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 ASOA06012Bulkhead · crackedDURING A C-CHECK, THE FS 280 BULKHEAD, OB OF LBL 9 AND RBL 9, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 BULKHEAD, OB OF LBL9 AND RBL 9, IAW EO 600-53-O123. (K)Jan 5, 2006 · N844AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA06011Floor Support · corrodedDURING A C-CHECK, THE FLOOR SUPPORT STRINGER, AT THE PASSENGER DOOR, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED THE FLOOR SUPPORT STRINGER IAW SRM 51-42-00, AND REPLACED THE FLOOR SUPPORT STRINGER IAW SRM 51-41-13 AND 51-42-06. (K)Jan 5, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06004Lamp · burned outDURING A GROUND INSPECTION, THE LT SIDE EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LT SIDE EXTERIOR EMERGENCY LIGHT. OPERSTIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jan 5, 2006 · N826AS · Cndair CL6002B19 · Emergency LightingSDR ASOA06003Lamp · burned outDURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHT, NEAR THE SERVICE DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT, NEAR THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jan 5, 2006 · N974EV · Cndair CL6002B19 · Emergency LightingSDR COMA0560795Engine · failedFLIGHT 5788 - FOUND RT ENGINE OIL PRESSURE WARNING. REPLACED THE RT ENGINE.Jan 4, 2006 · N498CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA200640002Floor Support · crackedFLOOR SUPPORT OB ANGLE PN 601R3471-9 CRACKED IN RADIUS MAINTENANCE REPAIRED IAW REO. (K)Jan 4, 2006 · N434AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06010Bulkhead · crackedDURING A C-CHECK, THE FORWARD PRESSURE BULKHEAD, AT FS 202.75, AROUND THE BRAKE CABLE, WAS FOUND TO BE CRACKED BEYOND LIMITS. THE MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)Jan 4, 2006 · N844AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA06009Doubler · crackedDURING A C-CHECK, THE FORWARD RT SIDE 718 DOUBLER, UNDER THE RADIUS BLOCK, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FORWARD RT SIDE 718 DOUBLER, UNDER THE RADIUS BLOCK, IAW EO 600-53-0066. (K)Jan 4, 2006 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06008Clip · crackedDURING A C-CHECK, THE AEB PRESSURE BULKHEAD LT AND RT SIDE CLIPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AEB PRESSURE BULKHEAD LT AND RT SIDE CLIPS IAW SRM. (K)Jan 4, 2006 · N844AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA06010SBulkhead · crackedDURING C-CHECK, THE FORWARD PRESSURE BULKHEAD, AT FS 202.75, AROUND THE BRAKE CABLE, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FORWARD PRESSURE BULKHEAD, AT FS 202.75, AROUND THE BRAKE CABLE, IAW REO. (K)Jan 4, 2006 · N844AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA200616454Pump · leakingCREW REPORTS IN FLT SHUT DOWN OF NR 1 ENG DUE TO LOW OIL PRESS MASTER WARNING MSG. INSPECTED LT ENG AND FOUND OIL LEAKING FROM SPLINE PLUG FOR NR 1 EDP DEACTIVATION. VERIFIED LPT AND HPT ROTATE FREE. INTERROGATED MDC ENG EXCEEDENCE AND FOUND LT ENG LOP/SEC Jan 4, 2006 · N906SW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA060108001Windshield · crackedRIGHT WINDSHIELD CRACKED DURING CLIMB. DIVERTED FLIGHT BACK TO DEPARTURE AIRPORT.Jan 4, 2006 · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA200616061Lamp · burned out2 OVERHEAD CABIN EMERGENCY LIGHTS INOP. RELAMPED AFT MOST AND 2ND FROM FWD CEILING EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD.Jan 3, 2006 · N432SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200616064Trim Switch · malfunctionedCAPTAIN TRIM SWITCH STICKS. REPLACED CAPTAIN TRIM SWITCH. OPERATIONAL CHECK GOOD IAW MM 27-41-00.Jan 3, 2006 · N923SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR CA060108002Windshield · crackedDURING APPROACH, THE LEFT WINDSHIELD CRACKED.Jan 3, 2006 · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200616062Door · bindingMAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE/LOCK FROM OUTSIDE/INSIDE. REPLACED INTERNAL CENTER BELLCRANK AND ALL ASSOCIATED HARDWARE IAW MM 52-11-02. OPERATIONAL CHECK OK.Jan 2, 2006 · N417SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200616066Window · crackedDURING DESCENT INTO SLC THRU 12,000 FT, APPROX NOTICED CAPTAIN'S SIDE WINDOW WAS CRACKED. REPLACED LT SIDE WINDOW IAW MM 56-12-01, PN OFF NP-139322-5; SN OFF 02131R5990.Jan 2, 2006 · N435SW · Cndair CL6002B19 · Flight Compartment WindowsSDR ASOA06002Engine · malfunctionedDURING CLIMB, CREW RECEIVED A LT ENGINE LOW OIL PRESSURE WARNING TRIPLE CHIME, AND AN EICAS MESSAGE THAT WENT OUT IMMEDIATELY AFTER IT ILLUMINATED. THE LEFT ENGINE OIL PRESSURE INDICATION FLUCTUATED BETWEEN 20 TO 45 PSI. THE QRH WAS COMPLIED WITH AND THE LEFJan 2, 2006 · N853AS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA200640001Bracket · bentGEARS UP DISAGREE CAS, AFTER TAKEOFF. MLG`S INDICATED UP AND LOCKED. NLG REMAINED DOWN. FOUND PROXIMITY SENSOR BRACKET BENT REMOVED AND REPLACED PROXIMITY SENSOR BRACKET IAW MM. REINSTALLED SENSOR TO WITHIN LIMITS IAW MM. PERFORMED GEAR SWING IAW MM. GEARJan 2, 2006 · N454AW · Cndair CL6002B19 · Main Landing GearSDR VNAA0601003Carbon Seal · leakingAFTER LANDING, THE CREW REPORTED THAT THE NR 1 ENGINE OIL PRESSURE DROPPED ON FINAL APPROACH TO 17 PSI WITH N1 AT 67 PERCENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE AGB/IDG CARBON SEAL. OIL LEAK AND CONSUMPTION CHECKS WERE GOOD. THE AIRCRAFT WAS RJan 2, 2006 · N244PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR SWIA200616059Control Unit · malfunctionedFLT SPLRS FAULT MESSAGE RECEIVED. REPLACED RT OB FLIGHT SPOILER PCU IAW MM 27-61-01. OPERATIONAL CHECK GOOD.Jan 1, 2006 · N955SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200616069Actuator · malfunctionedSPOILERON FAULT ON TAXI OUT. REPLACED THE PCU-FLIGHT IB SPOILERON ACTUATOR IAW AMM 27-62-01. OPERATIONAL CHECK GOOD.Jan 1, 2006 · N957SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200616071Control Unit · malfunctionedSPOILERON FAULT MSG INFLIGHT. REPLACED NR 1 SECU IAW CRJ 200 MM 27-61-05 AND REPLACED RT OB FLIGHT SPOILER IAW CRJ 200 MM 27-62-00. OPERATIONAL CHECK GOOD, PN 49-164-06 OFF 01840, PN 27000-7 SN MAL 6742.Jan 1, 2006 · N951SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200616073Control Unit · malfunctionedINFLIGHT, STAB CH1 INOP, STATUS MSG. REPLACED HSTCU IAW MM 27-41-01. OPERATIONAL CHECK GOOD.Jan 1, 2006 · N466SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR VNAA0601001Skin · ground damageDURING SERVICING A LAV TRUCK STRUCK THE RIGHT SIDE OF THE FUSELAGE, CAUSING A 1 X 1 PUNCTURE IN THE SKIN, APPROXIMATELY 16 AFT OF THE LAVATORY POTABLE WATER DOOR. MAINTENANCE REPAIRED THE FUSELAGE SKIN IAW BSC EO 601R-53-8002. PRESSURE LEAK CHECK OF THE REPAJan 1, 2006 · N262PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA200516063Support Beam · damagedDAMAGE FOUND ON LT LOWER OB ENGINE SUPPORT BEAM WEB (601-35006-147/SB) UNDER FWD IB PANEL NUT PLATE FWD OF FS640.00 AFT OF FS 625.30 AND OB OF LBL36.20, IB OF WL111.09 APPROX 3 INCH LONG, ITEM FOUND AT ROUTINE INSPECTION. C/W REPAIR OF LT LOWER OB ENGINE SUPPDec 31, 2005 · N446SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA200516065Apu · odorAFTER STARTING THE APU ON TAXI IN CABIN FILLED WITH STRONG SMELL OF FUEL. REPLACED APU ASSY IAW 49-20-01. OPERATIONAL CHECK GOOD.Dec 31, 2005 · N963SW · Cndair CL6002B19 · APU Core EngineSDR ASOA051162Warning Light · false activationDURING DESCENT FROM ATL-CAK, AT APPROXIMATELY 20,000 FEET, THE FIRE WARNING SYSTEM FOR THE RIGHT ENGINE SOUNDED. THE CREW SHUTDOWN THE RIGHT ENGINE AND FIRED BOTH FIRE BOTTLES. AN EMERGENCY WAS DECLARED, WITH ALL EMERGENCY VEHICLES DISPATCHED. THE AIRCRAFT Dec 31, 2005 · N900EV · Cndair CL6002B19 · Fire DetectionSDR SWIA200516068Pcu · malfunctionedFLIGHT SPOILERS FAULT STATUS MESSAGE DISPLAYED. REPLACED RT NR 2 PCU ON RT FLIGHT SPOILER IAW 27-62-01. OPERATIONAL CHECK GOOD.Dec 30, 2005 · N459SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200516072Pcu · malfunctionedFOUND SPOILERONS FAULT STATUS MSG. REPLACED RT SPOILERON IB PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD.Dec 30, 2005 · N924SW · Cndair CL6002B19 · Drag Control SystemSDR A6WA200540378Cover · crackedPASSENGER DOOR UPPER FORWARD CORNER CAP IS CRACKED. MAINTENANCE REPAIRED PASSENGER DOOR UPPER FWD CORNER CAP IAW REPAIR BY INSTALLING NEW COVER PN 6003190278. (K)Dec 30, 2005 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200540373Skin · corrodedLT WING LOWER PLANK HOLE NR4, WS 54.681 HAS CORROSION AT OB SIDE 5 INCH L X .002 INCH D AND AT IB SIDE 5 INCH L X .002 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 4 AT WS 54.681 IAW REO. (K)Dec 30, 2005 · N432AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540372Skin · corrodedLT LOWER WING PLANK HOLE NR 1, WS 54.897 HAS CORROSION AT IB SIDE FORWARD EDGE 2 INCH L .005 INCH D AND AT OB SIDE AFT 4 INCH L X .005 INCH D. NOT IN CRITICAL AREA. MAINT REPAIRED LT LOWER WING PLANK ACCESS HOLE NR 1 IAW REO. (K)Dec 30, 2005 · N432AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540371Skin · corrodedLT LWR WING PLANK HOLE NR 2, WS 12.245 HAS CORROSION AT OB SIDE AFT 2 INCH L X .005 INCH D AND AT IB SIDE 8 INCHES L X .005 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 2 IAW REO. (K)Dec 30, 2005 · N432AW · Cndair CL6002B19 · Wing, Plate/SkinSDR CA060103003Contact · burned"UPON POWER UP, GOT AC UTIL 1 OFF + MAIN BATT CHGR MESSAGES". MAINTENANCE DISCOVERED HEAT DAMAGE TO CONTACTOR 1K4XD. CONTACTOR REPLACED.Dec 30, 2005 · Cndair CL6002B19 · Electrical Power System WiringSDR A6WA200640005Handle · out of positionCREW ESCAPE HATCH OUTER HANDLE STICKS IN THE CLOSED POSITION. CLEANED AND LUBRICATED OUTER HANDLE MECHANISM IAW AMM. (K)Dec 29, 2005 · N432AW · Cndair CL6002B19 · Emergency ExitsSDR SWIA200516070Battery · dischargedFOUND EMERGENCY FLOOR LIGHTING (2 SECTIONS) INOP. REPLACED NR 3 ELBP IAW CRJMM 33-51-04. OPERATIONAL CHECK GOOD.Dec 28, 2005 · N954SW · Cndair CL6002B19 · Emergency LightingSDR VNAA0512024Flap System · malfunctionedDURING APPROACH WITH FLAPS AT 20 DEGREES THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW ABORTED THE APPROACH AND DECLARED AN EMERGENCY. THE APPROACH WAS RE-ESTABLISHED AND THE AIRCRAFT LANDED FLAPS 20 DEGREES WITH NO FURTHER INCIDENT. MAINTENANCE RESEDec 28, 2005 · N209PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200540379Rib · crackedRT BAH RIB ASSY WS 53.60, FS 523.8 CRACKED 1 INCH IN RADIUS. MAINTENANCE REPAIRED RT BAH RIB ASSY IAW REO. (K)Dec 28, 2005 · N432AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200540377Angle · crackedLT FS 625 OBLIQUE ANGLE IS CRACKED. MAINTENANCE REMOVED AND REPLACED OBLIQUE ANGLE LT SIDE PH 601R-35012-51 IAW CRJ 200 SRM 51-42-06. (K)Dec 28, 2005 · N432AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540361Acm · seizedON APPROACH GOT OIL TYPE SMELL FROM LT PACK, AND LT PACK OVERHEATED IN AUTO MODE. WHILE ON GROUND WAS UNABLE TO CONTROL LT PACK IN MANUAL MODE. INSPECTED LT PACK AND FOUND ACM SEIZED AND TO BE THE SOURCE OF THE OIL SMELL. REMOVED AND REPLACED AIR CYCLE MACHINDec 27, 2005 · N403AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200540362Dcu · malfunctionedAFTER DEPARTURE, UPON FLAP RETRACTION, FLAP FAIL CAUTION MESSAGE APPEARED ON ED1 FLAP POSITION INDICATION ON ED1 READS ZERO DEGREES, FLIGHT CONTROL PAGE ALSO READS ZERO ON ED2. RETURN TO DEPARTURE FOR (FLAP ZERO LANDING). FOUND GROUND PROXIMITY MESSAGE ON MDDec 27, 2005 · N419AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA051228003Pitot Head · bentBIRD STRIKE DURING FLIGHT. MAINTENANCE INSPECTION AFTER LANDING FOUND 2 SMALL DENTS ON THE RT WING LEADING EDGE AT WS89.34 AND RT PITOT HEAD DAMAGED/BENT. LEADING EDGE DENTS ALLOWABLE FOR CONTINUED SERVICE, RT PITOT HEAD REPLACED. AIRCRAFT RETURNED TO SERVIDec 27, 2005 · Cndair CL6002B19 · Pitot/Static SystemSDR A6WA200540359Coalescer Bag · inoperativeEXHAUST FUMES IN COCKPIT AND CABIN. WORSE WITH APU ON. INSPECTED APU, FOUND NO LEAKS. REPLACED AC PACKS COALESCER BAGS. OBSERVED CREW RUN UP ENGINES. NO FURTHER FUMES IN COCKPIT OR CABIN. IAW AMM. (K)Dec 26, 2005 · N446AW · Cndair CL6002B19 · Humidity Control SystemSDR A6WA200540360Windshield · crackedFO`S A WINDSHIELD CRACKED AT FLT LEVEL 350. REMOVED AND REPLACED WINDSHIELD IAW AMM, PRESSURE CHECK GOOD. WINDSHIELD HEAT CHECK GOOD. (K)Dec 26, 2005 · N457AW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200516060Switch · malfunctionedNR 1 STAB WOULD NOT ENGAGE. REPLACED BOTH PILOT YOKE STAB DISCONNECT SWITCHES. OPERATIONAL CHECK GOOD IAW MM 27-41-00.Dec 26, 2005 · N910SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200516067Light · inoperativeFOUND MAIN CABIN DOOR, FWD BULKHEAD, EMERGENCY EXIT SIGN (INOP). REPLACED EMERGENCY LIGHT ASSY. OPERATIONAL CHECK GOOD.Dec 26, 2005 · N442SW · Cndair CL6002B19 · Emergency LightingSDR VNAA0512022Flap System · malfunctionedTHE FLAPS FAIL MESSAGE ILLUMINATED ON APPROACH WITH FLAPS AT 20 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET AND TESTED THE FLAP SYSTEM IAW RJ-SL-27-084. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVIDec 26, 2005 · N209PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200540358Flap System · failedFLAPS FAIL AT 8 DEGREES UPON FLAP RETRACTION. COMPLIED WITH SUPPLEMENT 98-18, FLAPS RESET, NO HISTORY IN PAST 72 HOURS. (K)Dec 24, 2005 · N458AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0512017Structure · bird strikeDURING CLIMBOUT FROM BDL THE CREW REPORTED A POSSIBLE BIRD STRIKE. THE FLIGHT CONTINUED TO PIT AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED IMPACT DAMAGE ON THE RT WING INBOARD LEADING EDGE. MAINTENANCE REMOVED AND REPLACED THE RT WING INBOARD LEADING EDec 23, 2005 · N262PS · Cndair CL6002B19 · Wing Main, Frame Structure
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