Pratt & Whitney Canada PW535A

Service difficulty reports · 251

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 = 'PW535A'
  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 CA060817002Sensor · failed(CAN) INTERMITTENT FAILURE OF TEMPERATURE SENSOR CAUSING INDICATED OVERTEMP OF AIRCRAFT MAIN BATTERY FOR SEVERAL SECONDS AT A TIME IN FLIGHT CAUSING MASTER CAUTION WARNING LIGHT ALSO. REPLACED TEMPERATURE SENSOR, SYSTEM CHECKED OK. NOTE THIS IS SECOND SENSOMar 28, 2006 · Cessna 560CESSNA · Battery/Charger SystemSDR CA060303012Gauge · failedBRAKE HYDRAULIC RESERVOIR UPPER AND LOWER SIGHT GAGES UNSERVICEABLE, SIGHT GAGE FLOATS ABSORBED SKYDROL BRAKE FLUID AND WOULD NOT FLOAT, MAKING IT IMPOSSIBLE FOR THE (PILOT) TO DETERMINE THE BRAKE FLUID LEVEL.Feb 10, 2006 · Cessna 560CESSNA · Hydraulic Reservoir, MainSDR DXTA200601234Throttle Cable · out of rigRIGHT ENGINE SPOOLED DOWN WHILE TAXIING OFF THE RUNWAY, IT SPOOLED BACK UP WHEN THE BOOST PUMP CAME ON. SHORTLY THEREAFTER IT SPOOLED DOWN AGAIN AND QUIT COMPLETELY. FOUND THROTTLE CABLE OUT OF RIG AT FCU. RIGGED THROTTLE CABLE TO FCU. OPS CHECK ON RUN FROFeb 7, 2006 · N800QS · Cessna 560CESSNA · Power LeverSDR CA060303011Bypass Valve · failedBYPASS VALVE INTERMITTENTLY STICKING IN OPEN (HOT) POSITION, UNABLE TO CONTROL CABIN AIR TEMPERATURE IN AUTO OR MANUAL SELECTION. REPLACED VALVE, GROUND CHECK OF VALVE OPERATION SATISFACTORY.Feb 4, 2006 · Cessna 560CESSNA · Cabin Temperature Control SystemSDR IMJ2006F00001Pump · failedIN CRUISE, MASTER CAUTION, (LOW PRESS R) ILLUMINATED, OIL PRESSURE INDICATOR READ 20 PSI. CHECKLIST INITIATED, ENG WAS SHUTDOWN. UNEVENTFUL LANDING WAS MADE. INVESTIGATION REVEALED THAT A WASHER FOREIGN TO ENG HAD BROKEN THROUGH A SCREEN, ENTERED OIL PUMP, Jan 30, 2006 · N12MW · Cessna 560CESSNA · Turbine Engine Oil SystemSDR CA060129001Engine · low pressure(CAN) DURING CRUISE, THE LOW OIL PRESSURE WARNING ANNUNCIATED. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT DIVERTED FOR AN UNSCHEDULED LANDING. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20060129001)Jan 25, 2006 · Cessna 560CESSNA · Turbine Engine Oil SystemSDR CA060129006Engine · flamed out(CAN) THE ENGINE FLAMED OUT DURING GROUND HANDLING OPERATIONS. MFG WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20060129006)Jan 18, 2006 · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR CA060303005Filter · contaminatedRT ENGINE FUEL FILTER CONTAMINATED WITH LINT FROM LARGE (12" X 30") TOWEL WHICH WAS FOUND IN THE RT INTEGRAL WING TANK. THE TOWEL WAS "INSTALLED" BY CESSNA AIRCRAFT FACTORY WHEN THE AIRCRAFT WAS BUILT. THE TOWEL WAS OUTBOARD OF THE BOOST AND EJECTOR PUMPS ANJan 16, 2006 · Cessna 560CESSNA · Aircraft Fuel Filter/StrainerSDR CA060303006Control Cable · brokenRT AILERON CONTROL YOKE CROSSOVER CABLE BROKEN STRANDS. THIS WAS FOUND ON PHASE 5 INSPECTION AND IS A COMMON FINDING AT 1200 HOURS OF USE.Jan 16, 2006 · Cessna 560CESSNA · Aileron Control SystemSDR CA060303007Control Cable · brokenLT AILERON CONTROL YOKE CROSSOVER CABLE BROKEN STRANDS. THIS WAS FOUND AT PHASE 5 INSPECTION AND IS A COMMON FINDING AT 1200 HOURS.Jan 16, 2006 · Cessna 560CESSNA · Aileron Control SystemSDR CA060303008Seal · failedESCAPE HATCH SEAL MIGRATING UNDER CABIN PRESSURE TO THE EXTERIOR OF THE AIRCRAFT. DUE TO POOR BONDING TO THE HATCH STRUCTURE. REPLACED SEAL AND PRESSURIZED AIRCRAFT, SERVICEABLE.Jan 16, 2006 · Cessna 560CESSNA · Emergency ExitsSDR CA060303009Tire · separatedNOSE WHEEL TIRE, TREAD IS STARTING TO SEPARATE FROM TIRE.Jan 16, 2006 · Cessna 560CESSNA · TireSDR DXTA200501171Line · failedAFTER LANDING POWER BRAKE AND ANTISKID MASTER CAUTION ILLUMINATED AFTER 1 SECONDS. AFTER 10 SECONDS OF ILLUMINATION TOTAL BRAKE FAILURE OCCURRED. EMERGENCY BRAKES WERE USED. PRECHARGE IS OUTSIDE OF SHADED AREA AFTER EVENT, NO OTHER ABNORMAL CONDITIONS WERE PRDec 30, 2005 · N834QS · Cessna 560CESSNA · Hydraulic System, MainSDR DXTA200501061Bulb · burned outRT MAIN LANDING GEAR LIGHT WOULD NOT ILLUMINATE. FOLLOWED EMERGENCY CHECKLIST PRIOR TO LANDING. BLEW DOWN W/ EMERGENCY PNEUMATIC AIR. ROTARY TEST VERIFED LIGHT INOPERATIVE. REMOVED AND REPLACED BULB, OPS CHECK GOOD. CYCLED GEAR 10 TIMES AFTER RESETTING BONov 4, 2005 · N807QS · Cessna 560CESSNA · Landing Gear Position and WarningSDR O2G2005F00012Squat Switch · failedAFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT TO UP POSITION. AIRCRAFT DIVERTED. CHANGED RT MAIN GEAR SQUAT SWITCH. (K) (NE03200604804)Oct 21, 2005 · N23YZ · Cessna 560CESSNA · Landing Gear Position and WarningSDR CA050725013Manifold · punctured(CAN) DURING CLIMB, THE ENGINE FIRE WARNING ANNUNCIATED. ENGINE THRUST WAS SELECTED TO IDLE, AN EMERGENCY DECLARED AND AN UNSCHEDULED LANDING PERFORMED AT POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED A PUNCTURED ENGINE FUEL MANIFOLD, EVIDENCE OF AN ENGJul 6, 2005 · Cessna 560CESSNA · Engine Fuel DistributionSDR CA050824005Fuel Control · malfunctioned(CAN) IN CRUISE, THE ENGINE EXHIBITED A 2% ROLL-BACK IN N1 SPEED WITH NO RESPONSE TO THROTTLE INPUT. FOLLOWING A DESCENT TO 10,000 FEET, THE ENGINE RECOVERED AND RESPONDED NORMALLY. THE MECHANICAL FUEL CONTROL UNIT WAS SUBSEQUENTLY REPLACED.Jun 21, 2005 · Cessna 560CESSNA · Fuel Control/Reciprocating EnginesSDR CA060303004Shuttle Valve · leakingBRAKE SHUTTLE VALVE LEAKING HYDRAULIC FLUID (SKYDROL) INTO PNEUMATIC EMERGENCY BRAKE CONTROL SYSTEM NECESSITATING THE REPLACEMENT OF THE EMERGENCY BRAKE CONTROL VALVE P/N 895232-0875. SHUTTLE VALVE REPLACED SYSTEM CHECK SERVICEABLE.May 31, 2005 · Cessna 560CESSNA · Master Cylinder/Brake ValveSDR CA050405008Display · failed(CAN) DISPLAY COLORS CHANGED, FUNCTION NORMAL UNIT GROUND TESTED. NORMAL. REPLACED WITH REPAIRED EXCHANGE UNIT. THIS WAS APPROXIMATELY 14 HOURS AFTER LIGHTNING STRIKE.Mar 26, 2005 · Cessna 560CESSNA · Integrated Flight SystemSDR CA050405007Rmu · failed(CAN) DISPLAY COLORS CHANGED, FUNCTION NORMAL UNIT GROUND TESTED NORMAL. REPLACED WITH EXCHANGE UNIT. THIS WAS APPROXIMATELY 14 HOURS AFTER LIGHTNING STRIKE.Mar 26, 2005 · Cessna 560CESSNA · Flight Management Computing Hardware SystemSDR CA050405006Rmu · failed(CAN) DISPLAY SCREEN COLORS CHANGED AFTER LIGHTNING STRIKE, FUNCTION NORMAL. UNIT GROUND TESTED NORMAL EXCEPT FOR COLOUR CHANGE. REPLACED UNIT WITH EXCHANGE UNIT.Mar 16, 2005 · Cessna 560CESSNA · Integrated Flight SystemSDR CA050405005Display · failed(CAN) DISPLAY SCREEN COLORS CHANGED AFTER LIGHTNING STRIKE, FUNCTION NORMAL. UNIT GROUND TESTED NORMAL, EXCEPT FOR COLOR CHANGE. REPLACED UNIT WITH EXCHANGE UNIT.Mar 16, 2005 · Cessna 560CESSNA · Integrated Flight SystemSDR CA050315009Gyro · failed(CAN) VERY SLOW TO SLAVE WHEN COLD SOAKED OVERNIGHT AT -20 DEGREES C. TOOK APPROXIMATELY 15 MINUTES TO ALIGN. AFTER ENGINE START, OPERATED OK DURING FOLLOWING FLIGHTS, UNTIL COLD SOAKED OVERNIGHT AGAIN WHEN VERY SLOW TO SLAVE. REPLACED DIRECTIONAL GYRO, GROFeb 25, 2005 · Cessna 560CESSNA · Directional Gyro and Indicating SystemSDR 2005FA0001401Line · damagedHYDRAULIC LINE, PN 6556000-20, ON LT ENGINE IS MAKING CONTACT WITH FUEL LINE PN 3042937-01. THIS CAUSED CHAFFING IN EXCESS OF 20 PERCENT OF THE WALL THICKNESS ON THE HYDRAULIC LINE AND 10 PERCENT TO 15 PERCENT WALL THICKNESS ON THE FUEL LINE. BOTH LINES WEREJan 24, 2005 · N511TH · Cessna 560CESSNA · Hydraulic System, MainSDR 2005FA0001402Control Valve · shortedFLAP CONTROL VALVE PN 2710970 TO BE MAKING CONTACT WITH DUMP VALVE PN OA55319-1 CAUSING WAS SUBSTIALLY DAMAGE. BY SHORTING THE STAND OFF ON THE BOTTOM SIDE OF THE DUMP VALVE BY APROX .1250 OF AN INCH A CLEARANCE OF APROX .0625 OF AN INCH WAS OBTAINED. (K)Jan 24, 2005 · N511TH · Cessna 560CESSNA · Hydraulic System, MainSDR CA050315008Solenoid Valve · leaking(CAN) FLAP HYDRAULIC SOLENOID VALVE WEEPING FLUID EXTERNALLY, UNABLE TO LOCATE LOCATION OF LEAK. THE BOTTOM OF THE VALVE IS WET AFTER FLIGHT.Jan 11, 2005 · Cessna 560CESSNA · Trailing Edge Flap Control SystemSDR CA050104007Rmu · failed(CAN) DISPLAY SCREEN LOST YELLOW AND GREEN COLOR LEAVING ONLY RED AND BLUE. REPLACED RMU WITH EXCHANGE UNIT. NOTE: THIS IS THE SECOND UNIT TO FAIL. THE FIRST FAILED WITH 264 HOURS TSN.Dec 9, 2004 · Cessna 560CESSNA · Attitude and Direction Data SystemSDR CA050104008Brake Assy · failed(CAN) WEEPING OF HYDRAULIC FLUID PAST PISTON PACKINGS, MFG SB 2-1601-32-2 RECOMMENDS INSTALLATION OF OVERSIZE PACKINGS P/N 68-1507 TO REDUCE THE PROBLEM. THESE PACKINGS WERE INSTALLED WHEN THE BRAKES WERE MANUFACTURED. APPROXIMATELY 325 LANDINGS IS NOT VERYNov 26, 2004 · Cessna 560CESSNA · BrakeSDR CA041126001Cable · broken(CAN) AC DEPARTED, DURING CLIMB THE PILOTS NOTICED THAT THE FLAP INDICATOR DID NOT MATCH FLAP SELECTOR HANDLE. FLAP POSITION WAS VERIFIED VISUALLY BY CO-PILOT PRIOR TO RETURNING TO BASE. UPON MAINTENANCE INVESTIGATION IT WAS FOUND THAT THE FWD FLAP FOLLOW-UPNov 22, 2004 · Cessna 560CESSNA · Trailing Edge Flap ActuatorSDR CA050315007Seal · leaking(CAN) CABIN AIR LEAK PAST CABIN DOOR SEALS IN FLIGHT WITH CABIN DIFFERENTIAL PRESSURE GREATER THAN APPROXIMATELY 7 PSI. BOTH DOOR SEALS REPLACED AND SHIMMED TO GIVE CORRECT GAP BETWEEN DOOR SEAL AND CABIN DOOR FRAME. NOTE: THE GAP WAS INCORRECTLY SET BY THE Nov 10, 2004 · Cessna 560CESSNA · Passenger/Crew DoorsSDR CA050104009Starter Gen · failed(CAN) GENERATOR FUNCTION OK IN FLIGHT, AFTER SHUTDOWN. ON ENGINE START, ENGINE WOULD NOT ROTATE. FOUND COMMUNTATOR AND BRUSHES DAMAGED BY ARCING.Oct 31, 2004 · Cessna 560CESSNA · Starter-GeneratorSDR CA041013005Plug · leaking(CAN) MAIN WHEEL ASSEMBLY LEAKING 1-2 PSI PER DAY. REPLACED 2 THERMAL RELIEF PLUGS AND LEAK CHECKED. OK.Sep 24, 2004 · Cessna 560CESSNA · Wheel/Ski/FloatSDR DXTA200400404Warning Light · illuminatedAT ROTATION GOT LOUD NOISE AND EXCESSIVE HEAT AND A NOTICEABLE ODOR WAS PRESENT. ANNUNCIATOR PANEL WAS CLEAR, PRESSURE SOURCE WAS NORMAL, ANNUNCIATOR PANEL EMERGENCY PRESSURE LIGHT CAME ON WHEN CYCLED KNOB TO RIGHT. EMERGENCY PRESSURE THEN BACK TO NORMAL -14Sep 21, 2004 · N806QS · Cessna 560CESSNA · Cabin Pressure Control SystemSDR CA040830007Valve · failed(CAN) EMERGENCY PRESSURIZATION VALVE CAME ON UNCOMMANDED ONCE FOR SEVERAL SECONDS IN FLIGHT. VALVE WAS REPLACED.NOTE: MFG REPORTS THIS IS A FLEET WIDE PROBLEM AND A NEW VALVE IS UNDERGOING CERTIFICATION.Aug 11, 2004 · Cessna 560CESSNA · Cabin Pressure Control SystemSDR CA040830004Panel · inoperative(CAN) FRONT PANEL OF AUDIO CONTROL UNIT DOES NOT ILLUMINATE ON NIGHT SETTING.Aug 3, 2004 · Cessna 560CESSNA · Audio Integrating SystemSDR CA040830008Display · failed(CAN) DISPLAY SCREEN WENT INCREASINGLY BRIGHT. BLUE AND THEN DIMMED TO GREEN. REPLACED RADIO MANAGEMENT UNIT. BEFORE COMPLETE FAILURE OF DISPLAY.Jul 13, 2004 · Cessna 560CESSNA · Central DisplaySDR CA040830006Plug · leaking(CAN) MAIN WHEEL/TIRE ASSEMBLY LEAKING AIR 2-4 PSI PER DAY. REPLACED THERMAL RELIEF PLUG ASSEMBLY. THIS IS THE SECOND PLUG ASSEMBLY TO BE REPLACED ON THIS WHEEL (THERE ARE THREE PLUGS PER WHEEL ASSEMBLY).Jul 9, 2004 · Cessna 560CESSNA · Wheel/Ski/FloatSDR FCPR200400014Fairing · missingLT MAIN LANDING GEAR FAIRING DEPARTED AIRCRAFT IN FLIGHT DUE TO FAILURE OF 1 AN525-10R18 FASTENER THAT SECURES UPPER PART OF DOOR TO TRUNNION. THE HEAD OF THE FASTENER IS MISSING. PHILLIPS HEAD DESIGN SEEMS TO HAVE WEAKENED THE FASTENER. RECOMMEND A STRONGEApr 30, 2004 · N591DK · Cessna 560CESSNA · Landing Gear DoorsSDR CA040519002Tube · worn(CAN) TUBE CHAFED INSIDE SUPPORTING CLAMP P/N S2894-24 TUBE 6555511-17 AND CLAMP (REVISED P/N 471-24) REPLACED LT AND RT ENGINE. THIS WAS FOUND DURING PERFORMANCE OF SB 560-71-05 WHICH WAS TO INSPECT TUBE AND INSTALL REVISED CLAMP.Apr 19, 2004 · Cessna 560CESSNA · Compressor Bleed ControlSDR CA040830005Relay · failed(CAN) CABIN INDIRECT LIGHTING WOULD NOT SHUT OFF. REPLACEMENT OF RELAY K162 RECTIFIED PROBLEM.Apr 8, 2004 · Cessna 560CESSNA · Passenger Compartment LightingSDR CA040519001Solenoid · weak(CAN) SECONDARY THROTTLE RT UNABLE TO ADVANCE PAST FLIGHT IDLE AFTER RT THRUST REVERSER DEPLOYED DUE TO WEAK INTERLOCK SOLENOID. SOLENOID ASSEMBLY 183238-001 REPLACED. OPERATION OF RT AND LT SECONDARY THROTTLE INTERLOCKS CHECK SATISFACTORY.Apr 1, 2004 · Cessna 560CESSNA · Engine Thrust ReverserSDR CA040518009Switch · out of limits(CAN) LT ENGINE ANTI-ICE LIGHT SLOW TO EXTINGUISH. LT UNDERTEMP SWITCH GOES OFF AT 340 DEGREES F, SHOULD GO OFF AT 300+/-7 DEGREES F. NEW SWITCH INSTALLED AND OPERATION CHECKED SATISFACTORY.Mar 26, 2004 · Cessna 560CESSNA · Air Intake Anti/De-Ice SystemSDR CA040518010Drive Assy · leaking(CAN) AIR CONDITIONER COMPRESSOR DRIVE PULLEY SHAFT OIL SEAL LEAKING OIL. AIR COMPRESSOR REPLACED.Mar 26, 2004 · Cessna 560CESSNA · Cabin Compressor SystemSDR CA040518001Manifold · leaking(CAN) OIL MANIFOLD FLARE FITTING MADE VERY POORLY, VERY ROUGH/SCRAPPED SURFACE ON FLARE MATING SURFACE, ALLOWING FITTING TO WEEP OIL. REPLACEMENT PART WAS NOT MUCH BETTER BUT NO OIL LEAKS.Feb 3, 2004 · Cessna 560CESSNA · Engine Oil Distribution (Airframe Furnished)SDR DXTA200400232Engine · flamed outWHILE DESCENDING THROUGH FL 310 WITH THE RIGHT POWER LEVER AT FLIGHT IDLE, THE BOOST PUMP CAME ON AND OIL PRESSURE DROPPED TO ZERO, GENERATOR WENT OFF-LINE. THE RIGHT ENGINE FLAMED OUT, IT THEN AUTO RELIT AT FL 290. REMOVED AND REPLACED THE RT ENGINE IAW CESSJan 28, 2004 · N804QS · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR CNQ2004F00000Uplock Switch · pinchedTHE NOSE LANDING GEAR FAILED TO LOCK IN THE UP POSITION. THE NOSE GEAR WOULD RETRACT AND EXTINGUISH THE HYDRAULIC PRESSURE LIGHT, BUT WOULD THEN FALL BACK OUT OF THE WHEEL WELL. FOUND SHIMMY DAMPENER INTERFERING WITH THE NOSE GEAR UPLOCK SWITCH WIRE BUNDLE. Jan 22, 2004 · N647CE · Cessna 560CESSNA · Landing Gear Position and WarningSDR DXTA200300208Fuel Control · failedRIGHT ENGINE FLAMED OUT DURING DESCENT (THROUGH 22000) PERFORMED RESTART WITHOUT EVENT. ENGINE OPERATION WAS NORMAL THROUGH THE REST OF FLIGHT, AIRCRAFT CONTINUED TO DESTINATION. SUMPTED RT FUEL TANK TO CHECK FOR WATER OR CONTAMINATION, SYSTEM CHECKED GOOD, IDec 22, 2003 · N804QS · Cessna 560CESSNA · Fuel Control/Turbine EnginesSDR DXTA200300050Bleed Valve · closedDURING TAKEOFF ROLL, WINDSHIELD HEAT AND MASTER WARNING ANNUNCIATORS ILLUMINATED. VALVES WERE CLOSED AND SWITCHES WERE OFF. - RAN AIRCRAFT AND DUPLICATE SQUAWK. REMOVED AND REPLACED BLEED AIR VALVE IAW 560 MM CH 30-41-00.Jun 18, 2003 · N801QS · Cessna 560XL · Compressor Bleed ValveSDR CA030731011Line · chafed(CAN) LT AND RT BRAKE HYD LINES WERE FOUND TO BE CHAFING ON ELEVATOR CONTROL CABLES AT F.S.178.00. THIS DISCREPANCY IS BELIEVED TO HAVE OCCURRED AT MANUFACTURE. AS THIS WAS THE FIRST TIME THE FLOOR PANEL HAD BEEN REMOVED. THIS AREA IS A PLACE WHERE THE HYDRAUJun 9, 2003 · Cessna 560CESSNA · Landing Gear Brake SystemSDR CWQ2003F00004Bracket · brokenDURING ROUTINE INSP OF GEAR CYCLE AND UPLOCK CHECKS NOTICED THAT RT MAIN GEAR HAD PROBLEMS IN UP AND LOCKED POSITION. UPON FURTHER INSP FOUND (PN 6521641-2) UPLOCK HOOK ATTACH BRACKET CRACKED 2.25 INCHES, STARTING FROM LOWER EDGE OF BACKET MOVING IN VERTICAL Feb 21, 2003 · N800QS · Cessna 560CESSNA · Main Landing Gear
Back to Pratt & Whitney Canada PW535A