# Service difficulty reports: GE CF34-3B

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

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 158 reports

- [SDR DXTA2026091509695](https://openairdocs.org/sdr/DXTA2026091509695.md): Engine · faulted · Sep 13, 2026 · N200QS · Cndair CL6002B16 · Engine (Turbine/Turboprop)
  > DURING LT ENGINE START, TECHNICIANS ENCOUNTERED A RAPID INCREASE IN ITT AND THE FIRE WATCH NOTIFIED THEM OF VISIBLE FIRE. THE CHECKLIST WAS USED AND THE ENGINE FIRE BOTTLE WAS DISCHARGED. REMOVED CUSTOMERS LEFT ENGINE INSTALLED REPAIRED ENGINE. WORKED PE
- [SDR 2026FA0000529](https://openairdocs.org/sdr/2026FA0000529.md): Structure · ground damage · Jun 18, 2026 · N702LV · Bombdr CL6002D15 · Horizontal Stabilizer Structure
  > THE AIRCRAFT WAS PARKED OUTSIDE THE HANGAR AND UNOCCUPIED. WHILE OPENING THE BIFOLD HANGAR DOOR, THE DOOR CONTACTED THE TIP OF THE HORIZONTAL STABILIZER. THE AIRCRAFT HAD BEEN POSITIONED CLEAR OF THE PAINTED CLEARANCE LINE AT THE TIME OF THE EVENT. THE TECHNIC
- [SDR DXTA2026010906445](https://openairdocs.org/sdr/DXTA2026010906445.md): Engine · vibration · Jan 5, 2026 · N263QS · Cndair CL6002B16 · Engine (Turbine/Turboprop)
  > WHILE IN CLIMB POWER AT FL310 THE LEFT ENGINE VIBRATION INDICATOR TURNED AMBER AND WAS INDICATING 3.1. AT COMPLETION OF THE CLIMB TO FL390 POWER WAS REDUCED TO 95.7 AND THE VIBRATION INDICATOR WAS STILL AMBER INDICATING 2.7. WHEN POWER WAS REDUCED TO 89.0 TH
- [SDR DXTA2025071404204](https://openairdocs.org/sdr/DXTA2025071404204.md): Engine · vibration · Jul 10, 2025 · N212QS · Cndair CL6002B16 · Engine (Turbine/Turboprop)
  > IN FLIGHT, AT CRUISE, THE RIGHT ENGINE AMBER VIBRATION DISPAYED AT 2.7. PER QRH, AFTER PULLING BACK POWER, VIBRATION INDICATOR REDUCED BACK TO GREEN BUT AT AN ELEVATED READING OF 2.5 TO 2.6. A SLIGHTLY SLOWER CRUISE SPEED WAS REQUIRED TO KEEP INDICATOR IN
- [SDR DXTA2025071004166](https://openairdocs.org/sdr/DXTA2025071004166.md): Engine · no discrepancy · Jul 8, 2025 · N252QS · Cndair CL6002B16 · Engine (Turbine/Turboprop)
  > RH ENGINE - POTENTIAL FOD ISSUE WITH POSSIBLE BIRDSTRIKE (10'CLOCK POSITION WHEN FACING RH ENGINE). REQUESTING INSPECTION FOR POTENTIAL DAMAGE. CORRECTIVE ACTION; COMPLIED WITH ENGINE INSPECTIONS REF GECF34BJ SM72·0!HL0 M(L), NO EVIDENCE OF BIRD STRIKE ATTHI
- [SDR DXTA2025012001982](https://openairdocs.org/sdr/DXTA2025012001982.md): Engine · overtemp · Jan 15, 2025 · N200QS · Cndair CL6002B16 · Engine (Turbine/Turboprop)
  > LEFT ENGINE ENGINE OVERTEMP: FOLLOWING LEFT ENGINE START ITT ROSE RAPIDLY ACCOMPANIED BY A RED HOT MESSAGE ON THE ITT GAUGE. TEMP CONTINUED TO RISE AND CREW TERMINATED THE START AT 804°. CREW FOLLOWED THE HOT START QRH PROVEDURE. ALSO, THE MARSHALER HAD A C
- [SDR DXTA2025011401913](https://openairdocs.org/sdr/DXTA2025011401913.md): Cable · defective · Jan 10, 2025 · N239QS · Cndair CL6002B16 · Engine Indicating System Wiring
  > RIGHT ENGINE ENGINE TEMP INDICATION: AT APPROXIMATELY 100' AGL ON LANDING, RED ENGINE EICAS ILLUMINATED, ASSOCIATED WITH RED HOT INDICATION DISPLAY IN MFD ITT GUAGE AND RED ITT EXCEDENCE ON RIGHT ENGINE. CONTINUED LANDING AND SHUT DOWN RIGHT ENGINE ON GROUND I
- [SDR DXTA2024120901388](https://openairdocs.org/sdr/DXTA2024120901388.md): Engine · vibration · Dec 3, 2024 · N255QS · Cndair CL6002B16 · Engine (Turbine/Turboprop)
  > LEFT ENGINE ENGINE VIBRATION INDICATION: DURING INITIAL CLIMBOUT THE LEFT FAN VIB STARTED INCREASING AS HIGH AS 3.0. WE LEVELED OFF AND PULLED THE POWER BACK AND THE VIB DECREASED TO 2.0 AND REMAINED THIS HIGHER SETTING ON ARRIVAL. THE FLYING PILOT ALSO FELT
- [SDR 2024FA0000839](https://openairdocs.org/sdr/2024FA0000839.md): Bracket · cracked · Nov 13, 2024 · N541BA · Bombdr CL6002D15 · APU Start/Ignition System
  > ON THIS DATE, BRACKET PN: 3888525-2 UTILIZED TO ATTACH IGNITION UNIT TO HONEYWELL APU 36-150[CL] FOUND TO BE CRACKED. - SUSPECT POSSIBLE VIBRATION. ISSUE DISCOVERED DURING REMOVAL OF IGNITION UNIT.
- [SDR 2024FA0000840](https://openairdocs.org/sdr/2024FA0000840.md): Bracket · cracked · Nov 13, 2024 · N544BA · Bombdr CL6002D15 · APU Start/Ignition System
  > ON THIS DATE - BRACKET PN: 3888525.2 UTILIZED TO ATTACH IGNITION UNIT TO HONEYWELL APU 36-150[CL] FOUND TO BE CRACKED - SUSPECT POSSIBLE VIBRATION ISSUE. DISCOVERED DURING REMOVAL OF IGNITION UNIT. SECOND REPORT SENT. ISSUE NOTED ON TWO SEPARATE AIRCRAFT.
- [SDR DXTA2024112201240](https://openairdocs.org/sdr/DXTA2024112201240.md): Warning Light · illuminated · Nov 13, 2024 · N231QS · Cndair CL6002B16 · Engine Indicating System
  > DURING CLIMB TO CRUISE ALTITUDE JUST A FEW MINUTES PRIOR TO LEVEL OFF WITH AUTOPILOT AND ATS ON, THE RED ENGINE ICAS ILLUMINATED (FOR A DURATION OF 1-2 SECONDS). NO EXCEEDANCE LEVELS WERE OBSERVED FOR EITHER ENGINE FOR ITT, N1 NOR N2 THAT WOULD NORMALLY SPUR
- [SDR DXTA2024102100894](https://openairdocs.org/sdr/DXTA2024102100894.md): Blades · lack of lube · Oct 17, 2024 · N252QS · Cndair CL6002B16 · Turbine Engine Air Inlet Section
  > RIGHT ENGINE ENGINE VIBRATION: VIBRATION FELT AND HEARD DURING CLIMBOUT. RIGHT ENGINE FAN VIB WAS 3.0, AMBER COLOR. QRH RAN. FELT NO VIBRATION IN FLIGHT CONTROLS. FLIGHT ATTENDANT HEARD LOUD NOISES AND VIBRATION FROM THE CABIN. CORRECTIVE ACTION; REMOVED & CL
- [SDR 2024FA0000194](https://openairdocs.org/sdr/2024FA0000194.md): Spacer · missing · Feb 29, 2024 · N604DT · Cndair CL6002B16 · Wheel/Ski/Float
  > DURING A SCHEDULED MAINTENANCE INPUT AT BOMBARDIER SERVICES (UK) LTD AT BIGGIN HILL AIRPORT, UNDER WO 267540 - UPON REMOVAL OF #4 MAIN WHEEL ASSY, IT WAS DISCOVERED THAT THE SPACER WAS MISSING FROM THE INCOMING INSTALLATION. AIPC 32-41-01, ITEM 142, PN 19095-1
- [SDR V6NA2024022701.1](https://openairdocs.org/sdr/V6NA2024022701.1.md): Throttle · faulted · Feb 27, 2024 · Cndair CL6002B16 · Power Lever
  > DURING THE FIELD ACCIDENT INVESTIGATION FOR N823KD CL604 S/N 5584, IT WAS MENTIONED THAT SEVERAL YEARS AGO A CHALLENGER 600 SERIES, DURING TAXI ACROSS AN ACTIVE RUNWAY, HAD A DUAL ENGINE FAILURE CAUSED BY THE AUTO THROTTLE SYSTEM. IN AN INTERNAL INVESTIGATION,
- [SDR 2023F00204](https://openairdocs.org/sdr/2023F00204.md): Wire Harness · broken · Jun 17, 2023 · N69DT · Cndair CL6002B16 · Fire Protection System Wiring
  > ON ARRIVAL INTO HOU AFTER LEVELING AND THE THRUST LEVERS ADVANCING THE EICAS, AURAL WARNINGS, RH ENGINE FIRE PUSH, AND FIRE BOOTLE SWITCH LIGHTS ALL ILLUMINATED AND GAVE THE INDICATION OF THERE BEING A FIRE ON THE #2 ENGINE. RETARDING THE THRUST LEVERS CAUSED
- [SDR U5QA202212010110](https://openairdocs.org/sdr/U5QA202212010110.md): Engine · power loss · Dec 1, 2022 · N26JE · Cndair CL6002B16 · Engine (Turbine/Turboprop)
  > DIVERTED TO KDSM. DURING FLIGHT, FL380, AUX AOA CASE HEAT FAIL. COMPLETED THE CHECKLIST AND SHORTLY AFTER NR 1 ENGINE FAILED, ROLLED BACK TO 9% N2. TRIED INFLIGHT CROSSBLEED AND APU START WITH NO RESULTS. LANDING UNEVENTFUL.: AFTER APPLYING POWER TO AIRCRA
- [SDR 2022FA0000682](https://openairdocs.org/sdr/2022FA0000682.md): Line · destroyed · Nov 11, 2022 · N188CR · Engine Bleed Air System
  > DURING INSPECTION FOR ROUTINE MAINTENANCE, THE #2 ENGINE CORE COWLS DOORS WERE OPENED UP. UNDER THE UPPER DOOR FOR THE ENGINE, THE 14TH STAGE BLEED AIR LINE P/N 228-56336-103 (13866-101 REV B) S/N K97991 WAS FOUND TO BE RUPTURED. THE LINE IS DESTROYED AND
- [SDR U5OA_N36VV](https://openairdocs.org/sdr/U5OA_N36VV.md): Engine · low pressure · Sep 18, 2022 · N36VV · Cndair CL604 · Engine Oil Indicating System
  > ON A PART 91 TRIP SCHEDULED FROM KAUS TO KVNY CREW NOTICED THE RH ENG OIL PRESS FLUCTUATING BETWEEN 31 AND 39 PSI AT CRUISE FL340, AS FLIGHT PROGRESSED THE OIL PRESS CONTINUED TO DROP, WHEN PRESS READING DROPPED TO 25 PSI THE CAS MSG R LOW OIL PRESS ILLUMINATE
- [SDR 2022FA0000494](https://openairdocs.org/sdr/2022FA0000494.md): None · worn · Sep 2, 2022 · N314RC · Bombdr CL6002D15 · AC Generation System
  > ON TAKEOFR ROLL, AT 50 KNOTS, PILOT STATED "#2 GEN FAIL" CAS MESSAGE DISPLAYED, AND TAKEOFF ABORTED. FINAL INVESTIGATION REVEALED #2 ENG INTEGRATED DRIVE GENERATOR (IDG) DELTA P INDICATOR WAS SET. REMOVAL AND INSPECTION OF FILTER REVEALED NUMEROUS METAL PART
- [SDR GZXA2020061200001](https://openairdocs.org/sdr/GZXA2020061200001.md): Connector · chafed · Jun 12, 2020 · N142J · Cndair CL6002B16 · Fire Protection System Wiring
  > 14TH STAGE DUCT CAS MESSAGE.
- [SDR BN5A2019121200001](https://openairdocs.org/sdr/BN5A2019121200001.md): Sensor · faulty · Nov 27, 2019 · N18RC · Cndair CL6002B16 · Overheat Detection
  > AIRCRAFT DEPARTED, DURING CLIMB OUT THE RIGHT ENGINE 14TH DUCT OVERHEAT MESSAGE ALERTED THE CREW. POWER WAS PULLED BACK TO IDLE AND THE 14TH STAGE BLEED AIR VALVE WAS POSITION TO CLOSE. RIGHT 14TH DUCT MESSAGE REMAINED. RIGHT ENGINE WAS SHUT DOWN AND FLIGHT CR
- [SDR CA190814005](https://openairdocs.org/sdr/CA190814005.md): Oil System · low pressure · Aug 9, 2019 · Cndair CL604 · Engine Oil Pressure
  > (CAN) AIRCRAFT HAD AN ENGINE SHUT DOWN IN FLIGHT, DECLARED A PAN PAN AND DIVERTED INITIAL INFORMATION IS THAT DURING FLIGHT OIL PRESSURE DROPPED ON ONE ENGINE AND AFTER THEY THROTTLED BACK IT STABILIZED ABIT BUT THEN CONTINUED TO DROP. CREW SHUT DOWN THE ENGIN
- [SDR CA190802010](https://openairdocs.org/sdr/CA190802010.md): Computer · malfunctioned · Aug 1, 2019 · Cndair CL604 · Stall Warning System
  > (CAN) STALL ALT COMP LIGHT AND STALL FAIL ARE ANNUNCIATIED. FIELD SERVICE REPRESENTATIVE INPUT AUG 1, 2019: FAULT CLEARED THE NEXT MORNING. ADVISED CUSTOMER TO REPLACE THE STALL COMPUTER. (TC# 20190802010)
- [SDR CA190806003](https://openairdocs.org/sdr/CA190806003.md): Rib · cracked · Aug 1, 2019 · Cndair CL604 · Wing, Rib/Bulkhead
  > (CAN) L/H WING @ WS112.3, CANTED RIB, DRAWING #600-10332, IPC 57-51-01, P8 (ITEM 75) FOUND CRACKED, 1` LONG WITH SPIDER CRACKING AND 2 RIVETS SHEARED AT TRAILING EDGE GUSSET, IPC 57-51-001 (ITEM 155). (TC# 20190806003)
- [SDR CA190709004](https://openairdocs.org/sdr/CA190709004.md): Limiter · damaged · Jun 5, 2019 · Cndair CL604 · Spoilers
  > (CAN) CREW REPORTED THAT WHEN DEPLOYING SPOILERS THEY DEPLOYED ASYMMETRICALLY AND THE AIRCRAFT ROLLED TO THE RIGHT. THE CREW NOTED THAT ON THE EICAS THE INDICATION SHOWED THAT THE RH SPOILER HAD EXTENDED FURTHER THAN THE LEFT. ENGINEERS REVISITED THE AIRCRAFT
- [SDR CA190614011](https://openairdocs.org/sdr/CA190614011.md): Flt Controls · binding · Jun 3, 2019 · Cndair CL604 · Flight Control System
  > (CAN) THE CREW NOTED THE FLIGHT CONTROLS WERE EXTREMELY STIFF ABOUT PITCH AND ROLL AXIS WITH OR WITHOUT AIR LOAD. THE AIRCRAFT HYDRAULIC PRESSURE SHOWED NORMAL IN ALL THREE SYSTEMS. UPON LANDING THE FLIGHT CREW VERIFIED THE PROBLEM PERSISTED WITHOUT AIR LOAD
- [SDR CA190527011](https://openairdocs.org/sdr/CA190527011.md): Hose · leaking · May 25, 2019 · Cndair CL604 · Passenger Oxygen System
  > (CAN) APPROX 100PSI O2 LEAK OVERNIGHT. LOCATED LEAK AT BASE OF HOSE FITTING UNDER CO-PILOTS SIDE PANEL. FURTHER INVESTIGATION ALSO REVEALED THE HOSE WAS BULGING AT SAME LOCATION. ATTACHMENT POINT FOR THIS LINE IS TO THE `IN` PORT FITTING OF THE PASSENGER OXYGE
- [SDR CA190514008](https://openairdocs.org/sdr/CA190514008.md): Motor · failed · May 8, 2019 · Cndair CL604 · Trailing Edge Flap Actuator
  > (CAN) DURING PRE-FLIGHT, TECHNICIAN NOTICED THE #2 FLAP MOTOR C/B (CB2-B5) TRIPPED. PUSH C/B BACK IN AND SELECTED FLAPS TO 20 DEG. ONCE FLAPS STARTED TO MOVE THE C/B TRIPPED AGAIN. FLAP MOTOR REPLACED. (TC# 20190514008)
- [SDR CA190506011](https://openairdocs.org/sdr/CA190506011.md): Pump · failed · Apr 30, 2019 · Cndair CL604 · Hydraulic Pump (Electric/Engine), Main
  > (CAN) AIRCRAFT HAD AN INFLIGHT SYSTEM 3 HYDRAULIC PRESSURE LOW INDICATION IN FLIGHT AND DIVERTED FOR LANDING CREW INFORMED THAT CB HYD 3 A WAS POPPED. (TC# 20190506011)
- [SDR CA190430014](https://openairdocs.org/sdr/CA190430014.md): Pdu · overheated · Apr 25, 2019 · Cndair CL604 · Trailing Edge Flap Control System
  > (CAN) FLAP MOTOR 1 AND 2 OVERHEAT AT THE SAME TIME. CARRIED OUT OPS TESTS FLAPS AND CB PULLED OUT ONE BY ONE OF THE FLAP MOTORS. AND OPS CHECK ON ONE MOTOR EACH TIME. NO OVERHEAT OCCURRED. ALL SATISFACTORY DUE TO BOTH FLAP MOTORS OVERHEAT AT THE SAME TIME IT
- [SDR CA190425017](https://openairdocs.org/sdr/CA190425017.md): Flap System · stuck · Apr 18, 2019 · Cndair CL6002B16 · Trailing Edge Flap Control System
  > (CAN) FLAP STUCK AT 5 DEGREES. WE HAVE FIXED ALL THE DISCREPANCY`S ON A/C. THE FLAPS WE WHERE ABLE TO RESET AND PERFORMED MULTIPLE OPS CHECKS WITH SATISFACTORY RESULTS. (TC# 20190425017)
- [SDR CA190415007](https://openairdocs.org/sdr/CA190415007.md): Door · malfunctioned · Apr 12, 2019 · Cndair CL6013A · Landing Gear Door Retract Section
  > (CAN) DURING TAKE OFF THE NOSE LANDING GEAR (NLG) DOORS DID NOT CLOSE. AIRCRAFT LANDED AT DEPARTURE AIRPORT WITHOUT FURTHER INCIDENT. NO RECTIFICATION OR PARTS ISSUES HAVE BEEN PROVIDED. BOMBARDIER TRYING TO CONTACT SUBMITTER FOR DETAILS. SDR REVIEWED (TC# 20
- [SDR CA190820015](https://openairdocs.org/sdr/CA190820015.md): Servo Valve · defective · Mar 13, 2019 · Cndair CL604 · Landing Gear Steering System
  > (CAN) AC LANDED AT AIRPORT AND AFTER TOUCH DOWN, AT AROUND 80-60 KTS, NOSE WHEEL STEERING (NWS) FAILED. AC STOPPED ON RUNWAY AND NOSE WHEEL WAS FOUND 90 DEG DEFLECTED. MAINTENANCE MANAGED TO GET THE AC OFF RUNWAY AND INTO FACILITY. BOMBARDIER, CUSTOMER RESPONS
- [SDR A6WA2019013146348](https://openairdocs.org/sdr/A6WA2019013146348.md): Flap System · malfunctioned · Jan 29, 2019 · N457AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > ON FINAL APPROACH TO LAND, FLAP FAIL CAUTION MESSAGE WHEN FLAPS SELECTED TO 30 DEGREES. FLAPS FAILED IN 20 DEGREE POSITION. COMPLIED WITH QRH.
- [SDR CA190314018](https://openairdocs.org/sdr/CA190314018.md): Adc · malfunctioned · Jan 14, 2019 · Cndair CL604 · Airspeed/Mach Indicator
  > (CAN) OPERATOR REPORTED HAVING TWO UNRELIABLE AIRSPEED EVENTS ON THE SAME AIRCRAFT WITHIN TWO WEEKS, IN DECEMBER 2018 AND JANUARY 2019. THE FIRST EVENT OCCURRED ON DECEMBER 28TH, 2018, EN ROUTE PRIOR TO TOP OF DESCENT AT FL400. THE CREW RECEIVED AN EFIS COMP M
- [SDR DXTA2018101601558](https://openairdocs.org/sdr/DXTA2018101601558.md): Engine · unserviceable · Oct 15, 2018 · N235QS · Cndair CL6002B16 · Engine (Turbine/Turboprop)
  > AFTER ROTATION AND INITIAL CLIMB, LEFT ENGINE ITT HOT MESSAGE ILLUMINATED, RETURNED TO LAND, PRECAUTIONARY LEFT ENGINE SHUT DOWN. SIGNOFF REMOVED LEFT HAND ENGINE SERIAL NUMBER 801515. INSTALL REPAIRED ENGINE SERIAL NUMBER 801433. INSTALLED ENGINE SERIAL NUMB
- [SDR RU3A20180529022](https://openairdocs.org/sdr/RU3A20180529022.md): Accelerometer · faulty · May 22, 2018 · N86 · Cndair CL6002B16 · Engine Vibration Analyzer
  > RIGHT ENGINE VIBRATION LIGHT ILLUMINATED AT 75% N1 AT 16000 FEET. REMOVED AND REPLACED ENGINE VIBRATION ACCELEROMETER.
- [SDR 2018FA0000214](https://openairdocs.org/sdr/2018FA0000214.md): Track · cracked · Mar 28, 2018 · N43R · Cndair CL6002B16 · Engine Thrust Reverser
  > MAIN REVERSER TRACK, RIGHT SIDE AT THE 7 O`CLOCK POSITION, CRACKED ALMOST COMPLETELY THROUGH. FOUND DURING ROUTINE LUBRICATION OF REVERSER SCREWJACKS.
- [SDR CA160127002](https://openairdocs.org/sdr/CA160127002.md): Strut · leaking · Jan 24, 2016 · Cndair CL604 · Nose/Tail Landing Gear Strut/Axle
  > (CAN) AIRCRAFT ENCOUNTERED RETRACTION PROBLEMS (NLG TRANSIT LIGHT WOULD NOT EXTINGUISHED) AND HAD TO COMPLETE ITS FLIGHT WITH GEAR DOWN AND CONFIRMED LOCKED. FOLLOWING SUCCESSFUL LANDING AND PRELIMINARY INVESTIGATION THE NLG ASSY WAS FOUND DEFLATED AND COULD
- [SDR CA160111007](https://openairdocs.org/sdr/CA160111007.md): Outlet · arced · Jan 7, 2016 · Cndair CL604 · Passenger Compartment Equipment
  > (CAN) THE CABIN OUTLET AT THE LT FORWARD SEAT WHEN THE TABLET CHARGER WAS PLUGGED IN THE OUTLET, CHARGER HAD ELECTRICAL ARCHING AND SMOKE.
- [SDR CA151208008](https://openairdocs.org/sdr/CA151208008.md): Pdu · malfunctioned · Dec 6, 2015 · Engine Thrust Reverser
  > (CAN) AS REPORTED BY PILOT IN COMMAND IN INCIDENT REPORT DURING TAKEOFF ROLL, AT APPROXIMATELY 100 KTS, THE ATS DISENGAGED IMMEDIATELY FOLLOWED BY RT THRUST REVERSER UNLOCKED AMBER MESSAGE AND UNLOCK PBA AMBER. NO EVIDENCE OF YAW OR ACTUAL THRUST REVERSER DEP
- [SDR J7SA20151129001](https://openairdocs.org/sdr/J7SA20151129001.md): Fire Detector · failed · Nov 29, 2015 · N338FX · Cndair CL6002B16 · Fire Detection
  > RIGHT ENG FIRE WARNING ACTIVATED IN FLIGHT. SHUTDOWN THE ENG & WARNING ALARM STOPPED. DECLARED AN EMER & LANDED SAFELY WITHOUT NEED TO EXPEND FIRE EXTINGUISHER. ON LANDING CREW FOUND NO EVIDENCE OF ACTUAL FIRE ON THE ENG. FOUND THE RT ENG PYLON SENSING E
- [SDR CA151203011](https://openairdocs.org/sdr/CA151203011.md): Fire Warning · false activation · Nov 29, 2015 · Cndair CL604 · Fire Detection
  > (CAN) DURING CLIMBOUT, THE RT ENGINE FIRE WARNING TRIPPED OFF WITH RED, RT ENGINE FIRE, POSTED. CREW SHUTDOWN THE RT ENGINE AND WARNING WENT OUT. ACFT DECLARED EMERGENCY AND DIVERTED, LANDING WITHOUT INCIDENT. CREW DID NOT NOTICE ANY EVIDENCE OF A FIRE FROM
- [SDR CA151203017](https://openairdocs.org/sdr/CA151203017.md): Fire Loop · failed · Nov 24, 2015 · Cndair CL604 · Fire Detection
  > (CAN) IT WAS REPORTED TO THE CUSTOMER RESPONSE CENTER (CRC) THAT THE CREW OBSERVED A FIRE INDICATION FOR THE RIGHT-HAND ENGINE AS THE AIRCRAFT WAS CLIMBING OUT. THE CREW FOLLOWED THE CHECKLIST. THE CREW THEN SHUT DOWN THE ENGINE AND THE FIRE INDICATION WENT OU
- [SDR CA151118008](https://openairdocs.org/sdr/CA151118008.md): Bracket · chafed · Nov 13, 2015 · Cndair CL604 · Main Landing Gear
  > (CAN) NLG CHANNEL 600-33045 CHAFED BY RH EDGE OF DOWN LOCK SWITCH BRACKET 20046-101.
- [SDR CA150925017](https://openairdocs.org/sdr/CA150925017.md): Wheel · missing · Sep 23, 2015 · Cndair CL604 · Wheel/Ski/Float
  > (CAN) DOM REPORTED THAT CREW NOTICED THE RT OUTBOARD WHEEL ASSEMBLY MISSING UPON LANDING.
- [SDR CA150828010](https://openairdocs.org/sdr/CA150828010.md): Ribbon Heater · overheated · Aug 10, 2015 · Cndair CL604 · Buffet/Galleys
  > (CAN) DURING AN INSPECTION, THE OPERATOR NOTICED THAT THE INSULATION INSTALLED OVER THE HEATED SILICONE GALLEY DRAIN HOSE (INSTALLED BY MODIFICATION DATA SUMMARY D48100) SHOWED SIGNS OF OVERHEATING. AFTER REMOVING THE INSULATION, IT WAS DISCOVERED THAT THE RIB
- [SDR CA150703005](https://openairdocs.org/sdr/CA150703005.md): Stab System · failed · Jun 30, 2015 · Cndair CL604 · Stabilizer Control System
  > (CAN) AFTER DEPARTURE, HAD THE STAB TRIM AMBER CAS MESSAGE POST ON THE EICAS. CONTINUOUSLY RE-EVALUATED THE SITUATION AND EXPLORED SOME POTENTIAL OPTIONS. FLEW AT A REDUCED ALTITUDE AND AIRSPEED AND REMAINED CLEAR OF RVSM AIRSPACE. MAINTENANCE REPORTED FAU
- [SDR CA150527002](https://openairdocs.org/sdr/CA150527002.md): Bushing · migrated · May 27, 2015 · Cndair CL604 · Fuselage, Landing Gear Attach Fittings
  > (CAN) LEFT & RIGHT MAIN GEAR AFT MOUNTING BUSHINGS MIGRATING. DISCOVERED DURING SCHEDULED INSPECTION. MANUFACTURER CORRESPONDENCE HAS INDICATED THAT NO MIGRATION IS ALLOWED.
- [SDR EBVR20150423001](https://openairdocs.org/sdr/EBVR20150423001.md): Nut · missing · Apr 17, 2015 · N530SC · Cndair CL6002B16 · Turbine Engine Compressor Section
  > OPENING ENGINE COWLING FOUND A USED VARIABLE GEOMETRY VANE SPINDLE TAB WASHER P/N 3044T06P01 LAYING IN THE BOTTOM CORE COWLING. INSPECTION DISCOVERED ONE SPINDLE NUT, P/N 4037T84P04 MISSING. GENERAL ELECTRIC SERVICE BULLETIN CF34BJ 72-0157 - STAGES IGV-5 SEL

Next page: https://openairdocs.org/engine/ge-cf34-3b/reports.md?page=2

## 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 = 'CF343B'
ORDER BY difficulty_date DESC
```

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

---
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.