED AS THE TAB PASSES OVER THE SAFETY PLUNGER. THE TAB SHOULD CONTACT Sep 4, 2008 · Beech C90A · Emergency ExitsSDR 2008FA0000617Blower · failedPILOT DETECTED SMOKE IN CABIN, LANDED. TROUBLESHOT ODOR, CHECK IN ENGINE BAYS, NO DEFECT NOTED. FOUND CABIN VENT BLOWER NOT WORKING, CHECKED BLOWER SYSTEM WIRING, NO DEFECTS NOTED, CHECKED VENT BLOWER UNDER PILOT FLOOR AND FOUND BLOWER MOTOR LOCKED UP. REMOVAug 22, 2008 · N904RB · Beech C90A · Air Distribution FanSDR CA080805002Sleeve · wrong part(CAN) WHILE CARRYING OUT A SCHEDULED HOT SECTION INSPECTION ON THE ABOVE ENGINE, IT WAS DISCOVERED THAT 2 NOZZLE SHEATHS WERE OF AN INCORRECT PART NR FOR THE MODEL OF ENGINE INSTALLED. THE PART NRS ARE BOTH FOR A PT6A-50 ENGINE. EVEN THOUGH WE OPERATE THIS MODJul 28, 2008 · Beech C90A · Fuel Injector NozzleSDR EO72008F00000Fan · lockedCABIN FAN FAILED WHICH CAUSED SMOKE IN THE CABIN. AIRCRAFT WAS LANDED WITHOUT INCIDENT. (K)Jul 2, 2008 · N396AS · Beech C90A · Air Distribution FanSDR 2008FA0000489Inlet · crackedLT AND RT WELD ASSY CRACKED ALONG A WELDED SEAM. THE CRACKS ARE APPROXIMATELY 12 INCHES LONG. THESE WELD ASSY ARE A PORTION OF THE ENGINE INLET. A PORTION OF THE INLET AIR IS USED FOR THE OIL COOLER AND SOME AIR IS BYPASSED AND EXITS FROM THE LOWER PORTION Jun 20, 2008 · N5115H · Beech C90A · Nacelle/Pylon, Main FrameSDR 2008FA0000245Trim System · icedWHEN THE AIRPLANE HAS SET ON THE RAMP IN THE RAIN, THEN TAKES OFF WITH A QUICK CLIMB TO COLDER TEMPERATURES AT ALTITUDE, THE ELEVATOR TRIM FREEZES. THE AUTOPILOT KICKS OFF BECAUSE IT IS UNABLE TO RESPOND. THE PILOT THEN HANDFLYS WITH THE ELEVATOR FORCE LOADED Apr 9, 2008 · N200TR · Beech C90A · Elevator Tab Control SystemSDR 2008FA0000122Wire Harness · misinstalledAIR CONDITIONER NOT COOLING. FOUND WIRING FOR AC START CONTROL PANEL AS WELL AS COMPRESSOR CLUTCH NOT IN PROPER CONFIGURATION IAW WIRING PRINT. AFTER PROPER INSTALLATION OF WIRING AND SUBSEQUENT OPS CHECK, THE MOTOR AND SYS, THE AIR CONDITIONER WOULD CYCLE IFeb 6, 2008 · N4764A · Beech C90A · Air Conditioning System WiringSDR CA071213002Brushes · burned(CAN) CREW DECLARED EMERGENCY DUE TO SMOKE IN COCKPIT AND LANDED SAFELY. REPAIR PARTY LT FROM ANOTHER BASE. FOUND CAUSE WAS CABIN VENT BLOWER. DISABLED SYSTEM. AIRCRAFT FERRIED TO AIRPORT. MAINTENANCE WILL REPLACE VENT BLOWER. (TC NR 20071213002)Dec 12, 2007 · Beech C90A · Air Distribution FanSDR 2007FA0001097Bumper Block · unbondedCOMMUNIQUE NR 2000-04 ANNOUNCED THAT STARTING LJ-1088 AND AFTER THAT LANDING GEAR BUMPER BLOCK WILL BE BONDED TO THE MAIN SPAR WHERE IT CROSSES INSIDE THE LANDING GEAR WHEEL WELLS. THIS AC FOUND THE RT LANDING GEAR BUMPER BLOCK ON THE FLOOR OF HIS HANGER. NODec 12, 2007 · N266RD · Beech C90A · Wing Miscellaneous StructureSDR 702DKControl Head · faultyBOTH NR 1 AND NR 2 TRANSPONDER DISPLAYS WENT OUT DURING FLIGHT ATC REPORTED TRANSPONDER FAULTS. AIRCRAFT RETURNED TO POINT OF DEPARTURE WITHOUT INCIDENT. FAILURES TROUBLESHOT TO FAULTY TRANSPONDER CONTROL HEAD.Nov 13, 2007 · N702DK · Beech C90A · ATC Transponder SystemSDR WNH2007F00002Altimeter · malfunctionedENCODING ALTIMETER DISPLAY FADES IN AND OUT TO THE POINT THAT THE INFORMATION DISPLAYED IS ILLEGIBLE TO THE PILOT. (K)Jul 22, 2007 · N73PG · Beech C90A · Altimeter, Barometric/EncoderSDR WNH2007F00001Altimeter · failedENCODING ALTIMETER DISPLAY FADES IN AND OUT TO THE POINT THAT THE INFORMATION DISPLAYED IS ILLEGIBLE TO THE PILOT. (K)May 22, 2007 · N73PG · Beech C90A · Altimeter, Barometric/EncoderSDR WNH2007F00000Altimeter · malfunctionedENCODING ALTIMETER DISPLAY FADES IN AND OUT TO THE POINT THAT THE INFORMATION DISPLAYED IS ILLEGIBLE TO THE PILOT. (K)May 22, 2007 · N73PG · Beech C90A · Altimeter, Barometric/EncoderSDR FMOR20070002Control Cable · frayedTHE ELEVATOR TRIM CABLE BEGAN UNRAVELING JUST FORWARD OF THE CABIN DOOR. FROM THERE THE CABLE BEGAN BINDING IN A PULLEY UNDERNEATH THE PILOT'S SIDE FORWARD FACING PASSENGER CHAIR CAUSING STIFFNESS OF OPERATION BY HAND AND THE MALFUNCTION OF THE ELECTRIC TRIM Apr 10, 2007 · N120TT · Beech C90A · Elevator Tab Control SystemSDR J0UR200700001Motor · failedAIR CONDITIONING / VENT BLOWER MOTOR ASSEMBLY FAILED CAUSING SMOKE IN COCKPIT. PILOT DECLARED EMERGENCY AND LANDED AT CLOSEST AIRPORT WITHOUT FURTHER INCIDENT.Feb 18, 2007 · N1103G · Beech C90A · Air Distribution FanSDR CA070221004Buckle · damaged(CAN) COMPLIED WITH COMPANY CAMPAIGN NOTICE 010-25-10-011, NM-06-29. THE CREW SEATBELT ROTARY LATCH CAN BE CONTACTED WITH THE CONTROL YOKE WITH THE SEAT FULL FORWARD AND THE YOKE FULL AFT. IT IS POSSIBLE TO UNLATCH THE SEATBELT BY ROTATING THE YOKE AND MAKINGFeb 10, 2007 · Beech C90A · Emergency EquipmentSDR CA070209001Buckle · damaged(CAN) WITH A COCKPIT CREW MEMBER STRAPPED INTO THEIR SEAT WITH THE SEAT FULLY FORWARD, INTERFERENCE BETWEEN THE CONTROL COLUMN YOKE AND THE ROTARY SEAT BELT BUCKLE FINS OCCURS WHEN THE CONTROL YOKE IS PULLED FULLY AFT AND ROTATED. THE POSSIBILITY EXISTS THAT TFeb 7, 2007 · Beech C90A · Emergency EquipmentSDR CA070207003Buckle · damaged(CAN) CAMPAIGN NOTICE 010-25-10-011 / FAA SAIB NM-06-29. CREW SEAT BELT ROTARY LATCH IS CONTACED BY THE CONTROL YOKE AND THE POSSIBLITY EXISTS TO RELEASE THE BELT WITH ROTATION OF THE CONTROL YOKE WHEN FUNCTIONAL TEST WAS CARRIED OUT IAW SAIB. (TC NR 20070207Feb 6, 2007 · Beech C90A · Emergency EquipmentSDR CA070221003Buckle · malfunctioned(CAN) COMPLIED WITH COMPANY CAMPAIGN NOTICE 010-25-10-011 NM-06-29. THE CREW SEATBELT ROTARY LATCH CAN BE CONTACTED WITH THE CONTROL YOKE WITH THE SEAT FULL FORWARD AND THE YOKE FULL AFT. IT IS POSSIBLE TO UNLATCH THE SEATBELT BY ROTATING THE YOKE AND MAKING Feb 5, 2007 · Beech C90A · Emergency EquipmentSDR CA070202016Gasket · damaged(CAN) PILOTS NOTICED FUEL (STREAMING) FROM THE RT NACELLE TOP COVER SHORTLY AFTER TAKEOFF. THE AIRCRAFT RETURNED TO BASE WITHOUT INCIDENT. THIS HAPPENED (3) TIMES BEFORE THE PROBLEM WAS CORRECTED. 1ST NOTICE, AFT 86.9 HRS. MAINTENANCE ATTRIBUTED THE EXCESS FUEFeb 2, 2007 · Beech C90A · Fuel StorageSDR CA070202015Fire Detector · malfunctioned(CAN) DURING A ROUTINE MISSION, THE RT FIRE WARNING ANNUNCIATOR LIGHTS ILLUMINATED. THERE WAS NO VISUAL INDICATION OF FIRE. THE PILOT`S SECURED THE ENGINE IAW PUBLISHED PROCEDURES, ACTIVATED THE FIRE SUPPRESSION SYSTEM AND RETURNED TO THE BASE. MAINTENANCE WASFeb 2, 2007 · Beech C90A · Fire DetectionSDR E07A0709001Motor · burned outON APPROCAH THE CABIN FAN BLOWER GOT HOT AND PUT SMOKE IN THE CABIN.Jan 9, 2007 · N395AS · Beech C90A · Air Distribution FanSDR QVFA001Bushing · missingFOUND VERY SLIGHT MOVEMENT IN RT MLG OB PART OF MLG STRUT. UPON FURTHER INVESTIGATION, FOUND THAT P/N 10574X-YR1145 BUSHING WAS NOT INSTALLED IN MLG STRUT. FURTHER INVESTIGATION FOUND THAT THIS AREA HAD NOT BEEN THOROUGHLY INSPECTED SINCE DECEMBER 2004 DURING Jan 8, 2007 · N990TF · Beech C90A · Main Landing Gear Strut/Axle/TruckSDR C90ABushing · missingFOUND VERY SLIGHT MOVEMENT IN RT MLG OB PART OF MLG STRUT. UPON FURTHER INVESTIGATION, FOUND THAT PN 10574X-YR1145 BUSHING WAS NOT INSTALLED IN MLG STRUT. FURTHER INVESTIGATION FOUND THAT THIS AREA HAD NOT BEEN THOROUGHLY INSPECTED SINCE DECEMBER 2004 DURING 6Jan 8, 2007 · N990TF · Beech C90A · Main Landing Gear Strut/Axle/TruckSDR 2006FA0001082Tube · crackedTHE TUBES ARE CRACKING ALONG THE WELDS, WHICH CONNECT THEM TO THE INLET LIP ASSEMBLY. REQUIRES REMOVAL OF INLET LIP ASSY AND REPAIR OF THE CRACKED WELDS. (K)Nov 8, 2006 · N200HV · Beech C90A · Turbine Engine Air Inlet SectionSDR PAI52006S4330Wheel · crackedPILOT NOTED RT MAIN TIRE LOW PRESSURE ON PREFLIGHT. MAINTENANCE FOUND, UPON DISASSEMBLY OF WHEEL, THAT THE INNER WHEEL HALF WAS CRACKED IN THE O-RING GROOVE ADJACENT TO THE WHEEL TIE BOLT HOLES.Oct 25, 2006 · N511KV · Beech C90A · Wheel/Ski/FloatSDR CA060922001Bearing · destroyed(CAN) MAINTENANCE NOTICED FLUID LEAKING FROM THE RT MLG BRAKE ASSY. INVESTIGATION REVEALED THAT THE BRAKE ASSY. PISTON RETENTION BOLT WAS THE SOURCE OF THE LEAK. A MORE DETAILED INSPECTION DISCOVERED THAT THE RT MAIN WHEEL INNER WHEEL HALF CONE AND BEARING HADSep 22, 2006 · Beech C90A · Wheel/Ski/FloatSDR CA061108003Floor Support · cracked(CAN) FLOOR SUPPORT ANGLE P/N UNKNOWN FOUND CRACKED. ANGLE IS PART OF BULKHEAD ASSY. P/N 50420028-15. ANGLE IS LOCATED UNDER CENTRE FLOOR PANEL. (TC NR 20061108003)Sep 19, 2006 · Beech C90A · Fuselage Miscellaneous StructureSDR 2006FA0000894Bolt · overtorquedDURING 1ST SCHEDULED PHASE 1 AND PHASE 2 INSPECTION INVESTIGATED PILOT COMPLAINT OF STIFF NOSEWHEEL STEERING. VERIFIED COMPLAINT, FOUND NOSEWHEEL STEERING STIFF AND LOUD POPPING NOISES COMING FROM COCKPIT UNDER FLOOR AREA WHEN TAXIED FROM COPILOTS POSITION. Aug 24, 2006 · N405DD · Beech C90A · Rudder Control SystemSDR 2006FA0000893Fastener · overtorquedFOUND OTHER LT SIDE RUDDER CONTROL ATTACHING HARDWARE TIGHT OR OVERTIGHTENED. EXAMINED LT RUDDER CONTROL SYSTEM HARDWARE FOR SERVICEABILITY AND REINSTALLED AS REQUIRED WITH NORMAL RECOMMENDED TORQUES, ADJUSTED INTERCONNECT ROD AS REQUIRED WITH NORMAL RECOMMENAug 24, 2006 · N405DD · Beech C90A · Rudder Control SystemSDR 2006FA0000892Mount · distortedDURING FIRST SCHEDULED 1ST AND 2ND PHASE INSPECTIONS NOTED SQUEAKING AND METAL TO METAL CONTACT NOISES WHEN RUDDER MOVED SIDE TO SIDE. FOUND RUDDER SERVO CABLE RUBBING ON SMT-65 SERVO MOUNT CABLE DRUM COVER. REPLACED SMT-65 UNIT AND REINSTALLED, RIGGED SERVOAug 24, 2006 · N405DD · Beech C90A · Autopilot Main ServoSDR 2006FA0000890Control Cable · out of adjustDURING 1ST SCHEDULED PHASE 1 AND PHASE 2 INSPECTIONS NOTED ELEVATOR CONTROL SYSTEM CABLE TENSIONS OUT OF MM SERVICE LIMITS. FOUND ELEVATOR NEUTRAL POSITIONS OUT OF LIMITS FOLLOWING CABLE TENSION ADJUSTMENTS (WITH FORWARD AND AFT RIG PINS INSTALLED). FOUND FOAug 24, 2006 · N405DD · Beech C90A · Elevator Control SystemSDR 2006FA0000866Wheel · crackedAFTER SEVERAL ATTEMPTS TO FIND SOURCE OF ONGOING TIRE LEAKAGE, WHEEL ASSEMBLY WAS REMOVED FROM AIRCRAFT AND NSPECTED. FOUND 2 CRACKS OPPOSITE OF (1) OTHER ALONG INNER RADIUS OF INNER WHEEL HALF. DURING DISASSEMBLY IT WAS NOTED THAT WHEEL ASSEMBLY TIE BOLT NUAug 21, 2006 · N304TC · Beech C90A · Wheel/Ski/FloatSDR CA060619004Channel · cracked(CAN) THE P/N 109-910053-15 AND -16 COWL SUPPORT CHANNELS WERE FOUND CRACKED IN THE LOWER FLANGE AREA, AND SUBSEQUENTLY REPAIRED. MANY OF THE REPAIRS HAVE ALSO FAILED. IT APPEARS THAT A SUBSTANTIAL AMOUNT OF COWLING WEIGHT RESTS ON THESE CHANNELS. THE REPEAT DJun 15, 2006 · Beech C90A · Engine Cowling SystemSDR CA060619002Tab · cracked(CAN) CRACK DISCOVERED ON LOWER TAB SURFACE SKIN ADJACENT TO TAB HORN ATTACH RIB. SEE PICTURES ATTACHED.TRIM TAB ASSEMBLY P/N 50-610017-36 REPLACED WITH NEW. ELEVATOR AND TAB ASSEMBLY BALANCED (21.33 IN LBS TAIL HEAVY) AND REINSTALLED. INDEPENDENT CHECK ON R/HJun 12, 2006 · Beech C90A · Elevator Tab Control SystemSDR 2006FA0000567Bearing · failedTHE BEARING IN FUEL CONTROL UNIT FAILED CAUSING THE LT ENGINE TO SURGE AND EXCEED THE N1, ITT AND TORQUE LIMITS. THE ITT EXCEEDED 1000 C AND THE TORQUE EXCEEDED 1500 FT POUNDS FOR 5-10 SECONDS. SHORTLY AFTER TAKEOFF, PILOTS REPORTED PLANE HAD YAWED TO THE RTJun 1, 2006 · N530CH · Beech C90A · Fuel Control/Turbine EnginesSDR CA060530008Line · cracked(CAN) AIRCRAFT HAD TAXIED TO RUN-UP AREA PRIOR TO TAKEOFF. WHILE COMMENCING ENGINE RUN-UP NOTICED THAT THERE WAS NO THROTTLE RESPONSE ON THE RT ENGINE. CREW CONTACTED MAINTENANCE AND REQUESTED A TOW BACK TO THE HANGER. MAINTENANCE FOUND THAT THE FUEL FEED LINEMay 30, 2006 · Beech C90A · Engine Fuel DistributionSDR CA060509000Skin · worn(CAN) SKIN P/N 50-120156-82 (PRESSURE VESSEL) EXIBITING WEAR MARK ALONG FASTENER ROW ATTACHING FILLET P/N 50-420023-24 TO IT. WEAR MARK NOT READILY VISIBLE WITHOUT PULLING AWAY FILLET FROM SURFACE OF SKIN. WEAR MARK IS CAUSED BY LOOSENING OF FILLET TO SKIN FASMay 1, 2006 · Beech C90A · Fuselage Main, Plate/SkinSDR 2006FA0000463Wheel · crackedCRACKED IB WHEEL HALF CAUSING LOSS OF TIRE AIR PRESSURE. NOTE: THIS WAS A BRAND NEW PART ON A NEW AIRPLANE. NOT AN OVERHAULED PART (SEE 5(I) AND 6(I)Apr 27, 2006 · N164WS · Beech C90A · Wheel/Ski/Float
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