Fairchild SA227-CC

Service difficulty reports · 84

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 = 'SA227CC'
  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 KY7A2025093000038Brake · weakLEFT BRAKE SPONGEY, WILL GO ALL THE WAY TO THE FLOOR. BLED & SERVICED BRAKE SYSTEM IAW SA277 MM CH 32-41-00. RTS CHECKS COMPLETEDSep 17, 2025 · N31171 · Frchld SA227CC · Landing Gear Brake SystemSDR JIKA2022062301Indicator · inoperativeDURING APPROACH TO KCHS, GEAR SELECTED TO DOWN POSITION, LH MLG DOWN LOCK - GREEN LIGHT - DID NOT ILLUMINATE, GEAR WAS MANUALLY EXTENDED AND EMERGENCY WAS DECLARED. AIRCRAFT LANDED IN KCHS WITHOUT FURTHER ISSUE. AIRCRAFT WAS INSPECTED AND FOUND SAFE TO FERRY Jun 23, 2022 · N244DH · Frchld SA227CC · Main Landing GearSDR JIKA2022033101Controller · brokenAMF 1088 - DURING FLIGHT, JUST BEFORE LANDING, PILOT NOTED SMOKE IN THE COCKPIT. THE CONTROL AIR FAN SOUNDED LIKE IT WAS FULL OF MARBLES THEN IT STOPPED AND THERE WAS NO MORE SMOKE. LAN MAINTENANCE REMOVED AND REPLACED CABIN TEMP CONTROL. OPS CHECK GOOD.Mar 31, 2022 · N672AV · Frchld SA227CC · Cabin Temperature ControllerSDR JIKA2022020301Not Reported · not reportedLH MLG DID NOT COME DOWN ON APPROACH, RED INTRANSIT LIGHT REMAINED ON AFTER SEVERAL CYCELS. AFTER SEVERAL TRIES LH MAIN CAME DOWN AFTER LEAVING HANDLE DOWN. SJU MAINTENANCE PEROFRMED LANDING GEAR RETRACTION AND EXTENSION CHECK, OPS CHECK GOOD.Feb 3, 2022 · N152AF · Frchld SA227CC · Main Landing GearSDR JIKA2021121701Light · malfunctionedTHE PILOT REPORTED THAT WHEN THEY LOWERED THE GEAR HANDLE ONLY THE 2 MAIN GEAR GREEN LIGHTS ILLUMINATED. THE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE, AS WELL AS NO RED IN TRANSIT LIGHT ILLUMINATED. MAINTENANCE COULD NOT DUPLICATE THE NOSE GEAR DISCREPANCY ONDec 17, 2021 · N243DH · Frchld SA227CC · Nose/Tail Landing GearSDR JIKA2021102801Interface Unit · defectiveAMF FLT# 6905 EXPERIENCED A LH ENGINE FLAMEOUT AT 1500 FT DURING CLIMB, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. SJU MAINTENANCE TROUBLESHOT STARTING L/H ENGINE NORMALLY AND FOUND L/H ENGINE BYPASSING AND SURGING IN IDLE WITH NO OTHER INPUTS. DURINGOct 28, 2021 · N249DH · Frchld SA227CC · Engine ControlsSDR JIKA2021092101Warning Message · false activationDURING CLIMB THE RIGHT “HYD LOW PRESS” ANNUNCIATOR CAME ON, THE HYDRAULIC PRESSURE GAUGE WAS READING NORMAL. PHOENIX MAINTENANCE INSPECTED AND PERFORMED RIGHT HYDRAULIC SYSTEM OPERATIONAL CHECKS, ACTUATING THE FLAPS FULL UP TO FULL DOWN REPEATEDLY RH HYDRAULICSep 21, 2021 · N426MA · Frchld SA227CC · Hydraulic System, MainSDR JIKA2021072001Trim Cylinder · inoperativePILOT REPORTED HAVING A TRIM FAILURE IN FLIGHT. LANSING MAINTENANCE TROUBLESHOT TO THE TRIM ACTUATOR. PART ON HAND PENDING REPLACEMENT AT THIS TIME.Jul 20, 2021 · N672AV · Frchld SA227CC · Flight Control SystemSDR JIKA2021042801Connector · looseDURING CLIMB OUT FROM KBUR, THERE WAS A BURNING SMELL AND THEN A LITTLE BIT SMOKE COMING OUT FROM RIGHT ESSENTIAL PANEL. LOOKS LIKE SMOKE COMING OUT FROM ONE OF CIRCUIT BREAKER, PILOT PULLED OUT THAT CIRCUIT BREAKER. PILOT REQUESTED TO RETURN TO KBUR AND FOLApr 28, 2021 · N801AF · Frchld SA227CC · Air Distribution SystemSDR JIKA2021022601Unknown · smokeDURING CRUISE FLIGHT AT 13000 FT. FROM KELP TO KBUR, THE CREW NOTED THERE WAS SMOKE IN THE AFT CABIN. THE CREW REQUESTED DIVERTING TO KPHX. THE AIRCRAFT DESCENDED TO 10, 000 FT. AND TURNED OFF THE BLEEDS, THE SMOKE IN THE AFT CABIN WAS CLEARED. AIRCRAFT LANFeb 26, 2021 · N709TR · Frchld SA227CC · Air Distribution SystemSDR JIKA2020122101Control Handle · stuckAMF FLT NR 3928. DURING TAKEOFF FROM KBUR, UPON LEVELING AT 5000. PILOT ATTEMPTED TO MOVE THE GEAR HANDLE TO THE UP POSITION, BUT GEAR WOULD NOT RETRACT. PILOT CHECKED CIRCUIT BREAKERS WERE NORMAL AND ATTEMPTED TO MOVE THE GEAR HANDLE TO THE UP POSITION WITDec 21, 2020 · N475AF · Frchld SA227CC · Landing Gear SelectorSDR JIKA2020110901Cooling Turbine · brokenJUST PRIOR TO LEVEL OFF AT 13000, STEADY WING OVERHEAT ANNUNCIATOR LIGHT CAME ON AND SMALL AMOUNT OF SMOKE CAME INTO THE CABIN. THE PILOT WENT THROUGH THE MEMORY ITEMS AND CHECKLIST AND THE LIGHT WENT OUT AND NO MORE SMOKE. RETURNED TO THE DEPARTURE AIRPORT.Nov 9, 2020 · N422MA · Frchld SA227CC · Engine Bleed Air SystemSDR JIKA2020050142901Current Limiter · blownABOUT 15 MINUTES PRIOR TO ARRIVAL TO KLAN FROM KPLN, THE ELECTRICAL INSTRUMENTS STARTED SURGING AND OCCASIONALLY THE COMMS, GPS, AND NAVS ON THE PILOT SIDE WOULD FLASH OFF AND ON. PRIOR TO GETTING THE AIRPORT IN SIGHT, THE ELECTRICAL POWER SHUT OFF AND IT TOApr 29, 2020 · N709TR · Frchld SA227CC · DC RegulatorSDR JIKA20200227501Wire · damagedDURING TAKEOFF ROLL FROM DFW PITCH TRIM WAS ADJUSTED UP FOR CLIMB. THE TRIM CONTROLS STOPPED WORKING WHILE THE WHEELS LIFTING OFF FROM THE RUNWAY. IT WAS DIFFICULT TO MAINTAIN ALTITUDE ASSIGNED SINCE THE AIRCRAFT KEPT CLIMBING. THE PILOT HAD IMMEDIATELY ADVISEFeb 25, 2020 · N240DH · Frchld SA227CC · Auto Flight System WiringSDR KY7A202002240001Bearing · wornMECHANIC TURNED PROPELLER ON GROUND AND NOTICED GRINDING NOISE COMING FROM THE GEAR CASE. FOUND WORN BEARING ON TACH-GENERATOR GEAR ASSEMBLY. MX REMOVED AND REPLACED THE INTERMEDIATE HOUSING AND GEAR ASSEMBLY, ALSO REPLACED THE FUEL PUMP WHICH FIXED THE GRINDFeb 20, 2020 · N571KL · Frchld SA227CC · Engine RPM Indicating SystemSDR KY7A202002209001Oil System · overservicedFLIGHT CREW REPORTED TEMP CONTROL SELECTED AUTO OR HOT, FULL HOT ON CONTROL KNOB HAS SMOKE/HAZE COMING FROM FLOOR AREA IN COCKPIT. MX DRAINED EXCESS OIL FROM AIR CYCLE MACHINE.Feb 19, 2020 · N538KL · Frchld SA227CC · Cabin Cooling SystemSDR JIKA20200129301Mixing Valve · defectiveDURING INITIAL CLIMB FROM DFW, AFTER TURNING ON BLEED AIR VALVES, THE COCKPIT BECAME VERY HOT, EVEN THOUGH THE SYSTEM WAS SET AT THE LOWEST SETTING. TEMP SELECTOR SWITCH WAS RECYCLED THROUGH ALL POSITIONS AND CONTROL KNOB WAS KEPT AT LOWEST SETTING, BUT COCKPJan 23, 2020 · N240DH · Frchld SA227CC · Cabin Cooling SystemSDR JIKA2020011501Control Cable · malfunctionedAFTER TAKEOFF FROM KELM, APPROXIMATELY 600 AGL, RIGHT ENGINE FLAMEOUT. PILOT NOTICED THE RIGHT FUEL FLOW WAS AT ZERO AND PILOT CHECKED RIGHT ENGINE CONTROL LEVERS, STOP AND FEATHER, BOOST PUMPS AND IGNITION THEN ENGINE HAD WOUND DOWN. PILOT HAD REQUESTED AN Jan 10, 2020 · N544UP · Frchld SA227CC · Propeller Feathering/ReversingSDR JIKA2019120200501Overheat Sensor · defectiveSHORTLY AFTER TAKEOFF FROM DFW, RIGHT ENGINE OIL TEMP EXCEEDED TOLERANCES OVER HIGH RED LINE. PILOT PERFORMED PRECAUTIONARY ENGINE SHUT DOWN, ATC DECLARED AN EMERGENCY. AIRCRAFT LANDED BACK AT DFW WITH NO INCIDENT. MAINTENANCE REMOVED AND REPLACED OIL TEMPERANov 25, 2019 · N241DH · Frchld SA227CC · Engine Oil Indicating SystemSDR JIKA20191118601Accumulator · separatedON CLIMB OUT FROM KSMX THE PILOT REPORTED THAT THE LEFT AND RIGHT HYDRAULIC SYSTEM FAIL WARNING LIGHTS ILLUMINATED, FOLLOWED BY A LOSS OF HYDRAULIC PRESSURE. THE PILOT PERFORMED A MANUAL GEAR EXTENSION RECEIVED THREE GREEN DOWN AND LOCKED INDICATION, DECLAREDNov 18, 2019 · N673AV · Frchld SA227CC · Hydraulic Accumulator, AuxiliarySDR JIKA20191118201Unknown · smokeWHILE ENROUTE TO SAT, CREW REPORTED SMOKE IN THE COCKPIT WITH AN OILY SMELL. THEY SHUT OFF THE BLEED AIR AND PUT ON THEIR OXYGEN MASK. FLIGHT LANDED WITHOUT INCIDENT AT KSAT. SAT MAINTENANCE INSPECTED THE BLEED AIR SYSTEM FOR EVIDENCE OF OIL, NO DEFECTS FOUND.Nov 18, 2019 · N569UP · Frchld SA227CC · Air Distribution SystemSDR CA190402015Nozzle · failed(CAN) THE MAIN OIL JET CRACKED IN THE GEAR BOX CAUSING A BEARING TO FAIL DUE TO LACK OF OIL ON THE BEARING IN THE MAIN GEAR CASE. THE ENGINE WAS PULLED DUE TO THE OIL LAB BECAUSE OF MAJOR M50 MATERIAL THAT WAS NOTED FROM THE BEARING.THE ENGINE PART HAS 4612.9 Feb 25, 2019 · Frchld SA227CC · Turbine Engine Oil SystemSDR HKGA2015F00035Angle · crackedLT OTBD LOWER ANGLE IN BATTERY BOX CRACKED AT STA 80.87.Feb 12, 2015 · N26959 · Frchld SA227CC · Fuselage Miscellaneous StructureSDR HKGA2015F00034Angle · crackedLEFT OTBD LOWER ANGLE IN BATTERY BOX CRACKED AT STA 80.87.Feb 12, 2015 · N26959 · Frchld SA227CC · Fuselage Miscellaneous StructureSDR TN8A2015011500001Valve · failedFLIGHT RETURNING TO BASE AFTER FREIGHT CHARTER FLIGHT. UPON APPROACH PILOT SELECTED GEAR DOWN BUT DID NOT RECEIVE A GREEN LIGHT INDICATION FOR THE NOSE GEAR. PILOT RECYCLED GEAR AND REQUESTED TO TERMINATE LANDING. PILOT MANUAL EXTENDED THE LANDING GEAR IAW Dec 31, 2014 · N3114G · Frchld SA227CC · Hydraulic System, MainSDR CA140331003Pulley · noisy(CAN) THE FLIGHT CREW REPORTED ROUGHNESS IN CONTROL COLUMN IN FULL NOSE UP CONFIGURATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOISE IN TAIL IN THE FULL NOISE UP CONFIGURATION. MAINTENANCE FOUND A CABLE OFF THE PULLEY, FWD ELEVATOR DOWN SPRINMar 27, 2014 · Frchld SA227CC · Elevator Control SystemSDR CA140321015Unknown · smoke(CAN) DURING TAKEOFF WITH BLEEDS ON HIGH & TEMP CONTROLLER IN AUTO POSITION, THE CABIN BEGAN TO FILL WITH SMOKE. ACFT RETURNED TO BASE & MX COMPLETED NUMEROUS GND RUNS & NO SMOKE IN CABIN. TEST FLIGHT WAS COMPLETED & NO SMOKE IN CABIN. ACFT RELEASED TO SERVFeb 10, 2014 · Frchld SA227CC · Air Distribution SystemSDR KY7A20131217001Turbine · damagedPILOT REPORTED THAT ON CLIMB OUT THE ENG LOST OIL PRESS. PILOT SECURED THE ENG & RETURNED TO THE DEPARTURE AIRPORT & LANDED. MX FOUND SIGNIFICANT DAMAGE TO THE 3RD STAGE TURBINE & DISASSEMBLED ENG. AFT TURBINE BEARING WAS FOUND DESTROYED, FAILED. 1ST & 2ND Dec 17, 2013 · N2728G · Frchld SA227CC · Turbine SectionSDR CA131211002Fcu · unresponsive(CAN) ENGINE WAS STARTED, YET WHEN POWER LEVERS WERE MOVED FORWARD TO TAXI THE LT ENGINE WAS UNRESPONSIVE. ACFT WAS RETURNED TO MAINTENANCE AND AFTER TROUBLESHOOTING WAS CARRIED OUT THE DRIVE BETWEEN THE FUEL PUMP AND FCU WAS FOUND TWISTED AND THE VESPAL SPLIDec 11, 2013 · Frchld SA227CC · Fuel Control/Turbine EnginesSDR CA130812006Line · cracked(CAN) FLIGHT CREW SNAGGED HYD SIGHT GLASS EMPTY AND NO FLAP MOVEMENT WHILE SPOOLING ENGINE, LOCATED AND REPLACED CRACKED HYD LINE UNDER RT CABIN FLOORBOARD JUST FORWARD OF MAIN SPAR. LEAK CHECKED AND ACFT RETURNED TO SERVICE.Aug 11, 2013 · Frchld SA227CC · Hydraulic System, MainSDR CA120125012Bridge · failed(CAN) DURING TAKEOFF ROLL THE LT TORQUE GAUGE WAS READING ZERO. TAKEOFF WAS ABORTED. MAINTENANCE WAS CONTACTED AND THEY FOUND THE NR 1 TORQUE RING BRIDGE HAD FAILED. SYS WAS SWITCHED OVER TO THE NR 2 BRIDGE AND CALIBRATED. GROUND RUNS CARRIED OUT AND ACFT RJan 24, 2012 · Frchld SA227CC · Engine BMEP/Torque IndicatingSDR CA111118016Tee Fitting · cracked(CAN) AIRCRAFT RETURNED TO BASE AS LT ENGINE COULD NOT MAKE FULL POWER. LT ENGINE FUEL BOWL TEE FITTING FOUND CRACKED. FITTING REPLACED AND ACFT RETURNED TO SERVICE. ALSO CONNECTOR PLUG WIRE CONTROLLING THE BYPASS VALVE WAS REPAIRED AT THIS TIME.Oct 28, 2011 · Frchld SA227CC · Engine Fuel DistributionSDR CA110830013Indicator · intermittent(CAN) PILOT ABORTED TAKEOFF, WAS NOT ABLE TO GET MORE THAT 35 PERCENT TORQUE ON THE RT ENGINE. MX REPLACED THE FOLLOWING ITEMS AFTER CONFIRMING TORQUE WAS STICKING INTERMITTENTLY RT TORQUE SIGNAL CONDITIONER - PN 3102476-6 AND RT TORQUE GAUGE - PN 27-19158-0Aug 24, 2011 · Frchld SA227CC · Independent InstrumentsSDR CA110829015Screw · loose(CAN) TAKEOFF ABORTED DUE TO RT ENGINE NOT PRODUCING TAKEOFF POWER ON THE TAKEOFF ROLL. CREW TAXIED TO RUN UP AREA AND COULD NOT REPRODUCE THE FAULT. CREW CONTINUED ON AND TAKEOFF WAS IAW MFG PARAMETERS. MX REVIEWED RUN UP NRS AND TIGHTENED UP SCREW "X" WHIAug 19, 2011 · Frchld SA227CC · Power LeverSDR CA110802007Case · crackedUPON DISASSEMBLY, FOUND THE STUD AND DOWEL LOOSE ON THE FWD SIDE OF THE CASE AT THE 900 A-CLOCK POSITION LOOKING AT THE CASE. THE DOWEL AND STUD BASE WAS ALSO FOUND WITH CRACKS. BASE FOUND CRACKED ON BOTH SIDES OF THE DOWEL.Jul 28, 2011 · Frchld SA227CC · Accessory GearboxesSDR CA110628001Spline · wornEXTERNAL SPLINES HAVE MAJOR STEP WEAR IN THE ROOT AREA. SEVERAL SPLINES HAVE A SHARP STEP AT THE BASE OF THE TOOTH IN THE ROOT AREA, APPROX .005 INCH DEEP. THESE MARKS WERE VISIBLE BY USING A 10X POWER MAGNIFICATION LOOP. SPLINE OD WAS MEASURED AT 0.404" ACROJun 22, 2011 · Frchld SA227CC · Fuel Control/Turbine EnginesSDR CA110617010Fuel Control · contaminatedTHE CYLINDER BORE AND PISTON AREA WAS FOUND CORRODED AND PLUGGED WITH BLACK PARTICLES WHICH APPEAR TO HAVE GENERATED FROM THE PISTON RING SEALS. IT IS SUSPECT THAT THE PISTON AND CYLINDER BORE ARE NOT CONCENTRIC WITH EACH OTHER. FURTHER BLOCKAGE AND RESTRICTIJun 17, 2011 · Frchld SA227CC · Fuel Control/Turbine EnginesSDR CA110519002Tee Fitting · crackedAFTER AN OPERATIONAL RUN, FUEL WAS FOUND AROUND THE LT ENGINE FUEL BOWL TEE FITTING. THE FITTING WAS REMOVED AND PRESSURE TESTED. A SMALL CRACK WAS FOUND DIRECTLY ABOVE THE WELD LOCATION ON THE TEE FITTING. FITTING REPLACED AND AIRCRAFT RETURNED TO SERVICE.May 18, 2011 · Frchld SA227CC · Fuel Control/Turbine EnginesSDR CA110401006Blade · damaged(CAN) PILOT REPORTED VIBRATIONS AND DETERMINED IT WAS THE LT PROP. TECHNICAL HISTORY WAS REVIEWED AND FOUND THAT BALANCE WAS AN ISSUE IN THE LIFE OF THE PROP SINCE LAST OH. THE BLADES WERE INSPECTED FOR ROTATIONAL PLAY AND FOUND ALL 4 BLADES WERE LOOSE AND 1 BMar 30, 2011 · Frchld SA227CC · Propeller AssemblySDR CA110307002Windshield · cracked(CAN) AT 21000 FT DURING CRUISE, 20 MINUTES INTO FLIGHT DEPARTING BS RT WINDSHIELD OUTER GLASS PANE SHATTERED. ACFT DESCENDED, DEPRESSURIZED, TURNED AROUND AND CAME BACK TO BS.Mar 6, 2011 · Frchld SA227CC · Flight Compartment WindowsSDR CA101022002Strut · fracturedLT MAIN GEAR LOWER STRUT TORQUE KNEE ATTACH BOSS FRACTURED AND SEPARATED FROM MAIN LOWER ASSY DURING TAXI CAUSING SEVERE SHIMMY.Oct 20, 2010 · Frchld SA227CC · Main Landing Gear Strut/Axle/TruckSDR CA101019008Actuator · seizedFLIGHT CREW REPORTED RUDDER TRIM WOULD NOT MOVE LT OF NEUTRAL. ACTUATOR REMOVED AND FOUND SEIZED. ACTUATOR REPLACED AND ACFT RETURNED TO SERVICE.Oct 14, 2010 · Frchld SA227CC · Rudder Tab Control SystemSDR CA090522004Landing Gear · malfunctioned(CAN) ON DESCENT, GEAR WAS SELECTED DOWN AND THE RT GEAR DID NOT EXTEND AND LOCK DOWN ON FIRST ATTEMPT. AFTER MULTIPLE ATTEMPTS ALL 3 GEAR EXTENDED AND WERE VISUALLY CONFIRMED DOWN AND LOCKED. CREW ELECTED TO FLY TO ANOTHER BASE FOR ADDITIONAL MX INSTEAD OF LAMay 21, 2009 · Frchld SA227CC · Landing Gear Retraction/Extension SystemSDR CA081205008Windshield · failed(CAN) ON APPROACH THE LT WINDSHIELD SHATTERED. MX WAS DISPATCHED TO REPLACE THE WINDSHIELD. THE TEMP CONTROLLER WAS FOUND TO BE DEFECTIVE ALSO. TEMP CONTROLLER REPLACED ALONG WITH WINDSHIELD AND ACFT RETURNED TO SERVICE.Dec 4, 2008 · Frchld SA227CC · Flight Compartment WindowsSDR CA080922005Line · cracked(CAN) PILOT REPORTED HYD FLUID LEAKING IN LT WW. SMALL PINHOLE WAS FOUND IN LINE. LINE REPLACED AND ACFT RETURNED TO SERVICE.Sep 9, 2008 · Frchld SA227CC · Hydraulic System, MainSDR CA080905008A/C Pack · damaged(CAN) ON APPROACH, THE PILOT NOTICED SMOKE COMING OUT OF FRESH AIR VENTS AND MOMENTS LATER LT WING OVERHEAT LIGHT CAME ON. ACFT LANDED WITHOUT INCIDENT. MX WENT TO LOOK AND FOUND THAT THE LT COOLING TURBINE HAD A CATASTROPHIC FAILURE. THE LT BLEED SYSTEM WAS MSep 2, 2008 · Frchld SA227CC · Cabin Cooling SystemSDR CA080611007Bearing · spalled(CAN) THE REAR TURBINE WAS FOUND WITH HEAVY SPALLING, GALLING, HEAVY SCORING AND MISSING MATERIAL OFF THE OUTER RACEWAY AND ON THE ROLLING ELEMENTS. THE BEARING HAD ONLY 12.5 HOURS SINCE NEW/CAM. THE ENGINE WAS MAKING A STRANGE GRINDING SOUND THAT WAS NOTICED Jun 10, 2008 · Frchld SA227CC · Engine (Turbine/Turboprop)SDR CA071106008Retainer · cracked(CAN) WHILE ENGINE WAS BEING REPLACED MAINTENANCE NOTICED FATIQUE CRACKS EMINATING FROM THE (PROP SHAFT) RETAINING BOLT AREA. (TC NR 20071106008)Oct 25, 2007 · Frchld SA227CC · Propeller AssemblySDR CA070319005Impeller · fractured(CAN) ENGINE WAS REMOVED DUE TO NOT MAKING TARGET TAKEOFF TORQUE. UPON DISASSEMBLY THE 2ND STAGE COMPRESSOR IMPELLER FAILED AND HAS EXPERIENCED A FATIGUE TYPE FAILURE. THE PRESENT TIME ON THE IMPELLER IS 20,650.2 HOURS AND 28,175 CYCLES. A LARGE PIECE OF THEMar 16, 2007 · Frchld SA227CC · Turbine Engine Compressor SectionSDR CA070307009Regulator · malfunctioned(CAN) AC DEPARTED BASE AND UPON GEAR RETRACTION BOTH LT AND RT HYD PRESSURE LIGHTS ILLUMINATED FOR 3-4 SECONDS THEN WENT OUT. AIRCRAFT RETURNED TO BASE AND UPON INVESTIGATION IT WAS FOUND THAT NO RESIDUAL HYD PRESSURE WAS PRESENT AFTER ENGINE SHUTDOWN. UPON Mar 5, 2007 · Frchld SA227CC · Hydraulic System, Main
Back to Fairchild SA227-CC