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 VNAA0405003Warning Light · false activationDURING TAKEOFF, THE CREW RECEIVED AN ADC NR 1 FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE NR 2 AIR REFERENCE PANEL IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 34-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AMay 2, 2004 · N247JS · Cndair CL6002B19 · Central WarningSDR VNAA0405002Warning Light · illuminatedDURING FLIGHT, THE EMERGENCY DOOR MASTER CAUTION CAME ON AT 24,000 FEET, PRESSURE REMAINED GOOD. MAINTENANCE CONTROL DEFERRED WITH CREW, 52-70-03-C.May 1, 2004 · N250PS · Cndair CL6002B19 · Door Warning SystemSDR MASA200400237Fuel Control · inoperativeCREW REPORTED RT ENGINE FAILED IN FLIGHT. THE ENGINE SHUTDOWN UNCOMMANDED INFLT. MX CHANGED THE RT FCU. OPS CHECK GOODApr 30, 2004 · N17337 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA040429002Cable · damaged(CAN) BROKEN STRANDS ON MAIN ENTRANCE DOOR ASSIST CABLE AT THE POINT WHERE THE CABLE STARTS TO OVERLAP ITSELF ON THE DOOR ACTUATOR SERVO DRUM FOR THR FIRST TIME. CABLE REPLACED. IPC REFERENCE : CRJIPC MANUAL CHAPTER 52-11-08, FIGURE 1A , ITEM 45. NOTE: THE Apr 29, 2004 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA040428002Fairing · lightning strike(CAN) LIGHTNING STIKE ON APPROACH INTO AIRPORT. LIGHTNING ENTERED LT SIDE OF WEATHER RADAR. NO OBVIOUS EFFECT TO AIRCRAFT SYSTEMApr 27, 2004 · Cndair CL6002D24 · Wing, Control SurfacesSDR CA040427003Priority Valve · failed(CAN) AFTER TAKE OFF CREW SELECTED GEAR UP AND RECEIVED A (GEAR UP DISAGREE) MESSAGE WITH AMBER CAUTION MESSAGE ON THE RT MAIN GEAR INDICATOR. AFTER LANDING THE CREW RECEIVED HYD PUMP 3B (HIGH TEMP) MESSAGE . A/C WAS RETURNED TO DEPARTURE AIRPORT. MAINTENANCApr 24, 2004 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR 04115622Sensor · intermittentDURING DESCENT OF FLIGHT 7688 CREW REPORTED A LEFT HAND ENGINE FAILURE ON APPROACH. AN EMERGENCY WAS DECLARED AND FLIGHT LANDED UNEVENTFULLY. THE LOW LEVEL OIL SENSOR WAS FOUND TO GIVE FALSE INDICATIONS AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WASApr 23, 2004 · N622BR · Cndair CL6002B19 · Engine Oil QuantitySDR CA040425001Frame · cracked(CAN) DURING COMPLETION OF AD CF-2003-12/A DVI OF AFT FUSELAGE AND REINFORCING ANGLE AT FS640 ON BOTH LT AND RT SIDES BETWEEN STRINGERS 9 AND 12 IAW PART A OF MFG SB601-53-061, RT SIDE REINFORCEMENTS PLATE WAS FOUND CRACKED APPROX .8750 INCH LONG AND CORRESPOApr 23, 2004 · Cndair CL6002B19 · Fuselage Main, FrameSDR CA040507002Servo · failedDURING CRUISE FLIGHT, AP TRIM IS RWD POSTED ON AND OFF EVERY FEW SECONDS. AUTO-PILOT DISCONNECTED. NOTICED THAT AILERON IS EXTREMELY HARD TO MOVE ALMOST BLOCKED. IN DESCENT WITHOUT AUTO-PILOT, WE NOTICED THAT THE ELEVATOR ALSO COULD NOT BE MOVED (FL310-300 /Apr 23, 2004 · Cndair CL6002B19 · Autopilot Main ServoSDR SWIA200413231Warning Light · illuminatedDURING TAKEOFF ATTEMPT RECEIVED CONFIG SPOILER MESSAGE, THEN INBOARD AND FLIGHT SPOILER FAULT MESSAGE. COMPLIED WITH SPOILERON SYSTEM RESET PROCEDURE AS PER AMM 27-61-05. OPERATIONAL CHECK GOOD.Apr 22, 2004 · N446SW · Cndair CL6002B19 · Drag Control SystemSDR CA040423011Rivet · burned(CAN) UPON DESCENT AIRCRAFT WAS STRUCK BY LIGHTNING ON LT SIDE OF NOSE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE COMPLETED LIGHTNING STRIKE INSPECTION IAW AMM 05-51-05. INSPECTION OF AIRCRAFT STRUCTURE FOUND 25 RIVETS BURNED ALONG THE LENGTH OF THE LTApr 21, 2004 · Cndair CL6002B19 · FastenersSDR ASOA04287Oil System · lowDURING CLIMB-OUT FROM DFW-MEM, PASSING THROUGH 21,000 FT THE CREW RECEIVED AN ENGINE OIL PRESSURE WARNING MESSAGE FOR APPROXIMATELY TWO SECONDS ON THE RT ENGINE AND THEN IT EXTINGUISHED. THE OIL PRESSURE WAS MONITORED WHICH FLUCTUATED RAPIDLY BETWEEN 25 TO 45Apr 20, 2004 · N851AS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR SWIA200413360Sill · corrodedU-CHANNELS ON FUSELAGE, PAX DOOR SILL CORRODED (UNDER PANEL 231CLF). DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CHANNEL P/N 601R31527-217 AT FOWARD AND AFT LOCATIONS IAW CRJ SRM 51-42-06 AND 51-42-11.Apr 18, 2004 · N408SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413200Frame · crackedFS 364 STR 8R IS CRACKED FROM FASTENER HOLES ON UPPER AND LOWER FRAME TO SKIN FLANGE. (DISCOVERED DURING C-CHECK INSPECTION) FABRICATED, FIT, DRILLED AND INSTALLED ALL THE REPAIR PARTS IAW CRJ REO 601R-53-21-501 REV. NC.Apr 16, 2004 · N405SW · Cndair CL6002B19 · Fuselage Main, FrameSDR CA040427002Blade · damaged(CAN) DURING BOROSCOPE INSPECTION, DAMAGE FOUND ON COMPRESSOR BLADES . MAUFACTURER WAS ADVISED AND GE ADVISED ENGINE REPLACEMENT. ENGINE REPLACED IAW MM PROCEDURE.Apr 16, 2004 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA040420007O-Ring · leaking(CAN) DURING ROUTINE WALK AROUND , MAINTENANCE DISCOVERED FUEL LEAK AROUND RT WING DRYBAY DRAIN. DRY BAY PANELS WERE REMOVED AND DRY BAY FOUND TO HAVE SMALL AMOUNT OF FUEL PRESENT. THE COUPLING THAT ATTACHES THE AIR SCOOP TO THE FUEL TANK VENTLINES ON THE RTApr 15, 2004 · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR MASA200400201Engine · malfunctionedCREW REPORTED NR 2 ENGINE ITT 84 DEG HIGHER THAN THE NR 1 ENGINE. MX PERFORMED AN ENG COMP WASH AND PWR ASSURANCE CHECKS. MX BORESCOPED NR 2 ENGINE AND REJECTED IT. MX REPLACED NR 2 ENGINE. OP CHECKS GOOD.Apr 14, 2004 · N17231 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA200413172Floorbeam · crackedLEFT ELECTRICAL BAY FLOOR AT FS 193, LBL 30 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CRACK IAW CRJ REO 601R-53-11-081 NC.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200413173Floorbeam · crackedRIGHT ELECTRICAL BAY FLOOR AT FS 193, RBL 30 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CRACK IAW CRJ REO 601R-53-11-245 NC.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200413174Stringer Clip · crackedNOSE HYDRAULIC COMPARTMENT AT FS 202.75 STR 21 CLIP IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CLIP (CLEAT) IAW CRJ SRM 53-11-19 FIG 1, SHEET 1.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200413175Receptacle · crackedSEVERAL CRACKS FOUND RADIATING FROM 115 VAC RECEPTACLE CUTOUT. DISCOVERED DURING C-CHECK INSPECTION. REPLACED SUPPORT IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413176Beam · crackedMAIN FUSELAGE; LOWER TRANSVERSE BEAM CRACKED AT FS 280.00 LBL 11.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-171 REV NC AND RII 53-401.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA200413177Beam · crackedMAIN FUSELAGE; UPPER TRANSVERSE BEAM CRACKED AT FS 280.00 LBL 11.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-138 REV NC AND RII53-401.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA200413178Structure · crackedMAIN FUSELAGE FITTING CRACKED AT FS 460.00 LB19 OUTBOARD SIDE. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11 AND CONTINUATION SHEETS REF RII 53-401.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413179Intercostal · crackedMAIN FUSELAGE PULLEY INTERCOSTAL CRACKED AT 2 LOCATIONS FS 484.00 LBL 27.0 AND LBL 36.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-059 REV A REF RII 53-401.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413180Fitting · crackedMAIN FUSELAGE FITTING CRACKED AT FS 460.00 RBL 9.0 OUTBOARD SIDE. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11 AND RII 53 401.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200413181Intercostal · crackedMAIN FUSELAGE PULLEY INTERCOSTAL CRACKED AT 2 LOCATIONS FS 484.00 RBL 27.0 AND RBL 36.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-059 REV A.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413182Vertical Beam · crackedFUSELAGE LEFT VERTICAL BEAM LWR OUTBOARD FLANGE CRACKED AT FS 559 LBL 9. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED BEAM IAW CRJ REO 601R-53-41-057 REV NC AND IAW RII53-401.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA040417001Fairing · lightning strike(CAN) FLYING THRU SHOWERS AT 10000 FT , ON ARRIVAL, LARGE FLASH WAS OBSERVED. NO AIRCRAFT SYSTEM AFFECTED. AFTER LANDING, 2 BLACK MARKS WERE FOUND ON THE LOWER RT HORIZONTAL STABILIZER. REPAIR EO 670-55-12-153 ALONG WITH NON DESTRUCTIVE TEST (NDT) CARRIED OApr 13, 2004 · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR SWIA200413133Wire · brokenDURING STALL TEST -STALL FAIL- CAUTION MESSAGE APPEARED. REPAIRED BROKEN WIRE ON STICK SHAKER ON FIRST OFFICER'S YOKE AS REQUIRED. OPS CHECKED GOOD IAW MM 27-35-00.Apr 8, 2004 · N915SW · Cndair CL6002B19 · Stall Warning SystemSDR SWIA200413340Bracket · corrodedPAX DOOR SILL BRACKETS AND CLEATS AT FS 316 AND FS 343 CORRODED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SILL BRACKETS IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13.Apr 8, 2004 · N405SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200413341Angle · corrodedSERVICE DOOR; FRAME TO SILL ANGLE IS CORRODED AT FS 349.00. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED CORRODED ANGLE IAW CRJ SRM 51-42-21, 51-40-11, 51-23-00, 51-42-21, 20-21-00.Apr 8, 2004 · N405SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200413342Fitting · crackedMAIN FUSELAGE; PRESSURE FLOOR/WING TIE BEAM FITTING IS DENTED AND CRACKED ALONG LOWER FLANGE; LBL 3.0 FS 460.00. DISCOVERED DURING C-CHECK INSPECTION. NEW TIE BEAM FIT, DRILLED AND INSTALLED IAW CRJ SRM 51-40-11.Apr 8, 2004 · N405SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA200413343Floorbeam · cutMAIN FUSELAGE; FLOORBEAM CUT ALONG BOTTOM FLANGES, FS 467.0; LBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO-53-41-211.Apr 8, 2004 · N405SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR 04098670Switch · inoperativeDURING CLIMB OF FLIGHT 7351 CREW REPORTED A RIGHT HAND THRUST REVERSER UNLOCK MESSAGE AND RETURNED TO DEPARTURE FIELD. FLIGHT LANDED UNEVENTFULLY. THE RIGHT HAND THRUST REVERSER STOW SWITCH WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECKApr 7, 2004 · N670BR · Cndair CL6002B19 · Engine Thrust ReverserSDR SWIA200413122Computer · faultyAT 28,000 FT MACH TRIM STAB TRIM CAUTIONS ON EICAS. UNABLE TO RESET. REMOVED AND REPLACED FCC CARD NR 2 WITH A SERVICEABLE UNIT IAW 22-10-00. OPS CHECKS GOOD. ALSO REMOVED AND REPLACED HSTCU WITH A SERVICEABLE UNIT ALONG WITH STAB TRIM/MACH TRIM ENGAGEMENTApr 4, 2004 · N924SW · Cndair CL6002B19 · Autopilot ComputerSDR CA040402001Bracket · fractured(CAN) AIRSTAIR DOOR FREE FELL TO THE GROUND DUE TO THE FAILURE OF BOTH FWD/AFT (BOTH) SWIEL BRACKETS THAT HOLD THE CABLES TO THE FUSELAGE. IN THIS CASE THE DOOR WAS OPENED FROM INSIDE THE A/C AND NO HARM OR DAMAGE WAS DONE TO PERSONNEL OR EQUIPMENT , BUT THEREApr 2, 2004 · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200413079Window · failedDESCEND THROUGH FL180 FIRST OFFICER'S WINDOW CRACKED, THEN CRACKED AGAIN THROUGH 13,000 FT. REPLACED FIRST OFFICER'S RIGHT WINDOW. OPS CHECK GOOD IAW RII 56-402 AND CRJ MM 56-00-00. P/N OFF NP134322-001.Mar 24, 2004 · N958SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200413088Striker · crackedPASSENGER DOOR SEAL STRIKER CRACKED AT FORWARD AND AFT PIN RECEPTACLES. DISCOVERED DURING B003 INSPECTION. REPAIRED IAW REO 601R-52-11-008.Mar 24, 2004 · N427SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR MASA200400162Scavenge Pump · cloggedA/C RETURNED TO FIELD REPORTING THAT THE CAPT PERFORMED AN IN-FLIGHT SHUT DOWN DUE TO LOW OIL PRESSURE. MX REPLACED THE LUBE SCAVENGE PUMP. OP CHECKS GOOD ON TEST FLIGHT.Mar 24, 2004 · N77286 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA040326003Gearbox · binding(CAN) PILOT REPORTED THROTTLE ACTION STIFF. MAINTENANCE TROUBLESHOT PROBLEM TO NR 1 ENGINE THROTTLE CONTROL GEARBOX BINDING. NR 1 THROTTLE CONTROL GEARBOX REPLACED. IT IS NOTED THAT AD CF-2004-01, HAS BEEN ISSUED AGAINST GEARBOX P/N 2100140-007, ALTHOUGH IN Mar 22, 2004 · Cndair CL6002B19 · Power LeverSDR SWIA200413071Flap · out of rigON CLIMBOUT, FLAPS FAIL AT 8 DEGREES. RETURN TO SLC. RE-RIGGED FLAPS IAW 27-54-00. OPS CHECK GOOD.Mar 20, 2004 · N454SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA040318009Engine · failed(CAN) WHILE CARRYING OUT RELIGHT TESTS, RT ENGINE DID NOT RELIGHT VIA WINDMILL OR ATS.EMERGENCY WAS DECLARED AND SUCCESSFULL SINGLE ENGINE APPROACH WAS COMPLETED WITHOUT FURTHER INCIDENT. RT ENGINE WAS REPLACED AND AC FLOWN SINCE WITHOUT FURTHER INCIDENTS.Mar 17, 2004 · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR SWIA200413072Position Sensor · malfunctionedRECEIVED FLAPS FAIL, DID QRH. LANDED SLC 0 DEGREES FLAPS. REMOVED AND REPLACED LEFT BPSU IAW AMM 27-51-10 AND RIGGED FLAPS. OPS CHECKS GOOD.Mar 14, 2004 · N407SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR SWIA200413073Control Lever · malfunctionedON TAXI OUT RECEIVED INBOARD GROUND SPOILER FAULT STATUS MESSAGES. REMOVED AND REPLACED FLIGHT SPOILER CONTROL LEVER IAW MM 27-61-01. OPS CHECK GOOD. P/N: 365-209D, S/N OFF: F0621A.Mar 14, 2004 · N408SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200413074Actuator · malfunctionedAFTER LANDING IN BIL, STAB CH 1 INOP STATUS MESSAGE. REMOVED AND REPLACED HSTA AND MCU IAW CL 600 MM 27-42-01. OPS CHECKS GOOD. MCU P/N 7062-3, S/N OFF 943.Mar 14, 2004 · N912SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200413050Beam · crackedCRACK FOUND ON LOWER WEB OF ENGINE SUPPORT BEAM AT LEFT ACCESS PANEL CUTOUT, OUTBOARD OF LBL 36.2, BETWEEN FS 625.3 AND FS 640.0. CARRIED OUT ENGINE SUPPORT BEAM REPAIR ON LH SIDE IAW BRAD REO 601R-43-61-366 REV. E.Mar 9, 2004 · N412SW · Cndair CL6002B19 · Engine Mount SectionSDR SWIA200413051Beam · crackedCRACK FOUND ON LOWER WEB OF ENGINE SUPPORT BEAM AT RIGHT ACCESS PANEL CUTOUT, OUTBOARD OF RBL 36.2, BETWEEN FS 625.3 AND FS 640.0. CARRIED OUT ENGINE SUPPORT BEAM REPAIR RH SIDE IAW BRAD REO 601R-53-61-366 REV. EMar 9, 2004 · N412SW · Cndair CL6002B19 · Engine Mount SectionSDR SWIA200413052Intercostal · crackedDISCOVERED DURING C-CHECK INSPECTION, RIGHT FS 625 INTERCOSTAL ANGLE CRACKED. ANGLE REPLACED AT FS 625 RT STR 14 IAW CRJ SRM 51-40-11 AND 51-42-06.Mar 9, 2004 · N412SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413053Intercostal · crackedDISCOVERED DURING C-CHECK INSPECTION, LEFT FS 625 INTERCOSTAL CRACKED. REPLACED LEFT FS 625 INTERCOSTAL IAW CRJ SRM 51-40-11 AND 51-42-06.Mar 9, 2004 · N412SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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