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"

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SDR REXA201100185Engine · malfunctionedON TAKEOFF ROLL FROM KMCI THE FLIGHT CREW HEARD A LOUD NOISE FROM THE RIGHT ENGINE FOLLOWED BY HIGH ITT INDICATION AND ENGINE SHUTDOWN. THE FLIGHT CREW ABORTED THE TAKEOFF. AFTER INSPECTION OF THE AIRCRAFT BY CFR THE AIRCRAFT RETURNED TO THE GATE. OUTSTATIOMar 17, 2011 · N8458A · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA201100496Floorbeam · crackedCARGO BAY FLOORBEAM CAP AT LBL9 OTBD FLANGE AT FS 589 IS CRACKED. REPAIRED FLOORBEAM IAW EC/TC REO 601R-53-61-4009 AND REO 601R-53-61-4009. MAJOR REPAIR.Mar 16, 2011 · N820AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201100498Frame · corrodedFUSELAGE FRAME AT FS 333.00 HAS SEVERAL AREAS OF CORROSION ON FWD SIDE OF FRAME BETWEEN STR 25L AND STR 25R.Mar 16, 2011 · N829AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201100500Seat Track · corrodedLEFT SEAT TRACK, BTWN FS 449.85 AND 499.00 HAS CORROSION. REMOVED CORROSION FROM LT SIDE SEAT TRACK. DAMAGE OUT OF LIMITS IAW SRM 53-21-49, FIG 101. REMOVED SEAT TRACK IAW AMM 53-01-11-946-003. FABRICATED NEW SEAT TRACK IAW SRM 51-40-11. MINOR REPAIR.Mar 16, 2011 · N849AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201100507Seat Track · corrodedLBL 9.0 SEAT TRACK CORRODED MULTIPLE SPOTS BETWEEN FS 409-424 . REMOVED SEAT TRACK IAW AMM 53-01-11-946-003. FABRICATED NEW SEAT TRACK IAW SRM 57-41-02. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802. MINOR REPAIR.Mar 16, 2011 · N849AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201100508Seat Track · corrodedRBL 9.0 SEAT TRACK CORRODED MULTIPLE SPOTS BETWEEN FS 409-424. REMOVED SEAT TRACK IAW AMM 53-01-11-946-003. FABRICATED NEW SEAT RAIL IAW SRM 51-40-11. INSTALLED NEW SEAT RAIL IAW AMM 53-01-11-400-802. MINOR REPAIR.Mar 16, 2011 · N849AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR CA110323006Manifold · cracked(CAN) FLIGHT CREW REPORTED THAT WATER LEAKS FROM THE CABIN CEILING DURING TAKEOFFS. THIS WAS REPORTED FOLLOWING A NUMBER OF FLIGHTS. REMOVED THE CEILING PANELS & FOUND CONDENSATION THROUGHOUT CEILING OF THE CABIN & INSULATION SOAKED IN BEHIND THE CEILING & SMar 16, 2011 · Cndair CL6002B19 · Air Distribution SystemSDR ASOA201100491Seat Track · corrodedLT SIDE SEAT TRACK, BETWEEN FS 409.00+16 AND FS 409.00+112 HAS CORROSION. REMOVED CORROSION FROM LT SIDE SEAT TRACK. DAMAGE OUT OF LIMITS IAW SRM 53-12-49 FIG 101. DRILLED AND COUNTERSINKED NEW SERVICABLE SEAT TRACK IAW DWG 601R38312 AND SRM 51-40-11 AND 5Mar 15, 2011 · N849AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201100493Seat Track · corrodedLT, SEAT TRACK, BETWEEN FS 544.00 AND FS 559.00+80 HAS CORROSION. REMOVED CORROSION FROM LT, SIDE SEAT TRACK. DAMAGE OUT OF LIMITS IAW SRM 53-21-49, FIG 101/53-51-49. REMOVED SEAT TRACK IAW SRM 53-01-11-946-003. FABRICATED NEW SEAT TRACK IAW SRM 51-40-11. Mar 15, 2011 · N849AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201100495Placard · deterioratedRT OVERWING EXIT PLACARD MISSING HALF OF THE PLACARD. REPLACED RT EMERGENCY EXIT PLACARD IAW AMM 11-30-00.Mar 15, 2011 · N935EV · Cndair CL6002B19 · Placards and MarkingsSDR ASOA201100489Floorbeam · crackedFS 280 WEB CRACKED OTBD OF RBL 9 APPROX .250", FLOORBEAM CLIPS INBD OF LBL 9 & RBL 9 ARE CRACKED AND J-ANGLE OTBD OF LBL 9 CRACKED. OPS CHECK GOOD IAW AMM 27-11-00-710-801. FOUND TO BE SATISFACTORY. (CLOSED)Mar 14, 2011 · N936EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201140170Engine · flamed outAFTER 10,000 FT AND INCREASING TO CLIMB POWER, LEFT ENG ITT 854C, 62 DEGREE HIGHER THAN RT ENG ACARS`D MX, THEY REQUESTED CHECK WITH SPEED SWITCHES OFF, COMPLIED, NO DIFFERENCE NOTED REDUCED POWER, TURNED RT SPEED ON, NO DIFFERENCE. TURNED LT SPEED ON, ENGINEMar 7, 2011 · N464AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA110308006Pump · malfunctioned(CAN) 30 MINUTES AFTER TAKEOFF, THE CREW MADE A FORCED LANDING DUE TO 1 ENGINE IN FLIGHT SHUTDOWN. THAT IFSD WAS DUE TO A LOW OIL PRESSURE.Mar 6, 2011 · Cndair CL6002B19 · Engine Fuel PumpSDR CA110308001Flapper Valve · missing(CAN) DURING TAXI TO THE GATE, FLIGHT CREW RECEIVED A "SMOKE TOILET" CAUTION MESSAGE SHORTLY FOLLOWED BY A "RT PACK HI TEMP" CAUTION MESSAGE. THE F/A NOTICED LIGHT SMOKE AND A BURNING ODOR IN THE CABIN NEAR THE LAVATORY, LAV AREA. AS A PRECAUTIONARY MEASURE,Mar 5, 2011 · Cndair CL6002B19 · Cabin Cooling SystemSDR REXA201100154Oil System · low pressureRT ENG LOW OIL PRESS IN FLIGHT. AN EMERGENCY WAS DECLARED. A/C LANDED SAFELY.Feb 28, 2011 · N8888D · Cndair CL6002B19 · Turbine Engine Oil SystemSDR MASA2011030102047Actuator · leakingFUEL LEAKING FROM NR 1 ENG DRAIN MAST. MX R2 VG ACTUATOR.Feb 27, 2011 · N97325 · Cndair CL6002B19 · Compressor Bleed ControlSDR CA110301003Bpsu · failed(CAN) ON BASE LEG AT 3000, FLIGHT CREW RECEIVED A FLAP FAIL CAUTION MESSAGE WHEN THE FLAP SELECTOR WAS MOVED FROM TO THE 8TH POSITION. EMERGENCY SERVICES WERE REQUESTED AND A FLAP 0 LANDING CONDUCTED WITHOUT FURTHER INCIDENT. UPON ARRIVAL, LINE MAINTENANCE RFeb 25, 2011 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA201100141Pump · leakingFLIGHT DIVERTED DUE TO RIGHT ENGINE LOW OIL PRESSURE INDICATION ENGINE WAS SHUT DOWN IN FLIGHT EMERGENCY WAS DECLARED FOUND RT ENGINE EDP LEAKING. DEFERRED EDP IAW MEL 29-11-01 DM-39183.Feb 23, 2011 · N8516C · Cndair CL6002B19 · Turbine Engine Oil SystemSDR 2011F00053Bulkhead · crackedFS 559 BULKHEAD FOUND CRACKED. COMPLIED WITH 559 REPAIR IAW REO 601R-53-41-260, REV E STEP 1-14 AND REO601R-53-41-609, REV B, DEVIATION E.Feb 22, 2011 · N8709A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR 2011F00054Drag Angle · crackedASD AFT DRAG ANGLE CRACKED. R & R AFT DRAG ANGLE IAW SRM 51-42-00.Feb 22, 2011 · N8709A · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA201100131Engine · malfunctionedCREW REPORTED SMOKE IN THE CABIN EMERGENCY DECLARED. T/S TO THE RIGHT ENGINE CAUSING THE SMOKE IN CABIN WITH EITHER LT OR RT PACKS RUNNING OFF RT ENGINE, A/C WAS FERRIED TO TYS FOR BOROSCOPE AND POSSIBLE ENGINE CHANGE.Feb 21, 2011 · N8886A · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA110223001Selector Valve · failedON 21 FEB. 2011, THE ACFT DEPARTED. AFTER GEAR UP SELECTION THE CREW GOT A "GEAR DISAGREE" MESSAGE AND NOTED THAT THE NOSE GEAR HAD NOT RETRACTED. THE ACFT RETURNED AND LANDED NORMALLY. THE FAULT COULD BE DUPLICATED IN THE HANGAR ON JACKS. T/S REVEALED THAT TFeb 21, 2011 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR REXA201100107Engine · malfunctionedON CLIMBOUT OF KMSP FOR KLNK, THE FLIGHT CREW NOTED A FLUCTUATION OF THE LT ENGINE OIL PRESSURE. AFTER CONTACT WITH COMPANY MAINTENANCE CONTROL, THE FLIGHT CREW ELECTED TO RETURN TO KMSP. ATC WAS CONTACTED AND AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADFeb 11, 2011 · N8758D · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2011020900002Wire Harness · pinchedON DEPARTURE AND INITIAL CLIMBOUT FROM DAY, CREW REPORTED THE ENGINE NR 2 VIBRATION GAUGE SHOWED AMBER DASHES WITH VIB INDICATION ON THE N2 GAUGE. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE HARNESS FORFeb 4, 2011 · N253PS · Cndair CL6002B19 · Engine Indicating System WiringSDR VNAA2011020700001Thermocouple · crackedCREW REPORTED RIGHT ENGINE ITT ERRATIC AND RIGHT ENGINE ITT HOT ICON DURING APPROACH TO CLT. AIRCRAFT LANDED WITHOUT INCIDENT IN CLT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE RIGHT ENGINE OUTBOARD THERMOCOUPLE HARNESS AND PERFORMED CHECFeb 1, 2011 · N250PS · Cndair CL6002B19 · Engine EGT/TIT Indicating SystemSDR REXA201100074Engine · dirtyPASSING THROUGH 100 KNOTS ON TAKEOFF ROLL FROM KTYS THE SMOKE TOILET WARNING ILLUMINATED. THE FLIGHT CREW ABORTED THE TAKEOFF AND CLEARED THE RUNWAY. NO FIRE WAS NOTED AND THE WARNING EXTINGUISHED WHEN THE THRUST LEVERS WERE RETURNED TO IDLE. AFTER CLEARINGJan 30, 2011 · N8495B · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201140118Cowling · chafedLT LOWER CORE COWL IS CHAFED AT FWD LATCHES. REPAIRED LT LOWER CORE COWL IAW CMM 228-50142 TASK 71-12-01-300-822 AOL.Jan 27, 2011 · N412AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201140117Cowling · chafedRT LOWER CORE COWL IS CHAFED AT FWD LATCHES. REPAIRED RT LOWER CORE COWL IAW CMM 228-50142, TASK 71-12-01-300-822-A01.Jan 27, 2011 · N412AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201140119Structure · crackedUPPER OTBD CASCADE ON RT THRUST REVERSER CRACKED. REPAIRED RT T/R UPPER OTBD CASCADE IAW PROCESS SPEC 1 DWG AW-78-30-0711-04.Jan 25, 2011 · N412AW · Cndair CL6002B19 · Engine Thrust ReverserSDR VNAA2011013100011Compressor · damagedON CLIMBOUT FROM GNV, CREW REPORTED THE LEFT ENGINE FAILED AT ABOUT 3,000 FEET WITH SEVERE VIBRATION AND LOSS OF THRUST DOWN TO BELOW IDLE. ENGINE WOULD NOT RESPOND TO THRUST LEVER INPUTS. CREW SHUT DOWN THE LEFT ENGINE PER QRH, RETURNED TO GNV AND LANDED WIJan 24, 2011 · N202PS · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR VNAA2011012100005Anti-Ice Valve · malfunctionedCREW REPORTED A LEFT COWL ANTI-ICE AMBER MESSAGE UPON TAKEOFF FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE LEFT COWL ANTI-ICE VALVE AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENAJan 17, 2011 · N253PS · Cndair CL6002B19 · Air Intake Anti/De-Ice SystemSDR CA110117007Actuator · bindingDURING APPROACH AT 9000FT, FLAP SELECTION WAS MADE BUT THE FLAP FAIL MSG WAS POSTED. FLAPS DID NOT MOVE FROM THE ZERO POSITION. AIR SPEED WAS 200 KTS. CREW ELECTED TO RETURN TO DEPARTING STA. 2HR COLD SOAK IN CRUISE AT -38C. COMPLETED WITH WORK ACCOMPLISHEDJan 14, 2011 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA110114003Indicator · failedFLIGHT PHASE APPROACH, EVENT ON APPROACH - THE FLAPS FAILED AT 0 WHEN THEY WERE SELECTED. ACFT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. FLAP FAIL AT 0, SELECTION ON APPROACH 496489 (FLAP FAIL EVENT (OPERATING UNDER CREW RESET). CARRIED OUJan 13, 2011 · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR VNAA2011011700003Carbon Seal · defectiveCREW REPORTED MULTIPLE RIGHT ENGINE OIL PRESSURE MESSAGES ON DEPARTURE FROM MOB. CREW RETURNED TO MOB AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE AXIS-D CARBON SEAL (AT AIR TURBINE STARTER PAD) FOR THE RIGHT ENGIJan 9, 2011 · N251PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA110111007Plate · corrodedHEAVY CORROSION (LEVEL 2) FOUND ON THE SERRATIONS IN BETWEEN THE ANCHOR FITTING AND THE SERRATED PLATE FOR THE MAIN ENTRANCE DOOR FORWARD COUNTERBALANCE INSTALLATION. THE CORROSION WAS SEVERE ENOUGH TO CAUSE THE TWO ATTACH BOLT HEADS TO SEPARATE. CRACKS WERE AJan 8, 2011 · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201100001Flashlight · inoperativeF/O'S FLASHLIGHT INOP. R & R F/O'S FLASHLIGHT IAW AMM 25-61-01. OPS CHECK GOOD. DEFER CLEARED. PLACARD REMOVED. (CLOSED)Dec 30, 2010 · N975EV · Cndair CL6002B19 · Emergency EquipmentSDR VNAA2011010600019Carbon Seal · damagedCREW REPORTED A RIGHT ENGINE OIL PRESSURE MASTER WARNING ON CLIMBOUT FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE CARBON SEAL ASSEMBLIES FOR THE RIGHT ENGINE’S EDP (ENGINE DRIVEN PUMDec 30, 2010 · N261PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA201040977Oil System · fluctuatesLT ENGINE OIL PRESSURE FLUX 28-44 PSI. CW QRH DIVERTED, OIL PRESSURE WARNING OCCURRED WHENEVER OIL PRESSURE INDICATED 28 PSI. TT FLUX 25 MINUTES. SERVICED ENGINE 5 PINTS OIL CHECKED MASTER SHIP DETECTOR IAW EMM 72-00-00, FAULT ISOLATION 15, FUZZ ON CHIP DETDec 30, 2010 · N458AW · Cndair CL6002B19 · Engine Oil Indicating SystemSDR MALA100209Lamp · inoperativeFWD OVERWING EMERGENCY LIGHT INOP. FWD OVERWING EMERGENCY LIGHT RE-LAMPED PN ON/OFF 1317.Dec 28, 2010 · N833AY · Cndair CL6002B19 · Emergency LightingSDR ASOA201100002Web · brokenNUTPLATE ATTACHMENT FLANGE ON PAX DOOR AFT WEB BROKEN OFF AND MISSING AT BOTTOM STEP 832AT TOP AFT ATTACHMENT SCREW LOCATION WITH CRACK EXTENDING INTO VERTICAL FLANGE. REMOVED PAX DOOR STEP 832BT IAW AMM 52-11-04-000-804. OK TO INSTALL STEP 832BT. INSTALLEDDec 28, 2010 · N882AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA101230003Fan · failedJUST AFTER DEPARTURE THE CREW RECEIVED A "SMOKE TOILET" WARNING MESSAGE. THE PASSENGERS AND F/A COULD SEE AND SMELL SMOKE IN THE LAVATORY AREA. WHEN CB`S WERE PULLED AND THE LAVATORY DOOR OPENED THE SMOKE AND ODOR DISSIPATED. THE ACFT RETURNED UNEVENTFULLY.Dec 28, 2010 · Cndair CL6002B19 · Air Distribution SystemSDR VNAA2010123000017Anti-Ice Valve · malfunctionedCREW REPORTED A RIGHT COWL ANTI-ICE CAS MESSAGE IN FLIGHT AT CLIMB POWER SETTING ON DEPARTURE FROM DAY. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE RIGHT COWL ANTI-ICE VALVE AND PERFORMED CDec 26, 2010 · N254PS · Cndair CL6002B19 · Air Intake Anti/De-Ice SystemSDR REXA201000305Controller · failedINTERMITTENT ANTI-ICE DUCT MESSAGE (LT) R & R LT BLEED LEAK CONTROLLER IAW AMM 36-21-10. OPS CHECK GOOD.Dec 20, 2010 · N8986B · Cndair CL6002B19 · Engine Bleed Air SystemSDR REXA201000308Scavenge Pump · shearedEN ROUTE TO KSYR AT FL230 THE LEFT ENGINE OIL PRESSURE WARNING ILLUMINATED. THE ENGINE WAS SHUTDOWN AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT WAS VECTORED INTO KSYR AND AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE. CFR INSPECTED THE AIRCRAFT AND FOUNDec 20, 2010 · N8936A · Cndair CL6002B19 · Engine Oil Distribution (Airframe Furnished)SDR CA101221007Windscreen · failed(CAN) IN CRUISE, AT F340, CREW NOTICED A CRACK IN THE CAPTAINS WINDSCREEN. FLIGHT CONTACTED MAINTENANCE CONTROL AND HAS DIVERTED. FLIGHT HAS LANDED SAFELY AND NO EMERGENCY WAS DECLARED. THERE WAS NO ADVERSE PASSENGER REACTION. DEFECT-957320 LP 589672 - RH W/S Dec 18, 2010 · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA2010122200013Engine · vibrationCREW REPORTED A VIBRATION ON THE RT ENGINE. AIRCRAFT RETURNED TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE USING AIRCRAFT MANUALS REMOVED AND REPLACED THE RT ENGINE. CHECKS WERE MADE USING MAINTENANCE MANUALS AND AIRCRAFT RELEASED FOR SERVICE.Dec 17, 2010 · N261PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA201001979Support Angle · crackedCARGO DOOR SILL SUPPORT ANGLE AT STA 605 LBL 36 FOUND CRACKED WL 73. REPLACED IAW SRM 51-42-21. REPAIR IS CLASSIFIED AS A MINOR.Dec 16, 2010 · N882AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001984Strap · corrodedPAX DOOR SURROUND LOWER FLOOR STRAP IS CORRODED BETWEEN FS 310 AND FS 349. REMOVED CORROSION FROM THE TOP OF THE PAX DOOR FLOOR SILL PLATE, MAX DEPTH REMOVED IS .005 AND IS WITHIN ALLOWABLE LIMITS OF T/E SRM 53-21-23 & 53-00-00. BLENDED CORROSION IAW SRM Dec 16, 2010 · N882AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001985Control Unit · failedREPEAT WRITE-UP ENROTE FO'S PFD , MFD FLIGHT DIRECTOR, NAV2 AUTOPILOT WERE ALL LOST AND WENT BLANK MULTIPLE TIMES ALSO, CAPTAINS FLIGHT DIRECTOR WAS LOST DC TIE 1 CLOSED AT ONE POINT. NOTICED A DC BUS 2 MSG ALSO, BUT IT EXTINGUISHED ITSELF (ENROUTE, ACFT DIVEDec 16, 2010 · N901EV · Cndair CL6002B19 · Central DisplaySDR ASOA201001986Light · inoperativeEXTERIOR EMERGENCY LIGHT NR3 INOP. R & R EXTERIOR EMERGENCY LIGHT NR3 IAW AMM 33-51-21. OP'S CHECK GOOD. (CLOSED)Dec 16, 2010 · N923EV · Cndair CL6002B19 · Emergency Lighting
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