GE CF34-3A1

Service difficulty reports · 1,372

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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 = 'CF343A1'
  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 MASA2011040502329Transmitter · leakingNR 2 ENGINE LEAK CHECK REQUIRED. MX C/W NR 2 ENGINE LEAK CHECKS, CORRECTED ONE LEAK AT FUEL FLOW TRANSMITTER RE-CHECK FOUND NO FURTHER LEAKS.Apr 2, 2011 · N77302 · Cndair CL6002B19 · Fuel Flow SensorSDR MASA2011031702165Actuator · leakingFUEL LEAKING FROM NR 2 ENG. MX REPLACED SLAVE VG ACTUATOR, OPS AND LEAK CHECK GOOD.Mar 15, 2011 · N715SF · Cndair CL6002B19 · Compressor Bleed ControlSDR CA110315003Unknown · haze(CAN) IN THE INITIAL CLIMB, HAZE DEVELOPED IN THE CABIN, PROMPTING THE CREW TO LEVEL OFF AT 1800 FEET AND RETURN TO DEPARTURE AIRPORT. BY THE TIME THE AIRCRAFT TOUCHED DOWN, HAZE HAD DISSIPATED. RESPONDING EMERGENCY SERVICES FOUND NO TRACE OF FIRE, HEAT OR SMOMar 14, 2011 · Cndair CL6002B19 · Air Distribution SystemSDR CA110311005Fuel Sys · leaking(CAN) FUEL WAS FOUND IN THE BELLY OF THE AIRCRAFT BENEATH CARGO FLOOR. UPON FURTHER INSPECTION, IT WAS NOTED DRIPPING OFF THE SHROUD CROSS ADAPTOR ASSEMBLY WHICH HOUSES THE FUEL DISTRIBUTION LINES IN THE BELLY OF THE AIRCRAFT. WHEN THE ADAPTOR HOUSING ASSEMBLYMar 9, 2011 · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR CA110309004Socket · burned(CAN) DURING CLIMBOUT THROUGH 12,000 FT F/A REPORTED SMOKE IN THE CABIN. CREW STARTED TO TURN FOR AIRPORT. AT THIS POINT CREW DECLARED AN EMERGENCY FOR EXPEDITED ARRIVAL. ARFF MET ACFT TO DETERMINE IF RAPID DEPLANEMENT WAS REQUIRED. CREW DETERMINED IT WAS RMar 7, 2011 · Cndair CL6002B19 · Passenger Compartment LightingSDR CA110307006Floor Support · corroded(CAN) CORROSION ON PRESSURE FLOOR STRUCTURE BS 409+128 TO 559. DURING INSPECTION, SOME LOCATIONS WORE FOUND OUT OF ALLOWABLE LIMITS OR WHERE NO REWORK IS ALLOWED IAW SRM.Mar 1, 2011 · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA110211004Socket · burnedDEFECT-968113, ACRID ODOR IN CABIN. ELECTRICAL ODOR SEEMS TO BE COMING FROM F/A PANEL. CREW ADVISES THEY ARE RETURNING TO STATION AND WILL BE LANDING OVERWEIGHT. LANDING 48730LBS. TOUCHDOWN RATE 150 FPM. IAW ABOVE NOTED PARAMETERS FOR DESCENT SPEED AND LANFeb 9, 2011 · Cndair CL6002B19 · Passenger Compartment LightingSDR CA110201003Screw · loose(CAN) DURING CLIMB OUT, FLIGHT CREW RECEIVED A SERVICE DOOR CAUTION MESSAGE AND RETURNED TO THE DEPARTURE AIRPORT. UPON ARRIVAL AT THE GATE, MAINTENANCE TROUBLESHOOTED THE PROBLEM AND QUICKLY FOUND THAT THE SERVICE DOOR INNER HANDLE HOLDING SCREWS (4) (IPC 52-Jan 20, 2011 · Cndair CL6002B19 · Service DoorsSDR CA110117006Secu · unserviceableUNIT WAS RETURNED FOR REPAIR OF AN ELECTRONIC FAILURE. WHEN THE TECH COMMENCED WORK AND REMOVED THE TOP COVER IT WAS DISCOVERED THAT ALL VENTILATION HOLES IN THE TOP COVER WERE COVERED (BLOCKED) ON THE INSIDE SURFACE WITH MASKING TAPE. UPON FURTHER INVESTIGAJan 17, 2011 · Cndair CL6002B19 · Drag Control SystemSDR CA110104005Connector · burnedON A FLIGHT INBOUND THE CREW REPORTED AN ELECTRICAL BURNING ODOR AND ARCING NOISE COMING FROM THE OVERHEAD BIN AREA AT ROW 1 ON THE LT SIDE. MAINTENANCE INVESTIGATION FOUND AN ELECTRICAL CONNECTOR SHORTED, BURNED AND MELTED ABOVE THE LT ROW 1 OVERHEAD BIN. THDec 30, 2010 · Cndair CL6002B19 · Equipment/Furnishings WiringSDR CA110104009Bpsu · failedALTITUDE 070 FLIGHT PHASE LANDING EVENT AT AROUND FL070 THE CREW SELECTED FLAP 8 AND HAD THE FLAP FAIL MSG APPEAR. THEY DECLARED AN EMERGENCY AND RECEIVED VECTORS FOR RWY34. AT THAT TIME MTC AND DX WERE ADVISED. THEY LANDED WITHOUT FURTHER INCIDENT AND THEREDec 30, 2010 · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR CA110106002Wire · burnedAN ELECTRIC ODOR WAS NOTED. MAINTENANCE GAINED ACCESS TO WIRING ABOVE PSU PANELS AND DISCOVERED BURNED WIRING/CONNECTORS.Dec 30, 2010 · Cndair CL6002B19 · Electrical Power System WiringSDR CA101222012Fitting · cracked(CAN) WHILE PERFORMING A DETAIL INSPECTION OF THE CARGO DOOR INTERNAL STRUCTURE IN ACCORDANCE WITH TASK RJ2-52-830-506 , A CRACK WAS FOUND ON THE TOP FORWARD RADIUS OF SUPPORT FITTING. THE FITTING WAS REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-10-06.Dec 22, 2010 · Cndair CL6002B19 · Cargo/Baggage DoorsSDR CA101222013Powerplant · shutdown(CAN) BOTH ENGINES SHUTDOWN DURING LANDING ROLLOUT. PILOTS HAD APU RUNNING FOR BLEED, BUT APU GEN WAS NOT ON LINE. ADG ALSO AUTO DEPLOYED. NO WATER IN FUEL. THROTTLES WERE PULLED TO IDLE AT 50` AGL. THRUST REVERSERS WERE NOT USED ON LANDING ROLL OUT ASDec 22, 2010 · Cndair CL6013A · Engine (Turbine/Turboprop)SDR CA101222014Intercostal · cracked(CAN) WHILE CARRYING OUT A DETAIL INSPECTION OF THE CARGO DOOR INTERNAL STRUCTURE AS PER TASK CARD RJ2-52-830-506 DURING A "C" CHECK VISIT, A CRACK WAS OBSERVED IN THE INTERCOSTAL AT FS605.00 BETWEEN WL73.00 AND WL82.88. THE CRACKS WERE NOTED BY FOUR RIVET HOLDec 21, 2010 · Cndair CL6002B19 · Cargo/Baggage DoorsSDR CA101223004Angle · cracked(CAN) SUSPECT CRACKS WERE NOTED ON ANGLE MEMBER ALONG TWO VERTICAL STIFFENERS IN THE LHS AND RHS CENTRE WING FUEL TANKS. THE AME WAS PERFORMING AN INSPECTION OF THE INTERNAL FUEL TANKS IN ACCORDANCE WITH TASK RJ2-57-510-502 AND TASK RJ2-57-610-502 RESPECTIVELYDec 21, 2010 · Cndair CL6002B19 · Wing Miscellaneous StructureSDR COMA2010121350258Engine · vibrationON CLIMBOUT FROM DTW RECEIVED RIGHT ENGINE N2 AMBER VIB MSG. EMERGENCY DECLARED, A/C RETURNED TO DTW LANDED SAFELY. REMOVED AND REPLACED RIGHT ENGINE.Dec 9, 2010 · N595SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA101222016Windshield · cracked(CAN) FIRST OFFICERS WINDSHIELD CRACKED ON APPROACH. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD.Dec 9, 2010 · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA2010113050249Sensing Element · shortedEN ROUTE, RECEIVED ANTI-ICE DUCT WARNING MSG. EMERGENCY DECLARED, ACFT DIVERTED AND LANDED SAFELY. INSPECTED ACFT FOUND LT WHEEL WELL LOOP A41WK SHORTED. REPLACED LOOP A41WK, OPS CHECK GOOD.Nov 30, 2010 · N814CA · Cndair CL6002B19 · Pneumatic Indicating SystemSDR CA101112003Fitting · cracked(CAN) CRACK FOUND ON CARGO DOOR ROLLER FITTING AT THE RADIUS. LOCATION OF FITTING ON CARGO DOOR IS AT FS 576.00 AT WL 97.75. FITTING REPLACED IN ACCORDANCE BOMBARDIER SRM CHAP 51-10-06 SECTION 3 PART D.Nov 11, 2010 · Cndair CL6002B19 · Cargo/Baggage DoorsSDR CA101111002Clamp · broken(CAN) DURING CLIMB OUT FLIGHT ATTENDANT REPORTED A STRONG SMELL OF SMOKE IN THE CABIN. THERE WAS NO VISIBLE SIGN OF SMOKE OR SMELL FROM THE COCKPIT AREA. AIRCRAFT MADE AN AIR TURNBACK TO AIRPORT. FLIGHT HAS BEEN SUBSEQUENTLY CANCELLED. DEFECT 949377 WAS RANov 9, 2010 · Cndair CL6002B19 · Pneumatic Distribution SystemSDR CA101020005Windshield · crackedDEFECT 945435 CAPT OUTER PANE WINDSCREEN SHATTERED AT FL340. CREW REPORT THAT THEY HEARD A POP AND SAW A FLASH AND 2 SECONDS LATER THE WINDOW SHATTERED. PILOTS WINDSHIELD REPLACED IAW AMM 56-11-01 FUNCTION CHECKS & LEAK CHECKS COMPLETED & FOUND SERVICEABLE. Oct 20, 2010 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA101015003Actuator · failedDURING CRUISE, THE FLIGHT CREW NOTICED THAT THE AUTOPILOT COULDN`T KEEP THE ACFT LATERAL ATTITUDE LEVEL. THE AUTOPILOT WAS DISENGAGED AND THE PILOT IN COMMAND APPLIED PRESSURE ON THE CONTROL WHEEL AND THE SYS FREED UP. UPON ARRIVAL THE ACFT WAS REMOVED FROM Oct 7, 2010 · Cndair CL6002B19 · Aileron Control SystemSDR CA101015007Warning System · failedON DESCENT AT 10000 FT ANTI ICE DUCT WARNING ILLUMINATED CONTINUOUSLY. CREW DECLARED AN EMERGENCY AND STOPPED ON TAXIWAY FOR AIRPORT FIRE DEPARTMENT TO CHECK WINGS PRIOR TO PROCEEDING TO GATE. NO ISSUE FOUND BY AIRPORT FIRE DEPARTMENT, ACFT PROCEED TO THE GATOct 7, 2010 · Cndair CL6002B19 · Detection SystemSDR CA100928008Turbine · meltedSHORTLY AFTER TAKEOFF THE FLIGHT CREW HEARD A LOUD BANG FOLLOWED BY RISING ITT AND EXCESSIVE N2 VIBRATION ON THE LT ENGINE. THE ENGINE WAS SHUTDOWN, AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED AND LANDED UNEVENTFULLY. INITIAL INSP REVEALS EXTENSIVE DAMAGESep 27, 2010 · Cndair CL6002B19 · Turbine SectionSDR CA100928010Line · rupturedAFTER LANDING PILOT RECEIVED NR 2 HYD LOW PRESS INDICATION WITH THE PRESSURE DROPPING TO 2700 PSI AND QTY DOWN TO 5 PERCENT. MX MEET THE ACFT AND START INVESTIGATION AND FOUND A HYD PUDDLE COMING FROM THE RT WHEEL WELL AFTER INSP. THE AREA FOUND THE INBD GROUSep 24, 2010 · Cndair CL6002B19 · Drag Control SystemSDR CA100924005Cap · fracturedDURING PUSH BACK, THE FLIGHT CREW HEARD A LOUD BANG AND RECEIVED AN HYD SYS NR 2 LOW PRESSURE CAUTION LIGHT. THE ACFT WAS TOWED BACK AT THE GATE AND MX CONTROL CTR ADVISED. A CERTIFIED ENGINEER MET THE ACFT AND FOUND A RUPTURED OTBD BRAKE ACCUMULATOR. THE OSep 22, 2010 · Cndair CL6002B19 · Hydraulic Power Accumulator, MainSDR COMA2010092050206Engine · overtempON CLIMBOUT FROM BDL TO CVG LEFT ENGINE EXCEEDED ITT LIMITS, REDUCED THRUST TO 85 PERCENT TO MAINTAIN WITH IN LIMITS. EMERGENCY DECLARED, A/C DIVERTED TO ALB LANDED SAFELY. REMOVED AND REPLACED LEFT ENGINE.Sep 17, 2010 · N960CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA100908003Bulkhead · crackedWHILE CARRYING OUT A SPECIAL DETAILED INSP ON THE FWD FACE OF THE REAR PRESSURE BULKHEAD TASK RJ2-53-280-607, EDDY-CURRENT TESTING REVEALED CRACKING INDICATIONS IN EXCESS OF ALLOWABLE LIMITS AT THE FOLLOWING TEN(10) LOCATIONS. THESE INDICATIONS WERE REVIEWED Sep 3, 2010 · Cndair CL6002B19 · Fuselage Main, BulkheadSDR CA100813005Trunnion · crackedTASK RJ2-RJ2-57-510-614 ON LT SIDE MLG MOUNTING TRUNNION FITTING WEB WAS CARRIED OUT AS SCHEDULED DURING AN OVERNIGHTER AT OUR MAIN OPERATING HUB. DURING THIS ROUTINE SPECIAL INSP, A CRACK OF APPROX 0.080" TO 0.100" WAS FOUND ON THE AFT TOOLING HOLE. A DAMAGEAug 10, 2010 · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR CA100813001Control Valve · failed(CAN) ON AUGUST 5, 2010 UPON LANDING CREW REPORTED A TIRE BLOW AND BRAKE OVERHEAT. AIRCRAFT CLEARED RUNWAY AND SAT ON TAXIWAY NOVEMBER. ARFF ON SIGHT, MAINTENANCE DISPATCHED TO INSPECT AND SEE IF ABLE TO TOW. NO PASSENGER INJURIES WERE MOVED TO TERMINAL VIAAug 5, 2010 · Cndair CL6002B19 · Landing Gear Brake SystemSDR CA100802001Fcu · malfunctioned(CAN) FLIGHT CREW RECEIVED AN ENGINE INDICATION AND CREW ALERTING SYS (EICAS) FLAPS FAIL CAUTION MESSAGE DURING CLIMB OUT. DECISION WAS MADE TO CONTINUE TO DESTINATION WHERE AN UNEVENTFUL FLAP ZERO LANDING WAS CONDUCTED. THE ACFT WAS REMOVED FROM SERVICE, THJul 31, 2010 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA100707001Lever · jammedON FLIGHT DURING CLIMBING THROUGH FL080 THE CREW HEARD LOUD RUSHING AIR NOISE FROM NOSE LANDING GEAR AREA AFTER THE GEAR RETRACTION, APPEARS DOORS DID NOT CLOSE. THE CREW RECEIVED A NOSE GEAR DOOR OPEN WARNING MESSAGE. CONTINUED IS CLIMBING THROUGH FL110 WHEREJul 1, 2010 · Cndair CL6002B19 · Landing Gear Door Retract SectionSDR CA100623006Selector Valve · failedON DEPARTURE GOT GEAR DISAGREE, THE CREW ADVISED THE MAINS CAME UP BUT THE NOSE DID NOT. CREW ELECTED TO RETURN, DEFECT NR 922471 RAISED (RESOLVED ON W/O: 242075 TASKCARD: NR-00001) NLG DOOR SELECTOR VALVE REPLACED WITH REFERENCE TO AMM 32-22-20. GEAR SWING Jun 22, 2010 · Cndair CL6002B19 · Landing Gear Door Retract SectionSDR CA100617005Static Wick · debondedDURING HEAVY CHECK, REF WO 229655, NR-00050, FOUND STATIC WICKS ON THE RT STAB TIP T/E, FAILED BOND CHECK, REF TASK RJ2-23-900-120. BONDING AND MEGOHMMETER TEST OF THE STATIC DISCHARGERS SCHEDULED AT EVERY 5000HRS. MODIFICATION END CAP LIGHTING PROTECTION KIJun 9, 2010 · Cndair CL6002B19 · Static Discharge SystemSDR CA100610002Strap · crackedDURING COMPLETION OF TASK RJ2-53-220-604 (DETAILED INSP OF THE WINDSHIELD CTR POST AND BULKHEAD AFT POST AT FS202.75) FOUND WINDSHIELD AFT CTR POST LOWER STRAP CRACKED AT FS210.00 AND CL0.00 AND WL 110.00 REF W/O229655, NR00323. PART FABRICATED AND REPAIRS IAJun 8, 2010 · Cndair CL6002B19 · Fuselage Main, StructureSDR CA100604007Compressor · failedRT N2 VIBRATIONS ON DESCENT. CREW NOTICED 2 SIMULTANEOUS BUMPS- ALL ENGINE PARAMETERS OK. ON DESCENT, AT POWER REDUCTION, VIB ICON APPEARS ON RT N2 GAUGE. THE POWER REDUCED TO IDLE UNTIL LANDING AT DESTINATION AIRPORT. THE BORESCOPE INSP REVEALED THAT A BLADJun 4, 2010 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR SWIA201024312Engine · failedNR 2 ENGINE FAILED ON TAKEOFF CLIMB. (FLT 5863) REPLACED NR 2 ENGINE. P/N ON CF34-3B1, S/N OFF 807246C.May 30, 2010 · N988CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA100526004Antenna · looseDURING A POST-FLIGHT WALKAROUND THE CREW NOTICED WHAT APPEARED TO BE LOOSE SEALENT AROUND THE NR1 TRANSPONDER ANTENNA. UPON CLOSER INSP THE ANTENNA SNAPPED RIGHT OFF ITS BASE. ANTENNA REPLACED.May 24, 2010 · Cndair CL6002B16 · ATC Transponder SystemSDR CA100604001Cowl Door · damagedAIRCRAFT FLEW AND ARRIVED 14:18 Z DURATION 1:17. CREW REPORTED ON JLS 525995 DEFECT DESCRIPTION RT FRONT COWL SEPARATED FROM NACELLE UPON LANDING 21-MAY-2010 LINE MAINTENANCE WAS DISPATCHED FOR REPLACEMENT OF DAMAGED COWL. NEW COWL WOULDN’T FIT CORRECTLY ANDMay 21, 2010 · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR COMA2010041250096Engine · surgesON T/O FROM DTW LEFT ENGINE SURGE, NORMAL THRUST T/O PERFORMED. EMERGENCY DECLARED, A/C RETURNED TO DTW LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL 76-11-01.Apr 11, 2010 · N969CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA100223005Wire · broken(CAN) JUST AFTER PUSHBACK, CREW SELECTED FLAPS FROM 0 TO 8 DEGREES. FLAPS DID NOT MOVE AND FLAP FAIL CAUTION MESSAGE DISPLAYED. RESET ATTEMPTED BUT NOT SUCCESSFUL. MTC INVESTIGATION FOUND A BROKEN WIRE AT CONNECTOR 2P2CE AT THE RT WING BPSU. THE WIRE WAS REPAIFeb 21, 2010 · Cndair CL6002B19 · Flight Control System WiringSDR CA100219009Angle · cracked(CAN) AME WAS CARRYING OUT A GENERAL VISUAL INSP IN THE WHEEL WELLS, WHEN HE FOUND CRACKS ON AN ANGLE IN THE MLG UPLOCK AND APRON STRUCTURE AREA. THIS CRACK WAS EVIDENT ON THE UPPER JOGGLE OF THESE ANGLES IN BOTH THE LTS AND RTS WHEEL WELL AT STA.FS516.85 & WLFeb 17, 2010 · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA100215004Engine · shutdown(CAN) DURING CLIMB OUT AT 1,500 FT, WITH ENGINE PARAMETERS SHOWING NORMAL, NR 2 ENGINE SHUTDOWN. PILOTS REPORTED AN ACFT YAW AND A LOUD NOISE. PROCEEDED WITH SINGLE ENGINE APPROACH AND LANDED WITHOUT FURTHER INCIDENT. EVENT REPORT SUBMITTED TO MEXICAN DGACFeb 12, 2010 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA2010012850025Carbon Seal · blownEN ROUTE FROM LGA TO CHS RECEIVED SMOKE TOILET MSG, F/A CHECKED ALARM AND RESET AND MSG WENT OUT, MSG CAME BACK ON 3 TO 4 MIN LATER THEN WENT OUT AGAIN. F/A REPORTED HAZE WAS IN THE CABIN, COCKPIT REMAINED CLEAR. A/C DIVERTED TO MYR, LANDED SAFELY. REMOVED Jan 27, 2010 · N966CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA100129002Bleed Air Sys · odor(CAN) FLIGHT WITH 16 PASSENGERS AND 3 CREW, WAS ENROUTE AT FL320 ABOUT 110NM NORTHNORTHEAST OF MYRTLE BEACH,SC (USA), WHEN THE CREW REPORTED A SMOKEY ODOR ONBOARD AND DECIDED TO DIVERT. THE AIRPLANE LANDED SAFELY IN ABOUT 21 MINUTES LATER. ATTENDING EMERGENCY Jan 27, 2010 · Cndair CL6002B19 · Engine Bleed Air SystemSDR COMA2010012150019Engine · failedON CLIMBOUT FROM BTV LOSS OF RIGHT ENGINE OIL PRESSURE, PERFORMED IFSD OF RIGHT ENGINE. EMERGENCY DECLARED, A/C RETURNED TO BTV LANDED SAFELY. REMOVED AND REPLACED RIGHT ENGINE.Jan 20, 2010 · N954CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA100104009Carbon Seal · leaking(CAN) LT OIL PRESSURE MESSAGE IN FLIGHT. COMPLIED WITH QRH. EVENTUALLY SHUT DOWN LT ENG AND LANDED SINGLE ENG. R & R IDG B AXIS CARBON SEAL ASSY IAW AMM 72-60-00, AND SUP 05 018A. OPS CHECKED AND NO FURTHER DEFECTS NOTED.Dec 25, 2009 · Cndair CL6002B19 · Engine Oil PressureSDR CA100104007Controller · malfunctioned(CAN) FLIGHT AT LEVEL FL290 WAS DIVERTED DUE TO A LOSS OF PRESSURIZATION. THE CREW RECEIVED A CABIN ALT CAUTION MESSAGE WITH EICAS INDICATING 8500 FT CABIN ALTITUDE AND INCREASING SLOWLY. ATTEMPTS TO MANUALLY CONTROL THE CABIN ALTITUDE IAW THE QRH WAS UNSUCCESDec 22, 2009 · Cndair CL6002B19 · Cabin Pressure ControllerSDR CA100101003Engine · overtemp(CAN) DURING CLIMB AT FL 150 , CREW REPORTED THE ITT ENG NR 1 RAISING IN THE RED BAND AT 1000 DEG. CREW COMPLIED WITH QRH AND SHUTDOWN THE LT ENGINE. THE CREW ELECTED TO DO AN AIR TURNBACK AND LANDED TO DEPARTURE AIRPORT. MX FOUND EXCEEDANCE REPORT IN MDC AT Dec 16, 2009 · Cndair CL6002B19 · Engine (Turbine/Turboprop)
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