# Service difficulty reports: GE CF34-3B1

A list on [GE CF34-3B1](https://openairdocs.org/engine/ge-cf34-3b1.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 109 · 5,402 reports

- [SDR SWIA2026101977789](https://openairdocs.org/sdr/SWIA2026101977789.md): Elec Connector · faulted · Oct 19, 2026 · N916SW · Cndair CL6002B19 · Engine Indicating System Wiring
  > WHEN CLIMBING AFTER TAKE OFF, LEFT ENGINE N1 FLUCTUATED UP TO 5 WHEN ADDING MORE THRUST IT REDUCED THRUST AND CAUSED YAWING AND ROLLING ONCE WE DECLARED THE EMERGENCY AND PULL THE THRUST, N1 STABILIZED UNTIL LANDING FLIGHT 5470. TROUBLESHOT IAW FIM 76-10-00
- [SDR A6WA202609018913](https://openairdocs.org/sdr/A6WA202609018913.md): Fire Warning · activated · Sep 6, 2026 · N464AW · Cndair CL6002B19 · Detection System
  > LEFT FIRE WARNING AND THEN AFTER LANDING C/W IAC FOR LT ENGINE FIRE INDICATION DID NOT GO OUT AFTER 10 SECONDS PER IAC BOTH LT ENGINE BOTTLES DEPLOYED NO VISIBLE FIRE NOTED EMERGENCY WAS DECLARED. AIRCRAFT REMOVED FROM SERVICE.
- [SDR A6WA202609028910](https://openairdocs.org/sdr/A6WA202609028910.md): Heat Exchanger · faulted · Sep 2, 2026 · N420AW · Cndair CL6002B19 · Engine Oil Cooler
  > DURING CLIMB NR 2 ENG OIL TEMP REACHED 150'C. C/W QRH -PULLED PWR BACK AND REDUCED PWR. ENG OIL TEMP RETURNED TO NORMAL OPERATING RANGE. NR 2 ENG OIL TEMP CONSTANTLY 20' HOTTER THAN NR 1. MC- ON GRD @ IDLE READS 10-15' HOTTER THAN NR 1. AIRCRAFT REMOVED FROM
- [SDR SWIA2026080276712](https://openairdocs.org/sdr/SWIA2026080276712.md): Pump · failed · Aug 2, 2026 · N463SW · Cndair CL6002B19 · Engine Fuel Pump
  > NR 2 ENGINE WOUND BACK TO IDLE, PASSING FL190. SHUTDOWN AND RESTARTED. THRUST LEVER MOVEMENTS MADE NO CHANGE IN ENGINE INDICATIONS. VIBES NORMAL, TS & PS NORMAL. COMPLETED CHK LIST ACTIONS, BALANCED FUEL, & LANDED, NO FURTHER ISSUES. (FLT 6064). TROUBLESHOT
- [SDR A6WA202607128900](https://openairdocs.org/sdr/A6WA202607128900.md): Heat Exchanger · faulted · Jul 11, 2026 · N459AW · Cndair CL6002B19 · Engine Oil Indicating System
  > DURING CLIMB-OUT AT CLIMB POWER NR 2 ENGINE OIL TEMP WAS 150 DEG AND SLOWLY CLIMBING. IT RETURNED TO THE GREEN WHEN POWER WAS RETARDED. RTN TO AZA. AIRCRAFT REMOVED FROM SERVICE. R & R RT ENGINE HEAT EXCHANGER IAW AMM 79-21-07 OPS CHECK GOOD LEAK CHECK GOOD
- [SDR A6WA202604138885](https://openairdocs.org/sdr/A6WA202604138885.md): Oil System · low pressure · Apr 13, 2026 · N442AW · Cndair CL6002B19 · Engine Oil Pressure
  > RECEIVED RIGHT ENGINE OIL PRESSURE WARNING AT 1000 FEET ON FINAL FULLY CONFIGURED OIL PRESSURE WAS APPROX. 30-35PSI AT 83% N2 PULLED RH ENGINE TO IDLE OIL PRESSURE REMAINED 30-35PSI, NO EXCEEDANCE IN MDC. AIRCRAFT REMOVED FROM SERVICE. REF W/O 347513 FOR R&R
- [SDR FSEA2026020960005](https://openairdocs.org/sdr/FSEA2026020960005.md): Engine · shutdown · Feb 7, 2026 · N510SJ · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > ON 2/7 N510SJ HAD THE #2 ENGINE SHUT DOWN ON APPROACH INTO GYR WHEN THEY BROUGHT THE POWER LEVERS BACK TO FLIGHT IDLE. THEY DECLARED AN EMERGENCY AND DIVERTED INTO PHX AND LANDED WITHOUT FURTHER INCIDENT.
- [SDR SWI2026F00077](https://openairdocs.org/sdr/SWI2026F00077.md): Engine · malfunctioned · Jan 13, 2026 · N464SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > NUMBER 1 ENGINE STUCK AT 70% N1 WITH THRUST LEVER AT IDLE. ENGINE 1 INDICATED MCT DURING THIS TIME. NO CAUTION MESSAGE, NO WARNING MESSAGE. WE CYCLED THE THRUST LEVER BY MOVING IT FORWARD AND BACK TO UNBIND THE THRUST LEVER CABLE. I DID NOT FEEL ANY BINDING OR
- [SDR SWI2026F00086](https://openairdocs.org/sdr/SWI2026F00086.md): Fuel Control · broken · Jan 13, 2026 · N464SW · Cndair CL6002B19 · Fuel Control/Turbine Engines
  > NUMBER 1 ENGINE STUCK AT 70% N1 WITH THRUST LEVER AT IDLE. ENGINE 1 INDICATED MCT DURING THIS TIME. NO CAUTION MESSAGE, NO WARNING MESSAGE. WE CYCLED THE THRUST LEVER BY MOVING IT FORWARD AND BACK TO UNBIND THE THRUST LEVER CABLE. I DID NOT FEEL ANY BINDING OR
- [SDR SWIA202601080007](https://openairdocs.org/sdr/SWIA202601080007.md): Engine · failed · Jan 7, 2026 · N461SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > NUMBER 2 ENGINE FAILED AT CRUISE. HEARD A LOUD POPPING NOISE AND THE GAUGES ALL ROLLED BACK ON THE NUMBER 2. RAN QRC, QRH EMERGENCY AND ABNORMAL PROCEDURES. (FLIGHT 5584) OPEN
- [SDR SWIA2025110600001](https://openairdocs.org/sdr/SWIA2025110600001.md): Engine · dirty · Nov 1, 2025 · N477CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > AT NEXT MX OVERNIGHT, DUE TO ODI EVENT, TROUBLESHOOT L JET OVHT FAIL CAUTION MESSAGE AND L JETPIPE OVHT WARNING MESSAGE ON CLIMBOUT. DO NOT CARRY FORWARD WITHOUT APPROVAL FROM MCC. TROUBLESHOT WRITE UP FOR CABIN SMOKE AND OR ELECTRICAL BURNING ODOR IAW FIM 2
- [SDR SWIA2025091800017](https://openairdocs.org/sdr/SWIA2025091800017.md): Bleed Valve · warning message · Sep 17, 2025 · N218PS · Cndair CL6002B19 · Compressor Bleed Valve
  > R 14TH STAGE BLED AIR DUCT MASTER WARNING N CLIMB OUT (FLIGHT 5038) PERFORMED VISUAL INSPECTION OF THE RH 14TH STAGE BLEED DUCTS REFERENCING APPLICABLE STEPS OF AMM 36-12-00. NO DEFECTS NOTED AT THIS TIME. PERFORMED LEAK TEST OF THE 10TH STAGE BLEED AIR SYS
- [SDR SWIA2025082900008](https://openairdocs.org/sdr/SWIA2025082900008.md): Control Unit · faulted · Aug 28, 2025 · N471CA · Cndair CL6002B19 · Compressor Bleed Valve
  > L 14TH DUCT WARNING DURING CLIMB OUT OF DENVER. QRH RAN AND MESSAGE CLEARED. (FLIGHT 4679 - FILED CLOSED)TROUBLESHOT L WING 14TH DUCT MESSAGE PER CRJ 200 FIM 36-20-00 FIGURE 103. PERFORMED GVI OF LH 10TH AND 14TH STAGE DUCTING AND LEAK DETECTION SYSTEM IN ARE
- [SDR SWI2025F00768](https://openairdocs.org/sdr/SWI2025F00768.md): Engine · smoke · Jun 26, 2025 · N496CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > AFTER STARTING ENGINE 2 (FOR SINGLE ENGINE TAXI) TURNED PACKS ON AND STARTED TO HEAR A WHIRRING NOISE. SUBSEQUENTLY, SECONDS LATER WHAT WOULD APPEAR TO BE SMOKE WAS ENTERING THE COCKPIT WITH A BAD AROMA.IMMEDIATELY TURNED PACKS OFF.STARTED ENGINE 1 AND PULLED
- [SDR SWI2025F00525](https://openairdocs.org/sdr/SWI2025F00525.md): Engine · faulted · Apr 12, 2025 · N910EV · Cndair CL6002B19 · Engine Oil Quantity
  > MASTER WARNING LH OIL PRESSURE ON CLIMB OUT, THEN N1 AND N2 AND ITT SPOOLED DOWN ON ITS OWN TO ZERO. RAN QRH ATTEMPTED RESTART TWICE - BOTH TIMES FAILED. COMING OUT OF XWA DIVERTED TO RAP. DECLARED AN EMERGENCY. NO EXTERNAL DAMAGE NOTED ON WALKAROUND POSTFLI
- [SDR SWIA202503190018](https://openairdocs.org/sdr/SWIA202503190018.md): Bleed Valve · malfunctioned · Mar 18, 2025 · N958SW · Cndair CL6002B19 · Compressor Bleed Valve
  > DUE TO PACK AND PRESSURIZATION ISSUES A/C REQUIRES SMOD APPROVAL BEFORE FURTHER FLIGHT. REF. EAML 1564978MCI TYPE: SERVICEABLE / NEEDS ATTENTION (FLIGHT 5762 - FILED CLOSED) MAR 18, 2025 STATION: DEN--REMOVED AND REPLACED RH 10TH STAGE BLEED AIR SOV PER
- [SDR A6WA202502118861](https://openairdocs.org/sdr/A6WA202502118861.md): Anti-Ice Valve · faulted · Feb 11, 2025 · N417AW · Cndair CL6002B19 · Engine Anti-Icing System
  > L COWL ANTI ICE CAUTION LIGHT IN FLIGHT. DIVERTED TO PIA. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT ENGINE COWL ANTI-ICE VALVE PER AWA AMM SUPP 10-094.OPS CHECK GOOD. PERFORMED OPERATIONAL TEST OF THE ENGINE COWL AND ANTI-ICE SYSTEM PER A
- [SDR A6WA202502118860](https://openairdocs.org/sdr/A6WA202502118860.md): Anti-Ice Valve · faulted · Feb 11, 2025 · N465AW · Cndair CL6002B19 · Engine Anti-Icing System
  > INFIGHTING REC'D "R COWL A/I" CAUTION WITH SWITCH SELECTED OFF. FOUND R COWL PRV POPPED ON POST FLIGHT. AIRCRAFT REMOVED FROM SERVICE R&R RH COWL PRESSURE RELIEF VALVE REF 30-2204. OPS CHECK GOOD
- [SDR SWIA2024123000027](https://openairdocs.org/sdr/SWIA2024123000027.md): Shutoff Valve · stuck · Dec 27, 2024 · N969SW · Cndair CL6002B19 · Compressor Bleed Valve
  > LEFT 10TH STAGE BLEED AIR STUCK CLOSED.FO NOTICED NO AIR FLOW DURING SINGLE PACK OPERATIONS AT APPROXIMATELY 7000€™ PRIOR TO ANY EICAS MESSAGES.APPLIED CABIN ALT QRH WITH NEGATIVE RESULTS. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29385840 WITH THE FOLL
- [SDR SWIA20241221](https://openairdocs.org/sdr/SWIA20241221.md): Engine · failed · Dec 21, 2024 · N917EV · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > ENGINE FAILURE ON CLIMB OUT.
- [SDR A6WA202410158837](https://openairdocs.org/sdr/A6WA202410158837.md): Engine · faulted · Oct 15, 2024 · N429AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > IN CLIMB RIGHT ENGINE HAD SPIKE IN ITT AND REDUCTION IN N1 AND N2 AND WAS UNRESPONSIVE FOR 10-20 SECONDS. THEN RETURNED TO NORMAL. ON APPROACH RIGHT ENGINE AGAIN HAD SAME INDICATION AND AIRCRAFT HAD VIBRATIONS. DURING BOTH EVENTS THRUST WAS BEING REDUCED BY PI
- [SDR VGCA20241012001](https://openairdocs.org/sdr/VGCA20241012001.md): Hydraulic Line · leaking · Oct 12, 2024 · N811FL · Cndair CL6002B19 · Hydraulic System, Main
  > HYD 1 LO PRESS CAUTION MESSAGE IN EICAS DURING, ALONG WITH ASSOIATED FLUID LOSS
- [SDR SWIA2024080700003](https://openairdocs.org/sdr/SWIA2024080700003.md): Carbon Seal · leaking · Aug 3, 2024 · N947SW · Cndair CL6002B19 · Turbine Engine Oil System
  > L ENG OIL PRESS WARNING IN FLIGHT. INTERMITTENT AT CLIMB OUT AND CRUISE. COMPLIED WITH QRH. PRESSURE INDICATED BETWEEN 28-35PSI INITIALLY. BEGAN TO DECREASE ON DESCENT AND WARNING BECAME PERSISTENT. FOLLOWED QRH AND SHUT L ENG DOWN. (FLIGHT 5801 - FILED CLOSED
- [SDR SWIA20240713](https://openairdocs.org/sdr/SWIA20240713.md): Engine · shutdown · Jul 13, 2024 · N506CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > AT 11000 FT AND DESCENDING WE HEARD A METALLIC TWANGING SOUND LIKE A ROPE BRAKING. ENGINE TWO THRUST REDUCED TO AT NEAR IDLE AT ABOUT 30% N1. EMERGENCY DECLARED RAN QRH ABNORMAL 1-4 AND SECURED ENGINE. (FLIGHT 4318 - FILED CLOSED)THIS DISCREPANCY WAS TRANS
- [SDR A6WA202406128764](https://openairdocs.org/sdr/A6WA202406128764.md): Oil System · leaking · Jun 12, 2024 · N455AW · Cndair CL6002B19 · Turbine Engine Oil System
  > IN CLIMB, NOTICED L ENG OIL PRESSURE FLUCTUATING. RECEIVED L OIL PRESS WARN MSG. C/W QRH. DID NOT REQ ENG SHUT DOWN. MSG CLEARED AT IDLE. OIL PRESSURE WAS FLUCTUATING BETWEEN 27-32 AT IDLE AND WARNING CLEARED. OIL TEMP NORMAL ENTIRE TIME. DURING WALK AROUND F
- [SDR A6WA202312288685](https://openairdocs.org/sdr/A6WA202312288685.md): Engine · unknown · Dec 28, 2023 · N470ZW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > DURING CLIMB OUT RT ENG ITT SPIKED TO 980 PLUS DEGREES SOUND (BANG) AND VIBRATION HEARD, RT FUEL LOW PRESSURE CAUTION MSG RECEIVED C/W QRH RH ENGINE UNRESPONSIVE. CONT LOG PAGE 363235/1 SELECTED IDLE, INDICATIONS AS FOLLOWS, N1 28 %, ITT 750 DEG C, N2 57 %, A
- [SDR A6WA202305288615](https://openairdocs.org/sdr/A6WA202305288615.md): Engine · damaged · May 28, 2023 · N413AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > ITT ON RIGHT ENGINE INCREASED TO 840C ON 85% N1 ON BOTH ENGINES, WITH VIBRATIONS AT FLIGHT LEVEL 190. REDUCED POWER VIBRATION ON N2 TWICE FOR 1 SEC EACH. AND N1 VIBE AT 2.7MIL. AIRCRAFT REMOVED FROM SERVICE. PERFORMED BOROSCOPE INSPECTION OF RH ENGINE COLD S
- [SDR A6WA202304028540](https://openairdocs.org/sdr/A6WA202304028540.md): Fuel Control · unknown · Apr 2, 2023 · N454AW · Cndair CL6002B19 · Fuel Control/Turbine Engines
  > DURRING OUR DECENT WE NOTICED N1 WILL NOT REDUCE BELOW 67% ON LH ENGINE. THROTTLE LEVER DID MOVE TO FLIGHT IDLE POSITION. NO CHANGE IN N1. WAS ABLE TO INCREASE N1 WHEN COMMANDED. ********AIRCRAFT REMOVED FROM SERVICE******** R&R LH FUEL CONTROL IAW AMM 73-
- [SDR A6WA202212108404](https://openairdocs.org/sdr/A6WA202212108404.md): Warning Message · false activation · Dec 10, 2022 · N457AW · Cndair CL6002B19 · Engine Anti-Icing System
  > RECEIVED A RT COWL ANTI-ICE WARNING AFTER TAKE OFF. C/W QRH AND MSG CLEARED. RT COWL ANTI-ICE WAS OFF IAW QRH, PILOT DECLARED AN EMERGENCY, NO PLACE TO GET OUT OF ICING CONDITIONS. AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH OPS CHECK OF COWL ANTI-ICE I
- [SDR SWIA202266912](https://openairdocs.org/sdr/SWIA202266912.md): Blades · damaged · Nov 27, 2022 · N881AS · Cndair CL6002B19 · Cylinder Head Temperature (CHT) Indicating System
  > NR 2 ENGINE SEIZED ON CLIMB OUT. LOUD AGGRESSIVE BANG FROM ENGINE. ITT IN THE RED. N1 ROLLED BACK. RAN QRC QRH FOR SEVERE ENGINE FAILURE IN FLIGHT. SHUT DOWN ENGINE. NO OVERWEIGHT LANDING. NORMAL LANDING. (FLIGHT 5405) DUE TO RT ENGINE EXPERIENCING AN UNRECOV
- [SDR A6WA202210208350](https://openairdocs.org/sdr/A6WA202210208350.md): Engine · failed · Oct 20, 2022 · N462AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > RIGHT ENG FAILURE ON T/O, LOST THRUST AT PROX 50FT, VIBRATIONS IN RED PERFORMED IAC SHUT ENG DOWN WITH 6 MIN. LH ENG HAD APR INCREASED LANDING WEIGHT APROX 49,000LBS. AIRCRAFT REMOVED FROM SERVICE. REF WO 319228 JOB CARD 4-R&RENG FOR REMOVAL AND REPLACEME
- [SDR SWIA202266598](https://openairdocs.org/sdr/SWIA202266598.md): None · shutdown · Oct 9, 2022 · N693BR · Cndair CL6002B19 · Cylinder Head Temperature (CHT) Indicating System
  > IN CRUISE LEFT ITT IMMEDIATELY INCREASE 900+ FLASHING RED, LEFT ENGINE SPUTTERS, N1 DROPS TO ABOUT 30% AND STAYS. LEFT ENGINE WARNING MESSAGE APPEARS. RUN QRC/QRH FOR LEFT ENGINE SHUT DOWN. NO SMOKE. NO VISIBLE DAMAGE. (FLIGHT 5730 - FILED CLOSED) DUE TO AN
- [SDR A6WA202206088192](https://openairdocs.org/sdr/A6WA202206088192.md): Oil System · warning message · Jun 15, 2022 · N429AW · Cndair CL6002B19 · Engine Oil Storage (Airframe Furnished)
  > ****SUPPLEMENTAL INFORMATION ******AT CRUISE NOTICED LH ENG OIL PRES FLUCTURATE BETWEEN 25-53 PSI NO MSG PRESENT. NORMAL DESCENT. ON SHORT FINAL RCVD LH ENG OIL PRES WARNING MSG INTERMIATELY. RAN QRH SHUTDOWN LH ENG. LANDED SAFELY.
- [SDR SWIA202265837](https://openairdocs.org/sdr/SWIA202265837.md): None · failed · Jun 1, 2022 · N937EV · Cndair CL6002B19 · Window/Windshield System
  > TROUBLESHOOT R WINDOW HEAT CAUTION ON CLIMB OUT AT 3K FEET. RAN QRH AND MESSAGE CLEARED. GOT MESSAGE AGAIN DESCENDING THROUGH 5K FEET. (FILED - CLOSED) REPLACED RT SIDE WINDOW IN REFERENCE TO CRJ200 AMM 56-12-01 AND 56-220-1000-SKY. OPS CHECK GOOD. NO L
- [SDR REXA2022050300758](https://openairdocs.org/sdr/REXA2022050300758.md): Pump · inoperative · Apr 27, 2022 · N840AY · Cndair CL6002B19 · Turbine Engine Air Inlet Section
  > ON TAKE OFF WE WENT TO SET TAKE OFF THRUST TO 85.2% N1 THE FO SET IT TO 85.2% N1 THEN IT DROPPED APPROX 10% N1 ON RT ENG THEN HE PUSHED THE THRUST BACK UP TO 85% THEN IT DROPPED BACK DOWN AGAIN APPROX 10% WE BOTH CALLED ABORT @ ABOUT 70-75 KTS ON TAXI BACK TO
- [SDR SWIA202265276](https://openairdocs.org/sdr/SWIA202265276.md): None · reads low · Apr 6, 2022 · N926SW · Cndair CL6002C10 · Engine Oil Quantity
  > L ENG OIL PRESS WARNING IN FLIGHT. C/W QRH, SHUT DOWN ENGINE IN FLIGHT. RETURNED TO FIELD. (FLIGHT 5375 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24617621 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE THE FOLLOWING CAMPS FOR WORK PERFORM
- [SDR A6WA202203258141](https://openairdocs.org/sdr/A6WA202203258141.md): None · none · Mar 25, 2022 · N445AW · Cndair CL6002B19 · Engine Oil System (Airframe Furnished)
  > ****SUPPLEMENTAL INFORMATION****AT FL 280 RH OIL PRESSURE INDICATION DROPPED TO ZERO. RECEIVED OIL LOW PRES WARN AND AURAL WARN. ENGINE ROLLED BACK AND STOPPED RUNNING. CW QRH SHUT DOWN THE ENGINE. ***AIRCRAFT REMOVED FROM SERVICE*** REF WO#314605 JOB CARD 4
- [SDR SWIA202264820](https://openairdocs.org/sdr/SWIA202264820.md): None · cracked · Mar 10, 2022 · N975SW · Cndair CL6002B19 · Engine Exhaust System
  > L/H ENG LWR O/B THRUST REVERSER MAIN TRACK IS CRACKED (FILED CLOSED) REMOVED AND REPLACED LH ENGINE LOWER O/B THRUST REVERSER MAIN TRACK I REF TO CRJ200 AMM 78-34-15 / OPS CHECK GOOD AT THIS TIME.
- [SDR SWIA202264221](https://openairdocs.org/sdr/SWIA202264221.md): None · cracked · Feb 13, 2022 · N433SW · Cndair CL6002B19 · Engine Exhaust System
  > UPON INSPECTION FOUND RH ENGINE LOWER I/B THRUST REVERSER MAIN TRACK CRACKED. (FILED - CLOSED) REMOVED AND REPLACED RH ENGINE LOWER I/B THRUST REVERSER MAIN TRACK IN REFERENCE WITH CRJ200 AMM 78-34-11. OPS CHECK GOOD AT THIS TIME.
- [SDR SWIA202264096](https://openairdocs.org/sdr/SWIA202264096.md): None · worn · Jan 31, 2022 · N909EV · Cndair CL6002B19 · Powerplant System
  > RH ENGINE AFT MOUNT THRUST FITTING APPEARS TO BE WORN (FILED CLOSED) REMOVED AND REPLACED THE RH ENGINE AFT THRUST FITTING IN REFERENCE TO AMM: 71-22-01. / TORQUE WRENCH INFO: / S/N: 1021102692 DUE: 7/2022
- [SDR SWIA202264095](https://openairdocs.org/sdr/SWIA202264095.md): None · failed · Jan 30, 2022 · N909EV · Cndair CL6002B19 · Powerplant System
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: NDT ENG MOUNT SHAFT - ENGINE MOUNT THRUST SHAFT DUE NDT INSPECTION. REMOVE AND REPLACE ENGINE THRUST MOUNT SHAFT IN REFERENCE TO AMM 71-00-00 AND 71-430-603 AND 71-440-603. SEND TO VENDOR FOR COMPLIANCE OF NDT (MRB 71-21
- [SDR A6WA202112208030](https://openairdocs.org/sdr/A6WA202112208030.md): None · none · Dec 18, 2021 · N455AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > DURING DECENT RIGHT ENGINE BECAME UNRESPONSIVE AT LOW TO MID POWER SETTING. WAS ABLE TO SHUT DOWN ENGINE WITH THROTTLE QUADRENT. NO EICAS MSGS PRESENT. ***AIRCRAFT REMOVED FROM SERVICE*** R/R #2 ENGINE IAW MAINTENANCE TASK CARD 000-71-400-002AW TASK CARD 00
- [SDR SWIA202163091](https://openairdocs.org/sdr/SWIA202163091.md): None · power loss · Dec 11, 2021 · N967SW · Cndair CL6002B19 · Fuel Flow Sensor
  > LEFT FUEL LO PRESS IN FLIGHT. LOST POWER. COULD NOT GET FUEL PRESSURE TO LEFT ENGINE. (FLIGHT 5424 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 23989400 WITH THE FOLLOWING CORRECTIVE ACTION: "PERFOMED ENGINE RUNS ON L/H ENGINE. REFERENCE
- [SDR SWIA202163347](https://openairdocs.org/sdr/SWIA202163347.md): None · damaged · Oct 30, 2021 · N471CA · Cndair CL6002B19 · Engine Exhaust System
  > RH THRUST REVERSER HAS 1 UPPER BLOCKER DOOR THAT REQUIRES BUSHING REPAIR, NEED TO INSTALL NEW BUSHING. (C CHECK RO 12/28/2021) REPLACED BLOCKER DOOR HINGE BUSHINGS IAW CRJ 200 AMM 78-33-21-960-802. DIMENSIONAL INSPECTION PASS OF THE RH THRUST REVERSER B
- [SDR SWIA202163704](https://openairdocs.org/sdr/SWIA202163704.md): None · broken · Oct 11, 2021 · N207PS · Cndair CL6002B19 · Engine Cowl Flaps
  > RH ENGINE T2 SENSOR LINE OB MOUNT BRACKET IS BROKEN ATTACHED TO NOSE INLET COWL (C-CHECK RO 1/5/2022) REPAIRED RH ENGINE T2 SENSOR LINE OB MOUNT BRACKET ATTACHED TO THE NOSE INLET COWL IAW REO 601R-71-61-3941 REV B DATED5/2/2018 AND SKY CARD 51-900-10
- [SDR SWIA202163338](https://openairdocs.org/sdr/SWIA202163338.md): None · damaged · Sep 29, 2021 · N471CA · Cndair CL600* · Engine Exhaust System
  > L/H THRUST REVERSER IB DOOR # 1, DOOR ACTUATOR BUSHING NEEDS REPLACE. (C CHECK RO 12/28/2021) REPLACED BLOCKER DOOR HINGE BUSHING IAW CRJ 200 AMM 78-33-21-960-802.
- [SDR A6WA202109167880](https://openairdocs.org/sdr/A6WA202109167880.md): Warning Message · illuminated · Sep 16, 2021 · N444ZW · Cndair CL6002B19 · Engine Bleed Air System
  > L 14TH BLEED AIR WARNING FREQUENTLY CLIMBING THRU 20,000FT ONCE EVERY 3 SECONDS, C/W QRH BROUGHT ENG TO IDLE. MSG CONTINUED 1 EVERY MINUTE. STOPPED WHEN ENG SHUT DOWMN ON GROUND. (BK 4) SNYOPTIC SHOWED RED BETWEEN 14TH SATGE SOC, MSOV AND COWL SOV. ALSO RECE
- [SDR A6WA202108307865](https://openairdocs.org/sdr/A6WA202108307865.md): Engine · overspeed · Aug 28, 2021 · N418AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > NOTICED MCT ENGINE RH AND OVERSPEED CONDITION. RH THRUST LEVER EXERCISED FROM MINIMUM TO MAXIMUM WITHOUT RESPONSE. C/W IAC AND QRH, EVENTUALLY FOLLOWED ENG FIRE/SEVERE DAMAGE IAC QRH AND ACCOMPLISHED SHUTDOWN. AIRCRAFT REMOVED FROM SERVICE. REF 342527-1 FOR
- [SDR A6WA202109087871](https://openairdocs.org/sdr/A6WA202109087871.md): Skin · damaged · Aug 15, 2021 · N427ZW · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > NUMBER 2 ENGINE LOWER COWL HAS DAMAGE ON THE LOWER EDGE OF CORE BETWEEN XN170.73 AND XN176.5. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DOUBLER REPAIR TO NUMBER 2 ENGINE LOWER COWL ON THE LOWER EDGE OF CORE BETWEEN XN170.73 AND XN176.5. P/N 228-50162-4
- [SDR SWIA2021081260114](https://openairdocs.org/sdr/SWIA2021081260114.md): Engine · failed · Aug 7, 2021 · N910EV · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > RIGHT ENGINE FAILURE AFTER DEPARTING KBIS THROUGH 7000€™. PERFORMED QRC, QRH PROCEDURES, RETURNED TO KBIS. (FLIGHT 5729 - FILED CLOSED) REF AML 703489 FOR CORRECTIVE. MORE INFORMATION WAS ADDED TO AML 703489 BUT BOTH ARE THE SAME DISCREPANCY. THIS DISCRE

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## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/engine/ge-cf34-3b1/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.