GE CF34-3B1

Service difficulty reports · 5,402

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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 = 'CF343B1'
  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 VNAA2013072000018Fuel Control · failedCREW REPORTED RT ENGINE WOULD NOT PRODUCE TAKEOFF THRUST AT TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. MX TROUBLESHOT, R & R RT ENGINE FUEL CONTROL AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Jul 20, 2013 · N202PS · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR REXA2013071401369Engine · failedRT ENGINE FAILED ON CLIMBOUT AT APPROX 4500 FT. ENGINE APPEARED TO SEIZE. RAN QRH AND RETURNED TO DEPARTURE. R & R RT ENGINE IAW AMM 71-00-00 & CHECKLIST. OPS CHECKED GOOD, NO LEAKS.Jul 14, 2013 · N8977A · Cndair CL6002B19 · Powerplant SystemSDR REXA2013071301357Engine · failedSHORTLY AFTER TAKEOFF AND AT 4400 FT, RT ENGINE MADE A LOUD NOISE AND N2 WENT TO ZERO. SHORTLY AFTER, A HOT ICON POSTED. EMERGENCY DECLARED AND RETURNED TO DEPARTURE.Jul 13, 2013 · N8977A · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA130710003Selector Valve · failed(CAN) CREW REPORTED ON APPROACH THEY RECEIVED A GEAR DISAGREE MESSAGE. THEY PREFORMED QRH, FIRST TRY NOSE GEAR WOULD NOT COME OUT OF YELLOW, MATCHING GEAR UP. SECOND TRY NOSE EXTENDED BUT MAINS WOULD NOT. CREW RELEASED THE MAINS USING THE MANUAL EXTENSION. ACJun 30, 2013 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR CA130627008Shroud · corroded(CAN) THE FUEL SHROUDS AND FUEL LINES WERE REMOVED FORM THIS ACFT THAT IS CURRENTLY DOWN FOR HEAVY MAINTENANCE. THERE IS NO MFG REQUIREMENT TO DISASSEMBLE THIS SYS FOR INSPECTION. ONCE AGAIN THE INSIDES OF THESE COMPONENTS WERE COVERED WITH A BLACK SUBSTANCE,Jun 21, 2013 · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR CA130621001Director · failed(CAN) DURING CLIMB THROUGH 31,600 CREW OBSERVED PITCH UP COMMAND ON THE FLT DIRECTOR, WITH SPEED INDICATING 59 KTS. SPEED BUTTON SHOWED. 17 KTS. EVENT BUTTON PUSHED AT 1757Z DEFECT RAISED TO PROVIDE DATA FOR OPERATOR ACTION IAW SL 440-SL-22-014A WITH DEFECT NRJun 20, 2013 · Cndair CL6002B19 · Flight ControllerSDR CA130627006Seal · failed(CAN) CREW REPORTED THEY LOST ALL HYDRAULIC NR 3 SYS PRESSURE. COMPLETED MANUAL GEAR EXTENSION IAW QRH PROCEDURES. PERFORMED NORMAL LANDING WITHOUT INCIDENT. MAINTENANCE FOUND THE RT HYDRAULIC PUMP SYS 3B HYDRAULIC DAMPER SEALS BLOWN OUT.Jun 20, 2013 · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR A6WA201306181015Structure · chafedCOWL 434 AT GAS CHAFE ON INBD END THAT FITS INTOP CENTER PART OF STANG FAIRING. REPAIRED LT UPPER TRANS COWL 434 INBD END IAW REO 601R-78-33-4017.Jun 10, 2013 · N461AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201306181016Skin · dentedDENTS ON OUTER SKIN OF LT UPPER TRANS COWL ON OTBD END. BLENDED SMOOTH IAW REO 601R-78-33-4018.Jun 10, 2013 · N461AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201306181017Skin · dentedLEFT UPPER TRANS COWL HAS 1 DENT OUT OF LIMITS ON OUTER SKIN JUST FWD OF OIL PLACARD PLACED ON OTBD END. CUT OUT DAMAGE & REPAIR IAW REO 601R-78-33-4018.Jun 6, 2013 · N461AW · Cndair CL6002B19 · Engine Thrust ReverserSDR CA130606008Transmitter · failed(CAN) UPON REACHING 7000 FT, WE RECEIVED A HYDRAULIC 2B AND HYDRAULIC 3B YELLOW WARNING. AT THE SAME TIME THE RED SPEED TAPE WENT DOWN TO BETWEEN 180 AND 250 KTS. SECONDS LATER WE ALSO RECEIVED A FLAP INDICATION. THE FLAPS STARTED TO FLUCTUATE BETWEEN 0 AND Jun 5, 2013 · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR VNAA2013060400003Turbine · damagedTHE CREW REPORTED A VIBRATION IN THE RIGHT ENGINE. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE LOW PRESSURE TURBINE USING THE AIRCRAFT MANUALS. CHECKS WERE ACCOMPLISHED USING AIRCRAFT MJun 4, 2013 · N226JS · Cndair CL6002B19 · Turbine SectionSDR CA130617008Engine · multiple fail(CAN) ON TAKEOFF HAD A WINDSHEAR WARNING, PUSHED THRUST LEVERS TO MAX THRUST. RT ITT OVERTEMPED. OUT OF WINDSHEAR, PULLED THRUST LEVERS BACK CLIMBING OUT OF 13,000 FT. RT ENGINE OIL PRESSURE WARNING MESSAGE, RAN QRH PROCEDURE. MONITORED ENGINE GAUGES TO SEE Jun 2, 2013 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA130603012Bolt · corroded(CAN) WHILE REPLACING #2 BRAKE ASSEMBLY, THE RETAINING BOLTS WERE FOUND TO HAVE MISSING PLATING AND HEAVY PITTING. ALL 5 BOLTS WERE REPLACED. NOTE: THERE IS NO SPECIFIC REQUIREMENT IN THE AMM 32-43-26 FOR INSPECTION OF THESE BOLTS DURING BRAKE ASSEMBLY REPLAJun 1, 2013 · Cndair CL6002B19 · Landing Gear Brake SystemSDR VNAA2013053100018Fuel Control · failedCREW REPORTED RIGHT ENGINE OVERSPEED MASTER WARNING MESSAGE BELOW 80 KNOTS ON TAKEOFF. CREW REJECTED TAKEOFF AND SAFELY RETURNED TO GATE. MAINTENANCE INSPECTED, PERFORMED POWER ASSURANCE RUN AND FOUND RIGHT ENGINE EXCEEDED MAXIMUM PERMITTED N2. MAINTENANCE May 31, 2013 · N215PS · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR A6WA201306181018Fairing · crackedRIGHT TAIL PIPE FAIRING HAS TWO SMALL CRACKS FROM THE 4TH DRAIN HOLE FROM AFT. REMOVED 2 SMALL CRACKS BY INCREASING SIZE OF DRAIN HOLE BY 0.040, NO EO WAS AFFECTED.May 31, 2013 · N461AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR ASOA2013053103740Engine · overtempAFTER TAKEOFF, RT ENGINE REACHED APPROX 926, N1 WAS SET AT .91-4. TARGET WAS 91-5 POWER WAS REDUCED & RECREASED INTO NORMAL RANGE. RETURNED TO DEPARTURE, EMERGENCY DECLARED. R & R RT ENGINE ASSY OPS AND LEAK CHECKED GOOD.May 29, 2013 · N925EV · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR REXA2013052900676Frame · corrodedLOWE FS333, FRAME CORRODED BETWEEN S-26L AND S-26R. REPAIRED IAW SRM 51-21-06.May 26, 2013 · N8416B · Cndair CL6002B19 · Fuselage Main, FrameSDR CA130521012Engine · malfunctioned(CAN) CAPTAIN REPORTED LT TL JAM IN FLIGHT AT FL350 AT 92.5 PERCENT N1. DESCENT CONTINUED WITH TL JAMMED AT HIGH ENGINE N1 AND IAS 320 KNOTS. CONSIDERATION TO ENGINE FIRE PUSH WAS GIVEN, HOWEVER AT 7000 FT ALTITUDE TL FREED. LANDING CONDUCTED 2 ENGINES OPS.May 16, 2013 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA130515002Selector Valve · failed(CAN) WHEN TRYING TO TAKE GEAR DOWN, CREW RECEIVED A NOSE GEAR WARNING. THEY MADE A GO AROUND. WENT INTO HOLDING AND PERFORMED THE CHECKLIST. AFTER PULLING THE MANUAL RELEASE HANDLE THEY RECEIVED 3 GREEN GEAR LIGHTS. THE LANDING WAS NORMAL BUT THE NOSE WHEELMay 13, 2013 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR REXA2013050700870Engine · vibrationAIR TURNBACK DUE TO N2 VIBRATION AND IFSD.May 7, 2013 · N823AY · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2013050700004Engine · failedCREW REPORTED AIRCRAFT HAD SMOKE IN THE CABIN. AIRCRAFT RETURNED TO AIRPORT LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE LEFT ENGINE AND OXYGEN EQUIPMENT PER AIRCRAFT MANUALS. CHECKS WERE PERFORMED PER THE AIRCRAFT MANUALS ANDMay 7, 2013 · N253PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA130507001Pump · cracked(CAN) ON APPROACH INTO DESTINATION, CREW LOST NR 2 HYD SYS FLUID. ACFT LANDED SAFELY. UPON MAINTENANCE INSPECTION, IT WAS FOUND THAT THE HOUSING OF THE NR 2 ENGINE DRIVEN PUMP WAS SPLIT. THE EDP AS WELL AS THE CASE DRAIN FILTER WERE REPLACED. FLUID LEVEL WAMay 6, 2013 · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR CA130508003Fire Detector · malfunctioned(CAN) AT FIRST, RT ENGINE FIRE FAIL MESSAGE WAS INDICATED AT COCKPIT DURING TAXI AFTER LANDING. THEN, RT ENGINE FIRE MESSAGE WAS INDICATED WHEN PILOT STARTED PROCEDURE IAW RT FIRE FAIL MSG CHK LIST. THEREFORE, PILOT CARRIED OUT ENGINE SHUTDOWN PROCEDURE IAW EMay 6, 2013 · Cndair CL6002B19 · Fire DetectionSDR CA130506005Wire · broken(CAN) FLAPS 0 INDICATION CAME ON IN DESCENT THRU FL250 THEN FLAP FAIL MSG POSTED. FLAPS REMAINED AT 0. FLAP 0 LANDING COMPLETED. RESOLVED ON W/O: 382391, TASKCARD: NR-00002, TROUBLESHOOTING ON W/O: 382391, TASKCARD: NR-00001, FLAPS SET TO 8DEG IAW RJ-SL-2May 2, 2013 · Cndair CL6002B19 · Flight Control System WiringSDR CA130506002Tube · chafed(CAN) DURING TROUBLESHOOTING OF AN INOPERATIVE APU, EVIDENCE OF OIL LEAK WAS NOTICED ON THE ACFT TAIL SECTION. APU OIL COOLER TUBE 3881849-1 WAS FOUND DAMAGED, ATTACHING CLAMP CHAFED THROUGH THE TUBE.May 1, 2013 · Cndair CL6002B19 · APU Oil SystemSDR VNAA2013042800020Transducer · failedCREW REPORTED HIGH LEFT ENGINE OIL PRESSURE AND ABORTED TAKEOFF. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE LEFT ENGINE OIL PRESSURE TRANSDUCER PER AIRCRAFT MANUALS. OPERATION CHECKS WERE ACCOMPLISHED USING AIRCRAFT MANUALS AND AIRCRAFT RELEASED FOR SApr 28, 2013 · N206PS · Cndair CL6002B19 · Engine Oil PressureSDR CA130430004Handle · bent(CAN) THE RAMP CREW REPORTED THAT THE MAIN CABIN DOOR OUTER HANDLE WOULD NOT POP OUT WHEN THE RELEASE BUTTON WAS PRESSED. THIS PREVENTED THEM FROM OPENING THE DOOR FROM THE OUTSIDE. MAINTENANCE INVESTIGATION FOUND THAT THE MCD OUTER HANDLE SHAFT WAS VERY SLIApr 23, 2013 · Cndair CL6002B19 · Passenger/Crew DoorsSDR VNAA2013041700010Carbon Seal · leakingCREW REPORTED SMOKE TOILET CAUTION MESSAGE DURING CRUISE. FLIGHT ATTENDANT CONFIRMED LAVATORY SMOKE ALARM SOUNDED. SMOKE WAS VISIBLE FROM ROW SIX (6) THROUGH 11. SMOKE TOILET QRH (QUICK REFERENCE HANDBOOK) WAS PERFORMED AND SMOKE DISSIPATED SHORTLY THEREAFTEApr 17, 2013 · N218PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA130422002Engine · malfunctioned(CAN) FLIGHT DIVERSION DUE TO A LAVATORY SMOKE INDICATION AND SMOKE IN THE CABIN. APPROXIMATELY 25 MINUTES INTO THE FLIGHT, THE CREW RECEIVED A SMOKE TOILET CAUTION MESSAGE AND REQUESTED THE F/A TO VERIFY. THE F/A REPORTED TO THE CREW THAT THERE WAS FAIRLY HEApr 17, 2013 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2013041600008Carbon Seal · leakingCREW REPORTED SMOKE TOILET CAS MESSAGE CAME ON DURING DESCENT. PASSENGER NEAR LAV REPORTED ELECTRIC BURNING SMELL. CREW RAN QRH (QUICK REFERENCE HANDBOOK) AND LANDED SAFELY. MAINTENANCE INSPECTED LAV AND CABIN AREA, GROUND RAN AIRCRAFT WITH CREW AND RAN AIR Apr 16, 2013 · N218PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA130415003Pcu · failed(CAN) DURING MAINTENANCE 27-320-101, DETAILED INSPECTION OF THE RUDDER PANEL ASSY HINGE BEARINGS AND PCU ATTACHMENT POINTS IT WAS DICOVERED THAT THE CENTER PCU ATTACHMENT POINT TO THE RUDDER STRUCTURE HAD SHEARED. IT WAS ALSO NOTED THAT THE ROD END BEARING ISApr 13, 2013 · Cndair CL6002B19 · Rudder Control SystemSDR VNAA2013041000004Engine · malfunctionedCREW REPORTED HIGH ITT ON LEFT ENGINE WHEN THROTTLES ADVANCED AND BRAKES RELEASED FOR TAKEOFF. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED AND DETERMINED LEFT ENGINE REQUIRES REMOVAL AND REPLACEMENT. SUPPLEMENTAL INFORMATION WILL BE PROApr 10, 2013 · N216PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA130410018Shroud · corroded(CAN) THE FUEL SHROUDS AND FUEL LINES WERE REMOVED FORM THIS ACFT, CURRENTLY BEING PARTED OUT, TO SERVICE THE OTHER. ALTHOUGH IT WAS NOT AS SEVERE AS THE INITIAL ACFT, MODERATE CORROSION WAS FOUND IN THE SAME AREAS THOUGH OUT THESE COMPONENTS. AS WITH THE FIRApr 9, 2013 · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR CA130410014Shroud · corroded(CAN) DURING COMPLETION OF ROUTINE MAINTENANCE, TASK 060-28-900-753, 28-10-00-03, FUEL TANK VENT AND LINE SHROUDS PRESSURE LEAK TEST. WE WERE UNABLE TO PRESSURIZE SYS AND NO AIR, NOT PART OF THE TEST WAS COMING OUT OF THE VENT HOLES AT FS 572.35. FURTHER INVApr 8, 2013 · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR ASOA2013032503250Blades · damagedRT ENGINE FLAMED OUT ON DESCENT AT 4000 & 250 KIAS. ATTEMPTED RELIGHT UNSUCCESSFUL. COMPLIED WITH WITH AREA C BOROSCOPE INSPECTION IAW MANUAL 72-00-00. FOUND DAMAGE BLADES ON STAGE 6 T/E. R & R RT ENGINE IAW AMM 71-00-00. OP'S AND LEAK CHECK GOOD.Mar 19, 2013 · N826AS · Cndair CL6002B19 · Turbine SectionSDR A6WA201303144014Pump · malfunctionedDURING CLIMBOUT, LOSS OF POWER ON LEFT ENGINE (LOW FUEL LOW PRESS MESSAGE) N2 DROP 15% WITH VIBRATION AND YAW TO LEFT (LT MAIN EJECTOR) MESSAGE, POWER UP, LOSS OF POWER 3X. SMOOTHED OUT (LOW FUEL, LOW PRESS ON LANDING). REMOVED AND REPLACED LEFT ENGINE FUEL Mar 14, 2013 · N430AW · Cndair CL6002B19 · Engine Fuel PumpSDR CA130321004Warning Light · illuminated(CAN) ON CLIMB, RT REVERSER UNLOCKED, C. QRH APPLIED. ATB RETURN TO ORIGIN AIRPORT. MAINTENANCE DEFERRED RT REVERSE IAW MEL 78-30-1.Mar 11, 2013 · Cndair CL6002B19 · Engine Thrust ReverserSDR CA130308010Sign · overheated(CAN) ABOUT ONE MINUTE AFTER TAKEOFF THE CREW RECEIVED A LAVATORY SMOKE INDICATION IN THE COCKPIT. THERE WAS ALSO A ODOR REPORTED IN THE LAVATORY BUT NO VISIBLE SMOKE. THE SMOKE INDICATION WENT OFF AFTER ABOUT 3 MINUTES. THE ACFT RETURNED TO THE DEPARTURE AIRMar 7, 2013 · Cndair CL6002B19 · Passenger Compartment LightingSDR VNAA2013030600007Engine · malfunctionedCREW REPORTED LEFT ENGINE OIL PRESSURE CLIMBED TO APPROXIMATELY 133 PSI ON TAKEOFF ROLL. CREW REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT ENGINE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT REMar 6, 2013 · N215PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2013022700017Engine · failedCREW REPORTED A HIGH ITT AND VIBRATION WITH LOSS OF POWER IN NR 2 ENGINE. CREW RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND OPERATIONAL CHECKED THE NR 2 ENGINE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFTFeb 27, 2013 · N250PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2013022200011Carbon Seal · damagedCREW REPORTED LEFT ENGINE OIL PRESSURE CAS MESSAGE IN FLIGHT. LEFT ENGINE AT IDLE FOR REMAINDER OF FLIGHT AND OIL PRESSURE FLUCTUATING. CREW DECLARED EMERGENCY AND LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT LEFT ENGINE, REMOVED AND REPLFeb 22, 2013 · N218PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR REXA2013022100363Engine · malfunctionedFLIGHT 3723, CREW REPORTED VIBRATION 2 CAUTION ON NR 1 ENGINE AND SHUT DOWN ENGINE DURING FLIGHT. DECLARED EMERGENCY AND LANDED SAFELY. REPLACED LT ENGINE ASSY AND AFT THRUST SHAFT IAW AMM 71-00-00-40-801. OPS AND LEAK CHECKED GOOD. ALL REQUIRED BRAKE IN RUFeb 21, 2013 · N8930E · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA201332842Engine · failedSMOKE TOILET EICAS MSG ON TAKEOFF AT 100 KNOTS. BLEEDS FROM ENGINES. ABORTED TAKEOFF. (FLT 4464) REMOVED AND REPLACED RIGHT ENGINE. P/N: CF34-3B1 S/N ON: 873691 S/N OFF: 872710.Feb 17, 2013 · N702BR · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA130219003Light · overheated(CAN) DURING THE CLIMB THE CREW RECEIVED A LAVATORY SMOKE WARNING INDICATION. THE F/A NOTICED A LEATHER ODOR IN THE LAVATORY BUT NO EVIDENCE OF SMOKE OR FIRE. THE ACFT RETURNED TO THE DEPARTURE AIRPORT. ALL WIRING IN THE VICINITY OF THE LAVATORY WAS CHECKED Feb 17, 2013 · Cndair CL6002B19 · Passenger Compartment LightingSDR CA130307007Compressor · dirty(CAN) SMOKE TOILET CAUTION MESSAGE DURING TAKEOFF ROLL. CREW ABORTED TAKEOFF. MESSAGE CLEARED SHORTLY THEREAFTER. FOUND RT ENGINE COMPRESSOR BLADES TO BE SOILED. SUSPECT NR 3 CARBON SEAL IS LEAKING OIL INTO 10TH STAGE BLEED AIR AND CAUSING SMOKE TOILET EICAFeb 15, 2013 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA130214017Compressor · damaged(CAN) AFTER 40 MIN OF FLIGHT, PILOTS REPORTED LOUD BANG COMING FROM THE ALONG WITH HIGH ITT INDICATION OVERTEMP. THE FLIGHT CREW COMMANDED THE SHUTDOWN. ATB. EMERGENCY DECLARED. SINGLE ENGINE LANDING AT ORIGIN AIRPORT. MAINTENANCE CREW PERFORMED VISUAL INSPEFeb 12, 2013 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR SWIA201332792Engine · failedFELT A BIG BANG - LEFT ENGINE N1 WENT TO 30 PERCENT AND ITT WAS AROUND 920°C, SHUT DOWN THE LEFT ENGINE. (FLT 2958) REPLACED LEFT ENGINE IAW AMM P/N: CF34-3B1 S/N ON: 873869 S/N OFF: 873127 P/N: 755469E S/N ON: 1832/4738.Feb 9, 2013 · N875AS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA130218006Engine · failed(CAN) ON CLIMBOUT, FELT A BIG BANG- LT ENGINE N1 WENT TO 30 PERCENT AND ITT WAS AROUND 920 C. FOLLOWED QRH PROCEDURES AND SHUTDOWN LT ENGINE AND RETURNED TO ORIGIN. AFTER EXTENSIVE TROUBLESHOOTING MAINTENANCE R & R THE LT ENGINE.Feb 9, 2013 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2013020700005Engine · malfunctionedCREW REPORTED IN-FLIGHT SHUTDOWN OF NUMBER ONE ENGINE. SHAKER / PUSHER ACTIVATED AND FLIGHT SPOILER EXTENDED. NUMBER ONE ENGINE ITT AT 998 DEGREES WITH NO OIL PRESSURE. CREW DECLARED EMERGENCY, DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ANFeb 7, 2013 · N261PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)
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