U/A Canada PT6A-60A

Service difficulty reports · 596

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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 = 'PT6A60A'
  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 2010FA0000454Skin · corrodedTHE LT & RT CENTER WING FUEL CELL ACCESS HAD CORROSION ON THE FLANGE. THIS IS THE SECOND B300 THE REPAIR STATION HAS SEEN WITH THIS PROBLEM. THE FLANGE IS HIDDEN BY THE FUEL CELL ACCESS PANEL AND IS NOT READILY VISIBLE DURING NORMAL MAINTENANCE. THE KING AIMay 10, 2010 · N350FW · Beech B300 · Wing, Plate/SkinSDR P90R7138Controller · failed(P90R) PILOT REPORTED THAT AFTER TAKEOFF, THE PASSENGERS REPORTED SMOKE IN THE CABIN AND MADE A PRECATIONARY LANDING. HE STATED THAT THEY DID GROUND RUNS AND COULD NOT DUPLICATE THE PROBELM. DURING OUR TROUBLESHOOTING, WE FOUND THE ACFT NOT PRODUCING COLD AIR.May 5, 2010 · N545LC · Beech 200BEECH · Cabin Temperature Control SystemSDR 2010FA0000388Adapter · missingDURING ENGINE INSTALLATION OPERATOR REPORTED OIL LEAK FROM THE TORQUE TRANSDUCER BOSS ON REDUCTION GEARBOX (RGB) HSG. REPAIR STATION INVESTIGATION REVEALED MISSING OIL SLEEVE ADAPTER (PN 3103335-01, POST SB 13164) ON THE RGB TRANSDUCER BOSS. THE ADAPTER SERVApr 16, 2010 · Turbine Engine Oil SystemSDR 2010F00078Oil Filter · splitDURING A 200 HOUR OIL FILTER INSP THE ENGINE OIL FILTER INTERNAL FINGER SCREEN "CONE" WAS FOUND SPLIT AT THE WELDED OR SOLDIERED JOINT.Mar 31, 2010 · N32WC · Beech 200BEECH · Turbine Engine Oil SystemSDR CA100813013Starter Gen · failed(CAN) ON TAKEOFF ROLL, THE ACFT RT STARTER GENERATOR FAIL LIGHT ILLUMINATED, WHICH OCCURRED AT THE SAME TIME AS A DROP IN PROPELLER RPM. ACFT RETURNED TO MX AT WHICH TIME THE STARTER GENERATOR WAS REPLACED, A QAD RING INSP WAS COMPLETED SATISFACTORY, AND OIL Mar 10, 2010 · Beech B300 · Starter-GeneratorSDR GSPA49WCServo · bindingFLIGHT CREW REPORTED AILERON CONTROLS BINDING AND THEN A NOTICEABLE "CLUNK" WHILE TURNING THE AIRPLANE LT OR RT. AFTER THE "CLUNK" THE CONTROLS WOULD BE FREE UNTIL RETURNING THE CONTROL YOKE BACK TO THE NEUTRAL POSITION. AUTO PILOT SYS WAS NOT ENGAGED WHILE Mar 5, 2010 · N49WC · Beech B300 · Autopilot Main ServoSDR 2010FA0000191Access Panel · corrodedTHE CTR WING FUEL CELL ACCESS WAS FOUND TO HAVE CORROSION ON THE FLANGE. THIS FLANGE IS HIDDEN BY THE FUEL CELL COVER AND THE DAMAGE IS NOT READILY VISIBLE DURING NORMAL MX. THIS AREA HAS A HISTORY OF WATER/ CONDENSATION INGRESS AND SHOULD BE THOROUGHLY INSPMar 1, 2010 · N459M · Beech B300 · Wing, Plate/SkinSDR CA100216010Bearing · deteriorated(CAN) METAL GENERATION AND SUBSEQUENT BEARING DETERIORATION CAUSED A LOSS OF TORQUE ON WHEEL ASSY. (TC 20100216010)Feb 16, 2010 · Beech B300 · Wheel/Ski/FloatSDR CA100216011Support · damaged(CAN) DURING GEAR RETRACTION AFTER TAKEOFF, THE INBD DOOR JAMMED BETWEEN THE STRUT AND THE WHEEL ASSY CAUSING DAMAGE TO THE GEAR DOOR CLOSING MECHANISM. THIS REQUIRED REPLACEMENT OF THE SUPPORT ASSY. IT APPEARS THAT THE OVER CTR LOCK WAS NOT ENGAGED ALLOWINGFeb 12, 2010 · Beech B300 · Landing Gear Door Retract SectionSDR CA100212004Cross Tie · cracked(CAN) WHILE CARRYING OUT 10000 CYCLE INSP, (INITIAL) FOUND RT AFT EMERGENCY EXIT CROSS TIE CRACKED. CRACK TERMINATES AT RIVET HOLE. THIRD INSTANCE IN THIS FLEET, ALL BETWEEN 5000 AND 10000 CYCLES. CRACK APPEARS TO ORIGINATE DUE TO ROUGH MACHINED SURFACE ON Feb 11, 2010 · Beech B300 · Fuselage Main, StructureSDR CA100127017Seal · cut(CAN) ACFT WAS ENROUTE AT FL 260 WHEN THE CREW NOTICED A SLIGHT INCREASE IN CABIN RATE OF CLIMB. THE RATE CONTINUED FROM 500 FET PER MINUTE (FPM) TO A MAXIMUM OF 6000 FPM. THE CREW INITIATED AN EMERGENCY DESCENT AND LEVELED OFF AT 10,000 FEET. FLIGHT THEN DIVEJan 22, 2010 · Beech B300 · Passenger/Crew DoorsSDR CA100224005Oil System · leaking(CAN) DURING CLIMB THE NR 1 ENG OIL PRESSURE DROPPED AND ENGINE WAS SHUTDOWN. ACFT LANDED SAFELY. THERE WAS NO DAMAGE TO THE ACFT. AN EXTERNAL OIL LEAK WAS FOUND, HOWEVER, THE EXACT LOCATION OF THE OIL LEAK IS UNKNOWN. MFG WILL INVESTIGATE TO ESTABLISH ROOT Jan 14, 2010 · Turbine Engine Oil SystemSDR RU3A1002Tube · brokenON GROUND WHEN ENGINES STARTED (WITH BLEEDS IN ENVIRONMENTAL) STRONG EXHAUST SMELL IN CABIN. SMELL GOES AWAY ONCE AIRCRAFT PRESSURIZES. WHEN AIRCRAFT STARTED WITH BLEEDS OFF (PNEUMATIC AND ENVIRONMENTAL) NO EXHAUST SMELL IN CABIN. ON TOUCHDOWN IMMEDIATELY GJan 12, 2010 · N74 · Beech 300BEECH · Engine Anti-Icing SystemSDR CA100108005Inverter · failed(CAN) THIS AIRCRAFT WAS PREVIOUSLY HAD SMOKE IN THE CABIN AND NO CONCRETE SOURCE OF THE SMOKE WAS FOUND. REFER TO CADOR 2009P1941. DURING AN OVERNIGHT INSPECTION ON 1/7/10, THE MEDICAL EQUIPMENT POWER WAS TURNED ON AND THE AFT LIFEPORT MEDICAL PLUS UNIT (BASEJan 7, 2010 · Raythn B300RAYTHEON · AC InverterSDR YADA111709Exhaust Stack · crackedPILOT REPORTED OCCASIONAL EXHAUST FUMES IN CABIN. CONFIRMED THAT THE CREW SMELLED EXHAUST ON ROLLOUT WITH PROPS IN BETA AND HAD SMELLED IT AT AN ENGINE START (AS IS COMMON WHEN STARTING WITH A TAIL WIND). MX LOCATED A CRACKED HEATED INTAKE LIP STUB PIPE ON TNov 17, 2009 · N111AX · Beech 1900C · Engine Collector/Tailpipe/NozzleSDR CA091118006Skin · loose(CAN) THE FUSELAGE RIVETS ARE LOOSE AND LEAKING PRESSURIZATION. THESE RIVETS WERE SEALED IN AUGUST 2009 IAW MFG RECOMMENDED REPAIR. THE REPAIR WAS COMPLETED AT 1790.7 TTSN, IN 160.5 HOURS THE PROBLEM IS COMING BACK. MFG STATES THAT THIS IS NOT A STRUCTURAL PRONov 17, 2009 · Beech 300BEECH · Fuselage Main, Plate/SkinSDR RU3A0920Chip Detector · contaminatedLEVELED AT FL260, EXECUTED CRUISE CHECKLIST AND RIGHT ENGINE CHIP DETECT LIGHT ILLUMINATED. RAN THE APPROPRIATE CHECKLIST AND RETURNED TO BASE. LANDING WAS UNEVENTFUL. CHECKED WITH MAINTENANCE FOUND A VERY SMALL, ALMOST MICROSCOPIC PIECE OF FOD ON THE CHIP Sep 29, 2009 · N77 · Beech 300BEECH · Turbine Engine Accessory DriveSDR CA090928005Duct · deformed(CAN) FLIGHT CREW REPORTED NO HEAT IN AFT CABIN. INSPECTION OF THE DUCTING IN THE AFT CABIN FOUND TWO DUCTS DEFORMED DUE TO HEAT CAUSING A RESTRICTION OF AIRFLOW TO THE CABIN OUTLETS. NEW DUCTS INSTALLED. TEMPERATURE CONTROL WAS OPERATING IN MANUAL MODE DUE TSep 23, 2009 · Beech B300 · Air Distribution SystemSDR CA090928006Duct · deformed(CAN) FLIGHT CREW REPORTED NO HEAT IN AFT CABIN. INSPECTION OF THE DUCTING IN THE AFT CABIN FOUND TWO DUCTS DEFORMED DUE TO HEAT CAUSING A RESTRICTION OF AIRFLOW TO THE CABIN OUTLETS. NEW DUCTS INSTALLED. TEMPERATURE CONTROL WAS OPERATING IN MANUAL MODE DUE TOSep 23, 2009 · Beech B300 · Air Distribution SystemSDR CA100813014Fuel Cap · leaking(CAN) IN FLIGHT, THE CREW NOTICED FUEL CAP LEAKING, ON ARRIVAL AT MX FACILITY THE FUEL CAP WAS REPLACED WITH NEW, NO FURTHER INCIDENTS. THIS SDR BEING SUBMITTED NOW AS PART OF AMO ANNUAL AUDIT PROGRAM.Aug 25, 2009 · Beech B300 · Fuel StorageSDR 2009F00059Indicator · smokeDURING LEVEL OFF AT 5000 FT, CREW SMELLED AND OBSERVED SMOKE COMING FROM THE CAPTAIN'S SIDE GLARESHIELD. MX DETERMINED THE SMOKE CAME FROM THE CAPTAIN'S DME INDICATOR.Aug 19, 2009 · N336MV · Stbros SD330 · DME/TACAN SystemSDR RU3A0912Pump · malfunctionedDURING FLIGHT INSPECTION OF KNQX PAR, LEFT FUEL PRESSURE LOW ANNUNCIATOR ILLUMINATED IN FLIGHT. BOLD FACE IMMEDIATE ACTION ITEMS COMPLETED. FUEL PRESSURE LIGHT EXTINGUISHED UPON ACTUATION OF LEFT STANDBY BOOST PUMP. ACTION ITEMS BACKED UP WITH USE OF "FUEL Aug 19, 2009 · N79 · Beech 300BEECH · Engine Fuel PumpSDR CA090820011Mount Bracket · crackedWHILE CARRYING OUT SCHEDULED ENG INSP, WHICH INCLUDED LUBING AIR CONDITIONING COMPRESSOR QUILL SHAFT, FOUND BRACKET WHICH THE AIR CONDITIONING COMPRESSOR MOUNTS TO AND PIVOTS ON WAS CRACKED AND THE REAR LUG WAS BROKEN RIGHT OFF. REPLACED WITH A SERVICEABLE PAug 18, 2009 · Beech 300BEECH · Cabin Compressor SystemSDR JDWA31764AOil Filter · cloggedAFTER TAKEOFF DURING CLIMB, PILOT NOTICED RT OIL PRESSURE ANNUNCIATOR LIGHT AND NOTED OIL PSI TO BE 50PSI. PILOT REDUCED PWR AND RETURNED TO BASE WITHOUT INCIDENT.Aug 7, 2009 · N719GL · Beech 1900C · Turbine Engine Oil SystemSDR CA090709002Downlock Switch · failed(CAN) NLG DOWNLOCK SWITCH, MOUNTED ON DRAG BRACE, FAILED WHEN GEAR WAS SELECTED DOWN. NOSE GEAR WOULD NOT INDICATE GREEN FOR DOWN AND LOCKED. ACFT LANDED SAFELY. FOUND WIRE LOOSE IN SWITCH. SWITCH IS SEALED AT MFG WITH A SILICONE TYPE GASKET WHERE WIRES EJul 8, 2009 · Beech B300 · Landing Gear Position and WarningSDR 2009FA0000526Nut · crackedLT INBD FLAP ACTUATOR NUT (PN 50-521151-6) NUT WAS CRACKED FROM RIVET INTO CHROME. NO RECORD OF OVERHAUL. ALL OIL HAD LEAKED OUT OF ASSY. SERIOUS SAFETY AND FLIGHT ISSUE. NUT WAS LABELED AS CONDEMNED AND REPLACED ON ASSY.Jun 19, 2009 · N102FK · Beech C90 · Trailing Edge Flap ActuatorSDR 2009FA0000527Nut · crackedRT OTBD FLAP ACTUATOR NUT, PN 50-521223-4, NUT WAS CRACKED FROM RIVET INTO CHROME. NO RECORD OF OVERHAUL. ALL OIL HAD LEAKED OUT OF ASSY. SERIOUS SAFETY AND FLIGHT ISSUE. NUT WAS LABELED AS CONDEMNED AND REPLACED ON ASSY.Jun 19, 2009 · N102FK · Beech C90 · Trailing Edge Flap ActuatorSDR CA090611001Downlock Switch · faulty(CAN) LANDING GEAR UNSAFE LIGHT IN FLIGHT. NO LT MAIN INDICATION. LANDING GEAR RETRACTED AND EXTENDED TO CONFIRM 3 GREEN. INTERMITTENT ON TAXI IN. TROUBLESHOOT SYS TO FAULTY LT MAIN GEAR DOWNLOCK INDICATION SWITCH.Jun 1, 2009 · Beech 300BEECH · Landing Gear Position and WarningSDR RU3A0907Bracket · defectiveWHILE ON APPROACH, AIRCRAFT YAWED 15-20 DEGREES RIGHT OF RUNWAY CENTERLINE. MAIN GEAR TOUCHED PAVEMENT AS GO-AROUND WAS EXECUTED. ON RE-APPROACH, A FULL STOP LANDING WAS ACCOMPLISHED WITH NO FURTHER INCIDENT. BACKGROUND INFO RELATIVE TO CURRENT INCIDENT. RIMay 28, 2009 · N70 · Beech 300BEECH · Propeller Controlling SystemSDR T4OR 4995 70Roller · wornRT OTBD FLAP ATTACH POINT BRACKETS (RIBS) ARE WORN WHERE AFT FLAP TRACK ROLLERS ARE ATTACHED. BRACKETS ARE WORN APPROXIMATELY .015 INCH TO .020 INCH DEEP IN THE BRACKET SIDES FROM THE ROLLER IN THE SHAPE OF THE ROTATING ROLLER ENDS. SUSPECT CAUSE TO BE WORN Apr 23, 2009 · N965LG · Beech E90 · Trailing Edge FlapsSDR CA090415009Rib · cracked(CAN) RT OTBD FLAP L/E RIB ALSO FOUND CRACKED AT SAME LOCATION. THIS PROBLEM COMMON ON 200 SERIES AIRCRAFT. ON 200 SERIES PLANES THE PROBLEM IS DEALT WITH BY A SB. THE SB DOES NOT APPLY TO 300 SERIES PLANES. IT SHOULD. THE REPAIR KIT CALLED OUT BY THE 200 SERIApr 14, 2009 · Raythn B300RAYTHEON · Trailing Edge FlapsSDR CA090408009Fuel Control · inoperative(CAN) AFTER TAKEOFF PILOT REPORTED HE COULD ONLY GET A MAXIMUM OF 1600 TO 1800 POUNDS OF TORQUE WHEREAS 3200 SHOULD HAVE BEEN ACHEIVED. THE LOAD OF FERTILIZER HAD TO BE DUMPED TO BE ABLE TO MAINTAIN FLIGHT. THE PILOT RETURNED TO THE STRIP WHERE HE LANDED SAFELApr 2, 2009 · Ayres S2RT65 · Fuel Control/Turbine EnginesSDR CA090429003Float Switch · stuck(CAN) ENGINE SHUTDOWN INCIDENT. MFG CONSULTED. ENGINE STARTED AND RAN FINE IMMEDIATELY AFTER LANDING. ACFT DISPATCHED FOR NON-REVENUE TRAINING AFTER INSP, COMPLETED 6 HOURS WITH NO ISSUES. FLOAT SWITCH STUCK IN "FULL" POSITION IN AUX TANK AND FUEL PRESSURE SWMar 26, 2009 · Beech 300BEECH · Fuel Transfer ValveSDR 2009F00024Line · separatedLT MLG BEGAN LOWERING OUT OF NACELLE DURING FLIGHT.Mar 19, 2009 · N347D · Beech B200 · Hydraulic System, MainSDR CA090319011Link · bent(CAN) ON A PRE-FLIGHT INSP THE LT OTBD LINK ASSY DOOR ACTUATOR WAS FOUND BENT AND THE DOOR ACTUATOR ROLLER WAS FOUND DAMAGED. MANUAL RETRACTION TEST WERE CARRIED OUT AFTER THE DAMAGED PARTS WERE REPLACED AND NO FAULTS WERE FOUND. CAUSE OF THE DAMAGE TO THE BRMar 17, 2009 · Beech 300BEECH · Landing Gear Door Retract SectionSDR CA090320005Attach Fitting · damaged(CAN) DURING DI, NOTICED THAT THE OTBD LT FLAP SEEMED TO RETRACT TOO FAR INTO THE UP POSITION, ONCE INVESTIGATING, FOUND THAT THE INBD ATTACH BRACKETS (WING STATION 140.110) ON THE AIRFRAME SIDE THAT HOLDS THE OB FLAP ON HAD CRACKED. THE FLAP WAS REMOVED TO AMar 12, 2009 · Beech 300BEECH · Trailing Edge FlapsSDR CA090409002Bearing · failed(CAN)STARTER-GEN PN 23085-001 SN P1307. MOD STATUS B,C,F. 960.4 HRS TSO. AIRCRAFT: NR 2 AT 7903.0 HRS TTAF. DATE: MARCH 10, 2009. GENERATOR FAILED ON TAKEOFF. ACFT RETURNED TO AIRPORT. STARTER-GENERATOR WAS REMOVED. ON TEARDOWN OF ST-GEN, THE BRG AT THE DRIVMar 10, 2009 · Beech B300 · Starter-GeneratorSDR CA090302003Seal · damaged(CAN) NUMEROUS ISSUES WITH WHISTLING DOOR SEAL ON THIS ACFT. ACFT INCURS HIGH CYCLES/UTILIZATION AND DOOR SEAL DAMAGE, HAS ALWAYS BEEN A PROBLEM, BUT TYPICALLY LAST 800+ HOURS. RECENTLY THE DOOR SEAL HAS BEEN COMING OUT OF THE TRACK THAT IT SITS IN. OCCASIONALMar 2, 2009 · Beech 300BEECH · Passenger/Crew DoorsSDR CA090302004Fuel Control · failedAIRCRAFT WAS IN CRUISE AT FL210. FIRST OFFICER ATTEMPTED TO ADJUST THE RT POWER LEVER TO BRING THE TORQUE UP TO MATCH THE LT ENGINE. FOUND THE POWER LEVER ALREADY AT THE STOP. CREW THEN NOTICED A GRADUAL LOSS OF POWER (TORQUE, FUEL FLOW AND ITT) TO ABOUT 50Feb 27, 2009 · Raythn B300RAYTHEON · Fuel Control/Reciprocating EnginesSDR 2009FA0000139Fork · crackedPREVIOUSLY REPORTED TO MFG INSTRUCTIONS STIPULATED IN SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. NOSE GEAR FORK FAILED NDT IAW SUPPLEMENTAL INSPECTION 32-20-02. REPLACED NOSE FORK ASSEMBLY PN 5842000-5.Feb 26, 2009 · N425Z · Cessna 425 · Nose/Tail Landing Gear Strut/AxleSDR CA090302009Motor · unserviceable(CAN) ON APPROACH THE PILOTS SELECTED GEAR DOWN AND AFTER 15 SECONDS WITH THE GEAR NOT EXTENDING THE LANDING GEAR CONTROL CIRCUIT BREAKER TRIPPED. A COUPLE ATTEMPTS WHERE MADE BY THE CREW WITH THE SAME RESULT. THE CREW EXTENDED THE GEAR DOWN USING THE HAND PUMFeb 26, 2009 · Beech 300BEECH · Landing Gear ActuatorSDR CA090209004Windshield · crackedIN CRUISE FLIGHT, THE LT WINDSHIELD CRACKED. THE CREW LOWERED THE CABIN DIFFERENTIAL TO 4 PSI AND CONTINUED TO DESTINATION.Feb 8, 2009 · Beech 300BEECH · Flight Compartment WindowsSDR CA090128004Rivet · shearedDURING A PHASE 1A INSPECTION, THE PROPELLER CONTROL BRACKET LOCATED UNDER THE CENTER PEDESTAL WAS FOUND TO HAVE 2 SHEARED OFF RIVETS. IN LIEU OF RIVETS IT WAS FOUND THAT 2 C-CLAMPS WERE HOLDING THIS BRACKET IN PLACE. WHAT IS IMPORTANT TO NOTE IS THAT THIS WAJan 28, 2009 · Raythn B300RAYTHEON · Fuselage Main, Attach FittingsSDR CA090116012Bolt · broken(CAN) DURING POST FLIGHT WALK AROUND, FLIGHT CREW NOTICED A BOLT WAS MISSING FROM THE NR 4 MAIN WHEEL. MAIN WHEEL ASSEMBLY WAS REPLACED.Jan 5, 2009 · Beech 300BEECH · Wheel/Ski/FloatSDR CA090102004Door Frame · cracked(CAN) WHILE CARRYING OUT SPECIAL INSPECTION, INSPECT ESCAPE HATCHES AND ASSOCIATED CLOSURE AREA. FOUND THE RT AFT EMERGENCY EXIT CROSS TIE CRACKED THROUGH AT FS 201.775, AFT RT ESCAPE HATCH FRAME. THERE WERE TWO RIVETS SHEARED OFF IN THE SAME AREA AND THE .1Dec 31, 2008 · Beech 300BEECH · Fuselage Main, StructureSDR CA081222010Windshield · cracked(CAN) WINDSHIELD CRACKED AFTER TAKEOFF, CRACKS EMANATED VERTICALLY FROM THE BOTTOM INBOARD EDGE. UNIT TTSN 4500 HOURS.Dec 21, 2008 · Beech 300BEECH · Flight Compartment WindowsSDR 2009FA0000283Turbine Blades · damagedSTIFF PROP NOTICED ON SHUTDOWN. FOUND AT DISASSEMBLY: 1ST STG PT BLADES-7EA BLADES WITH PT SHROUD RUB. 1 EA COMPLETE BALDE COMING OUT OF PT DISK. 1ST STG PT STATOR, HEAVY BLADE RUB IN BLADE PATH AREA. 1ST STG PT DISK (PN 17B905 - MARKED K DIA. 6.1762. ACTDec 18, 2008 · N311GM · Beech 300BEECH · Turbine SectionSDR CA081210006Skin · cracked(CAN) WHEN COMPLYING WITH SPECIAL INSPECTION "ESCAPE HATCHES AND ASSOCIATED AREAS", A CRACK WAS FOUND AT THE LOWER FORWARD CORNER OF THE BONDED RT EMERGENCY EXIT DOOR SKIN, EXACTLY AS PICTURED IN THE MAINTENANCE MANUAL. REPLACED SKIN ASSEMBLY WITH NEW. CRACKDec 8, 2008 · Beech 300BEECH · Emergency ExitsSDR YADA112808Boot · shortedOBSERVED SPARKS FROM RT PROP INFLIGHT, SPARKS STOPPED WHEN PROP DEICE WAS TURNED OFF. A/C LANDED UNEVENTFULLY. MAINT REPLACED PROP DUE TO SHORTED DEICE BOOT.Nov 28, 2008 · N113AX · Beech 1900C · Propeller/Rotor Anti-Ice/De-Ice SystemSDR CA081203001Probe · separated(CAN) DURING A 3RD PHASE 600 HR INSP, A SNAG WAS CREATED TO FIX A DISCREPANCY IN THE RT FUEL QUANTITY INDICATING SYS. THE RT FUEL TANK READING WAS 300 LBS LOW. MAINT INSPECTED SYS AND ISOLATED THE PROBLEM TO THE RT AUX FUEL TANK PROBE. UPON A CLOSER INSP IT WNov 20, 2008 · Beech 300BEECH · Fuel Indicating System
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