Pratt & Whitney Canada PW305

Service difficulty reports · 78

Newest first. General aviation reporting is voluntary.

Query with SQL
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 = 'PW305'
  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 2026FA0000550Seal · leakingON 6/26/2026, N924PS, CYO924 DEPARTED KLAX AND DURING CLIMB, THE CAPTAIN REPORTED THE LH ENGINE FIRE DETECT LIGHT ILLUMINATED AND THEN WENT OUT. THE CAPTAIN ELECTED TO RETURN TO LAX. ATI JET MAINTENANCE WENT TO INVESTIGATE THE ISSUE, ENGINE COWLINGS WERE OPENEJun 26, 2026 · N924PS · Lear 60LEAR · Engine Bleed Air SystemSDR 9JLA2021020425345Exciter · defectiveTHE FLIGHT CREW REPORTED THAT DURING ENGINE START AN AMBER RIGHT ENGINE COMPUTER ANNUNCIATOR ILLUMINATED. THE MAINTENANCE TEAM DOWNLOADED THE ENGINE COMPUTER AND TROUBLESHOT PER THE PRATT AND WHITNEY MANUAL. IT WAS DETERMINED THAT UPPER AND LOWER EXCITER BOXESJan 3, 2021 · N821DF · Lear 60LEAR · ExciterSDR AJXA2019123000004Warning Message · illuminatedLH THRUST REVERSER ARM CAME ON DURING CLIMB WITH AMBER TR UNLOCK LIGHT. THE AIRCRAFT RETURNED TO ITS POINT OF ORIGIN AND WAS GROUNDED.Dec 29, 2019 · N917PG · Lear 60LEAR · Engine Thrust ReverserSDR RU3A20160330007Control Unit · failedBOTH BLEED AIR LIGHTS ILLUMINATED 17 MINS INTO FLIGHT. REPLACEMENT OF THE TAIL CONE OVERHEAT CONTROL UNIT SOLVED THE ISSUE.Mar 30, 2016 · N58 · Lear 60LEAR · Overheat DetectionSDR RU3A2016Warning System · activatedLEFT & RIGHT BLEED AIR LIGHTS ANNUNCIATED AFTER TAKEOFF, MCT POWER, WHEN NAC HEATS SELECTED ON.Mar 11, 2016 · N58 · Beech 300BEECH · Bleed Air Indicating SystemSDR RU3A20160311006Warning System · activatedLEFT & RIGHT BLEED AIR LIGHTS ANNUNCIATED AFTER TAKEOFF, MCT POWER, WHEN NAC HEATS SELECTED ON.Mar 11, 2016 · N58 · Beech 300BEECH · Bleed Air Indicating SystemSDR U5QA201603110076Engine · shutdownUPON ARRIVAL, DECLARED EMER, LANDED UNEVENTFUL. RT ENG SHUTDOWN INFLIGHT UNCOMMANDED. IN MX NOW ALONGSIDE OEM TECHNICAL ASSISTANCE. SUSPECT FADEC, PART ON ORDER.Mar 10, 2016 · N60GF · Lear 60LEAR · Engine (Turbine/Turboprop)SDR U5QA201601060073Connector · dirtyDURING CLIMB OUT RT ENG ROLLED BACK TO LESS THAN 35% N1. AUTO RELIGHT ENGAGED & ENG STARTED & RETURNED TO NORMAL. TROUBLE SHOT, CLEANED CONNECTORS ON EEC & RANG N2 SENSORS WITH SATISFACTORY RESULTS. SWAPPED EEC'S FROM SIDE TO SIDE & CLEANED CONNECTORS. ENGJan 2, 2016 · N405DC · Lear 60LEAR · Engine Fuel System WiringSDR CA151215001Engine · stalled(CAN) DURING DESCENT, WITH THE ENGINE AT IDLE SPEED, THE ENGINE STALLED AND SHUTDOWN BY ITSELF. THE PILOT WAS ABLE TO RESTART THE ENGINE. THE CUSTOMER HAD 2 IN-FLIGHT SHUTDOWNS WITH THE SAME ENGINE DURING DESCENT MODE. THE ACFT LANDED UNEVENTFULLY. TROUBLESNov 27, 2015 · Engine (Turbine/Turboprop)SDR RU3A201514014020Gasket · leakingBLEED AIR LT & RT ILLUMINATED. EXTINGUISHED AFTER FOLLOWING ABNORMAL CHECKLIST. ACFT HAD NOT FLOWN FOR SEVERAL MONTHS. REPLACED LEAKING SOV GASKET.Oct 14, 2015 · N58 · Lear 60LEAR · Compressor Bleed ControlSDR CA150629002Indication Sys · faulty(CAN) DURING FLIGHT, THE LT ENG TEMP GAUGE WENT INTO THE RED ZONE 3 TIMES & EACH TIME LASTED AROUND 3 TO 5 SECONDS. THE PILOT PULLED BACK THE POWER TO REDUCE THE OIL TEMP & OIL TEMP WAS NORMAL AT LOW POWER SETTING. CREW DECIDED TO TURN BACK TO THE AIRPORT & Jun 24, 2015 · Cessna 680CE · Engine Temperature Indicating SystemSDR U5QA20150316066Oil System · overservicedWHILE POSITIONING AT 2000 FEET ENCOUNTERED SMOKE IN THE COCKPIT. RAN BOTH ENGS FOUND BOTH ENGS TO BE OVER SERVICED WITH OIL. NR 1 ENG CHECKED OIL FILTER & REINSTALLED WITH NEW O RINGS, SERVICED ACCORDINGLY. NR 2 ENG DRAINED OIL TO CORRECT POSITION. RAN ENGMar 15, 2015 · N405DC · Lear 60LEAR · Turbine Engine Oil SystemSDR GQRA20140620001Thrust Reverser · malfunctionedON LANDING AFTER TOUCHDOWN PILOTS STATE THAT THRUST REVERSER LEVERS WERE PULLED BUT NEITHER THRUST REVERSER UNLOCKED. ON SECOND ATTEMPT PILOT STATES THAT RT REVERSER UNLOCKED & DEPLOYED PRIOR TO LT REVERSER UNLOCKING & DEPLOYING. ACFT YAWED TO THE RT & STRUCJun 17, 2014 · N898PA · Lear 60LEAR · Engine Thrust ReverserSDR 2014FA0000333Outflow Valve · malfunctionedLOUD SQUEALING DURING TAKEOFF AND CABIN PRESSURIZATION INDICATED 1500 TO 2000 FPM DOWN AND ABORTED TAKEOFF. TROUBLESHOOTING AND FURTHER ENGINE AND PRESSURIZATION RUNS COULD NOT DUPLICATE THE PROBLEM. BELIEVE TO HAVE BEEN A STICKY OUTFLOW VALVE DUE TO NOT FLYIMay 19, 2014 · N8889 · Lear 60LEAR · Pressure Regulator/Outflow ValveSDR V6NA 2011 01Line · crackedACFT EXPERIENCED A 10 PERCENT POWER REDUCTION IN THE LT ENGINE AT V1. PILOT CONTINUED UNEVENTFULLY. INVESTIGATION REVEALED CRACKED BOV AIR CONTROL LINE, PN 31B5667-01.Jan 25, 2011 · N88V · Lear 60LEAR · Engine Bleed Air SystemSDR 2011FA0000011Defog System · failedWINDSHIELD DEFOG FAILS FUNCTIONAL TEST. REMOVED AND INSTALLED REPAIRED WINDSHIELD DEFOG BOX ASSY. PERFORMED SATISFACTORY FUNCTIONAL TEST OF THE WINDSHIELD DEFOG CONTROL SYSTEM WITH NO DEFECTS NOTED.Dec 22, 2010 · N7734T · Lear 60LEAR · Windshield/Door Rain/Ice RemovalSDR 2011F00000Starter Gen · destroyedDURING CRUISE FLIGHT, EXPERIENCED VIBRATION, BELIEVED TO BE FROM ENGINE AREA. VIBRATION INCREASED, BUT DID NOT SHOW ON EVM INDICATOR, FOLLOWED BY GEN 1 FAIL INDICATION, WITH BUS TIE CLOSED IN FLIGHT. ACFT MADE UNSCHEDULED LANDING. MX FOUND NR1 STARTER GEN FDec 21, 2010 · N261PA · Beech 100BEECH · Starter-GeneratorSDR U5QA06025Switch · failedAT CRUISE FLIGHT RIGHT ENGINE LOW FUEL PRESSURE WARNING CAME ON. TURNED ON STANDBY AND LIGHT EXTINGUISHED. LANDED AT BUFFALO, NY AIRPORT WITHOUT INCIDENT. MAINTENANCE FOUND RT JET PUMP SWITCH BAD. REPLACED SWITCH AND OPS CHECKED GOOD.Sep 13, 2010 · N8783 · Lear 60LEAR · Aircraft Fuel Distribution SystemSDR EZK2010F00000Starter Gen · failedACFT RETURNING TO SERVICE, NOTED A VIBRATION IN THE ACFT. DETERMINED PROBLEM TO BE IN LT GENERATOR. ACFT LANDED TO DROP PASSENGER. CREW ADVISED MX OF PROBLEM, DISPATCHED A MECH THE FOLLOWING MORNING WITH A STARTER/GENERATOR. INSTALLED SAME, NO VIBRATIONS NAug 26, 2010 · N769DS · Lear 60LEAR · Starter-GeneratorSDR S8A2009F00004Fire Loop · false activationACFT DEPARTED ENROUTE WITH (4) PASSENGERS AND (2) CREW. AT CLIMB OUT AT APPROX 2000 FT AGL NR 1 ENG HAD FIRE INDICATION. CREW DECLARED AN EMERGENCY WITH ATC AND RETURNED TO DEPARTURE AIRPORT WITH AN UNEVENTFUL LANDING. OMP WAS CONTACTED TO INSPECT AND REPAIJul 12, 2009 · N547LR · Braero HAWKER1000 · Fire DetectionSDR S8A2009F00003Engine · leakingACFT DEPARTED WITH NO PASSENGERS AND 2 FLIGHT CREW. SHORTLY AFTER TAKEOFF AT APPROX 3500 FT, CREW NOTED SMOKE IN THE COCKPIT. CREW TOOK EMERGENCY PROCEDURES AND ASK ATC TO RETURN IMMEDIATELY WITH PREFERENTIAL TREATMENT. LANDING WAS UNEVENTFUL, ACFT TAXIED OJun 5, 2009 · N923SK · Lear 60LEAR · Engine (Turbine/Turboprop)SDR U5QA06014Engine · leakingSUNDAY MORNING 11-16-08 ON A PART 91 FLIGHT FROM KCLL TO KDAL APPROXIMATELY 20 MIKES SOUTH OF KDAL PILOT REPORTED SMOKE IN CABIN. AT THAT POINT THE CREW DECLARED AN EMERGENCY, AND WERE GIVEN PRIORITY LANDING. LANDED WITHOUT INCIDENT AT KDAL. MAINT RAN ENGINNov 16, 2008 · N923SK · Lear 60LEAR · Turbine Engine Oil SystemSDR E0X2008F00004Engine · damagedAC DEPARTED AND SHORTLY AFTER DEPARTURE, SMOKE WAS NOTED IN CABIN WITH BAGGAGE SMOKE DETECTOR INDICATING SMOKE IN BAGGAGE COMPARTMENT. FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE, APPROACH AND LANDING WERE UNEVENTFUL WITH NO OTHER INDICATION OJun 6, 2008 · N513LR · Braero BAE1251000 · Engine (Turbine/Turboprop)SDR E0X2008F00002Engine · failedNR 1 ENGINE QUIT AS AC WAS CLIMBING THROUGH FL370 WITH NO WARNING. FIRST INDICATION WAS LOSS OF OIL PRESSURE AS ENGINE SPOOLED DOWN. DIVERTED AND DECLARED AN EMERGENCY. THEIR WAS NOT AN ATTEMPT MADE TO AIRSTART THE FAILED ENGINE. SINGLE ENGINE LANDING WAS UNEMay 18, 2008 · N539LR · Braero BAE1251000A · Engine (Turbine/Turboprop)SDR E0X2008F00001Unknown · unknownON APPROACH, AT 3000 FT, EXPERIENCED A PARTIAL PANEL FAILURE ON THE CAPT EADI, EHSI, MFG. TRANSFERRED CONTROL OF AC TO THE F/O. SELECTED THE NR 2 AFSC AND 30 SECONDS THE AC DEPARTED LEVEL FLIGHT AND STARTED AN UNCOMMANDED DESCENT. AT 2700 FT BOTH FLIGHT CREFeb 7, 2008 · N542LR · Braero BAE1251000A · Auto Flight SystemSDR EOX2008F00000Starter Gen · vibrationAIRCRAFT WAS FL360 ENROUTE, FLIGHT CREW NOTED A VIBRATION IN THE RT ENGINE AND DID A PRECAUTIONARY SHUTDOWN OF THE RT ENGINE. THE AIRCRAFT DIVERTED AND MADE AN UNEVENTFUL LANDING WITH NO INJURIES TO PASSENGERS OR CREW. INSPECTED THE RT ENGINE AND FOUND THAT Jan 5, 2008 · N548LR · Braero HAWKER1000 · Starter-GeneratorSDR E0X2007F00000Scavenge Port · wornDEPARTED, ENROUTE, AT 22,000FT THE FLIGHT CREW DECLARED AN EMERGENCY WHEN THE NR 1 (LT) ENGINE OIL PRESSURE STARTED FLUCTUATING AND ALL LOW PRESSURE LIGHT CAME ON. FLIGHT CREW SHUTDOWN NR 1 ENGINE AND MADE AN EMERGENCY LANDING. THE LANDING WAS UNEVENTFUL WITNov 19, 2007 · N515LR · Braero BAE1251000 · Turbine Engine Oil SystemSDR 2007FA0000315Mixing Valve · out of toleranceDURING TAKEOFF ROLL CREW EXPERIENCED A RUSH OF WARM OILY SMELLING AIR IN THE COCKPIT. CREW ABORTED TAKEOFF AND RETURNED TO BASE. MAINTENANCE CREW RAN AIRCRAFT AND DUPLICATED PROBLEM FINDING THE DUCT OVRHT LIGHT AND LT BLEED LIGHT ON AT FULL POWER. FURTHER TROUApr 2, 2007 · N706CR · Lear 60LEAR · Pneumatic Distribution SystemSDR HAG07001Support Bracket · failedDURING FLAP OPERATION, FLAP ACTUATOR SUPPORT BRACKETS FAILED CAUSING FLAP ACTUATOR TO DAMAGE LT WING RIB SEGMENT.Feb 23, 2007 · N252FX · Lear 60LEAR · Trailing Edge FlapsSDR 2007FA0000205Mixing Valve · intermittentSHORTLY AFTER TAKEOFF, AIRCRAFT (L BLEED AIR) WARNING ILLUMINATED, AND (R BLEED AIR) WARNING ILLUMINATED APPROX 5 SEC LATER, SMELLED ODOR IN CABIN. REDUCED POWER AND WARNING WENT OUT. AIRCRAFT DIVERTED FOR MAINTENANCE. UNABLE TO DUPLICATE MALFUNCTION ON GROFeb 22, 2007 · N500 · Lear 60LEAR · Pneumatic Distribution SystemSDR 2007FA0000294Mixing Valve · intermittentSHORTLY AFTER TAKEOFF, AIRCRAFT (LT BLEED AIR) WARNING ILLUMINATED, AND (RT BLEED AIR) WARNING ILLUMINATED APPROX 5 SEC LATER, SMELLED ODOR IN MAINTENANCE. UNABLE TO DUPLICATE MALFUNCTION ON GROUND RUN; LT MIXING VALVE WAS SUSPECTED, SO REPLACED. PERFORMED GFeb 22, 2007 · N500 · Lear 60LEAR · Pneumatic Distribution SystemSDR AJCA200600004Landing Gear · lack of lubeDEC. 04, 2006 DURING CLIMB OUT, RETRACTED LANDING GEAR AND THE UNSAFE NOSE LANDING GEAR RED LIGHT ILLUMINATED. RECYCLED THE GEAR TWICE AND EACH TIME THE NLG LIGHT REMAINED ILLUMINATED. RETURNED AND LANDED SAFELY. INVESTIGATED AND FOUND THE GEAR NEEDED LUBRICADec 4, 2006 · N43NR · Lear 60LEAR · Nose/Tail Landing GearSDR 2006FA0001159Pump · failedTHREE FUEL BOOST PUMPS IN OVERHAULED CONDITION, SAME PN, ORDERED FROM THE SAME VENDOR HAVE FAILED AFTER SHORT TIME ON SAME AIRCRAFT USED ON LT AND RT SIDES. 1) FUEL BOOST PUMP OVERHAULED CONDITION SN 11A557 FAILED 5/24/06 AFTER 247 HOURS. 2) FUEL BOOST PUMP Nov 17, 2006 · N46WC · Braero BAE1251000 · Fuel Boost PumpSDR 2007FA0000045Adc · malfunctionedTHE FLIGHTCREW REPORTED INTERMITTENT LOSS OF ADC INFORMATION ON THE CAPTAIN`S PFD. THE PRIMARY AIR DATA COMPUTER WAS FOUND TO BE DEFECTIVE AND WAS REPLACED. THE SYSTEM WAS TESTED AND INSPECTED IAW MM AND WAS FOUND TO COMPLY WITH FAR 91.411, PART 43 AND RVSM Nov 16, 2006 · N160AN · Lear 60LEAR · Air Data ComputerSDR 2006FA0001157Pump · failedTHREE FUEL BOOST PUMPS IN OVERHAULED CONDITION, SAME PART NUMBER, ORDERED FROM THE SAME VENDER HAVE FAILED AFTER SHORT TIME ON SAME AIRCRAFT USED ON LT AND RT SIDES. 1) FUEL BOOST PUMP OVERHAULED CONDITION SN 11A557 FAILED 5/24/06 AFTER 247 HOURS. 2) FUEL BOOMay 24, 2006 · N46WC · Braero BAE1251000 · Fuel Boost PumpSDR 2006FA0001158Pump · failedTHREE FUEL BOOST PUMPS IN OVERHAULED CONDITION, SAME PN, ORDERED FROM SAME VENDOR HAVE FAILED AFTER SHORT TIME ON SAME AIRCRAFT USED ON LT AND RT SIDES. 1) FUEL BOOST PUMP OVERHAULED CONDITION SN 11A557 FAILED 5/24/06 AFTER 247 HOURS. 2) FUEL BOOST PUMP OVERMay 11, 2006 · N46WC · Braero BAE1251000 · Fuel Boost PumpSDR O2G2006F00003Sensor · faultyNOSE STEERING NORMAL STEERING WAS NOT AVAILABLE. REPLACED NOSE WHEEL STEERING COMPUTER AND BOTH SENSORS. (K)Mar 28, 2006 · N247CP · Lear 60LEAR · Landing Gear Steering SystemSDR 2006FA0000259Casting · bentINCOMING INSPECTION FOUND AILERON DRIVE YOKE ATTACH CASTING BENT. UPON FURTHER INSPECTION IT WAS DISCOVERED THE DRIVE YOKE UPPER OR LOWER SHIMS WERE NOT INSTALLED. DRIVE YOKE ATTACH BOLT WAS INSTALLED CAUSING THE CASTING TO BE BENT AND REQUIRES REPLACEMENT BMar 7, 2006 · N647TS · Lear 60LEAR · Aileron Control SystemSDR 2006FA0000440Adc · defectiveALL ADC OUTPUTS ON THE COPILOTS PFD (ALTIMETER, VSI AND AIRSPEED, ECT) FLAGGED IN FLIGHT INTERMITTENTLY AND WOULD RESET ITSELF. CREW REQUESTED TO LEAVE RVSM AIRSPACE. THE ADC WAS FOUND TO BE DEFECTIVE AND WAS REPLACED. THE SYSTEM WAS TESTED AND INSPECTED IAFeb 23, 2006 · N160AN · Lear 60LEAR · Air Data ComputerSDR YNO2006F00000Valve · failedTHIS AIRCRAFT WAS ENROUTE. THE PIC NOTICED AN AIR DISTRIBUTION DUCT OVERHEAT LIGHT ON IN THE COCKPIT. THE FLIGHT CREW ELECTED TO DIVERT FOR FURTHER INVESTIGATION AND TROUBLESHOOTING. MAINTENANCE REMOVED AND REPLACED THE COCKPIT TEMPERATURE SENSOR FAN, COCKFeb 8, 2006 · N61ZZ · Lear 60LEAR · Cabin Temperature Control SystemSDR AOQ2006F00000Switch · intermittentUPON TAKEOFF THE LANDING GEAR WOULD NOT RETRACT, REQUIRING NUMEROUS GEAR HANDLE CYCLES TOO RETRACT THE LANDING GEAR. MAINTENANCE INSPECTED AND OPERATED THE LANDING GEAR SYSTEM. DURING INSPECTION FOUND THE GEAR SELECTOR SWITCH TO BE INTERMITTENT. REMOVED ANFeb 5, 2006 · N298EF · Lear 60LEAR · Landing Gear Retraction/Extension SystemSDR DXTA200601201Indicator · activatedT/O ROLL ABORTED FOR ENG/FUEL LOOK UP LIGHT. ITEM IS UNDER INVESTIGATION.Jan 17, 2006 · N550QS · Braero HAWKER1000 · Engine Fuel Indicating SystemSDR ON717JB121405JCActuator · stickingNOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. INSPECTED LANDING GEAR SYSTEM AND FOUND NOSE GEAR FREE FALL ACTUATOR ARM TO BE STICKING IN EXTENDED POSITION. REPLACED NOSE GEAR FREE FALL ACTUATOR. ACCOMPLISHED NOSE GEAR UPLOCK ADJUSTMENT Dec 14, 2005 · N717JB · Lear 60LEAR · Landing Gear ActuatorSDR 2005FA0001528Extinguisher · incorrectREMOVING HAND HELD FIRE EXTINGUISHER FROM THE COCKPIT FOR ROUTINE INSPECTION IT WAS NOTED THAT THE HANDLE DID NOT APPEAR TO BE CORRECT. FURTHER INSPECTION SHOWED THAT THERE ARE TABS ON THE LOWER HANDLE THAT WOULD HAVE PREVENTED THE EXTINGUISHER FROM DISCHARGINov 8, 2005 · N551QS · Braero HAWKER1000 · Fire Bottle, PortableSDR 2005FA0001481Drain · chafedRT HYDRAULIC PUMP CASE DRAIN HYDRAULIC LINE RUPTURED IN FLIGHT, DRAINING HYDRAULIC FLUID FROM THE AIRCRAFT SYSTEM. FOUND RT HYDRAULIC PUMP CASE DRAIN LINE CRACKED WHERE LINE HAS BEEN CHAFING. INSPECTED AIRCRAFT AND FOUND SIMULAR CHAFE IN SAME LINE IN SAME LOOct 4, 2005 · N503QS · Braero BAE1251000A · Hydraulic Pump (Electric/Engine), MainSDR AJC2005F00010Downlock Switch · failedUPON GEAR EXTENSION FOR LANDING, 3 GREEN GEAR LIGHTS ILLUMINATED AND INNER GEAR DOORS OPEN RED LIGHT REMAINED (ON). CREW CYCLED LANDING GEAR TO NO AVAIL, EXECUTED TOWER FLY BY FOR CONFIRMATION AND WAS INSTRUCTED TO RETURN, WHERE ANOTHER ATC TOWER FLY BY WAS MJul 27, 2005 · N706CR · Lear 60LEAR · Landing Gear Position and WarningSDR AOQ2005F00001Outflow Valve · defective(REF: 1940060805JC) CLIMBING THROUGH 12,000 FEET, CABIN PRESSURE PANEL DISPLAYED A FAULT LIGHT. SIMULTANEOUSLY AN EMERGENCY PRESS LIGHT ILLUMINATED FOLLOWED BY EMERGENCY PRESSURIZATION SYS ACTIVATION. CABIN ALT ONLY REACHED APPROX 6000 FT INDICATED. CREW THJun 8, 2005 · N1940 · Lear 60LEAR · Pressure Regulator/Outflow ValveSDR 2005FA0000802Rudder · damagedUPON REMOVAL AND REPLACEMENT OF RUDDER CABLES, FOUND RUDDER SUPPORT STIFFENER ANGLE CRACKED UNDER RUDDER PRIMARY TRAVEL STOP AT FRAME STA 48, ALSO FOUND RUDDER LEADING EDGE PANELS 331,332, AND 333 TO BE CRACKED AND RUDDER FORWARD SPAR TO BE DAMAGED AT RUDDER CMay 23, 2005 · N249FX · Lear 60LEAR · Rudder StructureSDR JBGA20050003Engine · flamed outENGINE FLAMED OUT FOLLOWED BY AMBER ENGINE LIGHT.May 18, 2005 · N529KF · Lear 60LEAR · Engine (Turbine/Turboprop)SDR 2005FA0000716Unknown · malfunctionedDURING DEPARTURE, AFTER MAINTENANCE (ENGINE AND THRUST REVERSER) THE NOSE LANDING GEAR DID NOT RETRACT. THE AC RETURNED TO DEPARTURE FOR REPAIR. PROBABLE CAUSE: THE AC WAS JACKED, THE LANDING GEAR WAS FUNCTIONALLY TESTED IAW MM. THE DISCREPANCY COULD NOT BApr 20, 2005 · N797PA · Lear 60LEAR · Landing Gear Retraction/Extension System
Back to Pratt & Whitney Canada PW305