Textron 525

Service difficulty reports · 260

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 aircraft_model_key = '525'
  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 2007FA0000161Transistor · shortedINVESTIGATED COCKPIT OVERHEAD FLOODLIGHTS TRIPPING ASSOCIATED CB WHEN BATTERY POWER APPLIED TO AIRCRAFT. FOUND ATTACHING SCREW FOR QC001 TRANSISTOR SHORTING TO AIRFRAME. ALSO, FOUND RESISTOR NR150 ON THRUST ATTENTUATOR PC BOARD NZ017 BURNED. REPAIRS REQUIREDec 13, 2006 · N66AM · Cessna 525 · Flight Compartment LightingSDR D6J2006F00000Squat Switch · out of adjustLANDING GEAR WOULD NOT RETRACT AFTER DEPARTURE FROM RDU. NO PASSENGERS WERE ONBOARD. FLIGHT WAS CONTINUED WITH GEAR DOWN AND LOCKED TO GSO FOR REPAIRS. THE SERVICE CENTER AT GSO TROUBLESHOT AND FOUND THE LANDING GEAR SQUAT SWITCHES TO BE OUT OF ADJUSTMENT. Dec 8, 2006 · N525DG · Cessna 525 · Landing Gear Position and WarningSDR 120706N152CS1Connector · looseAFTER TAKEOFF, THE POWER BRAKE LOW PRESSURE AND ANTI-SKID WARNING INDICATION LIGHTS ILLUMINATED. THE AIRCRAFT DIVERTED AND DECLARED AN EMERGENCY. UPON LANDING, AFTER EXTENDING THE LANDING GEAR, THE BRAKE LOW PRESSURE AND ANT-SKID WARNING INDICATION LIGHTS EXTIDec 7, 2006 · N152CS · Cessna 525 · Landing Gear System WiringSDR 111406N420CS1Brake Assy · unknownON FINAL, THE CREW LOWERED THE GEAR AND HAD 3 GREEN AND A POWER BRAKE LOW PRESSURE ANNUNCIATOR. DO TO RUNWAY LENGTH THE CREW ELECTED TO CONTINUE WITH THE APPROACH AND LANDING. THE AIRCRAFT TOUCHED DOWN AND WAS ALLOWED TO SLOW DURING THE ROLLOUT, THE EMERGENCNov 14, 2006 · N420CS · Cessna 525 · BrakeSDR 103106N128CS1Anti-Skid Sys · malfunctionedAFTER LOWERING LANDING GEAR, THE ANTI-SKID AND BRAKE PRESSURE WARNING LIGHTS ILLUMINATED AND THE BRAKE SYSTEM CIRCUIT BREAKER POPPED. THE CHECKLIST WAS RUN AND THE CIRCUIT BREAKER FAILED TO RESET. THE CREW DECLARED AN EMERGENCY, THE AIRCRAFT LANDED AND STOPPOct 28, 2006 · N128CS · Cessna 525 · Brake Anti-Skid SectionSDR 101906N133CS1Seal · leakingAFTER TAKEOFF FROM CMH A STRONG BURNING ODOR WAS NOTICED BY THE CREW AND THERE WAS A HAZE FILLING THE CABIN. THE CREW ELECTED TO CALL ATC AND REQUEST A DIVERSION BACK TO CMH. AFTER EXPLAINING PROBLEM AIRCRAFT WAS CLEARED TO LAND. LANDING WAS NORMAL. PROBLEOct 19, 2006 · N133CS · Cessna 525 · Engine (Turbine/Turboprop)SDR 2006FA0001029Stud · brokenCOMPONENT STUD APPEARS TO HAVE BEEN CRACKED FOR SOME TIME, RUST EVIDENT HALF WAY THRU BOLT CROSS SECTION AT THE START OF THE THREADED AREA, NEAR CENTER OF THE STUD. COULD POSSIBLY HAVE BEEN CAUSED BY MFG FLAW, OVER TORQUEING OF SAFETY JAMB NUTS, TO OVER RIGGINOct 9, 2006 · N902GW · Cessna 525 · Landing Gear DoorsSDR 2006FA0001023Valve · failedCREW REPORTED ALL HYDRAULIC SYSTEMS INOPERATIVE IN FLIGHT. LANDING GEAR WAS EXTENDED PNEUMATICALLY AND AIRCRAFT LANDED WITHOUT INCIDENT. IT WAS DETERMINED THE HYDRAULIC LOADING VALVE WAS NOT CLOSING ALLOWING HYDRAULIC PRESSURE TO BUILD. THE HYDRAULIC LOADINOct 6, 2006 · N122CS · Cessna 525 · Hydraulic System, MainSDR 2006FA0001021Valve · malfunctionedCREW REPORTED (HYDRAULIC PRESSURE ON) LIGHT STAYED ILLUMINATED AFTER LANDING GEAR RETRACTION. REPLACED LOADING VALVE AND OPERATIONALLY CHECKED HYDRAULIC SYSTEM. AIRCRAFT WAS RETURNED TO SERVICE. (K)Oct 6, 2006 · N122CS · Cessna 525 · Landing Gear Retraction/Extension SystemSDR WI5R1005001Turbine Blades · fracturedDURING A PRE-BUY A/C INSPECTION, ENGINE SN 1903 WAS FOUND TO EXHIBIT A FRACTURED TRAILING EDGE OF HP TURBINE BLADE.Oct 5, 2006 · N103CS · Cessna 525 · Turbine SectionSDR Z5FA100206001Solenoid Valve · failedAFTER TAKING OFF FROM MKE ON A CHECK FLIGHT/POSITIONING LEG TO BDR THE AIRCRAFT EXPERIENCED A COMPLETE HYDRAULIC PRESSURE SYSTEM FAILURE. THE LANDING GEAR WAS UP AND LOCKED AND THE FLAPS HAD JUST REACHED 0 DEGREES. THE CHECK FLIGHT WAS TO VERIFY THAT THE REPOct 2, 2006 · N122CS · Cessna 525 · Hydraulic System, MainSDR DJFA2006325Window · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A WINDSHIELD PRISM INSPECTION MAINTENANCE DISCOVERED FIVE FRACTURES IN A ROW RUNNING ALONG THE CO-PILOTS SIDE WINDOW FASTENER HOLES. THE CO-PILOTS SIDE WINDOW AND SEALS WERE REPLACED. SATISFACTORY LEAK CHOct 1, 2006 · N239CW · Cessna 525 · Flight Compartment WindowsSDR 91606N133CS1Bulb · burned outON APPROACH INTO APA, AFTER EXTENDING THE LANDING GEAR THE CREW NOTED THAT A DOWN AND LOCKED RT MAIN GEAR WAS NOT ILLUMINATED. ALL OTHER INDICATIONS WERE NORMAL AND FLY-BY TOWER REPORTED GEAR LOOKED DOWN. CREW DECLARED AN EMERGENCY, FOLLOWED ABNORMAL CHECKLISep 16, 2006 · N133CS · Cessna 525 · Landing Gear Position and WarningSDR 91306N128CS1Unknown · odorDURING DESCENT FROM FL380 TO FL 330 THE DUCT OVERHEAT LIGHT ILLUMINATED AND A VERY STRONG BURNING SMELL ENTERED THE CABIN AND COCKPIT. THE DIFFICULTY IN BREATHING CAUSED CREW TO SUSPECT POSSIBLE SMOKE SO THEY DESCENDED QUICKLY AND DECLARED AN EMERGENCY, REQUESep 13, 2006 · N128CS · Cessna 525 · Air Distribution SystemSDR DJFA2006310Carbon Seal · leakingTHE CREW NOTED A STRONG MILDEW ODOR AND A BURNT PLASTIC SMELL DURING FLIGHT AFTER TAKE OFF. MAINTENANCE WAS ABLE TO VERIFY THE DISCREPANCY AS AN AFT EVAPORATOR THAT SMELLED MUSTY. THE FINS OF THE FORWARD AND AFT EVAPORATORS WERE CLEANED AND THE DRAINS WERE VAug 28, 2006 · N248CW · Cessna 525 · Pneumatic Distribution SystemSDR CA060901003Fadec · failed(CAN) THE RT ENGINE FADEC CHANNEL A FAULT LIGHT ILLUMINATED. MAINTENANCE ACCESSED FADEC DATA AND DOWNLOADED FAULT CODES. FAULT CODES FORWARDED TO MFG, DURING TELEPHONE CONVERSATION WITH MFG OF AC AND ENG, IT WAS DETERMINED THAT THE FADEC HAD AN INTERNAL FAULT.Aug 23, 2006 · Cessna 525 · Fuel Controlling SystemSDR 2006FA0000867Support Bracket · crackedFOUND THE LT AND RT ATTENUATOR ACTUATOR LOWER SUPPORT BRACKETS TO BE CRACKED. THESE BRACKETS HAVE BEEN REPLACED BY ACCOMPLISHMENT OF SB AT PRIOR DATE. WE HAVE REPEATEDLY FOUND THESE BRACKETS. CRACKED AGAIN AND AGAIN AFTER THEY ARE REPLACED BY THE SB. CUSTOAug 18, 2006 · N719D · Cessna 525 · Electrical Power SystemSDR 2006FA0000859Servo · malfunctionedTECH WAS IN TAILCONE AREA AND NOTICED METAL SHAVINGS UNDER RUDDER SERVO ASSY. INVESTIGATION REVEALED THAT THE SERVO DRUM CABLE WAS CUTTING THROUGH THE DRUM GROOVES ARE TO SEVERE SIDE LOADING ON THE CABLE. SUSPECT THAT THE SEVERE SIDE LOAD CONDITION RESULTEDAug 17, 2006 · N719D · Cessna 525 · Rudder Control SystemSDR DJFA2006293Filter Element · cloggedTRIP ID NR 051570 THE CREW REPORTED THAT AFTER 1 HOUR 27 MINUTES INTO THE FLIGHT TO KGSO THE LT ENGINE FUEL FILTER BY-PASS ANNUNCIATOR ILUMINATED. THE IGNITERS AND FUEL BOOST PUMPS WERE TURNED ON AS A PRECAUTION. WITHIN APPROX 60 SECONDS, THE RT ENGINE FUEL Jul 25, 2006 · N248CW · Cessna 525 · Engine Fuel DistributionSDR DJFA2006282Odor · unknownWHILE EN ROUTE, A STRONG BURNING ODOR WAS DETECTED BY BOTH CREW MEMBERS. THERE WAS NO SMOKE, NO CIRCUIT BREAKERS HAD POPPED, AND THERE WERE NO ABNORMAL COCKPIT INDICATORS. ALL NON ESSENTIAL ELECTRONICS WERE SHUT OFF, BLEED AIR SOURCE WAS SELECTED TO LT SIDE.Jul 10, 2006 · N247CW · Cessna 525 · Air Distribution SystemSDR 070206N133CS1Door · animal strikeDURING TAKEOFF FROM HTO, AT ROTATION, RIGHT HAND BOTTOM OF AIRCRAFT STRUCK DEER. CLIMBED TO A SAFE ALTITUDE TO EVALUATE SITUATION, CREW MADE DECISION TO DIVERT TO SWF. CALLED AHEAD TO ASK FOR FIRE TRUCK SUPPORT IN THE EVENT OF DAMAGE TO GEAR DOOR OR FLAT TIRJul 2, 2006 · N133CS · Cessna 525 · Landing Gear DoorsSDR DJFA2006279Motor · failedWHILE TAXIING NOTICED A SMELL OF ELECTRICAL SMOKE THAT DISSIPATED. A GREEN LIGHT FOR THE A/C SYS NOT ILLUM, & RT GENERATOR INDICATED A 10 AMP LOAD. FRESH AIR SELECTED OFF, ACFT WAS SHUT DOWN. SMELL APPEARED TO BE COMING FROM LT GENERATOR, WHEN REAR BAGGAGE Jul 2, 2006 · N253CW · Cessna 525 · Cabin Cooling SystemSDR DJFA2006268Seal · detachedWHILE PASSING THROUGH FL 320 FOR FL 360 THE CREW HEARD A LOUD HISSING NOISE COMING FROM THE CABIN ENTRY DOOR. NO CHANGE IN PRESSURIZATION WAS NOTED. OXYGEN MASKS WERE DONNED AS A PRECAUTION, AND THE AIRCRAFT WAS DIVERTED TO KTEB WHILE DESCENDING TO A LOWER AJun 20, 2006 · N291CW · Cessna 525 · Passenger/Crew DoorsSDR DJFA2006265Light · inoperativeGEAR WAS EXTENDED FOR LANDING, CREW DID NOT RECEIVE THE RIGHT MAIN GEAR INDICATION. THE SAME INDICATION OF 2 GREEN, AND NO RED WAS RECEIVED WHEN LANDING GEAR CYCLED. WHILE IN HOLDING PATTERN CREW CONFIRMED GEAR CONTROL CIRCUIT BREAKER WAS IN, AND THE GEAR LIJun 15, 2006 · N247CW · Cessna 525 · Landing Gear Position and WarningSDR 52106N116CS1Grommet · failedAIRCRAFT WAS EN ROUTE FROM MDW TO FTW, AT FL380 CABIN LOST PRESSURIZATION AFTER A NOISE WAS HEARD FROM MAIN CABIN DOOR. THE CABIN DOOR ANNUNCIATED AND CABIN CLIMBED TO 18,000 FEET, O2 MASK DEPLOYED. CREW DECLARED EMERGENCY AND BEGAN EMERGENCY DESCENT. AT 8,May 21, 2006 · N116CS · Cessna 525 · Passenger/Crew DoorsSDR 33106N406CS1Engine · malfunctionedEN ROUTE FROM PHX TO LAN,THE CREW NOTICED LOW AND FLUCTUATING OIL PRESSURE ON RIGHT ENGINE. DURING DESCENT, THE LOW OIL PRESSURE LIGHT ILLUMINATED. THE CREW THEN ELECTED TO DECLARE AN EMERGENCY AND SHUT DOWN THE RIGHT ENGINE. ATC DIVERTED THEM TO GRR AND THMar 31, 2006 · N406CS · Cessna 525 · Engine (Turbine/Turboprop)SDR CA060324001Engine · failedDURING CLIMB-OUT, ENGINE BEGAN TO VIBRATE AND COMPRESSOR STALL. OIL PRESSURE WENT TO ZERO. PILOT PERFORMED SHUTDOWN AND RETURNED TO AIRPORT. POST FLIGHT INSPECTION OF ENGINE REVEALED METAL ON CHIP COLLECTORS AND THE SPOOLS DID NOT TURN FREELY (BEARING NOISEMar 16, 2006 · Cessna 525 · Engine (Turbine/Turboprop)SDR CA060322006Valve · stuckLANDING GEAR DID NOT COME UP ON CLIMB. PILOT FOUND COMPLETE FAILURE OF ALL HYDRAULIC SYSTEM. ON TROUBLESHOOTING, FOUND SOLENOID LANDING VALVE SCREEN STUCK ON VALVE SEAT CAUSING COMPLETE BYPASS OF THE HYDRAULIC FLUID. THIS VALVE WAS PLANNED TO BE REPLACED ATMar 16, 2006 · Cessna 525 · Hydraulic System, MainSDR DJFA2006208Check Valve · leakingCLIMBING FROM 37,500 FT TO 40,000 FT BOTH MASTER CAUTION AND DOOR SEAL LIGHTS ILLUMINATED. OXYGEN MASKS WERE DONNED AND CLIMB WAS STOPPED. DECLARED AN EMERGENCY, AIRCRAFT WAS DIVERTED TO KTOL. THE DOOR SEAL LIGHT EXTINGUISHED BETWEEN 18,000 AND 20,000 FT. Feb 27, 2006 · N254CW · Cessna 525 · Pneumatic Distribution SystemSDR 20806N153CS1Warning Light · illuminatedAFTER TAKEOFF FROM SWF CREW NOTICED A HYDRAULIC LIGHT REMAINED ILLUMINATED AFTER FLAP RETRACTION. ALSO THERE WAS BRAKE AND ANTI-SKID WARNING LIGHTS AND A NOSE GEAR DOWN INDICATION AFTER GEAR RETRACTION. CREW DECIDED TO RETURN TO SWF DUE TO THE AVAILABLILITY Feb 8, 2006 · N153CS · Cessna 525 · Central WarningSDR 20406N151CS1Pressure Sensor · failedDURING CRUISE THE NR 2 ENGINE OIL PRESSURE DROPPED TO 6 PSI, PILOT REVIEWED CHECKLIST AND SHUT ENGINE DOWN. DECLARED AN EMERGENCY AND LANDED AT ORF WHICH WAS THE CLOSEST FIELD. THE PROBLEM WAS IDENTIFIED AS A FAULTY PRESSURE TRANSMITTER.Feb 4, 2006 · N151CS · Cessna 525 · Engine Oil Indicating SystemSDR 2006FA0000119Support Bracket · crackedDURING INSPECTION FOUND THE RT ATTENUATOR PIVOT SUPPORT BRACKET CRACKED. THERE IS A SB (SB525-78-03 R1) THAT ADDRESSES THIS PROBLEM HOWEVER IT IS ONLY FOR SN PRIOR TO AND INCLUDING -0135. HAVE BEEN FINDING THIS CONDITION ON ALL 525S EVEN IF THE SB HAS BEEN AJan 30, 2006 · N345MG · Cessna 525 · Door Warning SystemSDR 012206N401CS1Line · brokenON APPROACH INTO PHX ,THE CREW SELECTED FLAPS AND NOTICED A HYD FLOW LOW ANNUNCIATOR. THE APPROACH WAS ABORTED AND AN EMERGENCY WAS DECLARED. ATC CLEARED AIRCRAFT TO EXTENDED DOWNWIND APPROACH AND THE CREW EXTENDED THE LANDING GEAR WITH THE EMERGENCY BLOWDOWJan 22, 2006 · N401CS · Cessna 525 · Hydraulic System, MainSDR DJFA2005173Pcb · defectiveLANDING GEAR WAS SELECT DOWN, CREW RECEIVED LT AND RT MAIN GEAR GREEN DOWN, LOCKED IND WITH NO NOSE GEAR IND. RED GEAR UNLOCK LIGHT WAS NOT ILLUMINATED. FLAPS EXTENDED TO LANDING POSITION, THROTTLES RETARDED TO IDLE, NML GEAR DOWN, LOCKED IND WAS GIVEN BY ABDec 12, 2005 · N254CW · Cessna 525 · Landing Gear System WiringSDR 113005N133CS1Cabin Pressure · malfunctionedWHILE AT CRUISE, THE CABIN DEPRESSURIZED RAPIDLY. THE 10,000 FOOT CABIN ALTITUDE WARNING LIGHT ILLUMINATED AS THE CABIN WAS CLIMBING AT 3000 FEET/MINUTE, REACHING 16,000 FEET. CREW RECEIVED APPROVAL FROM ATC TO PERFORM EMERGENCY DESCENT TO 10,000 FEET. AT 1Nov 30, 2005 · N133CS · Cessna 525 · Cabin Pressure Control SystemSDR DJFA2005169Unknown · fumesTHE CREW REPORTED THAT WHILE IN FLIGHT, BLEED AIR WAS LEAKING INTO THE CABIN AND CREATING NOXIOUS FUMES. MAINTENANCE RAN BOTH ENGINES WITH THE BLEED AIR SOURCE IN ALL POSSIBLE CONFIGURATIONS. NO DEFECTS WERE FOUND. THE VAPOR CYCLE SYSTEM WAS CHECKED FOR OPENov 28, 2005 · N247CW · Cessna 525 · Air Distribution SystemSDR DJFA2005158Odor · unknownAFTER TAKEOFF THE CREW NOTICED A BURNING ODOR COMING FROM THE CABIN AREA. WHEN THE HEATER TEMPERATURE CONTROL WAS SELECTED TO MANUAL AND TOGGLED TO FULL COLD THE ODOR BEGAN TO DISSIPATE. THE AIRCRAFT WAS RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORNov 6, 2005 · N288CW · Cessna 525 · Air Distribution SystemSDR DJFA2005149Bulb · inoperativeTHE CREW REPORTED THAT WHEN THE GEAR WAS SELECTED DOWN FOR LANDING, RECEIVED THE NOSE AND LEFT MAIN GEAR ANNUNCIATORS. THERE WAS NO INDICATION OF A DOWN AND LOCKED RIGHT MAIN GEAR, BUT THE RED UNLOCK LIGHT WAS EXTINGUISHED. THE LANDING GEAR WAS MANUALLY BLOWOct 17, 2005 · N291CW · Cessna 525 · Landing Gear Position and WarningSDR 2005FA0001095Line · leakingDURING FLIGHT, THE LT AND RT HYDRAULIC LOW LEVEL LIGHTS ILLUMINATED ALONG WITH A MASTER CAUTION LIGHT. AFTER A SAFE LANDING, THE ENTIRE TAIL OF THE AIRCRAFT WAS FOUND TO BE SOAKED WITH HYDRAULIC FLUID. FURTHER INVESTIGATION FOUND THAT HYDRAULIC LINE HAD RUPTUAug 8, 2005 · N247CW · Cessna 525 · Hydraulic System, MainSDR 2005FA0001094Line · scoredDURING FLIGHT, THE LT AND RT HYDRAULIC LOW LEVEL LIGHTS ILLUMINATED ALONG WITH A MASTER CAUTION LIGHT. AFTER A SAFE LANDING, THE ENTIRE TAIL OF THE AIRCRAFT WAS FOUND TO BE SOAKED WITH HYDRAULIC FLUID. FURTHER INVESTIGATION FOUND THAT HYDRAULIC LINE HAD RUPTAug 8, 2005 · N247CW · Cessna 525 · Hydraulic System, MainSDR DJFA2005124Hydraulic System · leakingAFTER TAKEOFF CREW REPORTED HEARING A CAVITATION SOUND FROM THE REAR OF THE AIRCRAFT. AROUND 10,000 FT HYDRAULIC FLOW LOW LEFT AND RIGHT ANNUNCIATORS AND MASTER CAUTION LIGHTS WERE FLICKERING ON AND OFF. AFTER APPROXIMATELY 30 SECONDS, THE HYDRAULIC FLOW ANDAug 2, 2005 · N247CW · Cessna 525 · Hydraulic System, MainSDR CA050711008Cable · failed(CAN) FOUND FWD AILERON CABLE TENSION AT ZERO. CROSSOVER CABLES FOUND TO BE LOOSE. REMOVED AILERON CROSSOVER CABLES FROM CNTRL COLUMNS WITHOUT DISTURBING HUMBUCKLE LOCKING. INSPECTED CABLES, CHAINS, SWAGES AND HUMBUCKLE. DETERMINED ONE OF CROSSOVER CABLE CHAIJul 5, 2005 · Cessna 525 · Aileron Control SystemSDR DJFA2005108Connector · disconnectedON VISUAL APPROACH, LANDING GEAR WAS SELECTED DOWN, DID NOT RECEIVE A GREEN GEAR POSITION INDICATION OR A GEAR UNSAFE INDICATION. DECLARED AN EMERGENCY. CHECKED LANDING GEAR ANNUNCIATORS USING ROTARY SWITCH, STILL DID NOT RECEIVE INDICATION. A LOW PASS WAS Jun 13, 2005 · N253CW · Cessna 525 · Landing Gear System WiringSDR DJFA2005079Boot · looseMMSD TRIP ID NR 812728 CREW REPORTED FEELING AN UNUSUAL VIBRATION IN THE CONTROL COLUMN MOSTLY DURING PITCH MOVEMENT. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO MMSD. CREW DISCOVERED A LOOSE EROSION BOOT ON THE RIGHT HORIZONTAL STABILIZER TIP. MAINTApr 7, 2005 · N206LX · Cessna 525 · Horizontal Stabilizer StructureSDR 032805N152CS1Trim Scale · brokenUPON ROTATION AIRCRAFT REQUIRED EXCESSIVE BACK PRESSURE ON YOKE TO MAINTAIN CLIMB PITCH AND UNABLE TO CLIMB TO ASSIGNED ALTITUDE. DECLARED EMERGENCY AND RETURNED TO AIRPORT FOR UNEVENTFUL LANDING. REPAIR TO AIRCRAFT INVOLVED REPLACEMENT OF ELEVATOR TRIM WHEEMar 28, 2005 · N152CS · Cessna 525 · Elevator Tab Control SystemSDR DJFA2005072Bulb · inoperativeCREW DID NOT RECEIVE A LEFT MAIN GEAR DOWNLOCK INDICATION AFTER GEAR EXTENSION. AN EMERGENCY GEAR EXTENSION WAS PERFORMED BY BLOWING THE GEAR DOWN. THE AIRCRAFT LANDED IN MYAT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN GEAR LIGHT BULB AND Mar 26, 2005 · N226CW · Cessna 525 · Landing Gear Position and WarningSDR DJFA2005070Warning Light · illuminatedDURING CRUISING, APPROX 1 HR AFTER TAKING OFF WITH FULL FUEL, RT FUEL FILTER BY-PASS & MASTER CAUTIONS ILLUMINATED. RT BOOST PUMP TURNED ON. 10 MINS LATER, LT FUEL FILTER BY-PASS ILLUMINATED. LT BOOST PUMP TURNED ON & AN EMERGENCY DECLARED. DURING DESCENT,Mar 24, 2005 · N288CW · Cessna 525 · Engine Fuel DistributionSDR DJFA2005069Bulb · inoperativeWHILE LANDING IN KTEB THE LEFT MAIN LANDING GEAR INDICATION WAS NOT RECEIVED WHEN GEAR WAS SELECTED DOWN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LIGHT BULB FOR THE GEAR INDICATION TO BE BURNED OUT. Mar 24, 2005 · N239CW · Cessna 525 · Landing Gear Position and WarningSDR DJFA2005062Warning Light · illuminatedCREW REPORTED, 1 HR AFTER TAKEOFF AT 35,000 FT RIGHT FUEL FILTER BYPASS, & MASTER CAUTION LIGHTS ILLUMINATED. RIGHT FUEL BOOST PUMP WAS TURNED ON & ACFT BEGAN DIVERTING. LEVELING OFF 13,000 FT LEFT FUEL FILTER BYPASS LIGHT ILLUM. LEFT BOOST PUMP WAS TURNED Feb 20, 2005 · N254CW · Cessna 525 · Fuel Indicating SystemSDR 2005FA0000141Precooler · blownDURING A PREFLIGHT INSPECTION IT WAS NOTED THE PAINT ON THE LOWER SKIN OF THE LEFT PYLON WAS DISCOLORED AND BUBBLED UP. VISUAL INVESTIGATION REVEALED THE PRECOOLER ASSEMBLY HAD FAILED, ALLOWING BLEED AIR INTO THE 6312209-1, DUCT ASSEMBLY, WHICH CAUSED THE 63Feb 18, 2005 · N70KW · Cessna 525 · Pneumatic Distribution System
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