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 A6WA200640411Pushrod · out of adjustPASSENGER BOARDING DOOR WILL NOT OPEN FROM OUTSIDE, THE HANDLE WILL NOT TURN. ADJUSTED PUSHROD ASSY BETWEEN PIVOT LEVER ROLL LATCH TORQUE TUBE, OPS CHECK GOOD IAW AMM. (K)Dec 6, 2006 · N422AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA061206004Flap System · malfunctioned(CAN) (FIRST FLIGHT OF DAY, AIRCRAFT HAD BEEN OUTSIDE ON GATE OVERNIGHT, OAT AT -20DEG OR LOWER) DURING TAXI FROM GATE UPON SELECTING FLAP TO 8DEG POSITION, (FLAPS FAIL) MESSAGE AND FLAPS FAILED TO EXTEND. AIRCRAFT RETURNED TO GATE. FLAP CIRCUIT BREAKER RE-SETDec 6, 2006 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200640403Sensor · failedMESSAGE DURING FLAP RETRACTION ON CLIMBOUT, FLAP FAIL AT ZERO. FOUND LT BRAKE POSITION SENSOR UNIT HARD FAILED. REPLACED BPSU IAW AMM 27-51-10. FLAPS CHECK GOOD. (K)Dec 4, 2006 · N465AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA061205004Flap System · malfunctioned(CAN) THE CREW REPORTED THAT ON APPROACH THEY RECEIVED THE (FLAP FAIL) CAUTION MESSAGE. ON APPROACH INTO. CIRCUIT BREAKER RESET OF 1F4 AND 2F4 THE FLAPS RETURNED TO NORMAL FOR FLIGHT CONDITION. UPON ARRIVAL THE FLAPS WERE AT 0 DEGREES AND INSPECTED FOR BINDINDec 4, 2006 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200640400Unknown · unknownCLIMBING OUT AT 5000 FT FLAPS AT ZERO, FLAP FAIL AMBER CAUTION CAS MESSAGE, CW QRH. PERFORMED ZERO FLAP LANDING, APPLIED BRAKES AT 80 KNOTS, MAX BTMS READING WAS 3. NORMAL LANDING WEIGHT. PERFORMED INSPECTION IAW AWAC SUPPLEMENT 98-18, NO EVIDENCE OF TWISTIDec 3, 2006 · N428AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA061206003Blades · damaged(CAN) UNUSUAL NOISE AND VIBRATION FROM LT ENGINE. FOUND FAN BLADES NRS: 8,9,10,11,22,23,24 AND 25 BENT AND DAMAGED. AIRFRAME HOURS=5306:19. CYCLES=3929. (TC NR 20061206003)Dec 2, 2006 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR A6WA200640399Isolation Valve · leakingCARGO BOTTLE LOW MASTER CAUTION MESSAGE ILLUMINATED. REMOVED AND REPLACED LT CARGO FIRE BOTTLE, FOUND BOTTLE WAS THERMALLY DISCHARGED, CAUSED BY A LEAK ON THE 10TH STAGE ISOLATION VALVE CLAMP, TIGHTENED CLAMPS, NO LEAKS, REF AMM. (K)Dec 1, 2006 · N447AW · Cndair CL6002B19 · Extinguishing SystemSDR CA061205003Bpsu · out of rig(CAN) ON APPROACH THE CREW REPORTED THAT THE FLAPS WERE FAILED AT 4 DEGREES. THE AIRCRAFT WAS FERRIED WITH THE FLAPS AT 4 DEGREES. LINE MAINTENANCE COMPLETED TASK 27-51-10-830-801( RIGGING OF THE BPSU`S). BOTH WERE FOUND OUT OF RIG ALSO THE NR 7 DFECU POTENTIODec 1, 2006 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA061205007Flap System · malfunctioned(CAN) DURING APPROACH WHEN FLAPS SELECTED, FLAPS REMAINED RETRACTED (0 DEG). AIRCRAFT DID FLAPLESS LANDING. ON GROUND FLAP CIRCUIT BREAKER RE-SET CARRIED OUT, FLAPS FUNCTIONED NORMALLY. AIRCRAFT DEPARTED FOR MAINTENANCE BASE FOR ADDITIONAL INSPECTIONS (TC NR 2Dec 1, 2006 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0611038Carbon Seal · damagedCREW REPORTED A RIGHT ENGINE LOW OIL PRESSURE MESSAGE ON CLIMBOUT. CREW RETURNED TO ATL WITHOUT INCIDENT. MAINTENANCE INSPECTED AND SERVICED THE ENGINE OIL. MAINTENANCE ALSO FOUND DAMAGED THE ENGINE CARBON SEAL. MAINTENANCE REMOVED AND REPLACED THE DAMAGEDNov 28, 2006 · N202PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200640393Idg · failedDURING TAKEOFF IDG CAUTION MESSAGE FOLLOWED BY GEN NR 2 CAUTION MESSAGE, ABORTED TAKEOFF. REMOVED AND REPLACED IDG NR 2 IAW AMM. OPS CHECK GOOD. (K)Nov 28, 2006 · N411ZW · Cndair CL6002B19 · Alternator-Generator DriveSDR A6WA200640392Shutoff Valve · malfunctionedON TAKEOFF ROLL CAUTION MESSAGE FOR LT AND RT HIGH PACK PRESSURE, ABORT TAKEOFF. C/W QRH. RAN UP 2ND TIME AND BOTH HI PRESS CAUTION MESSAGE AGAIN. REMOVED AND REPLACED BOTH PRSOV VALVES IAW AMM, OPS CHECK GOOD. REMOVED PN 32156222, RT SN 1319 (TT 9618 HRS)Nov 27, 2006 · N414ZW · Cndair CL6002B19 · Cabin Cooling SystemSDR VNAA0611035Oil System · fluctuatesCREW REPORTED THE NR 2 ENGINE OIL PRESSURE INDICATION FLUCTUATED ON CLIMBOUT. CREW RETURNED TO MEM WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. MAINTENANCE ALSO SERVICED ENGINE OIL. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RNov 26, 2006 · N202PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA061127003Rib · chafed(CAN) IN LEFT HAND WING TANK INBOARD BAY, STEAL BRAIDED FUEL LINE PART NUMBER 00624-AE7013343N0220 WAS FOUND CHAFING ON THE WING RIB STIFFENER PART NUMBER 600-10221-1. CHAFING OCCURRED APPROXIMATELY 9 1/2 INCHES FROM BOTTOM OF TANK. DAMAGE EXTENDS OVER AN AREANov 23, 2006 · Cndair CL6002B19 · Wing, Rib/BulkheadSDR CA061124003Flap System · malfunctioned(CAN) DURING APPROACH UPON INITIAL FLAP DOWN SELECTION, FLAP FAILED TO MOVE AND CREW RECEIVED (FLAP FAIL) MESSAGE ON EIACS. APPROACH CONTINUED AND NORMAL FLAPLESS LANDING CARRIED OUT. MAINTENANCE INSPECTION CARRIED OUT, NO EVIDENCE OF TWISTING, SKEWING OR DEFONov 23, 2006 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200640390Control Unit · unknownSTAB CHANNEL 1 INOP STATUS MESSAGE IN FLIGHT, COULD NOT RESET. AIR RETURN TO DEPARTURE. REMOVED AND RETURNED HSTCU IAW AMM 27-41-01. OPS CHECK GOOD. (K)Nov 22, 2006 · N462AW · Cndair CL6002B19 · Stabilizer Control SystemSDR A6WA200640391Coffeemaker · odorCOFFEEMAKER HAS BURNING SMELL WHEN BREWING. NO SMELL WHEN OFF. PULLED AND COLLARED COFFEEMAKER CIRCUIT BREAKER. PLACARDED AND PLACED ON MEL. REMOVED AND REPLACED COFFEEMAKER IAW AMM. OPS CHECK NORMAL. REMOVED PLACARD AND MEL. (K)Nov 22, 2006 · N2530 · Cndair CL6002B19 · Buffet/GalleysSDR CA061122008Flap System · jammed(CAN) DURING MISSED APPROACH WHEN FLAP RETRACTION SELECTED, FLAPS REMAINED AT FULL 45DEG EXTENSION. CREW RECEIVED FLAP FAIL MESSAGE. DUE TO WEATHER CONDITIONS AIRCRAFT DIVERTED TO ALTERNATE AIRPORT WITH FLAPS REMAINING EXTENDED AT 45DEG. IN-FLIGHT FLAP RE-SET Nov 21, 2006 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200640389Coalescer Bag · dirtyDURING POST DE-ICING RUN UP, RECEIVED LAV SMOKE MESSAGE. COMP;IED WITH QRH AND MESSAGE CLEARED. PERFOMED LAV SMOKE DE4TECTOR TEST IAW AMM. OPPS CHECKED GOOD. REMOVED AND REPLACED COALESCER BAGS IAW AMM, OPS CHECK GOOD. NO MESSAGE OR SMOKE SMELL FOUND. (KNov 21, 2006 · N440AW · Cndair CL6002B19 · Humidity Control SystemSDR CA061212009Flap System · malfunctioned(CAN) ON APPROACH WHEN FLAPS SELECTED, (FLAP FAIL) MESSAGE AND FLAPS REMAINED AT ZERO DEG., FLAPLESS LANDING. ON GROUND FLAP CIRCUIT BREAKERS RESET PROCEDURE CARRIED OUT, FLAPS FUNCTION CHECKED NORMAL. (TC NR 20061212009)Nov 21, 2006 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200640388Door Seal · unknownSERVICE DOOR DIFFICULT TO LATCH AND UNLATCH. REMOVED AND REPLACED SERVICE DOOR SEAL IAW 52-41-07. (K)Nov 19, 2006 · N441ZW · Cndair CL6002B19 · Service DoorsSDR REXA200600102Warning Message · illuminatedRECEIVED FLAP FAIL MESSAGE WHEN SELECTED TO 30. RESET SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD 2006-12-21.Nov 16, 2006 · N813AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0611026A/C Pack · malfunctionedCREW REPORTED A RIGHT HAND PACK OVER PRESSURE INDICATION ON TAKEOFF. CREW RETURNED TO MGM WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. MAINTENANCE PERFORMED OPERATIONAL CHECKS AND OPS CHECKED GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.Nov 16, 2006 · N209PS · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200640387Recorder · malfunctionedWOW OUTPUT CAUTION IN FLIGHT, AS WELL AS WOW OUTPUT CAUTION PROX SYSTEM FAULT, WOW OUTPUT FAIL. REMOVED AND REPLACED CVR IAW AMM 23-71-01, OPS CHECK GOOD AT THIS TIME PERFORMED TEST OF PSEU IAW AMM. OPS CHECK GOOD. CRV FIXED THE PSEU AND WOW PROBLEM. (K)Nov 16, 2006 · N445AW · Cndair CL6002B19 · Data Recorders (Flight/Maintenance)SDR VNAA0611025Skin · damagedCREW REPORTED A LIGHTNING STRIKE. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE RIGHT HAND HORIZONTAL STABILIZER TIP. MAINTENANCE REPAIRED ALL DAMAGE. AIRCRAFT WAS RELEASED FOR SERVICE.Nov 15, 2006 · N256PS · Cndair CL6002B19 · Horizontal Stabilizer, Plate/SkinSDR ATWA200640386Carbon Seal · leakingON CLIMBOUT, ENGINE NR 1 LOW OIL PRESSURE WARNING, AT FLIGHT IDLE OIL PRESSURE AT 45 PSI. TEMP 84. AIRCRAFT DIVERTED. DURING CONSUMPTION TEST, FOUND ENGINE NR 1 AXIS F HYDRAULIC PUMP CARBON SEAL LEAKING. REPLACED AXIS (F) CARBON SEAL AND MATING RING IAW MMNov 15, 2006 · N459AW · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR A6WA200640385Fire Bottle · dischargedDURING SERVICE CHECK, FOUND ENGINE FIRE BOTTLES NR 1 AND NR 2 DISCHARGED. REMOVED AND REPLACED FIRE BOTTLES NR 1 AND NR 2 IAW CRJ 26-21-07. OPS CHECK GOOD. (K)Nov 14, 2006 · N454AW · Cndair CL6002B19 · Fire Bottle, FixedSDR VNAA0611019Warning Light · false activationCREW REPORTED A FLAPS FAIL CAS MESSAGE AFTER TAKEOFF. CREW DIVERTED AND LANDED IN ILM WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS NOTED AND OPS CHECKED GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.Nov 13, 2006 · N254PS · Cndair CL6002B19 · Central WarningSDR VNAA0611018Control Unit · failedCREW REPORTED AN ANTI-ICE DUCT MESSAGE ON TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE LT BLEED CONTROL UNIT. MAINTENANCE PERFORMED OPERATIONAL CHECKS AND OPS CHECKED GOOD. AIRNov 13, 2006 · N244PS · Cndair CL6002B19 · Engine Bleed Air SystemSDR CA061117006Apu · overserviced(CAN) APPROXIMATELY 10 MINUTES FROM DESTINATION, AIRCRAFT DECLARED AN EMERGENCY DUE TO SMOKE IN THE LAVATORY. AIRCRAFT WAS DESCENDING THROUGH 5,000 FT WHEN THE BLEEDS WERE SWITCHED FROM ENGINES TO APU. WITHIN A SHORT PERIOD OF TIME A BURNT OIL SMELL WAS OBSERVNov 13, 2006 · Cndair CL6002B19 · APU Oil SystemSDR A6WA200640382Pitot Tube · fodSMOKE ODOR IN COCKPIT AFTER ENGINE SHUTDOWN AND LEAVING AIRCRAFT CHECKLIST WITH BATTERY MASTER ON. INSPECTED PITOT SYS FOUND FOD IN RT PITOT TUBE REMOVED AND REPLACED RT PITOT TUBE RUN PITOT STATIC LEAK CHECK, NO LEAKS FOUND, SYSTEM CHECKS NORMAL. (K)Nov 13, 2006 · N428AW · Cndair CL6002B19 · Pitot/Static SystemSDR VNAA0611017Warning Message · false activationCREW REPORTED A CARGO DOOR EICAS MESSAGE ON CLIMBOUT. AIRCRAFT RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RE-SECURED THE CARGO DOOR LATCH. MAINTENANCE PERFORMED OPERATIONAL CHECKS AND FOUND NO DEFECTS. AIRCRAFT WAS RELEASED FOR SERVICE.Nov 12, 2006 · N261PS · Cndair CL6002B19 · Central WarningSDR A6WA200640380Windshield · delaminatedRT WINDSHIELD HEAT MESSAGE, FOLLOWED BY RT WINDSHIELD DELAMINATION. REMOVED AND REPLACED RT WINDSHIELD ASSY IAW AMM. (K)Nov 10, 2006 · N406AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200640381Manifold · inoperativeSTEERING INOP DURING TAXI. REMOVED AND REPLACED NOSEWHEEL STEERING SERVO MANIFOLD AMM. OPS AND LEAK CHECK GOOD. (K)Nov 10, 2006 · N404AW · Cndair CL6002B19 · Landing Gear Steering SystemSDR CA061116001Window · cracked(CAN) AIRPLANE DIVERTED FOUND: RT SIDE-WINDOW CRACKED. RT SIDE WINDOW REMOVED ACC.AMM. RT SIDEWINDOW INSTALLED ACC AMM 56-12-01-400-801. CABIN PRESS TEST PERF,. OKNov 9, 2006 · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200640379Window · failedF/O WINDOW SHATTERED. REMOVED AND REPLACED F/O SIDE WINDOW IAW AMM. OPS CHECK AND LEAK CHECK GOOD. (K)Nov 7, 2006 · N428AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200640401Wire · looseENROUTE, SPARKS OBSERVED COMING FROM F/O`S YOKE MAP LIGHT. CB2U6 POPPED. LOOSE CONNECTION ON F/O`S MAP LIGHT FOUND. RESECURED LOOSE CONNECTION. OPS CHECK GOOD IAW 33-13-13. (K)Nov 7, 2006 · N440AW · Cndair CL6002B19 · Flight Compartment LightingSDR TRAX200600998Attach Fitting · crackedRT BL 8 AND 10 280 ATTACH CLIPS CRACKED. S/D REPAIRED DAMAGE TO RT BL 8 AND 10 280 ATTACH CLIPS BY FABRICATING NEW CLIPS IAW EO 600-53-90.Nov 6, 2006 · N867AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR TRAX200600999Frame · crackedTHE 280 FRAME CRACKED AT BL 12 RT, LOWER LEG. REPAIRED 280 FRAME AT BL 12 RT LOWER LEG IAW EO 600-53-0090.Nov 6, 2006 · N867AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA200617372Bulb · failedRT AFT EMERGENCY LIGHT INOP. REPLACED BULB FOR EMERGENCY LIGHT.Nov 4, 2006 · N963SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200617376Connector · shortedLT LOWER EMERGENCY EXIT ROW LIGHT AND ASSOCIATED FLOOR STRIP LIGHT OUT. FOUND MOISTURE IN LIGHT STRIP. DRIED AND APPLIED SEALER TO CONNECTORS. OPS CHECKS GOOD IAW MM 33-51-00.Nov 4, 2006 · N866AS · Cndair CL6002B19 · Emergency LightingSDR VNAA0611011Warning Light · false activationCREW REPORTED AN APU OIL TEMP CAUTION MESSAGE IN FLIGHT. CREW PERFORMED AN UNSCHEDULED LANDING IN CMH WITHOUT INCIDENT. MAINTENANCE INSPECTED AND SERVICED THE APU OIL LEVEL. OPERATIONAL CHECKS WERE PERFORMED AND NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR Nov 4, 2006 · N220PS · Cndair CL6002B19 · Central WarningSDR CA061201006Flap System · malfunctioned(CAN) DURING APPROACH WHEN FLAPS SELECTED TO 45 DEG , FLAPS REMAINED AT 30DEG AND (FLAP FAIL) MESSAGE ON EICAS, CONTINUED APPROACH AND NORMAL LANDING WITH FLAPS AT 30 DEG EXTENSION. MAINTENANCE CLEANED AND LUBRICATED FLAP DRIVE SHAFTS, FLAP ACTUATORS GREASED/Nov 4, 2006 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR TRAX200600981Sign · unsecureEXIT SIGN ABOVE SERVICE DOOR UNSECURE AND INOPERATIVE.Nov 3, 2006 · N841AS · Cndair CL6002B19 · Emergency LightingSDR CA061107002Bolt · unsecure(CAN) AFT ENGINE MOUNT THRUST FITTING ATTACHMENT BOLTS ARE NOT SECURED (TORQUE IS UNKNOWN AND LOCKWIRE IS NOT INSTALLED) AT RH ENGINE. TO COMPLETE THE PROCEDURE IAW AMM 71-22-01 ENGINE TO BE REMOVED. (TC# 20061107002)Nov 3, 2006 · Cndair CL6002B19 · Engine Mount SectionSDR TRAX200600982Flap System · failedFLAPS FAIL MSG. FLAPS WOULD NOT EXTEND. (EMERGENCY DECLARED)Nov 2, 2006 · N931EV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200617363Window · crackedRT SIDE WINDOW CENTER PANE CRACKED. REPLACED RT SIDE WINDOW IAW CRJ MM 56-12-01 TO RII 56-220-1000, PN OFF: NP-139322-001 SN OFF: 03080H9298.Nov 1, 2006 · N954SW · Cndair CL6002B19 · Flight Compartment WindowsSDR CA061201007Flap System · malfunctioned(CAN) DURING APPROACH FLAPS 20DEG SELECTED AND FLAPS AT 20DEG, WHEN 30DEG SELECTED FLAPS REMAINED AT 20DEG. NORMAL LANDING WITH FLAPS AT 20DEG. MAINTENANCE UNABLE TO DUPLICATE FAULT ON GROUND. AIRCRAFT FERRIED TO MAINTENANCE BASE. MAINTENANCE CARRIED OUT TORQUNov 1, 2006 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA061102001Windshield · cracked(CAN) LT WINDSHIELD REMOVED AND REPLACED ACC AMM TASK 56-11-01-000-801. (TC# 20061102001)Oct 29, 2006 · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA0610043Fan Blade · damagedCREW REPORTED THAT THE NR 2 ENGINE FAN BLADES NEED INSPECTION. MAINTENANCE INSPECTED AND FOUND DAMAGE TO SEVERAL BLADES. MAINTENANCE REMOVED AND REPLACED FOUR DAMAGED BLADES. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.Oct 28, 2006 · N245PS · Cndair CL6002B19 · Turbine Engine Compressor Section
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