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 A6WA201141083Skin · chafedLOWER CORE COWL INNER SKIN CHAFED AND GOUGED IN 5 AREAS CUT OUT DAMAGE AND INSTALL REPAIR DOUBLER IAW CMM 71-12-01, AREAS 3, 4, 5 FOUND TO BE LIMITED TO PAINT ONLY.Oct 16, 2011 · N467AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR VNAA2011101900014Scavenge Pump · malfunctionedCREW REPORTED LEFT OIL PRESSURE DROPPED FROM 70 PSI TO 48 PSI ON TAKEOFF ROLL ON DEPARTURE FROM CLT. LEFT HAND OIL PRESSURE DROPPED TO 39 PSI AT 2,000 FEET. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT, REMOVED AND REPLACOct 13, 2011 · N244PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA201140866Cowling · missingLT LOWER FORWARD COWL MISSING, (FOUND COWL ON RUNWAY). INSTALL LEFT LWR NOSE COWL W/SERV COWL. INSTALL LEFT LOWER NOSE COWL WITH SERV COWL. S/N OFF C0360 S/N ON SB/RJNAC/C0791.Oct 13, 2011 · N403AW · Cndair CL6002B19 · Engine Cowling SystemSDR A6WA201141012Skin · damagedLT UPPER CORE COWL INBD L/E DAMAGE. REPAIRED DAMAGE TO LT UPPER CORE COWL IAW CMM 71-12-01.Oct 11, 2011 · N471ZW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR MASA2011101063832Engine · inoperativeLT ENG FAILURE IN FLT. R2 NR 1 ENGINE.Oct 8, 2011 · N77260 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201141034Transcowl · chafedRT LOWER TRANSCOWL HAS CHAFE DAMAGE AT AFT POINT. REPAIRED DAMAGE TO RT LOWER TRANSCOWL AFT OF HINGE POINT IAW REO 601R-78-33-3969.Oct 7, 2011 · N422AW · Cndair CL6002B19 · Engine Thrust ReverserSDR VNAA2011101200012Engine · malfunctionedCREW REPORTED LEFT ENGINE OIL PRESSURE RED WARNING AND THAT OIL PRESSURE WENT TO ZERO PSI IN FLIGHT EN ROUTE FROM PHL TO BNA. CREW PERFORMED IN-FLIGHT SHUTDOWN OF LEFT ENGINE AND DIVERTED TO GSO. AIRCRAFT LANDED IN GSO WITHOUT FURTHER INCIDENT. MAINTENANCEOct 6, 2011 · N242JS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201140947Doubler · chafedRT LOWER CORE COWL EXTERNAL DOUBLER CHAFED AROUND FWD LATCHES. BLENDED CHAFING AROUND RT CORE COWL EXTERNAL DOUBLER IAW CMM 71-12-01-300-822 AOL.Oct 6, 2011 · N425AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR MASA2011100563815Garlock Seal · damagedNR 2 ENG OIL PRESS FLUCT 24-45 PSI. R2 IDG GARLOC SEAL.Oct 4, 2011 · N17358 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA110930017Seal · dislodged(CAN) "CARGO DOOR" CAUTION MSG ON ED1. PRESSURISATION PROBLEMS REPORTED BY THE CREW. ATB. ACFT LANDS AT ORIGIN AIRPORT. MX FOUND A PORTION OF DOOR SEAL DISBONDED.Sep 30, 2011 · Cndair CL6002B19 · Cargo/Baggage DoorsSDR REXA201100619Unknown · malfunctionedRIGHT ENGINE FUEL FLOW RAPID FLUCUATION ON TAKEOFF BETWEEN 2500 PPH-2000 PPH FLUCTUATION STABALIZED AFTER 4 MIN INDICATION NORMAL THERE AFTER. PERFORMED OPS CHECK OF FUEL DISTRIBUTION IAW AMM 73-10-00. NO DEFECTS NOTED. OK FOR SERVICE.Sep 22, 2011 · N8913A · Cndair CL6002B19 · Engine Fuel Indicating SystemSDR A6WA201141011Skin · chafedCHAFE CAUSED BY BLOCKER DOOR ON RT LOWER CORE COWL BY FWD LATCHES. R & R CHAFED DOUBLER IAW CMM 71-12-01.Sep 22, 2011 · N471ZW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR REXA201100615Unknown · malfunctionedDURING CLIMBOUT AND CRUISE THE THRUST LEVERS HAVE AT LEAST ONE INCH SPLIT DURING CLIMB. THE RT ENGINE N1 WOULD CONTINUE TO RISE WITHOUT THE THRUST LEVER INPUT. PERFORMED ENGINE RUNS FOUND TO BE WITHIN LIMITS IAW AMM 71-00-00.Sep 21, 2011 · N8444F · Cndair CL6002B19 · Power LeverSDR CA111005007Skin · cracked(CAN) DURING A SCHEDULED IN-HOUSE TASK FOR SCRATCH AND DENT SURVEY OF THE EXTERNAL FUSELAGE, NOTICED A CRACK EMITING FROM THE AFT LATCH CUT-OUT FOR THE LT ELECTRONICS BAY DOOR IN THE NOSE OF THE ACFT. THE DAMAGE LOCATED AT BS 189, WL 75.25. JUST BELOW THE RVSep 19, 2011 · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR CA110914007Altimeter · failed(CAN) GROUND SPOILERS DEPLOYED DURING TAKEOFF. NO ASSOCIATED SECU FAULT CODES FOUND. PERFORMED AUTO AND MANUAL GLD TESTS IAW AMM 27-65-00. GLD MODES TEST CORRECTLY. GROUND SPOILER PROXIMITY SENSORS ARE ADJUSTED CORRECTLY IAW AMM 27-60-00, ALL GLD ASSOCIATSep 11, 2011 · Cndair CL6002B19 · Altimeter, Barometric/EncoderSDR A6WA201140875Skin · bentRIGHT ENGINE TAIL PIPE FAIRING CUT OUT FOR ACCESS PANEL 446BB IS BENT AND GOUGED. REPAIRED RT ENGINE TAIL PIPE IAW CMM 78-11-00, REPAIR SRS 062.Sep 10, 2011 · N466AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA201140876Lug · chafedLEFT THRUST REVERSER OTBD LOWER TRACK LUG CHAFED, BLENDED DISCREPANT AREA IAW SRM 51-21-06 AND COMPLIED WITH REO 601R-78-34-2435.Sep 9, 2011 · N466AW · Cndair CL6002B19 · Engine Thrust ReverserSDR VNAA2011090800003Pump · fluctuatesCREW REPORTED LEFT ENGINE OIL PRESSURE MESSAGE IN FLIGHT EN ROUTE FROM CAK TO PHL. CREW FOLLOWED QRH AND SHUT DOWN LEFT ENGINE. AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AIRCRAFT, REMOVED AND REPLACED LEFT ENGINE LUBE AND SCAVENGE PUMSep 2, 2011 · N253PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA201140792Pdu · out of rigRT REVERSER UNLOCK CAUTION MESSAGE INFLIGHT IN CRUISE FLIGHT 26.0. REMAINED ILLUMINATED UNTIL ENGINE SHUTDOWN. FOUND PDU OUT OF RIG ADJUSTED DIRECTIONAL CONTROL VLV IAW AMM 78-32-03. OPS CK GOOD CLEARS PLACARD & MEL.Sep 2, 2011 · N456ZW · Cndair CL6002B19 · Engine Thrust ReverserSDR CA110907003Selector Valve · failed(CAN) UPON LANDING THE CREW NOTICED THAT THE NLG DOORS OPENED BUT THE GEAR DID NOT RETRACT. THEY PERFORMED THE EMERGENCY RETRACTION WITH NO ISSUES AND LANDED WITH NO ISSUES. AFTER TROUBLESHOOTING, FOUND THE NLG SELECTOR VALVE FAILED. A NEW VALVE WAS INSTALLSep 1, 2011 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR 2011FA0000550Housing · arcedDURING DESCENT, THE F/A REPORTED A FAINT SMOKE OR ELECTRICAL ORDER AND FLICKERING LIGHTS IN THE GALLEY AREA. INSPECTED ON GROUND FOUND SIGNIFICANT DAMAGE TO A LIGHT ASSY DUE TO ELECTRICAL ARCING. NO RECENT MAINTENANCE HAS BEEN PREFORMED ON THE LIGHT ASSY. Aug 25, 2011 · N591ML · Cndair CL6002B19 · Passenger Compartment LightingSDR A6WA201140785Torque Box · damagedRT THRUST REVERSER TORQUE BOX HAS NUMEROUS DAMAGED AREAS, REO 78-30-4072.Aug 24, 2011 · N408AW · Cndair CL6002B19 · Engine Thrust ReverserSDR CA110822011Winglet · damaged(CAN) CREW REPORTED THEY HAVE BEEN STRUCK BY A LIGHTNING STRIKE ON THE LT WING DURING DESCENT. INITIAL INSPECTION REVEALED SOME DAMAGE TO THE LOWER LT WINGLET STATIC DISCHARGER. THE ACFT WAS REMOVED FROM SERVICE AND INSPECTED IAW THE ACT MM CHAP 05-51-05. IAug 21, 2011 · Cndair CL6002B19 · Wing Main, Frame StructureSDR VNAA2011081800011Blade · bentCREW REPORTED POSSIBLE BIRD STRIKE ON TAKEOFF. NO VIBRATION INDICATION NOTED. AT CLT, MAINTENANCE INSPECTED, FOUND THREE (3) BENT BLADES IN RIGHT ENGINE FAN, REMOVED AND REPLACED THREE (3) SETS OF BLADES AND PERFORMED CHECKS USING MAINTENANCE MANUALS. AIRCRAug 15, 2011 · N259PS · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR A6WA201140837Seal · crackedLT TRANSCOWL TORQUE BOX UPPER AND LOWER SEALS ARE CRACKED. R & R IAW SRM 51-42-13.Aug 10, 2011 · N461AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201140811Structure · chafedRT ENGINE LOWER NOSE COWL AFT EDGE IS KNIFE EDGED. R & R AFT EDGE STRIP IAW CMM 71-14-01, REPAIR.Aug 10, 2011 · N405AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201140739Fcu · leakingSTRONG FUEL ODOR PERMEATING CABIN AND COCKPIT. INCREASING IN INTENSITY. INSPECTED AND FOUND APU FCU LEAKING WHEN APU IS RUNNING. OPERATED BOTH PACKS WITH ENGINE BLEED AIR. ODOR HAS DISSIPATED. R & R LT FCU P LT AND SPLIT, NEVER EXCEED .5 INCH. OK FOR SERAug 8, 2011 · N456ZW · Cndair CL6002B19 · APU Engine Fuel and ControlSDR A6WA201140836Structure · crackedRT UPPER THRUST REVERSER CASCADE CRACKED IN 4 PLACES. REPAIRED CRACKS IN RT UPPER THRUST REVERSER CASCADE IAW AWAC PROCESS SPEC 1.Aug 8, 2011 · N461AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201140812Stiffener · crackedRT JET PIPE FAIRING HAS CRACKED STIFFENER. REMOVED UNSERVICEABLE STIFFENER ON RT JET PIPE FAIRING IAW CMM 20-421-06. LOCATED AND DRILLED SERVICEABLE STIFFENER IAW CMM 20-40-11 INSTALLED SERVICEABLE STIFFENER ON RT JET PIPE IAW CMM 20-42-06.Aug 5, 2011 · N405AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA201140689Structure · crackedRT LWR CORE COWL HAS CRACK ON FIREWALL OTBD OF DRAIN. REPAIRED UNSERVICEABLE DAMAGE ON RT LOWER CORE COWL OTBD OF DRAIN IAW CMM 71-12-01 SRS046. RESTORED TO ORIGINAL FINISH, ( ALODINED, PRIME PAINT) IAW SRM 51-21-11, 51-25-06, 51-25-16.Aug 3, 2011 · N461AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR SWIA201126981Engine · failedRIGHT ENGINE FAILURE ON TAKEOFF. (FLT 5307) REPLACED RIGHT ENGINE. P/N: CF34-3B1 S/N: 807356CAug 1, 2011 · N498CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR REXA201100505Engine · fluctuatesCREW REPORTED N1 AND N2 FLUX IN FLIGHT AND DID AIR RETURN TO MEM. OPS CHECK GOOD IAW AMM 71-00-00 RETURNED TO SERVICE.Jul 31, 2011 · N8896F · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201140620Skin · gougedRT LOWER CORE COWL INNER SKIN GOUGED. REPAIRED GOUGE IAW CMM 71-12-01 AND REO 601R-71-12-4073.Jul 24, 2011 · N420AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201140621Panel · crackedLT ENGINE LOWER NOSE COWL THRUST REVERSER PDU ACCESS DOOR VENT LOUVER CRACKED. R & R VENT IAW SRM 51-42-13.Jul 23, 2011 · N465AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR MASA2011072103281Engine · inoperativeORIGINAL INSTALLED NR 2 ENGINE WAS A CF34-3B1 WHICH WAS CANNED FOR USE ON ANOTHER AIRCRAFT; A CF34-3A1 WAS INSTALLED PER EO#CRJ-71-0007 ENGINE RETROFIT (ONE ENGINE ONLY).Jul 20, 2011 · N7305V · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201140612Oil System · leakingAT ALTITUDE, RECEIVED RT ENGINE OIL WARNING MESSAGE. (FL30.0 APPROX 80 PERCENT N1) RETARDED THROTTLE TO 76 PERCENT N1 WARNING EXTINGUISHED, PRESSURE READ 33 PSI. AFTER 5 MIN WARNING RETURNED. AT THROTTLE IDLE PRESSURE INDICATED 30 PSI. INDICATION FLUXUATEDJul 20, 2011 · N407AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR ASOA201101345Converter · failedIN FLIGHT, REX RA FAULT, TCAS FAIL, GPWS FAIL, & OTBD GND SPL FAULT. COMPLIED W/ QRH & RECEIVED INBD GND SPOILER, FLT SPOILER, OTBD GND SPOILERS, & SPOILERONS CAUTION MSGS. COMPLIED W/ QRH. EMERGENCY DECLARED AS A PRECAUTION. R & R RAD ALTIMETER CONVERTER AJul 18, 2011 · N824AS · Cndair CL6002B19 · Ground Proximity SystemSDR ASOA201101346Motor · failedPAX DOOR WILL NOT OPEN. REMOVED AND REPLACED PAX DOOR MOTOR ASSY IAW AMM 52-11-08. OPS CHECKED GOOD NO FURTHER DEFECTS FOUND.Jul 18, 2011 · N836AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140609Carbon Seal · failedON POST FLT WALK AROUND FOUND SMOKE COMING FROM NR 2 JET PIPE AND STRONG ODOR. R & R OF NR 7 CARBON SEAL. OPS AND LEAK CHECK GOOD. REF EMM 72-00-00, SEP 38.Jul 15, 2011 · N408AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR REXA201100446Fuel Control · out of rigCREW STATES THAT WHEN THE RIGHT TR WAS STOWED THE ENG FLAMED OUT. AFTER LANDING IN DTW FROM CWA RE-RIGGED RIGHT ENG. FUEL CONTROL IAW AMM 73-20-00 & RERIGGED RIGHT ENG THROTTLE GEARBOX IAW AMM 72-60-00 ALL SYSTEMS OP'S CHECKED GOOD. AWAITING RESULTS OF DFDRJul 14, 2011 · N8936A · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA110713003Block · wornDOING THE INSP FOR A/D CF-2011-18, WHAT WAS FOUND IS THAT ALL 5 FAIRLEAD BLOCK ON THE NR 2 HYD SYS ALL 5 BLOCKS ARE WORN COMPLETELY, CHAFING ON THE OTHER LINES, IAW IPC 29-11-00, FIG 20, ITEM 370.Jul 12, 2011 · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA201140604Skin · chafedLT LOWER CORE COWL HAS 4 CHAFED AREAS. REPAIRED IAW REO 601R-71-12-4064.Jul 11, 2011 · N463AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR MASA2011071103197Engine · malfunctionedDIVERT EMER RT ENGINE SHUT DOWN OIL PRESS WARNING. R2 ENGINE.Jul 9, 2011 · N17358 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201140701Skin · dentedLT LWR CORE COWL DENT BETWEEN FWD AND AFT HINGES. REWORKED DENT BY REO 601R-71-12-4066.Jul 8, 2011 · N419AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201140600Skin · dentedLT LWR CORE COWL INNER SKIN HAD 3 DENTS OUT OF LIMITS. CUT AWAY DAMAGE C/W, REO 601R-71-12-4064 AND CMM 71-12-01. REPAIR NR SRS 095 AND SRS 021.Jul 7, 2011 · N463AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR ASOA201101289Seat Track · corrodedFIRST 2 RT SIDE CABIN FLOOR SEAT TRACKS ARE CORRODED. FABRICATED SEAT TRACK IAW REO 601R-53-00-424. LOCATED, DRILLED & COUNTERSUNK EXTRUSION SEAT TRACK IAW SRM 51-40-11. INSTALLED FLOOR STEAT RAILS IAW AMM 53-01-11-400-802.Jul 6, 2011 · N873AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101287Sign · brokenWARDROBE VERTICAL EMERGENCY EXIT SIGN HAS BROKEN FRAME. R & R WARDROBE VERTICAL EMERGENCY EXIT SIGN IAW AMM 33-51-10. OPS CK GOOD.Jul 5, 2011 · N928EV · Cndair CL6002B19 · Emergency LightingSDR VNAA2011070800007Tire · separatedAT OAJ, CREW FOUND LEFT INBOARD MAIN TIRE TREAD SEPARATED, DAMAGE TO INBOARD FLAP AT WING ROOT AND DAMAGE TO LEFT ENGINE. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED LEFT INBOARD AND OUTBOARD MAIN LANDING GEAR TIRES, LEFT INBOARD FLAP AND LEFT FLAJul 1, 2011 · N254PS · Cndair CL6002B19 · TireSDR A6WA201140726Track · gougedLT UPPER PYLON TRACK PN 228-50200-809 GOUGE 0.4" X 0.4" MAX DEPTH 0.070" BLENDED AND APPLIED PROTECTIVE TREATMENT IAW REO 601R-78-30-4069.Jul 1, 2011 · N463AW · Cndair CL6002B19 · Engine Thrust ReverserSDR REXA201100435Engine · overspeedRT ENGINE N2 OVER SPEED PEAKED TO 99.5 AT 101F OAT. PER GE MANUAL 72-00-00 INSPECTION MUST BE PERFORMED WITHIN 10 FC OPENED DI-46424 IAW GE MANUAL FOR COMPLIANCE.Jun 30, 2011 · N8515F · Cndair CL6002B19 · Engine (Turbine/Turboprop)
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