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 SWIA200718348Engine · unknownRIGHT ENGINE OIL MESSAGE CAME ON IN FLIGHT WITH ENGINE OIL PRESSURE AT 0° ON SHORT FINAL. REPLACED RIGHT ENGINE PER AMM 71-00-00. OPS AND LEAK CHECK GOOD, P/N: CF34-3B1, S/N ON: 873098, S/N OFF: 873799.Jun 17, 2007 · N960SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA200740329Intercostal · crackedRT FS 621 TO FS 625 UPPER INTERCOSTAL (OBLIQUE) ANGLE IS CRACKED 1.5 INCH LONG. MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED A NEW ANGLE (PN 601-35012-52 IAW SRM 51-42-06. (K)Jun 17, 2007 · N460AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740330Intercostal · crackedLT FS 621 TO FS 625 UPPER INTERCOSTAL (OBLIQUE) ANGLE IS CRACKED 1..5 INCH LONG. MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED A NEW ANGLE PN 601-35012-51 IAW CRJ SRM 51-42-06. (K)Jun 17, 2007 · N460AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740331Channel · crackedCARGO DOOR FWD TRACK LOWER CHANNEL CRACKED. MAINTENANCE REMOVED AND REPLACED CHANNEL IAW CRJ 200 SRM 51-40-06. (K)Jun 17, 2007 · N460AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA200740309Unknown · odorLAV SMOKE TOILET MESSAGE APPEARED ON FINAL APPROACH. F/A REPORTED SMOKE AND STRONG ELECTRICAL ODOR COMING FROM CENTER OVERHEAD. APU AND PACKS ON. SMOKE DISSIPATED 3-5 MINUTES AFTER INDICATION. REMOVED CEILING PANELS. INSPECTED LIGHT FIXTURES AND WIRING. Jun 16, 2007 · N433AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA200740310Apu · smokeAFTER TRANSFERRING BLEEDS TO APU, THERE WAS A FAINT ODOR IN THE COCKPIT, ENGINES AT IDLE, (SMOKE TOILET) MESSAGE ON ED 1. MESSAGE CLEARED ON RUNWAY. FA REPORTS SMOKE AT CEILING AT ROW 11 AND 12. REPORTS SMOKE AT CEILING AT ROW 11 AND 12 REMOVED AND REPLACEDJun 16, 2007 · N433AW · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) SystemSDR A6WA200740317Rib · crackedRT WING STR 53.60 BATT RIB IS CRACKED 1.0 INCH ON UPPER AFT CORNER. MAINTENANCE REPAIRED IAW REO 601R-57-51-046. (K)Jun 16, 2007 · N434AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200740318Rib · crackedLT WING STR 53.60 BATTERY RIB IS CRACKED 1.0 INCH ON UPPER AFT CORNER. MAINTENANCE REPAIRED IAW REO 601R-57-51-046. (K)Jun 16, 2007 · N434AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200740316Intercostal · crackedLT FS 484 INTERCOSTAL ANGLE CRACKED APPROX .2 INCH LONG LBL 27 AT FLOORBEAM. MAINTENANCE REPAIRED IAW CRJ 200 SRM 51-42-21 AND BSC STANDARD REPAIR NR 601R-53-0029B. (K)Jun 15, 2007 · N434AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740384Panel · corrodedRT WING PLANK AT PANEL 640BB HAS CORROSION APPROX .004 DEEP X 4 INCH LONG X .2500 INCH WIDE IN NON-CRITICAL AREAS. MAINTENANCE PERFORMED MAJOR REPAIR TO WING PLANK ACCESS HOLE AT WS 54.897 (RT) BY REMOVING CORROSION IN NON-CRITICAL AREAS OF HOLE IAW REO 601R-Jun 15, 2007 · N434AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740385Skin · corrodedLT WING PLANK AT PANEL 540BB HAS CORROSION APPROX .004 DEEP X 4 INCHES LONG X .2500 INCHES WIDE IN NON-CRITICAL AREA. MAINTENANCE PERFORMED MAJOR REPAIR TO WING PLANK ACCESS HOLE AT WS 54.897 (LT) BY REMOVING CORROSION IN NON-CRITICAL AREAS IAW REO 601R-57-21Jun 15, 2007 · N434AW · Cndair CL6002B19 · Wing, Plate/SkinSDR CA070618009O-Ring · leaking(CAN) DURING FLIGHT, ENROUTE, THE CREW OBSERVED A RT FUEL LOW PRESS MESSAGE ON EICAS FOLLOWED BY FUEL IMBALANCE. AT 1000 LB FUEL DIFFERENTIAL BETWEEN TANKS, THE QRH PROCEDURE FOR FUEL IMBALANCE WAS INITIATED. AS A RESULT, THE RT ENGINE WAS SHUTDOWN. THE AIRJun 15, 2007 · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR VNAA0706007Screw · damagedCREW REPORTED DURING DESCENT A LIGHTNING STRIKE. CREW LANDED IN CHA WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED AN EN ROUTE VISUAL LIGHTNING STRIKE INSPECTION IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 05-51-05-210-801. DAMAGE WAS FOUND ONJun 14, 2007 · N209PS · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200740313Attach Fitting · crackedRT FLOORBEAM ATTACH CLIPS ARE CRACKED AT IB AND OB SIDES FS 280, RBL 9, WL 72. (K) [07-31-07] MAINTENANCE REPAIRED IAW BSC STANDARD REPAIR 601R53-0057A, AND CRJ 200, SRM 51-42-13 AND 51-42-21. (K)Jun 14, 2007 · N434AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740314Attach Fitting · crackedLT FLOORBEAM ATTACH CLIPS ARE CRACKED AT IB AND OB SIDES FS 280, LBL 9, WL 72. (K) [07-31-07] MAINTENANCE REPAIRED IAW CRJ 200 SRM 51-42-13 AND 51-42-21 AND BSC STANDARD REPAIR NR 601R-53-0057A. (K)Jun 14, 2007 · N434AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740315Bracket · corrodedLOWER SILL JOINT BRACKET (PN 601R38335-1) CORRODED AT FS 318.70, RBL 36, WL 73. MAINTENANCE REMOVED AND REPLACED BRACKET (PN 601R38335-1) IAW CRJ 200 SRM 51-42-21. (K)Jun 14, 2007 · N434AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740328Intercostal · crackedUNDERFLOOR SUPPORT INTERCOSTAL HAS A CRACKED FLANGE AT IB SIDE OF LBL 36, FS 484, WL 72.5. MAINTENANCE CUT OFF CRACKED FLANGE AND INSTALLED REPAIR ANGLE IAW REO 601R53-41-059. (K)Jun 14, 2007 · N460AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA0706006Ahrs · malfunctionedCREW REPORTED DURING CRUISE THE LOSS OF THE FIRST OFFICERS ATTITUDE AND HEADING INDICATIONS. CREW ELECTED TO DIVERT TO GSO AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CYCLED THE AHRS 2 CIRCUIT BREAKERS. MAINTENANCE ALSO COMPLIED WITH THE FUNCTIONJun 13, 2007 · N247JS · Cndair CL6002B19 · Integrated Flight SystemSDR CA070618004Connector · misinstalled(CAN) ON PATS RT AUXILARY TANK FOUND THE PRESSURE DIFFERENTIAL SWITCH, THE SOCKET OF THE SWITCH AND THE ELECTRICAL HARNESS CONNECTOR HAVING BOTH PINS, THE CONNECTOR SHOULD BE A FEMALE TYPE. THE DIFFERENTIAL SWITCH IS WORKING ONLY ON GROUND DURING FUELING. FOUNJun 13, 2007 · Cndair CL6002B19 · Fuel System WiringSDR A6WA200740308Priority Valve · inoperativeGOT GEAR DISAGREE WHEN LOWERING GEAR FOR LANDING. CYCLED GEAR UP AND DISAGREE WITH GEAR UP ALSO. COMPLIED WITH DISAGREE CHECKLIST AND HAD NORMAL INDICATION. REMOVED AND REPLACED MLG PRIORITY VALVE IAW AMM 32-32-15. OPS CHECK GOOD. (K)Jun 12, 2007 · N438AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR VNAA0706003Radome · damagedCREW REPORTED A LIGHTNING STRIKE WHILE IN FLIGHT. CREW LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE PERFORMED AN EN ROUTE LIGHTNING STRIKE INSPECTION. MAINTENANCE REMOVED AND REPLACED THE RADOME IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 53-81-01-400Jun 8, 2007 · N253PS · Cndair CL6002B19 · Aerodynamic FairingsSDR VNAA0706002Tire · failedCREW REPORTED ON TAKEOFF ROLL THE RIGHT HAND NOSE TIRE WENT FLAT. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED BOTH NOSE TIRES IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 32-42-01. MAINTENANCE FOUNDJun 5, 2007 · N228PS · Cndair CL6002B19 · TireSDR VNAA0706001Window · failedCREW REPORTED ON CLIMBOUT OF HSV THE RIGHT HAND SIDE WINDOW BROKE. CREW ELECTED TO RETURN TO HSV AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND SIDE WINDOW DUE TO INNER PANE SPIDER WEB CRACKS IN ACCORDANCE WITH THE AIRCRAFT MAINJun 3, 2007 · N209PS · Cndair CL6002B19 · Flight Compartment WindowsSDR CA070601002Adg · deployed(CAN) ADG DEPLOYED AS THE LANDING GEAR WAS SELECTED UP. THE FLIGHT RETURNED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING WAS CARRIED OUT AND THE ADG AUTO DEPLOY CONTROLLER WAS REPLACED AND TESTED SERVICEABLE. THE ADG WAS INSPECTED VISUALLY IAW MFG AND IS TOMay 31, 2007 · Cndair CL6002B19 · AC Generation SystemSDR A6WA200740284Intercostal · crackedLT SIDE FS 621.00 TO 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. [07-31-07] MAINTENANCE REMOVED CRACKED INTERCOSTAL AT LT STR 14L AND INSTALLED NEW INTERCOSTAL IAW CRJ200 SRM 51-42-06. (K)May 30, 2007 · N418AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740278Angle · crackedRT 625, OBLIQUE ANGLE IS CRACKED APPROX 1 INCH LONG. (K) [07-12-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW SRM 51-42-06. (K)May 28, 2007 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740279Angle · crackedLT 625, OBLIQUE ANGLE IS CRACKED APPROX 1 INCH LONG. (K) [07-12-07] MAINATENANCE REMOVED AND REPLACED ANGLE IAW SRM 51-42-06. (K)May 28, 2007 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740282Skin · dentedRT NOSE SKIN PANEL PN 600-33052-141 IS DENTED 3 INCHES LONG BY 2 INCHES WIDE BY 0.100 DEEP BETWEEN FS 169.00 AND FS 174.00. S/D - MAINTENANCE REMOVED AND REPLACED SKIN PANEL P/N 600-33052-141 BETWEEN FS 169.00 AND 174 IAW CRJ 200 SRM 51-42-06. (K)May 28, 2007 · N420AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200740283Panel · dentedRT NOSE SKIN PANEL PN 600-33010-27 IS DENTED 5 INCH LONG X 4 INCHES WIDE X 0.125 INCHES DEEP FROM FS 169.00 TO FS 193.00. S/D - MAINTENANCE REMOVED AND REPLACED SKIN PANEL P/N 600-33010-27, IAW CRJ 200 SRM 51-42-06 AND BSC EO 601R-53-11942. (K)May 28, 2007 · N420AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA0705007Unknown · unknownCREW REPORTED AN AMBER SPOILERON CAS MESSAGE ON APPROACH. CREW FOLLOWED THE QRH AND NOTIFIED ATC REQUESTING A GO-AROUND. AFTER THE GO-AROUND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RESET THE SYSTEM IN ACCORDANCE WITH THE SERVICE LETMay 27, 2007 · N218PS · Cndair CL6002B19 · Drag Control SystemSDR A6WA200740273Angle · crackedLT 484 ANGLE IS CRACKED AT LBL 36 AND LBL 27 APPROX .2500 INCH LONG. (K) [07-12-07] MAINTENANCE REPAIRED LT 484 ANGLE AT LBL 36 AND 27 IAW REO 601R-53-41-059 REV A, STANDARD REPAIR 601R-53-0029B AND STANDARD REPAIR 601R-53-0030A. (K)May 27, 2007 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740274Angle · crackedRT 484 ANGLE IS CRACKED AT RBL 27 APPROX .2500 INCH LONG. (K) [07-12-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW REO 601R-53-41-059, REV A AND BSC STANDARD REPAIR 601R-53-0029B. (K)May 27, 2007 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740275Floorbeam · crackedRT FS 621.00 FLOOR ATTACHMENT SUPPORT ANGLE IS CRACKED .5 INCH LONG IN OB RADIUS. (K) [07-12-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW REO 601R-53-61-117 REV C. (K)May 27, 2007 · N459AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740276Floorbeam · crackedRT FS 621.00 FLOOR ATTACHMENT SUPPORT ANGLE IS CRACKED .5 INCH LONG IN OB RADIUS. (K)May 27, 2007 · N459AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740277Floorbeam · crackedLT FS 621.00 FLOOR ATTACHMENT SUPPORT ANGLE IS CRACKED .5 INCH LONG ON OB RADIUS. (K) [07-12-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW REO 601R-53-61-117, REV C. (K)May 27, 2007 · N459AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR CA070528007Selector Valve · unserviceable(CAN) CLIMBING THROUGHT 13000 FT AT 290 KIAS, THE NLG DOOR WARNING/UNSAFE MESSAGE WAS DISPLAYED AND CREW COULD HEAR A CLUNKING NOISE FROM THE NLG AREA. ELECTED TO RETURN. MLG EXTENDED NORMALLY WITH (3) GREEN LIGHTS AND NO CAUTION/ADVISORY MESSAGES DISPLAYED. May 26, 2007 · Cndair CL6002B19 · Landing Gear SelectorSDR A6WA200740261Pump · failedENROUTE FROM DCA T 1252Z HYD2 LOW PRESSURE MESSAGE COMPLIED WITH QRH DIVERTED. HYD QTY NR 2 SYSTEM READS ZERO. PRESSED FDR EVENT BUTTON. LANDING WEIGHT 46900, BRAKE TEMP READS 4,5,4,4. REMOVED AND REPLACED ENGINE DRIVEN HYDRAULIC PUMP NR 2. OPERATIONAL ANMay 22, 2007 · N426AW · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR A6WA200740268Intercostal · crackedRT FS 625.00, OBLIQUE ANGLE IS CRACKED 1.5 INCH ON AFT RADIUS. S/D MAINTENANCE REMOVED AND REPLACED RT FS 625 OBLIQUE ANGLE IAW CRJ 200 SRM 51-42-21 AND BOMBARDIER REO 601R-53-61-422. (K)May 22, 2007 · N456ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740269Intercostal · crackedLT FS 625 OBLIQUE ANGLE IS CRACKED 1.5 INCH LONG IN AFT RADIUS. S/D MAINTENANCE REMOVED AND REPLACED LEFT FS 625 OBLIQUE ANGLE IAW CRJ200 SRM 51-42-21 AND BOMBARDIER REO 601R-53-61-422. (K)May 22, 2007 · N456ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740270Support Bracket · crackedLT MLG WHEEL WELL HYDRAULIC SUPPORT BRACKET IS CRACKED .2500 INCH ON OB RADIUS. S/D MAINTENANCE REMOVED BRACKET AND INSTALLED NEW BRACKET P/N 601R75262-159 IAW CRJ SRM 51-42-06. (K)May 22, 2007 · N456ZW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740271Support Bracket · crackedLT MLG WHEEL WELL HYDRAULIC SUPPORT BRACKET IS CRACKED .2500 INCH ON OB RADIUS. (K)May 22, 2007 · N456ZW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740272Support Bracket · crackedRT MLG WHEEL WELL HYDRAULIC SUPPORT BRACKETS ARE CRACKED .2500 INCH ON OB RADIUS. S/D - MAINTENANCE REMOVED BRACKETS AND INSTALLED NEW BRACKETS P/N 601R75262-153 AND 601R75262-157 IAW CRJ SRM 51-42-06. (K)May 22, 2007 · N456ZW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740262Angle · crackedLT 621 IS CRACKED .5 INCH LONG. S/D - MAINTENANCE CUT AWAY DAMAGED ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R53-61-117 REVC. (K)May 21, 2007 · N456ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740263Stringer Clip · crackedLT IB AND OB 280 CLIPS ARE CRACKED APPROX .5 INCH. S/D MAINTENANCE REPLACED INBOARD AND OUTBOARD CLIPS WITH NEW CLIPS P/N 601R31113-57 IAW BSC STANDARD REPAIR 601R-53-0057A AND CRJ SRM 51-42-13, 51-42-21. (K)May 21, 2007 · N456ZW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740265Angle · crackedRT 484 ANGLE IS CRACKED APPROX .2500 INCH LONG. S/D MAINTENANCE CUT AWAY CRACKED FLANGE AND INSTALLED REPAIR FLANGE IAW BOMBARDIER REO 601R-53-41-059 REV A. (K)May 21, 2007 · N456ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740266Angle · crackedLT 484 ANGLE IS CRACKED APPROX .2500 INCH LONG. S/D MAINTENANCE PERFORMED EDDY CURRENT INSPECTION IAW CRJ NDTM 51-20-06 PART 6 AND FOUND NO RECORDABLE INDICATIONS. (K)May 21, 2007 · N456ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740267Angle · crackedRT 621 IS CRACKED APPROX .5 INCH LONG. S/D MAINTENANCE REMOVED DAMAGED SECTION ANGLE AND INSTALLED REPAIR ANGLE AND DOUBLER IAW BOMBARDIER REO 601R-53-61-117 REVC. (K)May 21, 2007 · N456ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA0705003Check Valve · damagedCREW REPORTED RECEIVING A RIGHT HAND PACK OVERHEAT (TEMP) CAUTION MESSAGE WHILE SMELLED SMOKE IN THE CABIN DURING TAXI-IN TO THE GATE. MAINTENANCE INSPECTED AND DEFERRED THE RIGHT HAND PACK PER MEL 21-51-01 -C- OPT 1. MAINTENANCE TROUBLESHOT THE RIGHT HAND PMay 20, 2007 · N261PS · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200740259Carbon Seal · leakingAT FL320 RT ENGINE OIL PRESSURE MASTER WARNING ILLUMINATED OIL PRESSURE INDICATED 20 PSI. COMPLIED WITH QRH WITH REDUCED POWER SETTING, OIL PRESSURE IMPROVED TO 26 PSI MOMENTARILY, THEN LEVELED OFF TO 20 PSI. OIL TEMP NEVER EXCEEDED 115 DEGREES (C). [07-31-May 19, 2007 · N436AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200740260Carbon Seal · leakingAT FL320 RT ENGINE OIL PRESS MASTER WARNING ILLUMINATED OIL PRESS INDICATED 20 PSI. C/W QRH WIGH REDUCED POWER SETTING OIL PRESS INCREASED TO 26 PSI MOMENTARILY, THEN LEVELED OFF AT 23 PSI. OIL NEVER EXCEEDED 115 DEGREES. PERFORMED PRECAUTIONARY IFSD. REMOMay 19, 2007 · N436AW · Cndair CL6002B19 · Turbine Engine Oil System
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