Pratt & Whitney Canada PW535A

Service difficulty reports · 251

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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 = 'PW535A'
  ORDER BY difficulty_date DESC"

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SDR CA140310010Control Cable · misinstalledCABLE, PN 6560141-6, ORDERED FOR REPLACEMENT DURING PHASE 5 INSPECTION. PRIOR TO INSTALLATION AME NOTICED THE BALL END WAS SWAGED ON BACKWARDS. THE SHANK END OF THE BALL SWAGE THAT IS TO PROTRUDE THROUGH THE FORK WAS FACING THE WRONG WAY. A CABLE WAS RE-ORDMar 10, 2014 · Cessna 560CESSNA · Aileron Control SystemSDR CA140313005Generator · failedTHE AIRCRAFT HAD A GENERATOR NR 2 FAILURE, BUT THE PILOTS NEVER RECEIVED A SIGNAL MESSAGE. THE PILOTS THEN NOTICED THE GENERATOR VOLTAGE WAS LOW. THEY WENT THROUGH THE CHECK LIST FOR THE GENERATOR FAILURE, ENDED UP TURNING THE NR 2 GENERATOR OFF. CREW NOTICEDFeb 28, 2014 · Emb EMB505 · AC Generator-AlternatorSDR CA140302001Engine · flamed out(CAN) DURING TAXI MANEUVERS THE LT ENGINE FLAMED OUT. CONFIRMED COLD WEATHER, -31 CELSIUS, FLAMEOUT BEHAVIOR EXPERIENCED PREVIOUSLY.Feb 28, 2014 · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR CA140312003Hmu · malfunctionedWHILE TAXIING, AS THE THROTTLES WERE MOVED BACK TO IDLE, 1 ENGINE SHUTDOWN. THE HMU WILL BE REPLACED.Feb 24, 2014 · Cessna 560CESSNA · Fuel Controlling SystemSDR DXTA2014021705655Bleed Valve · malfunctionedWHILE LEVELING OFF AT 6000 FEET, LT ENG BEGAN TO VIBRATE, N1 BEGAN TO DECREASE, ITT INCREASED TO APPROXIMATELY 650 DEGREES. ITT DECREASED WITH POWER LEVER RETRACTION & VIBRATION BECAME NOMINAL AT APPROXIMATELY 35% N1. TROUBLE SHOT & REPLACED LT BOV TORQUE MOFeb 15, 2014 · N804QS · Cessna 560CESSNA · Compressor Bleed ValveSDR CA140224005Fuel Control · leaking(CAN) AFTER LANDING, A SIGNIFICANT FUEL LEAK WAS OBSERVED FROM THE FUEL CONTROL. TROUBLESHOOTING ONGOING.Feb 8, 2014 · Fuel Control/Turbine EnginesSDR 9JLA2014030704370Wire Harness · defectiveCREW REPORTED THE ITT GAUGE DISPLAYED AN INTERMITTENT RED X IN FLIGHT. TROUBLESHOOTING FOUND THE LT ENG ELEC HARNESS DEFECTIVE. SERVICE BULLETIN PW500-72-30474 WAS COMPLIED WITH ON BOTH ENGINES TO REPLACE THE WIRING HARNESS.Feb 4, 2014 · N732AC · Emb EMB505 · Engine Indicating System WiringSDR CA140202002Engine · power loss(CAN) THE ACFT EXPERIENCE AN ENGINE POWER ROLLED BACK DURING THE APPROACH. THE ACFT LANDED SAFELY WITH BOTH ENGINES RUNNING. THE FUEL SYSTEM INVESTIGATION IS ONGOING BY PERSONNEL.Jan 20, 2014 · Engine (Turbine/Turboprop)SDR CA131227001O-Ring · damaged(CAN) A FUEL LEAK WAS DISCOVERED PRIOR TO DELIVERY OF ACFT. A FEW DROPS OF FUEL IAW FLIGHT WAS LEAKING FROM A MANIFOLD. FOUND A DAMAGED O-RING ON A TRANSFER TUBE, ON THE FUEL MANIFOLD. THE ENGINE WAS REPAIRED AND RETURNED TO SERVICE.Dec 21, 2013 · Cessna 560CESSNA · Engine Fuel DistributionSDR CA131219010Rmu · frozen(CAN) RMU SCREEN FREEZES THEN GOES BLANK. THESE PARTS WERE A PRODUCT IMPROVEMENT INSTALLED. THERE HAVE BEEN 2 FAILURES OF THE NEW PARTS AND BOTH HAVE HAD INTERMITTENT PREVIOUS FAILURES PRIOR TO FINALLY FAILING AND BEING REPLACED. THIS UNIT WAS INSTALLED. THDec 14, 2013 · Cessna 560CESSNA · Communications SystemSDR DXTA2014022005659Cowling · departedDURING INITIAL DESCENT, WE NOTICED A SLIGHT VIBRATION. AT APPROXIMATELY 30000 FT & .73 MACH, WE HEARD A LOUD POP & FELT A SLIGHT YAW OF THE ACFT. WE THOUGHT A GEAR DOOR HAD DEPARTED THE ACFT & INFORMED ATC OF THAT. AUTOPILOT STAYED ENGAGED & ALL ENG INSTRUMEDec 2, 2013 · N810QS · Cessna 560CESSNA · Engine Cowling SystemSDR CA130916001Nut · missing(CAN) ENGINE MFG HAS COME ACROSS 1 UNAPPROVED PART OF MS9198-06 WHICH WAS INSTALLED ON A HIGHER LEVEL ASSY, PN 3073363-01, FUEL PRESSURE TUBE WHERE THE MS PART IS MISSING THE HOLE REQUIRED FOR THE SAFETY WIRE. ENGINE MFG IS CURRENTLY INSPECTING THE REST OF TSep 16, 2013 · Aircraft Fuel SystemSDR CA130909009Oil System · low pressure(CAN) DURING CLIMB THROUGH 200, 300, AGL THE CREW NOTED THAT THE NR 2 ENGINE OIL PRESSURE WAS LOW AND FLUCTUATING. THEY OBSERVED VALUES AS LOW AS 25 PSID. THE LOW OIL PRESSURE ANNUNCIATOR DID NOT ILLUMINATE. THROUGH 1000 FT AS THEY LEVELED THE ACFT AND REDUAug 29, 2013 · Cessna 560CESSNA · Engine Oil PressureSDR CA130903003Fire Detector · false activation(CAN) THE PILOT REPORTED THAT AT 25000 FT, THE RT ENGINE FIRE BELL AND LIGHT SOUNDED AND ILLUMINATED. THE RT ENGINE WAS SHUTDOWN, THE PILOT DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. ON GROUND, FIREMEN DID NOT NOTICE FIRE EVIDENCE AND DID NOT USE AAug 24, 2013 · Cessna 560CESSNA · Fire DetectionSDR CA130729013Engine · power loss(CAN) UPON STARTUP, THE CREW RECEIVED A WARNING OF "NO DISPATCH" FOR THE ENGINES. THE ACFT WAS COMPLETELY SHUTDOWN AND RE-BOOTED AND THE ISSUE WAS CLEARED. DURING THE SUBSEQUENT T/O, THE LT ENGINE POWER ROLLED BACK AND THE T/O WAS ABORTED. AS THE ACFT WAS TAJul 24, 2013 · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR CA130823005Bracket · misinstalled(CAN) A PRESSURE OIL TUBE SUPPORT BRACKET WAS FOUND CRACKED DURING ROUTINE MAINTENANCE. THE BRACKET WAS WELDED BACKWARD ONTO THE TURBINE EXHAUST CASE ASSY FROM PRODUCTION CAUSING THE STRESSES TO CRACK THE BRACKET. AN SB WILL BE ISSUED SHORTLY TO INSPECT ALL PJul 3, 2013 · Cessna 560CESSNA · Turbine SectionSDR 2013FA0000331Controller · multiple failON APPROUCH AT 5000’MSL, WITH ALL A/I ON; THE CAS MESSAGES BLEED 1 FAIL AND BLEED 2 FAIL CAME ON AT THE SAME TIME. THE AIRCRAFT HAD NO SOURCE OF BLEED AIR BUT WAS LANDED WITHOUT INCIDENT. ON THE GROUND WITH THE RH ENGINE STILL RUNNING THE CAS MESSAGES WERE CApr 24, 2013 · N195MC · Emb EMB505 · Pneumatic Distribution SystemSDR DXTA2013050805380Lock Nut · unserviceableREMOVED NR 2 ENGINE FROM SN 560-0786 DUE TO FAILURE OF THE COMBUSTION CHAMBER LINER COOLING RING SEGMENT SELF LOCKING NUTS. REF THE SPECIAL INSTRUCTIONS 35-2013, BORESCOPE INSPECTION.Apr 19, 2013 · N819QS · Cessna 560CESSNA · Turbine Engine Combustion SectionSDR DXTA2013050805382Ring Assembly · damagedDURING BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINER COOLING RING SEGMENT SELF LOCKING NUTS. FOUND TWO NUTS MISSING AT THIS TIME AT POSITION NR 18 AND NR 31. COMPLIED WITH A HOT SECTION REPAIR & SI 36-2013.Apr 9, 2013 · N823QS · Cessna 560CESSNA · Turbine Engine Combustion SectionSDR CA130416016Pin · missing(CAN) DURING TAKEOFF,M THE RT ENGINE FIRE WARNING WAS ACTIVATED AND THE PILOT SHUTDOWN THE ENGINE. THE ACFT LANDED SAFELY AT POINT OF DEPARTURE. PRELIMINARY EXAMINATION REVEALED THAT A COMBUSTION CHAMBER PIN WAS FOUND MISSING/BURNED. THE ENGINE HAS ABOUT 8Apr 7, 2013 · Turbine Engine Combustion SectionSDR UG8A2013031901Wire Harness · openDESCENDING, THE LT THRUST REVERSER UNLOCK LIGHT ILLUMINATED. REMOVED LT THRUST REVERSER AND INSTALLED NEW DEPLOY/ STOW WIRE HARNESS, PN 53ND78303-1 AND RIGGED IAW CMM PN 03ND-78002, 78-30-12 PARA C, PAGE 703. INSTALLED LT THRUST REVERSER IAW MM 78-31-00. BLMar 19, 2013 · N911UM · Cessna 560CESSNA · Engine Exhaust System WiringSDR DJFA20130309002Window · failedCREW REPORTED DURING FLIGHT A LOUD THUD WAS HEARD FOLLOWED BY THE RIGH SIDE COCKPIT WINDOW SHATTERED. AN EMERGENCY WAS DECLARED AND ACFT DIVERTED, ACFT LANDED SAFELY. MX R & R THE WINDOW. OPERATION CHECK OF THE HEATING CHECK WAS PEFORMED WITH NO DISCREPANCIMar 9, 2013 · N335FL · Emb EMB505 · Flight Compartment WindowsSDR CA130227006Controller · failed(CAN) BLEED 1 FAIL CAS, BLEED 2 FAIL CAS MESSAGE ANNUNCIATED DESCENDING THROUGH 10,000. CABIN DEPRESSURIZED. NOTED RED X THROUGH BOTH PRSOVS. VCS FAIL RED X THROUGH VCS ON ECS PANE. AMS CONTROLLER PN ON/OFF SYLZ-53632-203, SN OFF: 0177, SN ON: 0120 REPLACED.Feb 18, 2013 · Emb EMB505 · Cabin Pressure ControllerSDR CA130212005Cable · loose(CAN) VENTRAL RUDDER FAIL" CAS UPON LANDING. VENTRAL AUTO-PILOT SERVO CABLE FOUND AT O LBS TENSION. CABLE TENSIONED TO 45 LBS AND FUNCTION SYS IS SERVICEABLE.Feb 8, 2013 · Emb EMB505 · Autopilot SystemSDR DJFA20130113001Control Unit · failedCREW REPORTED DURING APPROACH IN FULL LANDING CONFIGURATION A "BRAKE FAIL" CAS MESSAGE ILLUMATED. AN EMERGENCY WAS DECLARED AND EMEGENCY BRAKE SYS WAS USED TO STOP ACFT SAFE AND UNHARMED. MX FOUND THE BRAKE CONTROL MODULE HAD FAILED AND REPACED IT.Jan 13, 2013 · N329FL · Emb EMB505 · Landing Gear Brake SystemSDR CA130109004Wire Harness · failed(CAN) ON LANDING THE FLIGHT CREW HAD AN ANTI-SKID FAIL, FLAP FAIL & LANDING GEAR WOW SYS FAIL CAS MESSAGE. AFTER THE ACFT WAS SHUTDOWN AND POWERED BACK ALL 3 MESSAGES DID NOT REAPPEAR. ON CLIMBOUT THE MLG WOULD NOT RETRACT UTILL THE MANUAL OVERRIDE BUTTON WASJan 6, 2013 · Emb EMB505 · Landing Gear System WiringSDR CA121212012Strut · damaged(CAN) AFTER TAKEOFF, CREW NOTED A RED GEAR UNLOCKED ANNUCIATOR. MASTER CAUTION THEN ILLUMINATED WITH A HYD PRESSURE ANNUNCIATOR. ABNORMAL CHECKLIST CALLED FOR HYD CONTROL CIRCUIT BREAKER TO BE OPENED. THE LT GEAR LEG FELL TO DOWN AND LOCKED. CREW RETURNEDDec 9, 2012 · Cessna 560CESSNA · Main Landing Gear Strut/Axle/TruckSDR CA121130013Engine · flamed out(CAN) FOLLOWING NORMAL ENGINE STARTS, THE THROTTLE LEVERS WERE ADVANCED TO BEGIN TAXING AND THE RT ENGINE FLAMED OUT. THE AFT WAS STOPPED AND A RESTART OF THE RT ENGINE ATTEMPTED WHICH WAS UNSUCCESSFUL. WHEN THE CREW ATTEMPTED TO MANUVER BACK TO THE HANGAR ANNov 28, 2012 · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR DJFA20121112001Access Door · detachedCREW REPORTED DURING POST FLIGHT INSPECTION THAT MOST OF THE BATTERY DOOR WAS MISSING FROM THE ACFT. MX INSTALLED A SERVICABLE DOOR.Nov 12, 2012 · N317FL · Emb EMB505 · Electrical/Electronic Compartment DoorsSDR DJFA20121024001Starter Gen · vibrationTHE CREW ADVISED AT FL450 THEY EXPERIENCED A HIGH VIBRATION FROM THE NR 2 ENGINE ACCOMPANIED BY A NR 2 GENERATOR FAILURE, THE CREW FOLLOWED THE CHECKLIST FOR HIGH VIBE WHICH ULTIMATELY RESULTED WITH SHUTTING NR 2 ENGINE DOWN IN FLIGHT AND DECLARING AN EMERGENOct 24, 2012 · N311FL · Emb EMB505 · Starter-GeneratorSDR CWQR20120914049Drag Angle · crackedDURING A SCHEDULED INSPECTION, FOUND THE LT WING TO FUSELAGE FAIRING DRAG ANGLE THAT ATTACHES TO THE WING, WAS CRACKED A 3 FASTENER LOCATIONS.Sep 14, 2012 · N804QS · Cessna 560CESSNA · Fuselage Main, StructureSDR CWQR20120914050Drag Angle · crackedDURING A SCHEDULED INSPECTION, FOUND RT WING TO FUSELAGE FAIRING DRAG ANGLE THAT ATTACHES TO THE WING, WAS CRACKED AT THREE FASTENER LOCATIONS.Sep 14, 2012 · N804QS · Cessna 560CESSNA · Fuselage Miscellaneous StructureSDR DXTA2012083005111Bungee · failedWHILE TAXIING FOR 1ST FLIGHT CREW COULD HEAR INTERMITTENT GROANING TYPE OF NOISE IN NOSE GEAR AREA WHILE MAKING LEFT, RIGHT TURNS AND HEADING STRAIGHT AHEAD. BRAKING APPEARED NORMAL AND DIDN'T EFFECT NOISE. NOSE STRUT AND TIRE LOOK NORMAL. RUDDER STEERING SEEMAug 30, 2012 · N801QS · Cessna 560CESSNA · Landing Gear Steering SystemSDR DXTA2012082705106Warning Light · false activationGEAR UNLOCKED WARNING OCCURRED AFTER TAKEOFF. CHECKLIST FOLLOWED WITH A NORMAL GEAR EXTENSION. ACFT JACKED, GEAR OPS CHECKED AND FOUND NORMAL. UPLOCK SWITCHES CHECKED BY PERFORMING RESISTANCE CHECKS AND FOUND SATISFACTORY. LANDING GEAR DISCONNECT CONNECTORAug 26, 2012 · N839QS · Cessna 560CESSNA · Landing Gear Position and WarningSDR DXTA2012080605079Outflow Valve · failedIN CRUISE FLIGHT (FL450) CABIN BEGAN TO LOSE PRESSURE. EXECUTED RAPID DESCENT, CABIN BUMPED A COUPLE OF TIMES, CABIN DESCENT STOPPED BRIEFLY, THEN CONTINUED. MANUAL CABIN CONTROL HAD ABSOLUTELY NO EFFECT. R & R THE PRIMARY OUTFLOW VALVE IAW MM 21-32-00. COMPAug 6, 2012 · N825QS · Cessna 560CESSNA · Pressure Regulator/Outflow ValveSDR CA120619007Unknown · odor(CAN) DURING DESCENT, VIBRATIONS WERE FEL, ACCOMPANIED WITH THE ODOR OF OIL IN THE CABIN. ENG PARAMETERS WERE DECREASING WITH NO RESPONSE TO THROTTLE LEVER MOVEMENT. THE ENGINE WAS SHUTDOWN & AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPLISHED. POST FLIGHTJun 13, 2012 · Gulstm 560 · Air Distribution SystemSDR CA120207006Screw · sheared(CAN) CREW NOTED WHILE CLEANING ACFT A MISSING SCREW IN THE LT MAIN GEAR TRUNION FAIRING. SCREW WAS REPLACED WITH NEW. THIS HAS HAPPENED BEFORE ON THE OTHER ENCORE ACFT AND WILL LIKELY HAPPEN AGAIN. THE FAIRING COULD COME OFF IN FLIGHT IF THIS SCREW IS MISSFeb 6, 2012 · Cessna 560CESSNA · Landing Gear SystemSDR CA111128008Lock Nut · loose(CAN) LOCK NUT HAS NO LOCKING CAPABILITY, CAME LOOSE THUS REDUCING THE LT TURN RANGE OF THE NOSE STEERING. NUT WAS REPLACED WITH NEW AND SYSTEM IS SERVICEABLE.Nov 22, 2011 · Cessna 560CESSNA · Steering UnitSDR CA111019011Engine · malfunctioned(CAN) WHILE TAXING JUST BEFORE T/O, THE ENGINE ACCELERATED UNCOMMANDED. THE FUEL WAS CUTOFF AFTER 10-15 SEC. THE PILOT REPORTED THE ENGINE TEMPERATURE REACHED THE MAXIMUM GAUGE LIMIT OF 750 DEG. THE ENGINE WILL BE REMOVED AND FORWARDED FOR INVESTIGATION.Oct 16, 2011 · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR CA111019002Transfer Sys · inoperative(CAN) DURING CRUISE, AT FL430, THE ENGINE SHUT ITSELF DOWN WITH NO PRIOR WARNING OR ABNORMAL PARAMETERS. RELIGHT ATTEMPTS WERE UNSUCCESSFUL AND THE ACFT MADE A SAFE SINGLE ENGINE LANDING. DURING DESCENT, THE PILOT WAS UNABLE TO TRANSFER FUEL CROSS FEED INOPEROct 4, 2011 · Cessna 560CESSNA · Aircraft Fuel Distribution SystemSDR CA110914004Engine · power loss(CAN) DURING REVENUE FLIGHT, CREW REPORTED LT ENGINE WAS AT 87 PERCENT N1 AND THEY WERE NOT ABLE TO MODULATE THRUST. CREW ELECTED TO SHUTDOWN ENGINE AND WERE UNSUCCESSFUL AT RE-STARTING THE ENGINE. AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED. TROUBLESHSep 11, 2011 · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR DJFA2011032Skin · crackedDURING INSPECTION OF ENGINE INLETS, CRACKS AND MISSING/DAMAGED FASTENERS WERE FOUND ON THE LT ENGINE INLET. THE FASTENERS WERE REPLACED. ADDITIONAL C/A REQUIRE THE REPLACEMENT OF THE INLET WITH A -405 UNIT; IN THE MEAN TIME, THE ACFT MFG HAS DETERMINED THATJun 28, 2011 · N300FL · Emb EMB505 · Engine Air Intake SystemSDR DJFA2011028Inlet · crackedDURING INSPECTION OF ENGINE INLETS, CRACKS AND MISSING/DAMAGED FASTENERS WERE FOUND ON THE RT ENGINE INLET. AIRCRAFT MANUFACTURER HAS DETERMINED THAT THE DAMAGE IS ACCEPTABLE AND HAS ALLOWED THE INLET TO CONTINUE IN SERVICE WITH ADDITIONAL PERIODIC INSPECTIONJun 10, 2011 · N307FL · Emb EMB505 · Engine Air Intake SystemSDR DJFA2011014Inlet · crackedDURING INSP OF LT ENGINE INLET, CRACKS WERE FOUND AT THE 9 AND 3 OCLOCK POSITIONS. DURING INSPECTION OF LH ENGINE INLET, CRACKS WERE FOUND AT THE 9 AND 3 OCLOCK POSITIONS. REPAIRED CRACKS ON INLET IN ACCORDANCE WITH ISR 8000027867R1.Apr 3, 2011 · N304FL · Emb EMB505 · Engine Air Intake SystemSDR CA110315013Pitot Line · malfunctioned(CAN) ON TAKE ROLL THE RT AIRSPEED WOULD LAG BEHIND LT AIRSPEED BY APPRORX 70 KNOTS ALL OTHER INDICATIONS ASSOCAITED WITH PITOT/STACTIC SYSTEM NORMAL. NO WARNINGS EXPECT AIRSPEED MIS COMPARE. WOULD CORRECT ITSELF SHORTLY. THIS HAPPEND INTERMITTENTLY NOT ON EVMar 11, 2011 · Cessna 560CESSNA · Pitot/Static SystemSDR E07A392ASInlet · crackedON PREFLIGHT INSP, 2 CRACKS WERE FOUND IN THE RT ENGINE INLET. THE INLET WAS INSPECTED WITH EDDY CURRENT AND ANOTHER 8 CRACKS WERE FOUND. INLET WAS REPLACED AND ACFT WAS RETURNED TO SERVICE. A VIBRATION AND SONIC SURVEY WERE COMPLIED WITH, NO DEFECTS WERE Feb 11, 2011 · N392AS · Emb EMB505 · Engine Air Intake SystemSDR KNQ2011F00000Pump · obstructedAFTER A NORMAL START, LT POWER LEVER WAS ADVANCED TO TAXI, AND WHEN RETARDED SLIGHTLY TO ADJUST POWER SETTING, THE "LOW FUEL PRESSURE" ANNUNCIATOR WAS NOTED TO BE ILLUMINATED BRIEFLY FOLLOWED BY THE "LT FUEL PUMP ON" ANNUNCIATOR. TURNING THE ELECTRIC FUEL PUMJan 17, 2011 · N700NK · Cessna 560CESSNA · Aircraft Fuel Distribution SystemSDR DXTA2011010304389Gyro · malfunctionedSTBY GYRO DISPLAYED "EXT MANUV" ANNUNCIATOR AND SHOWED A 10 DEGREE RT BANK AND HEADING PRECESS OF MORE THAN 180 DEGREES. HEADING PRECESS ABOUT 10 DEGREES EVERY 2 MINUTES. REPLACED STANDBY GYRO (SECONDARY FLIGHT DISPLAY) WITH REPAIRED UNIT, OPS CHECKED NORMAL.Jan 1, 2011 · N818QS · Cessna 560CESSNA · Attitude and Direction Data SystemSDR E07A20101220001Inlet · crackedDURING POSTFLIGHT, IT WAS DISCOVERED THAT THE INLET LIP ON THE NR2 ENGINE IS COMING APART. IT HAS A SEGMENT OF MATERIAL MISSING. CRACKED IN 2 OTHER LOCATIONS AND 3 RIVET HEADS MISSING IN ANOTHER LOCATION.Dec 20, 2010 · N392AS · Emb EMB500 · Engine (Turbine/Turboprop)SDR CWQR201006Door · stuck(CWQR) DURING A SCHEDULED MX EVENT, THE EMERGENCY EXIT DOOR WAS REMOVED. REMOVAL OF THE EMERGENCY EXIT DOOR WAS FOUND TO BE VERY DIFFICULT. REQUIRED 2 TECHS AND 10 MINUTES TO WORK DOOR LOOSE. THE OPERATOR VERIFIED THAT EMERGENCY DOOR INSP ASL-560-52-04 HAD PDec 14, 2010 · N844QS · Cessna 560CESSNA · Emergency Exits
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