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 ASOA04872Support Beam · crackedDURING A C-CHECK, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT LB0 WAS FOUND TO BE CRACKED UNDER THE FIRE LOOP BRACKET BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO 600-53-0072.Nov 2, 2004 · N845AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR ASOA04873Step · brokenDURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR IAW AMM 52-11.Nov 2, 2004 · N853AS · Cndair CL6002B19 · Entrance StairsSDR CA041104012Window · crackedRIGHT SIDE COCKPIT WINDOW REPLACED ACCORDING AMM PROCEDURE.Nov 1, 2004 · Cndair CL6002B19 · Flight Compartment WindowsSDR ASOA04869Power Supply · inoperativeDURING HANGAR MAINTENANCE, THE AFT SECTION OF EMERGENCY LIGHTS IN THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY UNIT FOR THE AFT SECTION OF EMERGENCY LIGHTS IN THE CABIN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SNov 1, 2004 · N859AS · Cndair CL6002B19 · Emergency LightingSDR ASOA04870Step · crackedDURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR.Nov 1, 2004 · N859AS · Cndair CL6002B19 · Entrance StairsSDR CA041103002Stator · open(CAN) WHILE IN THE CLIMB, CREW REPORTED AN UNCOMMANDED RT ENGINE OVERSPEED. AIRCRAFT RETURNED TO DEPARTURE STATION. TROUBLESHOOTING TRACED FAULT TO AN OPEN CIRCUIT IN THE RT ENGINE STATOR-ALTERNATOR. STATOR-ALTERNATOR REPLACED. ENGINE OVERSPEED INSPECTIONS COMNov 1, 2004 · Cndair CL6002B19 · Alternator-Generator DriveSDR VNAA0410013Skin · bird strikeAFTER LANDING AT CLT THE PILOT OF FLIGHT 2421 REPORTED A BIRD STRIKE BELOW THE CAPTAIN'S WINDSHIELD. A BIRD STRIKE INSPECTION WAS PERFORMED AND TWO DENTS WERE FOUND ON THE FORWARD FUSELAGE AT FS 589 & FS 202. THE AIRCRAFT WAS FERRIED TO CAK WHERE PSA MAINTENOct 30, 2004 · N220PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA04851Light · brokenDURING A C-CHECK, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE SERVICE DOOR. OPERATIONAL CHECKS GOOD.Oct 30, 2004 · N877AS · Cndair CL6002B19 · Emergency LightingSDR REXA04025Proximity Sensor · out of positionON CLIMB-OUT FROM TAKEOFF, GOT (NOSE DOOR) MESSAGE AND (GEAR DISAGREE) MESSAGE. ORH FOLLOWED, EMERGENCY DECLARED RETURNED TO AIRPORT, UNEVENTFUL LANDING. FOUND PROXIMITY SENSOR ON NOSE GEAR OUT OF POSITION. RIGGED SENSOR IAW AMM, PERFORMED GEAR SWINGS.Oct 29, 2004 · N8515F · Cndair CL6002B19 · Landing Gear Position and WarningSDR ASOA04846Support Beam · crackedDURING AN A-CHECK, THE ENGINE SUPPORT BEAM AT 36.20 ON THE LT AND RT SIDES WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR TO THE ENGINE SUPPORT BEAM AT 36.20 ON THE LT AND RT SIDES LOWER WEB IAW EO 600-53-0071. THIS MRR WILL Oct 29, 2004 · N906EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR ASOA04847Frame · crackedDURING AN A-CHECK, THE LT FS 640 DOUBLER, LT FS 640 FRAME AND THE SKIN BUTT JOINT STRAP ON THE LT SIDE AT FS 640, STRINGER 8-13 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT FS640 DOUBLER AND LT FS640 FRAME IAW SRM 53-00Oct 29, 2004 · N821AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA04848Sill · crackedDURING A C-CHECK, THE FLOOR SILL PLATE AT THE CARGO ENTRANCE TWO INTERCOSTAL ATTACH FASTENERS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SILL PLATE AT THE CARGO ENTRANCE IAW EO 600-53-0117.Oct 29, 2004 · N877AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA04850Step · crackedDURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED AT THE LIFT POINT. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.Oct 29, 2004 · N852AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR 04302639Transducer · failedEVENT SUMMARY STATED STALL FAIL. REMOVED AND REPLACED RT AND LT MACH TRANSDUCER. OPS CHECK GOOD.Oct 28, 2004 · N639BR · Cndair CL6002B19 · Stall Warning SystemSDR SWIA200414026Actuator · malfunctioned(FLAPS FAIL) CAUTION MESSAGE ON APPROACH, AFTER SELECTING FLAPS 8. REPLACED LT IB NR 1 AND NR 2 FLAP ACTUATORS WITH SERVICEABLE UNITS IAW MM 27-53-01. P/N: 852D100-19, S/N OFF: 3561, P/N: 852D100-19, S/N OFF: 3612.Oct 28, 2004 · N446SW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR A6WA200440171Floorbeam · crackedFS280 UNDER FLOORBEAM AT LBL 12 AND WL 69 LOWER FLANGE IS CRACKED. CUT AWAY DAMAGED SECTION OF FLOOR ANGLE, PERFORMED LPI TO ENSURE NO CRACKS EXIST. FAB REPAIR ANGLE AND FILLER FROM S-6144-3, S-6144-13 AND INSTALLED WET USING SOLID RIVETS AND LOCK FASTENERS.Oct 28, 2004 · N404AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200440170Floorbeam · crackedFS 280 UNDER FLOORBEAM AT RBL 12 AND WL 69 LOWER FLANGE IS CRACKED. CUT AWAY DAMAGED SECTION OF FLOOR ANGLE, PERFORMED LPI TO ENSURE NO CRACKS EXIST. FABRICATED REPAIR ANGLE AND FILLER FROM S-6744-3 AND S6744-13 AND INSTALLED WET USING SOLID RIVETS AND LOCK Oct 28, 2004 · N404AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200440169Plate · corrodedSERVICE DOOR RAMP PLATE, PN 601R38957-19, CORRODED AROUND OPENINGS AND FASTENER HOLES. REPLACED RAMP PLATE WITH NEW RAMP PLATE IAW SRM 51-41.02.Oct 28, 2004 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440172Angle · crackedFS 280, RBL 9 IB ANGLE PN 601R3113-58 IS CRACKED IN RADIUS AT WLK 73. REMOVED AND REPLACED ANGLE WITH NEW ANGLE PN 601R3113-58 IAW SRM 51-42-06 AND 51-42-21.Oct 28, 2004 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440173Angle · crackedFS 280, RBL 9 OB ANGLE PN 601R31113-58 IS CRACKED IN RADIUS AT WL73. REMOVED AND REPLACED ANGLE WITH PRE-FABBED ANGLE IAW REO 601R53-11-171 REV A AND BRAS EO 601R-53-5447 AND M.Oct 28, 2004 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440174Angle · crackedFS 280, LBL9 OB ANGLE PN 601R31113-57 IS CRACKED IN RADIUS AT WL 73. REMOVED AND REPLACED ANGLE WITH PRE-FABBED ANGLE IAW REO 601R-53-11-171 REV A AND BRAS EO 601R-53-5547.Oct 28, 2004 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440184Plate · corrodedSERVICE DOOR RAMP PLATE, PN 601R38957-19, CORRODED AROUND OPENINGS AND FASTENER HOLES. REPLACED RAMP PLATE WITH NEW RAMP PLATE IAW SRM 51-41-02.Oct 28, 2004 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA04845Door · bindingDURING A GROUND INSPECTION, THE MAIN PASSENGER DOOR WAS HARD TO CLOSE USING THE HANDLE. MAINTENANCE CLEANED AND LUBRICATED THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.Oct 28, 2004 · N875AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200440175Landing Gear · malfunctionedWHEN C/W QRH FOR GEAR DISAGREE, MLG DID NOT EXTEND WHEN LANDING. MANUAL RELEASE HANDLE WAS PULLED PERFORMED OPS TEST OF MANUAL RELEASE SYSTEM FOR LANDING GEAR. NO FAULTS FOUND, ALL CHECKED IAW AMM32-34-00.Oct 27, 2004 · N406AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA04842Switch · jammedDURING CLIMB-OUT, EN ROUTE, AT APPROXIMATELY 7000 FT, THE CREW REPORTED STAB AND MACH TRIM FAILURE. AFTER COMPLYING WITH THE QRH THE TRIMS STILL COULD NOT BE ENGAGED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY AFTER RETURNING. MAINTENANCE INTEOct 27, 2004 · N856AS · Cndair CL6002B19 · Stabilizer Position IndicatingSDR ASOA04837Floorbeam · crackedDURING A C-CHECK, THE FLOOR SUPPORT BEAMS AT FS 621 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT BEAMS AT FS 621 ON THE LT AND RT SIDES IAW EO 600-53-0105.Oct 26, 2004 · N877AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200440183Structure · damagedLT BOOST PUMP CANISTER SATELLITE HOLE AFT SIDE LBL 11.18 FAILED EDDY CURRENT INSPECTION. INDICATION NOTED ON OB SIDE OF HOLE. REPAIRED SATELLITE HOLE BY REAMING THE HOLE TO .4150 AND INSTALLING A FREEZE PLUG. (OD EO 601R-57-21-526).Oct 26, 2004 · N404AW · Cndair CL6002B19 · Wing, Attach FittingsSDR CA041031001Pump · leaking(CAN) DURING SCHEDULED CHECKS ON ENGINE, WE FOUND FUEL LEAK COMING FROM 'MAIN FUEL PUMP INLET PORT BODY' OF RT ENGINE. LEAK WAS DETECTED ACTIVATING THE FUEL BOSST PUMP. LEAK CAN BE DESCRIBED AS FOLLOW: CAPILLARY LEAK, LEAK JET ABOUT 3 INCHES LONG VAPOURIZINGOct 26, 2004 · Cndair CL6002B19 · Engine Fuel PumpSDR SWIA200414017Actuator · failedFLAPS FAIL CAUTION MESSAGE ON APPROACH. FLAPS FAILED AT ZERO. REMOVED AND REPLACED NR 4 FLAP ACTUATOR IAW MM 27-53-01, 27-53-05. OPERATIONAL CHECK GOOD.Oct 25, 2004 · N446SW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR A6WA200440167Ahrs · inoperativeAFTER SWITCHING ATT/HDG FROM NORM TO (2) AT 31000, BOTH CAPT AND F/O AHRS WENT BLANK. A/P KICKED OFF AND YAW NR 2 DISENGAGED SWITCHED TO NORM AND CAPT AHRS CAME BACK. THEN 5 SECS LATER F/O AHRS CAME BACK. REENGAGED A/P AND YAW DAMP, TO FURTHER PROBLEM. REMOct 25, 2004 · N437AW · Cndair CL6002B19 · Attitude and Direction Data SystemSDR A6WA200440168Computer · unreliablePITCH AND ROLL ANNUNCIATOR ILLUMINATED ON CAPTS EFIS IN FLIGHT. PITCH UNRELIABLE, MORE THAN 6 DEGREES THAN F/O EFIS ATTITUDE. PITCH ILLUMINATED ON GROUND DEPOWERED AND REPOWERED. TAXI TEST OK. PROBLEM REOCCURRED IN FLIGHT. REMOVED AND REPLACED NR 1 AHRS COct 25, 2004 · N437AW · Cndair CL6002B19 · Attitude and Direction Data SystemSDR ASOA04835Rib · crackedDURING A C-CHECK, THE RT MAIN LANDING GEAR BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT MAIN LANDING GEAR BATT RIB ASSEMBLY AT WS 53.60 IAW EO600-57-039A.Oct 25, 2004 · N877AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR ASOA04836Doubler · crackedDURING A C-CHECK, THE RT DOUBLER AT FS 640 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT DOUBLER AT FS 640.Oct 25, 2004 · N824AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200440162Rib · crackedBATT RIB ASSY IS CRACKED 1.2500 INCH LONG IN AFT UPPER RADIUS. CORRECTIVE ACTION IN PROGRESS.Oct 25, 2004 · N404AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200440163Rib · crackedRT WS 53.60 BATT RIB ASSY IS CRACKED, 1 INCH LONG IN AFT UPPER RADIUS. REPAIRED BATT RIB ASSY BY CUTTING OUT DAMAGED SECTION. FABBED REPAIR ANGLE FROM S6144-0 AND FILLER FROM 7075T62 P.O. NR 35850, INSTALLED REPAIR PARTS WET USING SOLID RIVETS AND HI-LIGHT FOct 25, 2004 · N404AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200440164Attach Angle · crackedINTERCOSTAL AT FS 484 LT SIDE IS CRACKED NEAR RADIUS OF ATTACHMENT FLANGE AT LBL36. CUT AWAY DAMAGED ATTACHMENT ANGLE. PERFORMED LPI TO ENSURE NO CRACKS EXIST, FAB REPLACEMENT ANGLE FROM 6144-14 AND INSTALLED USING SOLID RIVETS AND HI-LITE FASTENERS. ALL WOOct 25, 2004 · N404AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6W2005F00001Intercostal · crackedINTERCOSTAL LT SIDE IS CRACKED NEAR RADIUS OF ATTACHMENT FLANGE AT LBL 36. CUT AWAY DAMAGED ATTACHMENT ANGLE. PERFORMED LPI TO ENSURE NO CRACKS EXIT, FAB REPLACEMENT ANGLE FROM 6144-14 AND INSTALLED USING SOLID RIVETS AND HI-LITE FASTENERS. ALL WORK DONE IAOct 25, 2004 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200414014Odor · detectedA STRONG FUEL SMELL COMES INTO THE CABIN WHEN SHUTTING DOWN NR 1 ENGINE AFTER LANDING WITH THE APU RUNNING. CHECKED VENT SYSTEM. PRESSURIZED A/C WITH ALL SYSTEMS AND PERFORMED SHUTDOWN PROCEDURES. NO INDICATION OF FUEL SMELL NOTED. NO DISCREPANCIES NOTED.Oct 24, 2004 · N432SW · Cndair CL6002B19 · Air Distribution SystemSDR SWIA200414015Sensor · malfunctionedCAPTAINS 1.27 STALL GREEN LINE SHOWS 280 KTS AT FLIGHT LEVEL 290 WHEN CO-PILOT'S IS NOT EVEN VISIBLE. NO STALL TAPE INDICATION. REMOVED AND REPLACED BOTH LT AND RT AOA VANES IAW MM 27-35-05. OPERATIONAL CHECK GOOD IAW AMM 27-35-01. PN 45150340 SN OFF 338 Oct 24, 2004 · N416SW · Cndair CL6002B19 · Stall Warning SystemSDR MASA200400599Control Unit · malfunctionedABORTED TAKE OFF AND RETURNED TO GATE FOR SPOILER CONFIGURATION WARNING MESSAGE ON TAKE OFF ROLL. MECHANIC SENT AND REPLACED THE NR1 SECU. PART INFORMATION TO FOLLOW.Oct 24, 2004 · N75992 · Cndair CL6002B19 · Drag Control SystemSDR ASOA04826Clip · crackedDURING A C-CHECK, THE IB AND OB CLIPS AT FS 484, LBL 27 AND LBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE IB CLIP AT FS 484, LBL 36 IAW EO 600-53-0098.Oct 24, 2004 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA04827Clip · crackedDURING A C-CHECK, THE IB AND OB CLIPS AT FS 484, RBL 27 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE IB CLIP AT FS 484, RBL 27 AND REPAIRING THE OB CLIP AT FS 484, RBL 36 IAW EO600-53-0098.Oct 24, 2004 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA04828Support Beam · crackedDURING A C-CHECK, THE ENGINE SUPPORT BEAMS AT BL 36.20 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED AT THE AFT IB CORNERS UNDER THE ACCESS PANEL BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAMS AT BL 36.20 ON THE LT AND RT SIDES IAW EO 600-Oct 24, 2004 · N877AS · Cndair CL6002B19 · Engine Mount SectionSDR ASOA04829Support Beam · crackedDURING A C-CHECK, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED AT THE FIRE LOOP CLIP BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO 60053-0072.Oct 24, 2004 · N877AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA04831Bracket · crackedDURING A C-CHECK, THE RT AIR CYCLE MACHINE SUPPORT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT AIR CYCLE MACHINE SUPPORT BRACKET IAW SRM 51-42-00.Oct 24, 2004 · N877AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA04833Clip · crackedDURING A C-CHECK, THE RT CLIP AT FS 625 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT CLIP AT FS 625 IAW SRM 51-42-00.Oct 24, 2004 · N877AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA04834Stringer Clip · crackedDURING A C-CHECK, THE OB CLIPS AT FS 625, STRINGER 15R WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE OB CLIP AT FS 625, STRINGER 15R IAW SRM 51-42-00.Oct 24, 2004 · N824AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA04840Bracket · crackedDURING A C-CHECK, THE RT FS 484.00, RBL 36 AFT BRACKET WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CRACKED BRACKET IAW EO 600-53-0194.Oct 24, 2004 · N877AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA04814Charger · inoperativeDURING A GROUND INSPECTION, THE AFT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY CHARGER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.Oct 23, 2004 · N859AS · Cndair CL6002B19 · Emergency LightingSDR ASOA04812Floor Support · crackedDURING C-CHECK, THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 IAW EO600-53-0105.Oct 23, 2004 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
Back to GE CF34-3B1