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"

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 VNAA0508032Skin · damagedRAMP EMPLOYEES REPORTED A TWO INCH SCRATCH ON THE FUSELAGE SKIN BELOW THE CARGO DOOR SILL PLATE. MAINTENANCE COMPLIED WITH A TEMP REPAIR IAW BOMBARDIER REO 601R-53-61-1510. THE AIRCRAFT WAS RELEASED FOR SERVICE.Aug 31, 2005 · N229PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA05751Rib · crackedDURING A C-CHECK IN MCN, THE RIGHT WHEEL WELL BATT RIB ASSY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT WHEEL WELL BATT RIB ASSY AT WS 53.60 IAW ASA EO 600-57-039A. (M)Aug 31, 2005 · N834AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR VNAA0508029Bpsu · failedDURING FINAL APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE REMOVED & REPLACED THE RT FLAP BRAKE AND POSITION SENSOR UNIT IAW CRJ200 AMM 27-51-10-400-801. OPERATIONAL CHECKS WERE GOOD. THE AIRCAug 29, 2005 · N218PS · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR VNAA0508031Fcu · malfunctionedDURING APPROACH WITH FLAPS 30 DEGREES THE FLAPS HALFSPEED STATUS MESSAGE ILLUMINATED. AT FLAPS 45DEGREES THE FLAPS FAIL MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE RESET THE FECU IAW CRJ200 SL-00-001. OPERATIONAL CHECKS WEAug 29, 2005 · N244PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0508028Fcu · malfunctionedDURING CRUISE FLIGHT WITH FLAPS AT 0 DEGREE THE FLAPS FAIL MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND PERFORMED A NO FLAP LANDING AT DESTINATION. MAINTENANCE INTERROGATED THE MDC, FECU, AND SDU. NO FAULTS WERE DISPLAYED. THE FLAP SYSTEM WAS RESET AAug 28, 2005 · N218PS · Cndair CL6002B19 · Flight Control SystemSDR VNAA0508026Valve · failedDURING CLIMBOUT WITH THE RT PACK DEFERRED PER MEL 21-51-01(C), THE LT PACK TEMP CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND RETURNED TO CLT. MAINTENANCE REMOVED & REPLACED THE DUAL POSITION VALVE IAW CRJ200 AMM 21-21-10-400-801. OPERATIONAL CAug 27, 2005 · N230PS · Cndair CL6002B19 · Cabin Cooling SystemSDR VNAA0508027Skin · crackedDURING THE INTERMEDIATE INSPECTION THE CREW DISCOVERED A CRACK AND DELAMINATION DAMAGE ON THE LEFT WINGLET TRAILING EDGE FAIRING. AFTER INSPECTION THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE PERFORMED A TEMPORARY REPAIR IAW BOMBARDIER REO 601R-57-31-668Aug 27, 2005 · N256PS · Cndair CL6002B19 · Wing, Plate/SkinSDR VNAA0508024Detector · failedON FINAL APPROACH THE CREW REPORTED A FLAPS FAIL MESSAGE AT 45 DEGREES. MAINTENANCE DETERMINED THAT THE SKEW DETECTION UNIT WAS INOPERATIVE. THE SKEW DETECTION SYSTEM WAS DEFERRED IAW CRJ200 MEL 27-51-03(C). THE AIRCRAFT WAS RELEASED FOR SERVICE. CAK MAINTAug 26, 2005 · N244PS · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR VNAA0508025Flap System · malfunctionedON DOWNWIND THE FLAPS FAIL MESSAGE ILLUMINATED WITH FLAPS AT 8 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED. MAINTENANCE RESET THE FECU IAW CRJ200 SL:00-001. FLAP SYSTEM OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Aug 26, 2005 · N218PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REX2005F00003Fcu · failed( REF NR: 05-104) FLAP FAILURE. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT (FECU) IAW AMM. (K)Aug 24, 2005 · N8524A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REX2005F00004Lever · failed( REF NR: 05-103) FLAP FAILURE ON TAXI OUT. REMOVED AND REPLACED FLAP HANDLE IAW AMM. (K)Aug 24, 2005 · N8696C · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0508016Radome · bird strikeAFTER LANDING INSPECTION REVEALED DAMAGE TO THE RADOME FROM A BIRD STRIKE. AFTER INSPECTION THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE REPLACED THE RADOME WITH A SERVICEABLE UNIT IAW CRJ200 AMM 53-81-01-000(400)-801. NO FURTHER DAMAGE WAS NOTED. THE Aug 24, 2005 · N226JS · Cndair CL6002B19 · Aerodynamic FairingsSDR REX2005F00006Control System · failed(REF NR: 05-101) FLAP FAILURE MESSAGE ON TAXI. RESET SYSTEM PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01. (K)Aug 23, 2005 · N8980A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0560463Screen · cloggedFLIGHT 5653 - LEFT ENGINE OIL PRESSURE WARNING, I.F.S.D. FOUND C-SUMP SCAVENGE PUMP INLET SCREEN CLOGGED. REPLACED SUMP SCREEN FITTING.Aug 23, 2005 · N868CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA0508015Detector · malfunctionedCLIMBING OUT OF DCA THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT AT IAD. MAINTENANCE RESET THE SKEW DETECTION UNIT, PERFORMED A BITE CHECK, AND OPERATIONALLY CHECKED THE FLAP CONTROL LEVER IAW CRJ200 AMM 2Aug 23, 2005 · N209PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR UG82005F00005Probe · damaged(REF CNTRL NR: PA05004) ALTITUDE SPLIT BETWEEN NR 1 AND NR 2 ALTIMETERS OF 250 FT AT 17,000 FT. THE RT PITOT/STATIC PROBE HAS IMPACT DAMAGE. (K)Aug 21, 2005 · N599DA · Cndair CL6002B16 · Pitot/Static SystemSDR A6WA200540292Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE CRAKED APPROX 1 INCH LONG ADJECENT TO DOOR ASSIST CABLE PULLEY BRACKET. CUT OUT DAMAGED AREA, PERFORMED EDDY CURRENT, FABED REPAIR ANGLE, SPLICES AND INSTALLED IAW EO. (K)Aug 21, 2005 · N466AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200540293Angle · crackedLT FS 625 OBLIQUE ANGLE CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. REPLACED ANGLE IAW SRM. (K)Aug 21, 2005 · N466AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REX2005F00010Fcu · failed(REF NR: 05-097) FLAP FAILURE AT 30, QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED FLAP ELECTRONIC UNIT (FECU) IAW AMM. (K)Aug 20, 2005 · N8506C · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA05680Step · 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. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Aug 20, 2005 · N850AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA05681Fitting · crackedDURING A C-CHECK, THE FITTING UNDER THE FLOOR AT FS 461, RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FITTING UNDER THE FLOOR AT FS 461, RBL 9. (K)Aug 20, 2005 · N839AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA05682Doubler · corrodedDURING A C-CHECK, THE DOUBLERS AT FS 422 TO FS446, RBL 34-44 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (K) MAINTENANCE REMOVED THE CORROSION ON TAug 20, 2005 · N839AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA05683Doubler · corrodedDURING A C-CHECK, THE DOUBLERS AT FS 427, LBL 34-44 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (K) S/D - MAINTENANCE REMOVED THE CORROSION ON THE DAug 20, 2005 · N839AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA05684Doubler · corrodedDURING C-CHECK, THE DOUBLER AT FS 470, RBL 34-44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (K) S/D - MAINTENANCE REMOVED THE CORROSION FROMAug 20, 2005 · N839AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA05685Doubler · corrodedDURING C-CHECK, THE DOUBLER AT FS 478, LBL 35-45 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (K) S/D - MAINTENANCE REMOVED THE CORROSION FROMAug 20, 2005 · N839AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA05686Doubler · corrodedDURING A C-CHECK, THE DOUBLERS AT FS 499 TO FS 516, LBL 44 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMNE THE APPROPRIATE CORRECTIVE ACTION. (K)Aug 20, 2005 · N839AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA05687Doubler · corrodedDURING A C-CHECK, THE DOUBLER AT FS 508, RBL 44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (K) S/D - MAINTENANCE REMOVED THE CORROSION FROM Aug 20, 2005 · N839AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA05759Handle · crackedDURING A C-CHECK IN MCN, THE AVIONICS BAY DOOR HANDLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AVIONICS BAY DOOR HANDLE. OPS CHECKS GOOD. (M)Aug 20, 2005 · N839AS · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR ASOA05688Finger Doubler · corrodedDURING C-CHECK, THE FINGER DOUBLERS AT FS439, LBL44, RBL44 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (K) S/D - MAINTENANCE REMOVED THE CORAug 20, 2005 · N839AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REX2005F00007Acm · overheated(REF NR: 05-100) AT GATE LT AIR CYCLE MACHINE (ACM) PACK OVERHEAT MESSAGE AND SMOKE NOTED IN COCKPIT. DEFERRED LT ACM IAW MEL. (K)Aug 19, 2005 · N8921B · Cndair CL6002B19 · Cabin Cooling SystemSDR REX2005F00008Control System · failed( REF NR 05-099) UPON CLIMBOUT, FLAPS FAIL WHEN SELECTED UP. DECLARED EMERGENCY, DIVERTED. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)Aug 19, 2005 · N8696C · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REX2005F00009Fcu · failed(REF NR: 05-098) FLAP FAILURE AT 0, QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED FLAP ELECTRONIC UNIT (FECU) IAW AMM. (K)Aug 19, 2005 · N8524A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA050825004Window · cracked(CAN) RT SIDE WINDOW CRACKED IN FLIGHT. A/C LANDED. A/C FERRIED FOR WINDOW REPLACMENT. WINDOW REMOVED AND INSTALLED = P/N NP139322-12, S/N 05200H6110.Aug 19, 2005 · Cndair CL6002B19 · Flight Compartment WindowsSDR ASOA05673Engine · malfunctionedFLT 4534 - DURING CRUISE FROM ATL-SBN, THE CREW RECEIVED A LOW OIL PRESSURE WARNING ON THE RIGHT ENGINE. THE QRH WAS COMPLIED WITH AND THE RIGHT ENGINE WAS REDUCED TO IDLE FOR THE REMAINDER OF THE FLIGHT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TAug 19, 2005 · N851AS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR ASOA05678Floor Support · corrodedDURING A C-CHECK, THE RT FLOOR SUPPORT WEB AT FS 559.112 TO FS 605 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL DETERMNE THE APPROPRIATE REPAIR UPON FURTHER INSPECTION ON THE RT FLOOR SUPPORT WEB AT FS 559.112 TO FS 605. THIS MRR WILL REMAIN OPENAug 19, 2005 · N839AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05679Web · corrodedDURING A C-CHECK, THE LT FLOOR ATTACH WEB AT FS 559.80 TO 574 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL DETERMNE THE APPROPRIATE REPAIR UPON FURTHER INSPECTION ON THE LT FLOOR WEB AT FS 559.80 TO FS 574.Aug 19, 2005 · N839AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05679SWeb · corrodedDURING A C-CHECK, THE LT FLOOR ATTACH WEB AT FS 559.80 TO FS 574 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED THE CORROSION ON THE LT FLOOR ATTACH WEB AT FS 559.80 TO FS 574 BY COMPLYING WITHAug 19, 2005 · N839AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA05678SFloor Support · corrodedDURING C-CHECK, THE RT FLOOR SUPPORT WEB AT FS 559.112 TO FS 605 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED THE CORROSION ON THE RT FLOOR SUPPORT WEB AT FS 559.112 TO FS 605 BY COMPLYING WITH EO. (K)Aug 19, 2005 · N839AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540290Selector Valve · inoperativeON APPROACH, WHEN SELECTED GEAR DOWN GOR (GEAR DISAGREE AND NOSE DOOR) MASTER WARNING. NLG INDICATED UP AND LOCKED MLG DOWN. CYCLED GEAR WITH SAME INDICATIONS. PERFORMED QRH AND OBTAINED 3 GREEN. REMOVED AND REPLACED NLG SELECTOR VALVE AMM. OPS CHECK GOODAug 18, 2005 · N414ZW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR VNAA0508011Flap System · malfunctionedTHE FLAPS FAIL CAUTION MESSAGE ILLUMINATED ON APPROACH. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED AIRCRAFT POWER. THE FLAP SYSTEM OPERATIONALLY CHECKED GOOD IAW CRJ200 AMM 27-54-00-710-801. THE AIRCRAFT WAS RELEASED FOR SERVAug 18, 2005 · N218PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200540286Skin · lightning strikeFUSELAGE SKIN HAS SUSTAINED LIGHTNING STRIKE DAMAGE AT FS 654.5 BETWEEN STR 26R AND 27R. REPAIRED DAMAGED AREA BY INSTALLING AN EXTERNAL DOUBLER AT FS 654.5 BETWEEN STR 26R AND 27R IAW EO AND SRM. (K)Aug 16, 2005 · N465AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200540284Indicator · inoperativeTAKEOFF ABORTED DUE TO STANDBY AIRSPEED INDICATION READING ZERO AT 80 KNOTS. TAKEOFF ABORTED AT 90 KNOTS, BRAKE TEMPS 8,8,6,5, NORMAL BRAKING. REMOVED AND REPLACED STANDBY AIRSPEED INDICATOR. (K)Aug 16, 2005 · N459AW · Cndair CL6002B19 · Airspeed/Mach IndicatorSDR MASA200500645Engine · shutdownASH 6373 DSM - CREW SHUTDOWN THE NR 1 ENG DECLARED AN EMERGENCY AND RTF FOR THE 14TH STAGE DUCT WARNING, WITH THE SYSTEM TURNED OFF. MX OPS CHECK SYSTEM WITH ENGINE RUN UP AND NO FURTHER MSG NOTED.Aug 15, 2005 · N27318 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA0508010Warning Light · illuminatedDURING TAKEOFF ROLL CONFIG AILERON WARNING MESSAGES ILLUMINATED AND SOUNDED. THE CREW PERFORMED A REJECTED TAKEOFF. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE AILERON TRIM SYSTEM IAW CRJ200 AMM 27-11-00-710-801 AND A REJECTED TAKEOFF INSPECTION IAW CRAug 10, 2005 · N220PS · Cndair CL6002B19 · Aileron Control SystemSDR VNAA0508009Skin · lightning strikeAFTER LANDING THE CREW REPORTED POSSIBLE LIGHTNING DAMAGE ON THE LEFT WINGLET TRAILING EDGE. MAINTENANCE COMPLIED WITH EN ROUTE & DETAILED LIGHTNING STRIKE INSPECTIONS IAW CRJ200 AMM 05-51-05-210-801, AMM 05-51-05-220-801, AND AMM 05-51-05-220-803. THE LT WIAug 10, 2005 · N229PS · Cndair CL6002B19 · Wing, Plate/SkinSDR REX2005F00011Control System · failed(REF NR: 05-096) FLAPS FAILED AT 20 WHEN SELECTED TO 30 ON APPROACH. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)Aug 10, 2005 · N8505Q · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA050909002Windshield · cracked(CAN) PILOT'S WINDSHIELD CRACKED AFTER LANDING.Aug 10, 2005 · Cndair CL6002B19 · Flight Compartment WindowsSDR VTZA200500143Line · leakingLT ENG OIL PRESSURE WARNING, PRESS FLUXUATION IN FLIGHT DOWN TO 19-22 PSI IN-FLIGHT ENGINE SHUTDOWN. C SUMP SCAVENGE LINES LEAKING - REPLACED LINES,OIL FILTER, INSPECTED CHIP DETECTOR.Aug 8, 2005 · N655BR · Cndair CL6002B19 · Turbine Engine Oil SystemSDR ASOA05660Engine · overservicedDURING CRUISE, AT APPROX 28,000 FEET, RT ENGINE OIL TEMP INDICATED IN YELLOW RANGE AT APPROX 160 DEGREES C, THEN INCREASED INTO RED RANGE INDICATING A HIGH OF 165 DEGREES C WITH RT ENGINE OIL PRESSURE INDICATING 44-50 PSI. CREW COMPLIED WITH THE QRH AND REDUCAug 8, 2005 · N871AS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA051011003Landing Gear · malfunctioned(CAN) UPON SELECTING THE LDG DOWN, THE NLG DID NOT COME DOWN AND A (GEAR DISAGREE) MESSAGE FOLLOWED. QRH FOLLOWED, NLG FINALLY EXTENDED. AN UNEVENTFUL LANDING FOLLOWED. NUMEROUS TROUBLESHOOTING STEPS WERE PERFORMED DURING THE TROUBLESHOOTING PERIOD THAT FOLAug 8, 2005 · Cndair CL6002B19 · Landing Gear Retraction/Extension System
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