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 VNAA0705005Unknown · unknownCREW REPORTED A NR 2 GENERATOR OFF MESSAGE ILLUMINATED DURING TAKEOFF. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED AN OPERATIONAL TEST OF THE NR 2 ENGINE GENERATOR IN ACCORDANCE WITH THE AIRCRAFT MAINTEMay 18, 2007 · N221PS · Cndair CL6002B19 · Central WarningSDR A6WA200740258Sensor · malfunctionedFLAPS FAIL MASTER CAUTION OCCURRED 15 MINUTS AFTER DEPARTURE. QRH WAS ACCOMPLISHED. FLAPS FAILED AT ZERO DEGREES. EMERGENCY LANDING DECLARED FOR PRECAUTIONARY MEASURES. INTERROGATED FECU, FOUND L-BPSU MISRIGGED, NO EVIDENCE OF TWISTING OR ABNORMAL DEFORMATMay 17, 2007 · N415AW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR VNAA0705004Unknown · unknownCREW REPORTED A CAS MISCOMP SPOILERON, RIGHT HAND SPOILER AND INBOARD GROUND SPOILER FAULT MESSAGE ON INITIAL TAKEOFF. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CYCLED THE SECU IN ACCORDANCE WITH THE SERVICE LEMay 15, 2007 · N259PS · Cndair CL6002B19 · Central WarningSDR A6WA200740254Skin · corrodedLT WING LOWER PLANK ACCESS HOLE NR 2 FOR PANEL 510AB HAS FRETTING/ CORROSION DAMAGE AT IB END, ALL ALONG FWD SIDE AND OB END, IN AND OUT OF CRITICAL AREA. S/D MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 2 PANEL 510AB IAW BOMBARDER REO 601R-57-21-May 15, 2007 · N458AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740255Skin · corrodedLT WING LOWER PLANK ACCESS HOLE NR 3 FOR PANEL 510BR HAS FRETTING/ CORROSION DAMAGE AT IB END 1 INCH LONG NOT IN CRITICAL AREA. S/D MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 3 PANEL 510BB IAW BOMBARDIER REO 601R-57-21-030 REV A. (K)May 15, 2007 · N458AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740256Skin · corrodedLT WING LOWER PLANK ACCESS HOLE NR 1 FOR PANEL 540BR HAS FRETTING/ CORROSION DAMAGE AREA ABOUT 2 INCHES LONG AT FWD/ OB QUADRANT, NO IN CRITICAL AREA. S/D MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 1 PANEL 540BB IAW BOMBARDIER REO 601R-57-21-030May 15, 2007 · N458AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740257Skin · corrodedLT WING LOWER PLANK ACCESS HOLE NR 9 FOR PANEL 550AB HAS FRETTING/ CORROSION DAMAGE 1 INCH AREAS AT IB END NOT IN CRITICAL AREA. (K) [07-17-07] MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 9 PANEL 550AB IAW BOMBARDIER REO 601R-57-21-030 REV A. (May 15, 2007 · N458AW · Cndair CL6002B19 · Wing, Plate/SkinSDR CA070521002Control Unit · malfunctioned(CAN) THERE WAS A STAB TRIM RUNAWAY EVENT THAT OCCURRED. AN EMERGENCY WAS DECLARED AND A RETURN TO BASE. FURTHER AC DAMAGE AFTER SUCCESSFUL LANDING. BASED ON THE ATTACHED CREW REPORT, IT WAS A STAB TRIM RUNAWAY NOSE DOWN EVENT. PLEASE NOTE THAT A DFDR DOWNLOAMay 14, 2007 · Cndair CL6002B19 · Stabilizer Control SystemSDR VNAA0705002Tire · failedCREW REPORTED AT AROUND 100 KTS ON TAKEOFF ROLL THAT THE RIGHT NOSE GEAR TIRE SHREDDED AND THE LEFT TIRE WENT FLAT. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED BOTH NOSE TIRES IN ACCORDANCE WITH THE AIRCRAMay 14, 2007 · N246PS · Cndair CL6002B19 · TireSDR A6WA200740247Floorbeam · crackedFS 280 FLOORBEAM CLIP AT OB SIDE OF RBL 9.0 IS CRACKED IN RADIUS APPROX .60 INCH LONG. (K) [07-17-07] MAINTENANCE REPLACED CLIP IAW BSC EO 601R-53-0057A. (M)May 14, 2007 · N458AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740248Floorbeam · crackedFS 280, FLOORBEAM CLIP AT IB SIDE OF RBL 9.0 IS CRACKED IN RADIUS APPROX .30 INCH LONG. S/D MAINTENANCE REPLACED CLIP IAW BSC EO 601R-57-0057A. (K)May 14, 2007 · N458AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740249Floorbeam · crackedFS280, FLOORBEAM CLIP AT IB SIDE OF LBL 9.0 IS CRACKED IN RADIUS APPROX. .20 INCH LONG. S/D - MAINTENANCE REPLACED CLIP IAW BSC EO 601R-53-0057A. (K)May 14, 2007 · N458AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740250Floorbeam · crackedFS 280 FLOORBEAM CLIP AT OB SIDE OF LBL 9.0 IS CRACKED IN RADIUS APPROX .20 INCH LONG. (K) [07-17-07] MAINTENANCE REPLACED CLIP IAW BSC EO 601R-53-0057A. (M)May 14, 2007 · N458AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740251Intercostal · crackedINTERCOSTAL AT FS 484.00 HAS CRACKED FLANGE AT RBL 27.0 CRACK MEASURES APPROX .20 INCH LONG. S/D MAINTENANCE REPLACED CLIP IAW BSC SR 601R-53-0029B. (K)May 14, 2007 · N458AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740252Intercostal · crackedINTERCOSTAL AT FS 484.00 HAS CRACKED FLANGE AT LBL 27.0 CRACK MEASURES APPROX .50 INCH LONG. S/D MAINTENANCE REPLACED CLIP IAW BSC SR 601R-53-0029B. (K)May 14, 2007 · N458AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740253Intercostal · crackedINTERCOSTAL AT FS 484.00 HAS CRACKED FLANGE AT LBL 36.0 CRACK MEASURES APPROX .20 INCH LONG. S/D MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-53-41-059. (K)May 14, 2007 · N458AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740243Structure · crackedRT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER PLUMBING (Z) MEMBER ASSY PN 601R75262-153, IS CRACKED THRU ON OB LEG. (K) [07-17-07] MAINTENANCE REPLACED ZEE MEMBER IAW CRJ SRM 51-42-06. (M)May 13, 2007 · N458AW · Cndair CL6002B19 · Main Landing GearSDR A6WA200740244Channel · crackedRT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER HAT CHANNEL PN 601R75262157, IS CRACKED THRU ON IB LEGS. (K) [07-17-07] MAINTENANCE REPLACED CHANNEL IAW SRM 51-42-06. (M)May 13, 2007 · N458AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740245Channel · crackedLT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER HAT CHANNEL, PN 601R75262159, IS CRACKED AT OB LEGS LONGEST CRACK IS APPROX. .25 INCH LONG. (K) [07-17-07] MAINTENANCE REPLACED CHANNEL IAW CRJ SRM 51-42-06. (M)May 13, 2007 · N458AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740246Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE IS CRACKED. (K) [07-17-07] MAINTENANCE REMOVED DAMAGED SECTION OF DRAG ANGLE AND INSTALLED REPAIR PARTS IAW REO 601R-52-11-513 REV A. (M)May 13, 2007 · N458AW · Cndair CL6002B19 · Fuselage Main, StructureSDR VNAA0705001Unknown · unknownCREW REPORTED THE PLANE SUDDENLY JUMPED ON TAKEOFF ROLL AT 20-30 KTS. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE PERFORMED AN INSPECTION OF THE MAIN LANDING GEAR AND FOUND NO DEFECTS. MAINTENANCE ALSO PERFORMED A TAXI CHECK May 10, 2007 · N254PS · Cndair CL6002B19 · Standard Practices/StructuresSDR A6WA200740238Angle · crackedFS484.0 ANGLE AT RBL 36 IS CRACKED APPROX 1.0 INCH. (K) [07-17-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW BOMBARDIER REO 601R-53-41-059 AND BSC SR 601R-53-0030A. (M)May 10, 2007 · N455AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740239Angle · crackedFS 484.0 ANGLE AT LBL36 IS CRACKED APPROX 1.0. CORRECTIVE ACTION IN PROGRESS. (K) [07-17-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW BOMBARDIER REO 601R-53-41-059. (M)May 10, 2007 · N455AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740240Angle · crackedFS 484.0 ANGLE AT RBL 27 IS CRACKED APPROX 1.0 INCH. (K) [07-17-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW BOMBARDIER SR 601R-53-0029B AND CRJ 200 SRM 51-42-06. (M)May 10, 2007 · N455AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740241Angle · crackedFS 484.0 ANGLE AT LBL 27 IS CRACKED APPROX 1.0 INCH. (K) [07-17-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW BOMBARDIER SRM 601R-53-0029B AND CRJ 200 SRM 51-42-06. (M)May 10, 2007 · N455AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740242Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED. (K) [07-17-07] MAINTENANCE REMOVED DAMAGED SECTION OF DRAG ANGLE AND INSTALLED SERVICEABLE SECTION IAW BOMBARDIER REO 601R-52-11-513. (M)May 10, 2007 · N455AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0760375Scavenge Pump · failedFLIGHT 5679 - EN ROUTE CVG-PVD RECEIVED A LOW LEFT ENGINE OIL PRESSURE WARNING, CREW DECLARED AN EMERGENCY, PERFORMED IFSD OF THE LEFT ENGINE AND DIVERTED TO PIT. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT ENGINE LUBRICATION/SCAVENGE PUMP.May 8, 2007 · N416CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA070509004Cowling · separated(CAN) ON DESCENT, THROUGH FL280, CREW FELT SLIGHT VIBRATION TO THE AIRCRAFT. FIRST OFFICER (FO) FELT A SLIGHT SHUDDER IN THE CABIN. ON ARRIVAL, IT WAS FOUND NR 1 LOWER ENGINE COWL HAD SEPARATED FROM THE AIRCRAFT. UPON MAINTENANCE INITIAL INSPECTION, IT WASMay 3, 2007 · Cndair CL6002B19 · Engine Cowling SystemSDR A6WA200740236Floorbeam · crackedRT FS 621..00 FLOOR SUPPORT ANGLE IS CRACKED 1.2500 INCH LONG IN OB RADIUS. (K) [07-17-07] MAINTENANCE CUT AWAY DAMAGED AREA AND INSTALLED SERVICEABLE REPAIR IAW BOMBARDIER REO 601R-53-61-117. (M)May 3, 2007 · N455AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WQA200740237Floorbeam · crackedLT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED 1.2500 INCH LONG IN OB RADIUS. (K)May 3, 2007 · N455AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR TRAX200700606Drain · leakingSTRONG FUEL SMELL IN FLT DECK ON DESCENT AND AT GATE LT ENG WAS LEAKING FUEL FROM DRAIN. FLT 4532 CX.May 2, 2007 · N870AS · Cndair CL6002B19 · Fuel Controlling SystemSDR CA070511011Handle · cracked(CAN) DURING ROUTINE MAIN CABIN DOOR INSPECTION FOUND MAIN CABIN PHASE IV DOOR HANDLE WITH (2) CRACKS. DOOR HANDLE REPLACED. AIRCRAFT RETURNED TO SERVICE (TC NR 20070511011)May 2, 2007 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA070507010Wheel · cracked(CAN) DURING ROUTINE NDT HFEC INSP ON RJ MAIN WHEEL, ACCORDING TO ABSC NDT MANUAL PART 1, 32-42-03, CRACKS WERE FOUND IN THE LOCKING RING GROOVE. THE CRACKS HAVE A DEPTH OF .040 INCH, .020 INCH AND .010.INCH. COMPONENT COULD BE SENT FOR MACHINING, BUT THE DEFMay 2, 2007 · Cndair CL6002B19 · Wheel/Ski/FloatSDR A6WA200740234Angle · crackedRT FS 621.00 TO 625.00 OBLIQUE ANGLE HAS A 1.2500 INCH LONG CRACK IN AFT RADIUS. (K) [07-17-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALL NEW ANGLE IAW CRJ200 SRM 51-42-06. (M)May 1, 2007 · N455AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740235Angle · crackedLT FS 621.00 AND 625.00 OBLIQUE ANGLE HAS A 1.5 INCH LONG CRACK IN AFT RADIUS. (K) [07-17-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE IAW CRJ200 SRM 51-42-06. (M)May 1, 2007 · N455AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740232Floorbeam · crackedLT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED .5 INCH LONG ON OB RADIUS. (K) [07-17-07] MAINTENANCE CUT AWAY DAMAGED ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R53-61-117 REV C. (M)Apr 30, 2007 · N452AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740233Floorbeam · crackedRT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED .5 INCH LONG IN OB RADIUS. (K) [07-17-07] MAINTENANCE REPAIRED IAW BOMBARDIER AEROSPACE REO 601R-53-61-117. (M)Apr 30, 2007 · N452AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR 554304292007Flap System · malfunctionedFLAPS FAILED AT 13 DEGREES ON APPROACH. CREW DECLARED AN EMERGENCY AND PERFORMED AN UNEVENTFULL LANDING. MX DISPATCHED WITH BREAKOUT BOX. AFTER RESET, FLAPS OPERATIONAL CHECKS PERFORMED ON COMPLETE AND ISOLATED SYSTEMS. COULD NOT DUPLICATE ERROR. NO MX HISTOApr 29, 2007 · N332FX · Cndair CL604 · Trailing Edge Flap Control SystemSDR A6WA200740231Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE CRACKED APPROX .5 INCHES LONG AT DOOR ASSIST CABLE PULLEY BRACKET. (K) [07-17-07] MAINTENANCE CUT AWAY CRACKED ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R52-11-513 REV A. (M)Apr 29, 2007 · N452AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740216Bracket · crackedPAX DOOR ASSIST MOTOR BRACKET (PN 601R317743-7) CRACKED AT BOTTOM END APPROX. 12 INCHES LONG. (K)Apr 27, 2007 · N417AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740215Floor Support · corrodedRT FWD FLOOR SUPPORT ANGLE (PN 601R31148-79) BETWEEN FS 310.00 AND FS319.70 CORRODED ON AFT END. REMOVED AND REPLACED SUPPORT (PN 601R31148-79) IAW SRM 51-23-00, SRM 51-42-06 AND DRWG 601R31148. (K)Apr 26, 2007 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740218Warning Message · illuminatedHIGH SPEED ABORTED TAKEOFF DUE TO (SPOILERON) CAUTION MESSAGE. SPEED WAS 110 KNOTS. BRAKE TEMPS WERE 7-8-8-8. FAULT CLEARED USING FIM RESET PROCEDURE IAW AMM 05-51-27-210-801. NO FURTHER INSPECTION REQUIRED FOR REJECTED TAKEOFF. AC OK FOR SERVICE. (K)Apr 25, 2007 · N435AW · Cndair CL6002B19 · Central WarningSDR A6WA200740219Wheel · vibrationHIGH SPEED ABORTED TAKE-OFF DUE TO NOSEWHEEL VIBRATION. SPEED WAS 135 KNOTS, BRAKE TEMPS WERE 7-7-7-7. COMPLIED WITH REJECTED TAKEOFF INSPECTION IAW AMM 05-51-27-210-801. NO DAMAGE NOTED. (K)Apr 25, 2007 · N429AW · Cndair CL6002B19 · Nose/Tail Landing GearSDR CA070426002Pump · leaking(CAN) DURING ENGINE START UP, GROUND CREW OBSERVED A LEAK COMING FROM BELOW THE ENGINE NR 2. LINE MAINTENACE FOUND A FUEL LEAK FROM A MICROSCOPIC PIN HOLE CLOSE TO A PLUGGED FITTING ADAPTOR ON ENGINE NR 2 FUEL PUMP AFT CASING. THE EXACT PIN HOLE LOCATION WAS Apr 24, 2007 · Cndair CL6002B19 · Engine Fuel PumpSDR VNAA0704015Ecu · malfunctionedCREW REPORTED AFTER TAKEOFF A FLAPS FAIL MESSAGE AT 8 DEGREES. CREW ELECTED TO RETURN TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RESET THE FECU. MAINTENANCE ALSO CYCLED THE FLAPS PER THE SERVICE LETTER 00-001. OPERATIONAL CHECKS GOOD AT Apr 24, 2007 · N250PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740217Handle · lack of lubeAT ROTATION GOT PAX DOOR CAUTION MESSAGE ILLUMINATED COMPLIED WITH QRH GREEN WITNESS MARKS NOT ALIGNED AT GATE DOOR STILL WOULD NOT CLOSE PROPERLY. INSPECTED DOOR AND FOUND EXTERNAL HANDLE WOULD NOT STOW WITHOUT USE OF EXCESSIVE FORCE FROM INTERNAL STOW HANDLApr 24, 2007 · N406AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740212Floorbeam · crackedLT FS 621.00 FLOOR SUPPORT ANGLE CRACKED. MAINTENANCE REPAIRED CRACK IAW REO 601R-53-61-117, REV C. (K)Apr 24, 2007 · N454AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740214Skin · corrodedRT WING PLANK AT ACCESS HOLE 640DB HAS CORROSION ON LOWER IB SIDE MEASURES APPROX .5 X .25 X .002 IN NON-CRITICAL AREA. REPAIRS ACCOMPLISHED IAW EO E06/021/457. (K)Apr 24, 2007 · N417AW · Cndair CL6002B19 · Wing, Plate/SkinSDR VNAA0704010Sensor · damagedCREW REPORTED A LIGHTNING STRIKE ON CLIMBOUT. MAINTENANCE PERFORMED AN ENROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. AIRCRAFT WAS FERRIED TO DAYTON FOR REPAIR. MAINTENANCE INSPECTED AND REPAIRED ALL DAMAGE. MAINTENANCE ALSO REMOVED AND REPLACED THE RApr 19, 2007 · N242JS · Cndair CL6002B19 · Stall Warning SystemSDR VNAA0704014Regulator Valve · failedCREW REPORTED THE LEFT PACK BLOWING SMOKE ON FLIGHT DECK. MAINTENANCE INSPECTED AND DEFERRED THE LEFT HAND AIR CONDITIONING PACK PER MEL 21-51-01. MAINTENANCE REMOVED AND REPLACED THE PRESSURE REGULATING VALVE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUApr 18, 2007 · N241PS · Cndair CL6002B19 · Cabin Cooling System
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