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 A6WA200740391Angle · crackedZ-ANGLE (PN 601R75262-153) IN RT MLG WHEEL WELL IS CRACKED. (K) MAINTENANCE INSTALLED SERVICEABLE ANGLE P/N 601R75262-153 IAW CRJ 200 SRM 51-42-06. (M)Jul 7, 2007 · N409AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740368Floorbeam · crackedLT FS 621 FLOOR SUPPORT ANGLE CRACKED, 2 INCH LONG. (K) MAINTENANCE REPAIRED LEFT FLOOR SUPPORT ANGLE AT FS 621 IAW BOMBARDIER REO 601R-53-61-117. (M)Jul 6, 2007 · N461AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740369Floorbeam · crackedRT FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .2 INCH LONG. (K) MAINTENANCE REPAIRED RIGHT FLOOR SUPPORT ANGLE AT FS 621 IAW BOMBARDIER REO 601R-53-61-117. (M)Jul 6, 2007 · N461AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740372Angle · crackedLT 484 ANGLE IS CRACKED APPROX .5 INCH L AT LBL 27. (K) MAINTENANCE REMOVED ANGLE IAW SRM 51-42-06 AND 51-42-21. FABRICATED AND INSTALLED REPAIR ANGLE IAW BSC SR 601R-53-0039B. (M)Jul 6, 2007 · N461AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740373Angle · crackedLT 484 ANGLE IS CRACKED APPROX .2500 INCH AT LBL 36. (K) MAINTENANCE REMOVED FLANGE IAW BOMBARDIER REO 601R-53-41-059 REV A. FABRICATED AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R-53-1-059 AND BSC SR 601R-53-0030A. (M)Jul 6, 2007 · N461AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740374Angle · crackedRT 484 ANGLE IS CRACKED APPROX .2500 INCH LONG AT RBL36. (K) MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M)Jul 6, 2007 · N461AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740375Angle · crackedRT 484 ANGLE IS CRACKED APPROX .5 INCH LONG AT RBL 27. (K) MAINTENANCE REMOVED FLANGE IAW BOMBARDIER REO 601R-53-41-059 REV A. FABRICATED AND INSTALLED REPAIR ANGLE IAW REO 601R-53-41-059 AND BSC SR 601R-53-0030A. (M)Jul 6, 2007 · N461AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA070707001Accumulator · separated(CAN) DURING TAXI-OUT, HYD 1 LO PRESS MESSAGE CAME ON. THE CREW REPORTED LOUD BANG FROM AFT PART OF CABIN. CREW EXECUTED RELEVANT ABNORMAL CHECKLISTS AND RETURNED TO RAMP. AFTER VERIFICATION BY THE MTCE CREW, THEY FOUND OUT THAT THE NR 2 HYDRAULIC ACCUMULATJul 6, 2007 · Cndair CL6002B19 · Hydraulic System, MainSDR VNAA0707001Skin · damagedCREW REPORTED A LIGHTNING STRIKE WHEN THE AIRCRAFT TERMINATED IN CLT. MAINTENANCE INSPECTED AND FOUND LIGHTNING STRIKE DAMAGE TO THE LEFT HAND WINGLET TIP. MAINTENANCE COMPLIED WITH A DETAILED LIGHTNING STRIKE INSPECTION FOR DAMAGE IN ACCORDANCE WITH THE AIRJul 4, 2007 · N248PS · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740358Angle · crackedLT FS 621.00 TO 625.00 OBLIQUE ANGLE IS CRACKED 1.5 INCH LONG IN AFT RADIUS. (K) MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED A NEW ANGLE P/N 601-35012-51 IAW CRJ SRM 51-42-06. (M)Jul 3, 2007 · N409AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA0706017Sleeve · wornCREW REPORTED A CARGO BOTTLE LOW CAUTION MESSAGE IN CRUISE. CREW FOLLOWED THE QRH AND DIVERTED TO ATL. CREW LANDED WITHOUT INCIDENT IN ATL. MAINTENANCE INSPECTED AND DEFERRED THE CARGO COMPARTMENT FIRE EXTINGUISHING SYSTEM PER MEL 26-25-01 CODE C. MAINTENAJun 30, 2007 · N259PS · Cndair CL6002B19 · Cabin Cooling SystemSDR MASA200700366Oil System · overservicedASH 7007 RDU. RIGHT ENGINE LOW OIL PRESSURE WARNING IN FLIGHT. CREW REPORTED GETTING THE RIGHT ENGINE LOW OIL PRESSURE WARNING IN FLIGHT WITH 25 PSI INDICATED. CREW DECLARED AN EMERGENCY AND DIVERTED TO PIT. CREW DID NOT SHUT DOWN THE ENGINE. FOUND OIL OVJun 27, 2007 · N75993 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200740333Filter · failedAIRCRAFT FAILED HYDRAULIC SYSTEM TEST ON THE FIRST FLIGHT OF THE DAY CHECK. (NR2 SYSTEM) REMOVED AND REPLACED HYDRAULIC MANIFOLD NR 2, REF 29-11-05. (K)Jun 26, 2007 · N418AW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA200740353Floorbeam · crackedRT FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 621.00. MAINTENANCE REPAIRED RT FS 621 IAW REO 601R53-61-117 REV C. (K)Jun 25, 2007 · N463AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740354Floorbeam · crackedLT FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 621.00. MAINTENANCE REPAIRED FLOOR SUPPORT BY CUTTING OUT DAMAGED ANGLE, FABBING REPAIR PARTS AND INSTALLING IAW REO 601R53-61-717, REV C AND BSC EO 601R-53-12256. (K)Jun 25, 2007 · N463AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740334Floor Support · crackedRT FS 621 FLOOR SUPPORT ANGLE APPROX .2 INCH LONG. MAINTENANCE REMOVED DAMAGED AREA AND INSTALLED REPAIR ANGLE IAW REO 601R-53-61-117. (K)Jun 25, 2007 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740335Floorbeam · crackedLT FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .2 INCH LONG. MAINTENANCE CUT OUT DAMAGED AREA AND INSTALLED REPAIR ANGLE IAW REO 601R-53-61-117. (K)Jun 25, 2007 · N462AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740342Transducer · crackedHYDRAULIC PRESSURE TRANSDUCER (PN 610R75262-157) CRACKED APPROX .2 INCH LONG INRT MLG WHEEL WELL CEILING. MAINTENANCE REMOVED CRACKED HAT CHANNEL AND INSTALLED SERVICEABLE HAT CHANNEL PN 601R75262-157 IAW SRM 51-42-06. (K)Jun 25, 2007 · N462AW · Cndair CL6002B19 · Hydraulic Indicating SystemSDR A6WA200740343Bracket · crackedHYDRAULIC LINE Z-BRACKET (PN 601R75262-153) CRACKED APPROX .1 INCH LONG IN RT MLG WHEEL WELL. MAINTENANCE REMOVED AND REPLACED BRACKET (PN 601R75262-153) IAW SRM 51-42-06. (K)Jun 25, 2007 · N462AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740345Channel · crackedHYDRAULIC PRESSURE TRANSDUCER HAT CHANNEL (PN 601R75262-159) CRACKED APPROX .2 INCH LONG IN LT MLG WHEEL WELL CEILING. MAINTENANCE REMOVED AND REPLACED CHANNEL PN 601R75262-159 IAW SRM 51-42-06. (K)Jun 25, 2007 · N462AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740349Angle · crackedFS 484.0 LT LBL 27.0, WL 71.0 TO 73.5 ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED CRACKED ANGLE AT FS 484.00, LBL 27.0 IAW REO 601R53-41-059. (K)Jun 25, 2007 · N463AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740355Angle · cracked2 EA, CRACKED ANGLES AT FS 280, LBL 9.0. MAINTENANCE REMOVED AND REPLACED ANGLES AT FS280, LBL 9 CRJ 200, SRM 51-42-21 AND BSC SR 601R-53-0057A. (K)Jun 25, 2007 · N463AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740356Angle · cracked(2) EA CRACKED ANGLES AT FS 280.0, RBL 9.0. MAINTENANCE REMOVED AND REPLACED ANGLES AT FS 280.00, RBL 9 IAW SRM AND BSC SR 601R-53-0057A. (K)Jun 25, 2007 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740352Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED APROX .7 INCH LONG IN AREA OF PULLEY BRACKET. MAINTENANCE CUT AWAY CRACKED SECTION OF DRAG ANGLE AND INSTALLED REPAIR ANGLE IAW REO 601R52-11-513, REV A. (K)Jun 24, 2007 · N463AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740322Unknown · unknownPASSENGER DOOR WILL NOT OPEN. (DISCOVERED AT GATE, WHEN TRYING TO DEPLANE PASSENGERS). PERFORMED OPERATIONAL CHECK OF PASSENGER DOOR, COULD NOT DUPLICATE MALFUNCTION IAW AMM 52-11-00. (K)Jun 24, 2007 · N470ZW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740338Channel · crackedCARGO DOOR FWD TRACK C-CHANNEL HAS A .5 INCH LONG CRACK WL. (K)Jun 24, 2007 · N462AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA200740339Floorbeam · crackedLT FS 484 ANGLE IS CRACKED AT LBL 36 AND 27 APPROX 1.4 INCH L. MAINTENANCE REPAIRED LT FS 484 IAW REO AND SRM. (K)Jun 24, 2007 · N462AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740340Floorbeam · crackedRT FS 484 ANGLE IS CRACKED AT RBL 27 AND 36 APPROX 1.4 INCH L. MAINTENANCE REPAIRED RT FS 484 ANGLES AT RBL 27 AND RBL 36 IAW REO 601R-53-41-059 AND BSC STANDARD REPAIR 601R-53-0030A. (K)Jun 24, 2007 · N462AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740344Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED JUST ABOVE ASSIST MOTOR PULLEY BRACKET. MAINTENANCE CUT OUT DAMAGED AREA AND INSTALLED REPAIR ANGLE IAW REO 601R-52-11-513. (K)Jun 24, 2007 · N462AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740357Actuator · inoperativeELEVATOR STIFF DURING FLIGHT CONTROL CHECK. REMOVED AND REPLACED PITCH FEEL LINEAR ACTUATOR NR 2, DUE LOW INPUT IMPEDANCE. (K)Jun 24, 2007 · N457AW · Cndair CL6002B19 · Elevator Tab Control SystemSDR CA070627002Carbon Seal · damaged(CAN) ON CLIMB OUT, CREW REPORTED NR 2 OIL PRESSURE WAS LOW AND FLUCTUATING BETWEEN 30-41 PSI. INTERMITTENTLY TRIGGERING THE LOW OIL WARNING. THE AIRCRAFT WAS DIVERTED AND LANDED NORMALLY. AT LOCATION, CONTRACT MAINTENANCE ADDED (4) QUARTS OF OIL AND A/C WAS Jun 24, 2007 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200740350Intercostal · crackedRT SIDE FS 621.00 TO 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. MAINTENANCE REMOVED AND REPLACED RT SIDE FS621.00 TO 625..00 INTERCOSTAL AT STR 14 R IAW CRJ 200 SRM 51-42-06. (K)Jun 23, 2007 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740351Intercostal · crackedLT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. MAINTENANCE REMOVED AND REPLACED LT SIDE FS 621.00 TO 625.00 INTERCOSTAL AT STR 14L IAW CRJ 200, SRM 51-42-06. (K)Jun 23, 2007 · N463AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740336Intercostal · crackedLT FS 625 OBLIQUE ANGLE IS CRACKED APPROX 1 INCH L. MAINTENANCE REMOVED AND REPLACED ANGLE IAW SRM 51-42-06, 51-42-21 AND REO 601R-53-61-422. (K)Jun 23, 2007 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740337Intercostal · crackedRT FS 625 OBLIQUE ANGLE IS CRACKED APPROX 1 INCH L. MAINTENANCE REMOVED AND REPLACED ANGLE IAW SRM 51-42-21 AND REO 601R-53-61-422. (K)Jun 23, 2007 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740324Bulkhead · crackedREAR PRESSURE BULKHEAD WEB AT RBL 9.5 NL 85.5 HAS AN INDICATION NOTED APPROX .5 INCHES IN LENGTH IN VERTICAL DIRECTION FAILED NDT INSPECTION. [07-31-07] MAINT REPAIRED REAR PRESSURE BULKHEAD WEB AT RBL 9.5, WL 85..5 BY CUTTING AWAY DAMAGE, FABBIN REPAIR PARJun 22, 2007 · N434AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA0706014Manifold · failedCREW REPORTED ON APPROACH A NOSE WHEEL STEERING INOP MESSAGE WAS DISPLAYED. CREW AS A PRECAUTION DECLARED AN EMERGENCY. CREW LANDED IN CLT WITHOUT INCIDENT AND WAS TOWED FROM THE TAXIWAY TO THE GATE. MAINTENANCE INSPECTED THE NOSE LANDING GEAR ASSEMBLY. MAJun 21, 2007 · N216PS · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA200740321Flap System · malfunctionedFLAP FAIL CAS CAUTION MESSAGE IN CRUISE FLIGHT. FLAPS FAILED AT ZERO. QRH COMPLIED WITH. BRAKE TEMPS INDICATE 4,4,5,6, COMPLIED WITH RESET PROCEDURE IAW SUPP 98-018B, STEPS 1.3 AND 1.4. FLAP SYSTEM RESET, OK. REMOVED AND REPLACED LT BPSU, OPS CHECK GOOD IJun 21, 2007 · N418AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0706011Ecu · failedCREW REPORTED ON APPROACH A FLAPS FAIL CAS MESSAGE AT 45 DEGREES. MAINTENANCE INSPECTED AND FOUND FECU BITE CHECK NOT WORKING AND RIGHT HAND BPSU RIG INDICATION ERRATIC. MAINTENANCE REMOVED AND REPLACED THE FECU IN ACCORDANCE WITH THE MAINTENANCE MANUAL 27-5Jun 20, 2007 · N249PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0706010Flap · malfunctionedCREW REPORTED ON APPROACH A FLAPS FAIL CAS MESSAGE AT 20 DEGREES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED A RESET OF THE SDU. MAINTENANCE INSPECTED FLAP LEFT HAND AND RIGHT HAND, NO SKEW NOTED IN ACCORDANCJun 20, 2007 · N249PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740332Connector · failed10TH STAGE ISO VALVE WILL NOT OPEN. REINSTALLED CONNECTOR ON 10TH STAGE VALVE, OPS CHECK GOOD, OK FOR SERVICE. (K)Jun 20, 2007 · N401AW · Cndair CL6002B19 · Pneumatic Distribution SystemSDR VNAA0706012Skin · damagedCREW REPORTED ON DESCENT A LIGHTNING STRIKE. MAINTENANCE COMPLIED WITH AN EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE INSPECTED AND FOUND EVIDENCE OF A STRIKE TO THE LOWER RIGHT FORWARD FUSELAGE. MAINTENANCE FOUND ALL DAMAGE TO BE WITHIN Jun 19, 2007 · N250PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200740325Drag Angle · crackedPAX DOOR AFT DRAG ANGLE HAS A CRACK APPROX 1 INCH LONG AT UPPER EDGE OF CABLE PULLEY BRACKET. [07-31-07] MAINTENANCE REPAIRED IAW REO 601R-52-11-513, STEPS 1-10. (K)Jun 19, 2007 · N460AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740326Drag Angle · crackedPAX DOOR AFT DRAG ANGLE HAS A CRACK APPROX .5 INCH LONG AT LOWER CORNER OF NR 2 STEP. MAINT REPAIRED IAW REO 601R-52-11-702. REV A STEPS 1 THRU 12. (K)Jun 19, 2007 · N460AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740327Skin · crackedAFTER REMOVING PAX DOOR TOP STEP 832DT FOR ACCESS FWD PAX DOOR FWD SIDE SKIN CRACKED APPROX .750 INCH L LOWER CORNER OF NR 2 STEP IN RADIUS. MAINTENANCE CUT AWAY DAMAGE FABBED REPAIR PARTS AND INSTALLED IAW REO 601R52-11-702, STEPS 1 THRU 12. (K)Jun 19, 2007 · N460AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740312Push-Pull Rod · out of positionPASSENGER DOOR WILL NOT OPEN/CLOSE FROM OUTSIDE. OPCV NORMAL FROM INSIDE. PLACARDED AND PLACED ON MEL. REPOSITIONED OUTER DOOR HANDLE PUSHPULL TUBES IAW CMM. OPS CHECK GOOD. REMOVED FROM MEL. (K)Jun 18, 2007 · N431AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740319Floorbeam · crackedFLOOR SUPPORT ANGLE AT FS 621, WL 73, RBL 27 - 45 IS CRACKED .5 INCH LONG. MAINTENANCE REPAIRED FS 621 ANGLE IAW REO 601R-53-61-117, REV C. (K)Jun 18, 2007 · N460AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740320Floorbeam · crackedFLOOR SUPPORT ANGLE AT FS 621, WL 73, LBL 27 - 45 IS CRACKED .5 INCHES LONG. MAINTENANCE REPAIRED FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117, REV C. (K)Jun 18, 2007 · N460AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740323Skin · crackedNLG AFT DOOR CUTOUT CRACKED IN LT AND RT RADIUS .5 INCH EACH SIDE. (K)Jun 18, 2007 · N434AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA2007410323Skin · crackedNLG AFT DOOR CUTOUT CRACKED IN LT AND RT RADIUS .5 INCH EACH SIDE. MAINTENANCE REPAIRED CRACKED AREAS IAW REO 601R53-11-010, REV C. (K)Jun 18, 2007 · N434AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
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