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 REXA201000014Compressor · damagedON CLIMBOUT OF KDTW, THE RIGHT ENGINE WOULD NOT REACH TARGET POWER SETTING WITHOUT OVER TEMPING. THE FLIGHT CREW ELECTED TO RETURN TO KDTW. CENTER WAS NOTIFIED AND THE AIRCRAFT WAS VECTORED FOR A RETURN APPROACH. ON THE APPROACH THE RIGHT ENGINE WAS MAKING Jan 26, 2010 · N8674A · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR A6WA201040182Attach Fitting · crackedCLIP CRACKED, R & R DAMAGED CLIP ON RT INBD 484 INTERCOSTAL IAW SRM 51-24-21, 51-42-06, 51-42-21.Jan 22, 2010 · N428AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR CHQA201000011Connector · malfunctionedDURING APPROACH, AFTER STARTING APU & TRANSFERRING BLEEDS TO APU WITH NO ISSUES, NR 2 GEN DROPPED OFF-LINE. NR 1 GEN DROPPED OFF-LINE SHORTLY AFTER. APU GEN TOOK OVER ALL ELECTRICAL LOADS. QRH FOLLOWED & GEN NR 1 BROUGHT BACK ON-LINE FOLLOWED BY GEN NR 2. Jan 19, 2010 · N667BR · Cndair CL6002B19 · Electrical Power System WiringSDR A6WA201040041Hinge Fitting · gougedRT ENGINE UPR TRANS COWL INNER INBD HINGE FITTING IS GOUGED. REPAIRED GOUGE IAW REO 601R-78-33-3923.Jan 19, 2010 · N410AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201040042Hinge Fitting · gougedRT ENGINE LWR TRANS COWL INNER INBD CTR HINGE FITTING IS GOUGED. REPAIRED GOUGE IAW REO NR 601R-78-33-3922.Jan 19, 2010 · N410AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201040151Arm · gougedLT INBD FLAP OTBD HINGE ARM HAS DAMAGE ON L/E FWD LOWEST ATTACH POINT. REPAIRED GOUGE IAW REO 601R-57-54-158.Jan 14, 2010 · N432AW · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR CA100114003Window · cracked(CAN) DURING DESCENT THE RT COCKPIT SIDE WINDOW INNER PLY CRACKED. THE A/C LANDED SAFELY AND THE WINDOW WAS REPLACED BEFORE FURTHER FLIGHT. WINDOW P/N 601R33033-12, S/N 99116H6100. WINDOW HOURS AND CYCLES, TSN 21815, CSN 16578. (TC NR 20100114003).Jan 13, 2010 · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA201040150Fitting · gougedRT WING OTBD FLAP OTBD AFT HINGE BOX FILLING ON A/C GOUGED. REPAIRED GOUGE IAW REO 601R-57-54-157.Jan 12, 2010 · N432AW · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR CA100121003Connecting Rod · broken(CAN) MCD PRESS DUMP DOOR CONNECTING ROD BROKEN. CREW DEPARTED AND COULD NOT PRESURIZE. NO INDICATIONS. THEY RETURNED TO DEPARTURE. (RESOLVED ON W/O: 221552 TASKCARD: NR-00001) MCD PRESS DUMP DOOR CONNECTING ROD REPLACED, RIGGED AND TESTED.Jan 11, 2010 · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201040161Seat Track · corrodedRT NR 2 FLOOR SEAT TRACK CORRODED BEYOND LIMITS REQUIRES REPLACEMENT. REPLACED RT NR 2 FLOOR SEAT TRACK.Jan 11, 2010 · N432AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040154Link · interferenceLT AND RT 513 DOGBONE LINKS TOUCHING. INSP AND DEFERRED IAW REO 601R-53-41-1148 5000 HR PERM REPAIR 1000 HR REINSPECT.Jan 10, 2010 · N432AW · Cndair CL6002B19 · Fuselage, Wing Attach FittingsSDR A6WA201040152Tube · chafedRT INBD FLAP INBD VANE ACTUATOR INNER TUBE WORN UNDER BOTTOM ROLLER. REPAIRED IAW REO 601R-57-52-1557.Jan 10, 2010 · N432AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040153Tube · chafedRT INBD FLAP MIDDLE VANE ACTUATOR INNER TUBE WORN UNDER BOTTOM ROLLER. REPAIRED IAW REO 601R-57-52-1552.Jan 10, 2010 · N432AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040158Angle · crackedRT MIDDLE WING L/E. INBD ATTACH ANGLE IS CRACKED. REPLACED ANGLE PN 600-12025-8 IAW SRM 51-41-02, 51-40-11.Jan 9, 2010 · N432AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA201040139Frame · crackedPAX DOOR FRAME UPPER FLANGE AT FS 338 CRACKED. REPAIRED IAW REO 601R-52-11-402.Jan 9, 2010 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040159Bracket · brokenLT JET PIPE FIRE LOOP MOUNT COVER FWD MOUNT STANDOFF BRACKET BROKEN. REMOVED BROKEN BRACKET AND REPALCED WITH FABRICATED BRACKET.Jan 8, 2010 · N432AW · Cndair CL6002B19 · Nacelle/Pylon, Attach FittingsSDR A6WA201040140Door · crackedAPU ENCLOSURE DOOR CRACKED TOP CENTER AS MARKED. REPAIRED 3 EA CRACKS IAW REO 601R-49-11-070.Jan 8, 2010 · N432AW · Cndair CL6002B19 · APU Cowling/ContainmentSDR A6WA201040157Attach Angle · crackedRT INBD WING L/E, OTBD ATTACH ANGLE IS CRACKED. REMOVED DAMAGED RT INBD WING L/E OTBD ATTACH ANGLE PN 600-12045-12.Jan 8, 2010 · N432AW · Cndair CL6002B19 · Wing, Attach FittingsSDR A6WA201040149Angle · crackedINTERCOSTAL ATTACH ANGLE ABOVE LINTEL FITTING ON AFT SIDE OF F/S 621 IS CRACKED. R & R IAW SRM 51-40-00, 53-61-19.Jan 6, 2010 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040155Angle · crackedLT WING CTR L/E INBD ATTACH ANGLE CRACKED. REMOVED DAMAGED ANGLE, LOCATED FASTENER HOLES IN SERVICEABLE ANGLE AND INSTALLED SERVICEABLE ANGLE IAW SRM 51-41-02.Jan 6, 2010 · N432AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA201040142Pressure Blkhd · chafed10TH STAGE BLEED AIR SHUTOFF VALVE ABOVE APU ENCLOSURE CHAFING CTR BEAM. REO 601R-53-61-1523 BLEND EDDY CURRENT INSPECT TREAT PRIME AND TOP COAT.Jan 5, 2010 · N432AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040141Angle · corrodedPAX DOOR AFT CORNER HAS CORROSION. R & R UPPER AND LOWER ANGLES.Jan 4, 2010 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040144Intercostal · crackedPAX DOOR FWD LOWER CORNER HAS A CRQCKED INTERCOSTAL. DUPLICATED ORIGINAL PART IAW SRM 51-24-21.Jan 4, 2010 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040160Seat Track · corrodedRT FLOOR SEAT TRACK CORRODED, R & R TRACK.Jan 4, 2010 · N432AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040162Seat Track · corrodedLT NR 1 FLOOR SEAT TRACK CORRODED. R & R SEAT TRACK.Jan 4, 2010 · N432AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR CHQA200900273Oil System · overservicedWITH THE NR 2 IDG ON MEL REQUIRING OPERATION OF THE APU DURING FLIGHT, THE CREW RECEIVED AN APU OIL TEMP MESSAGE ON EICAS. THE AIRCRAFT DIVERTED TO LIT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE APU OIL OVER SERVICED AND REMOVED EXCESS OIL TO THE CORDec 31, 2009 · N645BR · Cndair CL6002B19 · APU Oil SystemSDR CHQA200900275Windshield · crackedDURING CRUISE AT FL330 THE FIRST OFFICER'S OUTER WINDSHIELD CRACKED THEN SPIDER WEBBED COVERING THE REST OF THE RIGHT WINDSHIELD. THE AIRCRAFT DIVERTED TO KALB AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 WINDSHIELD WITH NO FURTHER DEFECTS NOTEDec 31, 2009 · N647BR · Cndair CL6002B19 · Flight Compartment WindowsSDR CA091231003Drive Unit · failed(CAN) CREW SELECTED FLAP 45 AND FOUND THAT THE FLAPS STOPPED AND STAYED AT 30 DEGREES. THIS WAS DISCOVERED ON APPROACH AT APPROX 2000 FT. THE CREW OVERSHOT DUE TO A SMALL TAILWIND ON RUNWAY 07 AND THEN GOT THEMSELVES RE-ESTABLISHED FOR THE APPROACH ONTO RUNWADec 31, 2009 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA201040148Attach Fitting · corrodedPAX DOOR LOWER AFT SIDE AT F/S 320.10 HAS CORROSION ON CLIP. REMOVED OLD CLIP AND FABRICATED NEW CLIP IAW SRM 51-31-59.Dec 31, 2009 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040145Attach Fitting · corrodedPAX DOOR LOWER AFT AT F/S 338.0 JAS CORROSION ON CLIP. REMOVED OLD CLIP, FABRICATED NEW CLIP IAW SRM 51-31-59.Dec 31, 2009 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040143Attach Fitting · corrodedPAX DOOR LOWER FWD SIDE AT F/S 320.10 HAS CORROSION CLIP. REMOVED CORRODED CLIP, FABRICATED NEW CLIP IAW SRM 51-31-59.Dec 31, 2009 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040146Attach Fitting · corrodedPAX DOOR LOWER FWD AT FS 338.00 HAS CORROSION ON CLIP. REMOVED OLD CLIP AND FABRICATED NEW CLIP IAW SRM 51-31-54.Dec 31, 2009 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040147Attach Fitting · corrodedPAX DOOR LOWER AFT SIDE AT F/S 329.50 HAS CORROSION ON CLIP. REMOVED OLD CLIP AND FABRICATED NEW CLIP IAW SRM 51-31-59.Dec 31, 2009 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040156Bracket · crackedLT JETPIPE UPPER INBD ATTACH POINT NUTPLATE BRACKET CRACKED. REMOVED DAMAGED BRACKET, DUPLICATED SERVICEABLE BRACKET IAW CMM 78-11-00, AND INSTALLED SERVICEABLE BRACKET IAW CMM 20-42-06.Dec 30, 2009 · N432AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR REXA200900142Fcu · defectiveWHEN REDUCING THRUST FOR DESCENT INTO KDTW, IT WAS OBSERVED THAT THE LEFT ENGINE HAD LIMITED RESPONSE TO THRUST INPUT. WITH THE THRUST LEVER AT IDLE, THE ENGINE WOULD NOT RETARD BELOW 66-68 PERCENT N1. THE FLIGHT CREW PERFORMED THE QRH, CONTACTED ATC AND COMDec 27, 2009 · N8908D · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR A6WA200940813Oil System · low pressureLT OIL PRESSURE MESSAGE INFLIGHT. COMPLIED WITH QRH. EVENTUALLY SHUTDOWN LT ENGINE AND LANDED SINGLE ENGINE. (K)Dec 25, 2009 · N459AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA091230001Door Frame · cracked(CAN) CRACK WAS FOUND ON THE CARGO DOOR FWD FRAME SURROUND RADIUS AT STA FS576 AND WL 97.75. THIS CRACK IS NOT EASILY VISABLE DUE TO APPLICATION OF SEALANT UNDER THE FITTING. TASK 52-31-02-01 CALLS OUT DETAILED VISUAL INSP (DVI) OF THE AREA - BUT DOES NOT REQUDec 24, 2009 · Cndair CL6002B19 · Fuselage Main, StructureSDR CA091218001Socket · shorted(CAN) PASSENGER IN 4F, REPORTED SEEING SPARKS COMING FROM THE OVERHEAD PANEL AND A PUFF OF SMOKE THAT LASTED JUST A MINUTE. FLIGHT CREW COULD SMELL THE SMOKE JUST AS FLIGHT ATTENDANT WAS ADVISING THEM OF THE SITUATION. SMOKE AND SMELL DISSIPATED VERY QUICKLYDec 18, 2009 · Cndair CL6002B19 · Passenger Compartment LightingSDR A6WA201040168Track · chafedLT TR MAIN LOWER OTBD TRACK CHAFED REO 601R-78-2435 CARRIED OUT.Dec 15, 2009 · N430AW · Cndair CL6002B19 · Engine Thrust ReverserSDR CA091208002Bracket · cracked(CAN) DEFECT-885812, SERVICE DOOR HANDLE PROX/STOP BRACKET CRACKED. BRACKET REPLACED.Dec 7, 2009 · Cndair CL6002B19 · Service DoorsSDR CA091208005Bracket · cracked(CAN) SERVICE DOOR HANDLE PROX/STOP BRACKET CRACKED. REPLACED. DEFECT-885812.Dec 7, 2009 · Cndair CL6002B19 · Service DoorsSDR A6WA201040138Bracket · crackedNUT BRACKET UNDER PANEL 326CL, LT SIDE OF VERTICAL STAB, CRACKED. REMOVED DAMAGED BRACKET AND INSTALLED SERVICEABLE PN 600-21137-5 BRACKET.Dec 7, 2009 · N432AW · Cndair CL6002B19 · Vertical StabilizerSDR A6WA200940781Engine · fluctuatesON CLIMB ABOVE 10000 FT RT ENG FLUCTUATIONS, APPROX 2 PERCENT N1 AND N2, 200 LBS F/F AND 20/30 DEG ITT FOR SEVERAL MIN, THEN ENG STABILIZED, ON DESCENT AND APPROACH MULTIPLE REPEAT EPISODE OF FLUX EXPERIENCED FDR EVENTS NOTED. EMERGENCY DECLARED, LANDED WITHONov 28, 2009 · N458AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA200940757Pressure Switch · malfunctioned2 INDICATION OF RT ENGINE LOW OIL PRESSURE WARNING. ENG OIL INDICATION NORMAL. PERFORMED HIGH POWER ENGINE RUN A T/O PWR FOR APPROX 10 MINUTES. OPERATION NORMAL. OIL PRESSURE INDICATION GOOD. INSPECTED LOP SWITCH CONNECTOR AND HARNESS. R & R LOP SWITCH INov 17, 2009 · N415AW · Cndair CL6002B19 · Engine Oil Indicating SystemSDR A6WA200940771Access Panel · crackedLT ENG LOWER ACCESS COWL PANEL 432 AC VENT COVER CRACKED LT ENG LOWER ACCESS COWL PANEL 432 AC VENT COVER REPLACED IAW SRM 51-42-13.Nov 11, 2009 · N426AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR VNAA2009111300001Carbon Seal · leakingCREW REPORTED A LEFT ENGINE OIL PRESSURE FLUCTUATION OF 20 TO 30 PSI AFTER TAKEOFF. CREW FOLLOWED QRH AND RETURNED TO DCA. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT USING AIRCRAFT MAINTENANCE MANUAL, CONFIRMED OIL LEAKING FROM LT ENGINov 5, 2009 · N250PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200940772Seal · crackedON RT COWL TORQUE BOX 2 FWD SEALS (BOTTOM AND OTBD BOTTOM) FOUND CRACKED ON RT COWL TORQUE BOX 2 FWD SEALS REPLACED IAW SRM 51-42-12.Nov 5, 2009 · N426AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR CA091103004Actuator · unserviceable(CAN) THE ACFT WAS PUSHED BACK FROM THE GATE FOR DEPARTURE. WHEN THE NOSE WHEEL STEERING WAS SELECTED ON THE NOSE WHEEL STEERING INOP MESSAGE ILLUMINATED. A RESET WAS CARRIED OUT BY THE FLIGHT CREW AND THE MESSAGE CLEARED. AS THE ACFT TAXIIED TOWARDS THE DEPARNov 3, 2009 · Cndair CL6002B19 · Landing Gear Steering SystemSDR CA091107001Windshield · cracked(CAN) DIVERSION DUE TO LT WINDSHIELD CRACKED IN FL150 FLIGHT LH 391 SCHEDULED, DIVERTED BECAUSE OF A CM 1 FRONT WINDSHIELD CRACKED IN FL 150. NO EXTERNAL IMPACT. CM 1 WINDSHIELD REMOVED IAW AMM TASK 56-11-01-000-801 REV.41 CM 1 WINDSHIELD INSTALLED IAW AMM Nov 2, 2009 · Cndair CL6002B19 · Flight Compartment WindowsSDR CHQA200900230Flap · malfunctionedON APPROACH TO IAH THE CREW REPORTED A FLAP FAIL AT ZERO DEGREES BEFORE THE FLAPS EXTENDED. THE APPROACH WAS ABORTED AND THE AIRCRAFT ATTEMPTED ANOTHER LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FAULT USING AD2009-06-12. NO FAULT CODES WERE FOUNDOct 26, 2009 · N648BR · Cndair CL6002B19 · Trailing Edge Flap Control System
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