GE CF34-3B1

Service difficulty reports · 5,402

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 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 CA120112003Fitting · worn(CAN) AME WAS PERFORMING A DETAILED INSPECTION OF THE RT SIDE AILERON ASSY IAW TASK RJ2-27-690-100 WHEN HE FOUND RT AILERON OTBD PCU LINK ATTACHMENT FITTING ON THE AILERON TO BE WORN 011-.012" OVERSIZE WHERE THE ATTACHMENT BOLT HAT BUSHING IS INSTALLED. THE Jan 10, 2012 · Cndair CL6002B19 · AileronsSDR A6WA201240172Link Assy · chafedRT THRUST REVERSER NR 1 LINK ARM CHAFED. BLENDED CHAFE IAW REO 601R-78-30-2940, FOUND TO BE WITHIN LIMITS.Jan 6, 2012 · N410AW · Cndair CL6002B19 · Engine Thrust ReverserSDR SWIA201229158Oil System · overservicedRETURNED TO THE FIELD WITH LEFT ENGINE HIGH OIL TEMPERATURE. (FLT 6403) INSPECTED LEFT ENGINE OIL LEVEL FOUND TO BE OVERSERVICED, REMOVED 2 QTS OF OIL.Jan 5, 2012 · N405SW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA120105009Guide · sheared(CAN) THE AME WAS OPENING THE MAIN PASSENGER DOOR MANUALLY FROM THE OUTSIDE WHEN THE SHAFT GUIDE OFF THE AFT LEVER SWIVEL WHICH IS PART OF THE MAIN DOOR COUNTERBALANCE, SHEARED OFF WHILE THE DOOR WAS STILL IN TRANSIT. THE SHEARED OFF PART OF THE SHAFT GUIDE FLJan 5, 2012 · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201229089Unknown · malfunctioned(FLT 4456) DURING CLIMBOUT, CREW REPORTED A SERIES OF LOUD NOISES AND THE AIRCRAFT YAWED LEFT. LEFT ENGINE ITT CLIMBED. CREW PULLED POWER BACK TO IDLE AND RETURNED TO THE FIELD. REMOVED AND REPLACED LEFT ENGINE.Jan 3, 2012 · N461SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA120106001Control Cable · failed(CAN) L/H ENGINE IDLE PARAMETERS WERE OUT OF TOLERANCE. UNABLE TO SHUT DOWN ENGINE WITH THROTTLE LEVER. UPON INVESTIGATION, FOUND THROTTLE CABLE BROKEN. MANUFACTURER OF CONTROL CABLE IS TRANSDIGM INC.*CCDBA AEROCONTROLLEX DIV AERO CONTROLE (TC# 20120106001)Jan 3, 2012 · Cndair CL6002B19 · Power LeverSDR CA120118003Compressor · damaged(CAN) CREW REPORTED DURING CLIMB OUT AT APPROX 14,000 FT, X3 LOUD BANGS FROM LT ENGINE, ITT WENT INTO RED, AND HIGH VIBRATION. ENGINE RETURNED TO IDLE AND CREW ELECTED TO RETURN TO FIELD. MAINTENANCE DISCOVERED COMPRESSOR DAMAGE ON LT ENGINE.Jan 3, 2012 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR A6WA201240160Skin · erodedRT ENGINE NOSE COWL HAS EROSION ON L/E SKIN. REMOVED LIGHT EROSION FROM L/E LIP SKIN AND POLISHED WITH SCOTCHBRITE IAW REO 601R-71-61-2532. MON THICKNESS PRIOR TO BLENDING 0.050. MIN THICKNESS AFTER BLENDING 0.048. WITHIN LIMITS IAW REO 601R-71-61-2532.Dec 31, 2011 · N410AW · Cndair CL6002B19 · Engine Air Intake SystemSDR VNAA2011123000017Wire Harness · defectiveCREW REPORTED RIGHT ENGINE REV UNLOCKED CAUTION MESSAGE DURING FLIGHT EN ROUTE FROM CLT TO DCA. CREW DIVERTED TO RIC AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THRUST REVERSER SYSTEM, REMOVED AND REPLACED RIGHT ENGINE ORANGE ELECTRICAL HARNESS AND Dec 27, 2011 · N241PS · Cndair CL6002B19 · Engine Exhaust System WiringSDR CA111222009Angle · cracked(CAN) WHILE PERFORMING A DETAILED INSPECTION OF THE LT SIDE AND RT SIDE CENTER FUEL TANK FOR TASKS RJ2-57-510-502 AND RJ2-57-610-502, RESPECTIVELY, THE AME NOTED CRACKS EMINATING FROM EACH OF THE 2 RELIEF CUTOUTS FOR THE STRINGERS IN THE WEB OF THE SUPPORT ANGDec 21, 2011 · Cndair CL6002B19 · Wing Miscellaneous StructureSDR CA111222003Skin · cracked(CAN) WHILE CARRYING OUT A SCHEDULED SCRATCH AND DENT SURVEY OF THE FUSELAGE ASSY, THE AME FOUND A CRACK EMANATING FROM THE AFT LATCH CUT-OUT FOR THE LT SIDE ELECTRONICS BAY DOOR IN THE NOSE OF THE ACFT. THE DAMAGE LOCATED AT BS FS189 JUST BELOW THE RVSM AREADec 20, 2011 · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201141145Engine · oil consumptionRIGHT ENGINE OIL PRESSURE WARNING MESSAGE INFLIGHT, QRH PERFORMED INFLIGHT. ENGINE SHUTDOWN PRIOR TO SHUTDOWN ENGINE OIL PRESSURE WAS 5 PSI OIL TEMP NORMAL. AFTER ENG SHUTDOWN, PRESSURE INDICATED 0 PSI, 15 MIN TOTAL SHUTDOWN TIME. INSTALLED RT ENGINE CRANK PDec 19, 2011 · N427ZW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA201141142Engine · oil consumptionRIGHT ENGINE OIL PRESSURE WARNING MSG IN FLIGHT. COMPLIED WITH QRH PERFORMED INFLIGHT ENGINE SHUTDOWN. PRIOR TO SHUTDOWN ENGINE OIL PRESSURE WAS 5 PSI, OIL TEMP NORMAL. AFTER ENGINE SHUTDOWN PRESSURE INDICATED 0 PSI. 15 MIN TOTAL SHUTDOWN TIME. REINSTALLEDec 19, 2011 · N427ZW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA201141146Pdu · failedRIGHT THRUST REVERSER UNLOCK MESSAGE DURING TAKE OFF ROLL, ABORTED TAKE OFF AT 102 KTS BTMS MAX READS 7744. R & R RT PDU IAW 78-32-03. OPS CHECKED GOOD.Dec 17, 2011 · N446AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201240215Structure · chafedRT UPPER NOSE COWL AFT EDGE STRIP IS CHAFED. R & R RT UPPOER NOSE COWL AFT EDGE STRIP IAW CMM 71-14-01-300-814-A01.Dec 16, 2011 · N432AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR VNAA2011122000012Actuator · bindingCREW REPORTED R REV UNLOCK CAS MESSAGE JUST BEFORE V1 ON TAKEOFF FROM CAK. CREW RETURNED TO CAK AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THRUST REVERSER SYSTEM AND REMOVED AND REPLACED THE FOLLOWING COMPONENTS FOR THE RIGHT THRUST REVERSER: PDU Dec 15, 2011 · N241PS · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201240082Skin · dentedRT NACELLE CORE COWL HAS SEVERAL DENTS IN SAME AREA. REPAIRED RT ENG LOWER CORE COWL DENTS IAW CMM 71-12-01.Dec 15, 2011 · N427ZW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201240112Skin · chafedLEFT LOWER CORE COWL OUTER SKIN CHAFED BY FWD LATCHES LT LOWER CORE COWL OUTER SKIN. REPAIRED IAW CMM 71-12-01-300-822. REPAIRE NR SR104.Dec 14, 2011 · N433AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR CA111215003Handle · corroded(CAN) DURING INSPECTION TASK RJ2-52-830-100, DETAILED INSPECTION OF THE CREW ESCAPE HATCH, THE OUTER HANDLE WOULD NOT RELEASE. UPON DISASSEMBLY, THE HANDLE & HANDLE HOUSING ASSEMBLY WAS FOUND BADLY CORRODED. MOISTURE WAS FOUND WITHIN THE ASSEMBLY WHEN DISASSDec 14, 2011 · Cndair CL6002B19 · Emergency ExitsSDR CA111215009Coupling · corroded(CAN) FUEL BALANCING PIPES ASSOCIATED WITH L/H & R/H COLLECTOR TANK REMOVAL HAVE BEEN FOUND WITH VARYING LEVELS OF CORROSION. THIS CORROSION IS DUE TO THE GROUNDING COUPLINGS WEARING AWAY THE FLANGES OF THE PIPES. ONCE THE FLANGES ARE WORN THEY ARE SUSCEPTABLEDec 13, 2011 · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR A6WA201240086Heat Shield · dentedRT LOWER CORE COWL FIRE SHIELD DENTED. REPAIRED RT LOWER CORE COWL FIRE SHIELD IAW CMM 71-12-01, SRS 095.Dec 12, 2011 · N427ZW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR CA111212012Proximity Switch · frozen(CAN) AFTER TAKEOFF & GEAR UP SELECTION, THE GEAR DISAGREE WARNING CAME ON. THIS HAPPENED WITHIN 6 SEC AFTER GEAR UP SELECTION. NOSE GEAR EICAS INDICATION BOX WENT RED. CREW BELIEVED THAT THE MLG DID MOVE BUT THE NLG DID NOT. NO TURBULENCE OR EXCESSIVE MOVDec 12, 2011 · Cndair CL6002B19 · Landing Gear Position and WarningSDR REXA201100964Gearbox · out of rigLEFT THRUST LEVER WILL NOT ADVANCE PAST 94 PERCENT AT FLIGHT LEVEL 170 IT APPEAR TO HIT STOPS 4 PERCENT PRIOR BEFORE READING MAX. FOUND LT ENG THROTTLE GEARBOX SPLINE TO BE OUT OF RIG. RIGGED PER AMM 76-11-17 AND PERFORMED ENGINE RUNS PER AMM 71-00-00. OP/CDec 11, 2011 · N8982A · Cndair CL6002B19 · Power LeverSDR CA111212001Engine · malfunctioned(CAN) THE CREW DECLARED EMERGENCY, REPORTING AN ENGINE FAILURE. RT ENGINE OIL WARNING MESSAGE APPEARED IN-FLIGHT. MINIMAL SIGN OF SMOKE IN THE CABIN. RT ENGINE REPLACED.Dec 11, 2011 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2011121200004Anti-Ice Valve · failedCREW REPORTED RIGHT ENGINE ANTI-ICE INOPERATIVE IN FLIGHT AFTER DEPARTURE FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED RIGHT ENGINE COWL ANTI-ICE VALVE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANDec 6, 2011 · N248PS · Cndair CL6002B19 · Air Intake Anti/De-Ice SystemSDR A6WA201240083Seal · chafedLEFT LOWER COLW T/E SEAL CHAFED. REPAIRED LT LOWER NOSE COWL T/E SEAL IAW CMM 71-14-01, SUBTASK 71-14-01-110-013-A01.Dec 2, 2011 · N427ZW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA201240039Skin · chafedRT UPPER NOSE COWL T/E STRIP CHAFED. REPAIRED RT UPPER NOSE COWL T/E STRIP IAW CMM 71-14-01.Nov 30, 2011 · N426AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR REXA201100874Fuel Control · leakingLEFT ENG MFC LEAKING. REMOVED AND REPLACED LT ENG MAIN FUEL CONTROL IAW AMM 73-21-01. VERIFIED PART EFFECTIVITY, LEAK CHECK GOOD. PERFORMED ALL NECCESSARY ENGINE RUNS FOR LT MFC. REMOVED AND REPLACED IAW AMM 71-00-00 OP/C & FC GOOD.Nov 26, 2011 · N8928A · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR REXA201100875Engine · making metalLEFT OIL MASTER WARNING MESSAGE. EMERGENCY DECLARED. FOUND METAL CONTAMINATION ON LT ENGINE CHIP DETECTOR AND ON LUBE AND SCAVENGE PUMP FILTER. R&R LT ENG IAW AMM 71-00-00 AND CHECKLIST PROVIDED. PART EFFECTIVITY VERIFIED. PERFORMED ALL REQUIRED BREAK-IN Nov 26, 2011 · N8721B · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA111125005Support Angle · cracked(CAN) WHILE PERFORMING A DETAILED INSPECTION OF THE LT & RT CTR FUEL TANK FOR TASKS RJ2-57-510-502 & RJ2-57-610-502 RESPECTIVELY, THE AME NOTED CRACKS EMANATING FROM EACH OF THE TWO RELIEF CUT OUTS FOR THE STRINGERS IN THE WEB OF THE SUPPORT ANGLE, PN 601R-100Nov 24, 2011 · Cndair CL6002B19 · Wing Miscellaneous StructureSDR REXA201100871Engine · malfunctionedRT ENGINE FAILURE SHORTLY AFTER TAKEOFF. LOUD POP, FOLLOWED BY ENGINE SPOOL DOWN AND R ENG OIL WARNING MSG, ITT SPIKED IN RED. REMOVED AND REPLACED RT ENGINE IAW CHECKLIST. VERIFIED PART EFFECTIVITY. ALL LEAK & OPS CHECKS GOOD PER AMM 71-00-00. ALL RUNS RNov 23, 2011 · N8836A · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA111121002Selector Valve · failed(CAN) ON APPROACH, THE TWO MLGS FAILED TO EXTEND UPON GEAR DOWN SELECTION AND THE CREW RECEIVED A "GEAR DISAGREE" WARNING MESSAGE. THE FLIGHT CREW EXECUTED A GO AROUND, LOWERED THE GEARS USING THE ALTERNATE HANDLE AND LANDED WITHOUT FURTHER INCIDENT. THE MLG Nov 20, 2011 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA201240040Track · chafedLT THRUST REVERSER OTBD TRACK ATTACHING LUG CHAFED. BLENDED LT LOWER OTBD TRACK ATTACHING LUG DAMAGE IAW REO 601R-78-34-2435.Nov 19, 2011 · N426AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201240041Blocker Door · chafedLT THRUST REVERSER BLOCKER DOORS 3-10 CHAFED FROM STOPS. AFTER FURTHER INVESTIGATION, FOUND DAMAGE ON ALL 10 BLOCKER DOORS. BLENDED DAMAGED AREAS ON LT T/R BLOCKER DOORS IAW CMM 78-30-00.Nov 19, 2011 · N426AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201240042Blocker Door · chafedLEFT THRUST REVERSER BLOCKER DOORS 3-10 CHAFED FROM STOPS. BLENDED DAMAGED AREAS ON RT BLOCKER DOORS IAW CMM 78-30-00.Nov 19, 2011 · N426AW · Cndair CL6002B19 · Engine Thrust ReverserSDR CA111121004Spring · broken(CAN) DURING PREFLIGHT, NOTICE THE RT NOSE DRAG BRACE SPRING BROKEN OFF. GOT ANOTHER SPRING AND REPLACED IT. NO DAMAGE TO ACFT.Nov 18, 2011 · Cndair CL6002B19 · Nose/Tail Landing GearSDR REXA201100848Carbon Seal · leakingACFT DID AN AIR TURNBACK INTO BTV FOR SMOKE TOILET CAUTION MESSAGE AND THE LAV SMOKE DETECTOR WAS GOING OFF. EMERGENCY WAS DECLARED. UPON ARRIVAL BACK TO BTV THE FIRE DEPT SAID NO EVIDENCE OF SMOKE WAS DETECTED OUTSIDE THE ACFT, AND THEY USED A SMOKE SNIFFERNov 17, 2011 · N8505Q · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA201140972Engine · failedLT ENGINE MADE A LOUD POP THEN N1 AND N2 WENT TO ZERO. COMPLIEED WITH QRH, RETURNED TO DEPARTURE. OPENNov 16, 2011 · N427ZW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2011112100009Engine · vibrationCREW REPORTED NUMBER 1 ENGINE HAD N2 VIBRATION WITH ITT OF 998 DEGREES AFTER TAKEOFF FROM DCA. CREW COMPLIED WITH QRH, SHUT DOWN LEFT ENGINE, DIVERTED TO IAD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT ENGINE AND PERNov 15, 2011 · N216PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA111116003Unknown · smoke(CAN) ABORTED TAKEOFF DUE TO SMOKE IN THE COCKPIT AND CABIN.Nov 14, 2011 · Cndair CL6002B19 · Air Distribution SystemSDR A6WA201140965Skin · chafedRT UPPER CORE COWL IS CHAFED ON INNER FWD SIDE. BLENDED CHAFED AREA ON RT UPPER CORE COWL FWD SIDE AND REPAIRED IAW CMM 71-12-200-802-A01, MATT LOSS .002 MAT REMAINING .028. REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW CMM 71-12-200-802-A01.Nov 8, 2011 · N468AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR VNAA2011110900002Engine · malfunctionedCREW REPORTED RIGHT ENGINE OIL PRESSURE WARNING MESSAGE AND RIGHT ENGINE OIL INDICATION READ ZERO ON DESCENT INTO PHL. CREW COMPLIED WITH QRH AND SHUT DOWN RIGHT ENGINE. AIRCRAFT LANDED IN PHL WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPNov 4, 2011 · N209PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201140966Skin · dentedRT LOWER CORE COWL IS DENTED IN 2 LOCATIONS OF FWD INNER SIDE. REPAIR AREA IAW CMM 71-12-01-300-805-A01.Nov 4, 2011 · N468AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201141070Stiffener · crackedCRACKED FWD STIFFENER ON PANEL 446L, REPAIRED CRACKED STIFFENER IAW CMM 78-11-00-997-022-A07.Oct 31, 2011 · N411ZW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA201141072Skin · gougedRT LOWER CORE COWL INNER SKIN GOUGED 3EA SEATS 85-3. REPAIRED 3 EA LOCATION ON RT LWR INNER CORE COWL SKIN IAW CMM 71-12-01. REPAIR NR SRS046.Oct 28, 2011 · N411ZW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201141124Skin · dentedLT LOWER CORE COWL DENTED ON INNER FWD SIDE. REPAIR AREA IAW CMM 71-12-01.Oct 28, 2011 · N468AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR VNAA2011102800025Compressor · stalledCREW REPORTED LOUD BANG (COMPRESSOR STALL) AND HIGH ITT FROM RIGHT ENGINE ON TAKEOFF FROM DCA. CREW SHUT DOWN ENGINE AND DIVERTED TO IAD. MAINTENANCE INSPECTED RIGHT ENGINE AND DETERMINED REMOVAL AND REPLACEMENT OF ENGINE REQUIRED. REMOVED AND REPLACED RIGHOct 25, 2011 · N213PS · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA111021006Aileron · unknown(CAN) AFTER TAKE OFF CREW EXPERIENCED AILERON STIFFNESS IN FLIGHT, A/P DIS-CONNECTED AND CONTROLS FELT STIFF, ONCE CTRL WORKED STIFFNESS, WENT AWAY AND A/P WAS RE-ENGAGED AND THERE WERE NO FURTHER FAULTS FOR REMAINDER OF FLIGHT. AILERON SYS INSPECTED IAW SL-2Oct 21, 2011 · Cndair CL6002B19 · Aileron Control SystemSDR CA111021005Pulley · stiff(CAN) CAPTAIN ADVISED THAT AT 18,500 FT THEY RECEIVED AN AUTO-PILOT TRIM LT WING DOWN CAUTION LIGHT FOR 2 SECONDS THEN IT WENT OUT. THE LIGHT ILLUMINATED AGAIN THROUGH 18,000 FT. CREW THEN DISENGAGED THE AUTO PILOT TO SEE IF THEY HAD CONTROL AND NEITHER PILOTOct 20, 2011 · Cndair CL6002B19 · Aileron Control SystemSDR REXA201100734Fuel Control · faultyNR 2 N1, N2 AND FUEL FLOW FLUXATIONS IN CLIMB AND CRUISE. N1 DEVIATED ROUGHLY 1 PERCENT AND FUEL FLOW ROUGHLY 100LBS FLUXATIONS WERE CONTINUOUS AND ASSOCIATED WITH YAW. REMOVED AND REPLACED FUEL CONTROL UNIT IAW AMM 73-21-01, PERFORMED OPS CHECK OF RT ENG FCOct 18, 2011 · N819AY · Cndair CL6002B19 · Fuel Control/Turbine Engines
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