# Service difficulty reports: GE CF34-3A

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

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 174 reports

- [SDR 2021FA0000132](https://openairdocs.org/sdr/2021FA0000132.md): Flap Track · binding · Feb 19, 2021 · N601RC · Cndair CL6002A12 · Trailing Edge Flaps
  > FAILURE OF THE FLAPS AT 10 DEGREES. CORRECTIVE ACTION WAS LUBRICATION OF THE FLAP ACTUATORS IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUALS FOLLOWED BY AN OPERATIONAL CHECK
- [SDR CA190416014](https://openairdocs.org/sdr/CA190416014.md): Actuator · failed · Apr 8, 2019 · Cndair CL6013A · Stabilizer Actuator
  > (CAN) AOG DUE TO HSTA FAILURE PREVIOUSLY INSTALLED HSTA HAS BEEN A NFF. (TC# 20190416014)
- [SDR WWQA20180213001](https://openairdocs.org/sdr/WWQA20180213001.md): Carbon Seal · leaking · Jan 29, 2018 · N908DG · Cndair CL6002B16 · Turbine Engine Oil System
  > WITH PACKS SELECTED OFF AND APU BLEED AIR SELECTED ON, STARTED THE RT ENGINE. NOTICED SMOKE COMING OUT OF FORWARD AIR CONDITIONING VENTS IN COCKPIT. STARTED THE LT ENGINE AND SMOKE BEGAN BILLOWING OUT OF COCKPIT FORWARD AND SIDE CONSOLE AIR CONDITIONING VENT
- [SDR MXIA2016051800001](https://openairdocs.org/sdr/MXIA2016051800001.md): Hinge · cracked · May 18, 2016 · N500L · Cndair CL6002B16 · Fuselage, Door Hinge
  > DURING A SCHEDULED NDI INSPECTION OF THE CABIN DOOR HINGE A CRACK WAS DETECTED ON 1 OF THE LOBES OF THE DOOR SIDE HINGE HALF. EDDY CURRENT METHOD OF NDI WAS USED.
- [SDR 2016FA0000247](https://openairdocs.org/sdr/2016FA0000247.md): Tire · failed · May 17, 2016 · N601RC · Cndair CL6002A12 · Tire
  > RIGHT MAIN INBD TIRE HAS A PORTION OF THE TREAD THAT SEPARATED ON LANDING. NEW TIRE WAS INSTALLED AT WHEEL ASSY O/H.
- [SDR CA160311002](https://openairdocs.org/sdr/CA160311002.md): Lever · stuck · Mar 10, 2016 · Cndair CL600* · Landing Gear Selector
  > (CAN) DURING OPERATIONAL CHECKS OF LANDING GEAR SYSTEM GEAR SWINGS, THE EMERGENCY SYSTEM HAS BEEN ACTIVATED. THE GEAR EXTENDED WITH OUT ANY ISSUES. FOLLOWING STEPS CALLED FOR PLACEMENT OF TARGETS ON THE MAIN GEAR TO ACTIVATE NR 2 ELECTRICALLY DRIVEN HYDRAULIC
- [SDR CA150327002](https://openairdocs.org/sdr/CA150327002.md): Screw · broken · Mar 18, 2015 · Cndair CL6013A · Rudder Structure
  > (CAN) LT ACME SCREW ADJUSTING FOUND BROKEN FOLLOWING PILOT REPORT.
- [SDR CA150108002](https://openairdocs.org/sdr/CA150108002.md): Engine · shutdown · Dec 27, 2014 · Cndair CL6013A · Engine (Turbine/Turboprop)
  > (CAN) CUSTOMER REPORTS THE LEFT ENGINE SHUT DOWN UN-COMMANDED. THE AIRCRAFT WAS ON DESCENT. THE PILOTS THINK THEY HAD A COMPRESSOR STALL. THE LEFT ENGINE SHUTDOWN. THE PILOTS DIVERTED TO HOME BASE AND LANDED UNEVENTFULLY.
- [SDR LOMA2015F00009](https://openairdocs.org/sdr/LOMA2015F00009.md): Shutoff Valve · leaking · Nov 18, 2014 · N807MM · Cndair CL6002A12 · Compressor Bleed Valve
  > RIGHT 10TH STAGE BLEED AIR WARNING ILLUMINATED. DIVERTED FOR REPAIR. REPLACED 10TH AND 14TH STAGE BLEED AIR SHUTOFF VALVES.
- [SDR CA141114001](https://openairdocs.org/sdr/CA141114001.md): Landing Gear · failed · Nov 11, 2014 · Cndair CL6013A · Landing Gear Retraction/Extension System
  > (CAN) AT APPROX. 5 MILES FINAL RUNWAY 16, AN EXECAIRE CANADAIR CL600-2B16 REPORTED A POSSIBLE NOSE GEAR PROBLEM. DID A FLY BY AND NOSE GEAR WAS NOT OBSERVED TO BE DOWN. DID A VFR CIRCUIT AND RECYCLED THE GEAR WHICH RESULTED IN A "THREE GREEN" INDICATION. AIRCR
- [SDR CA140606002](https://openairdocs.org/sdr/CA140606002.md): Control Cable · failed · Jun 5, 2014 · Cndair CL6002A12 · Elevator Tab Control System
  > (CAN) DURING AN 60 MONTH INSPECTION. THE TECH FOUND BY VISUAL CHECK UP, WHEN HE OPEN THE PANEL IN THE VERTICAL STABILIZER RT SIDE.
- [SDR CA140408007](https://openairdocs.org/sdr/CA140408007.md): Switch · malfunctioned · Apr 8, 2014 · Cndair CL600* · Cabin Cooling System
  > (CAN) DURING A MAINTENANCE INSPECTION OF THE AIR CONDITION OVERHEAT SWICHES ON BOTH ACU FAIL THE TEST, FOUND INOPERATIVE, DURING THE FUNCTIONAL TEST AS REQUIRED BY THE MM PSP 601-2, CHAP 21-51-3, P201, THIS CHECK IS REQUIRED AT EVERY 4800 HRS MCN 05-0000-048
- [SDR KW3R2014032617085](https://openairdocs.org/sdr/KW3R2014032617085.md): Windshield · cracked · Mar 26, 2014 · N156RC · Cndair CL6002B16 · Flight Compartment Windows
  > DURING APPROACH, LT WINDSHIELD CRACKED, CREW PERFORMED ABNORMAL PROCEDURES AND LANDED WITH NO FUTHER PROBLEMS.
- [SDR CA130626005](https://openairdocs.org/sdr/CA130626005.md): Wire · failed · Jun 25, 2013 · Cndair CL600* · Flight Control System Wiring
  > (CAN) DURING A PREFLIGHT CHECK THE PILOT COULD NOT OPERATE THE PITCH TRIM AND FOUND THE BREAKER CHANNEL NR 2 POP OUT. AFTER THE INVESTIGATION BY THE AME HE FOUND THAT THE BUNDLE WIRES THAT GOES ON THE CANNON PLUG P8CD ATTACH TO THE TRANSIENT SUPPRESSOR BOX WAS
- [SDR CA130610014](https://openairdocs.org/sdr/CA130610014.md): Selector Valve · failed · Jun 6, 2013 · Cndair CL600* · Landing Gear Retraction/Extension System
  > (CAN) ON DEPARTURE WHEN THE LANDING GEAR WAS SELECTED TO THE UP POSITION THE NOSE GEAR WOULD NOT RETRACT, A FERRY FLIGHT PERMIT WAS ISSUED TO FACILITATE POSITIONING TO BASE FOR REPAIR. THIS IS THE SECOND TIME THIS FAILURE OCCURED ON THIS ACFT, THE PREVIOUS OCC
- [SDR CA130528010](https://openairdocs.org/sdr/CA130528010.md): Control Handle · failed · May 18, 2013 · Cndair CL600* · Landing Gear Selector
  > (CAN) DURING TAKE-OFF THE GEAR HANDLE WAS SELECTED TO THE UP POSITION. THE MAIN LANDING GEAR RETRACTED AND INDICATED AS BEING RETRACTED HOWEVER, THE NOSE LANDING GEAR INDICATED DOWN ON THE LANDING GEAR LIGHT PANEL AND THE GEAR HANDLE FLASHING RED. THE QRH GEAR
- [SDR CA120529001](https://openairdocs.org/sdr/CA120529001.md): Door · separated · May 23, 2012 · Cndair CL6002B16 · Passenger/Crew Doors
  > (CAN) PASSAGER DOOR DEPARTED IN FLIGHT. INVESTIGATION TEAM HAS RETURNED FROM THE ACCIDENT SITE. THE ACFT DAMAGE AND GOLF COURSE, WHERE THE PASSENGER DOOR LANDED, WAS SURVEYED BY THE INVESTIGATION TEAM. ADDITIONAL DOOR REMAINS WERE FOUND AT THE GOLF COURSE. THE
- [SDR CA120405004](https://openairdocs.org/sdr/CA120405004.md): Fuel Control · malfunctioned · Apr 4, 2012 · Cndair CL6013A · Fuel Control/Turbine Engines
  > (CAN) DURING DESCENT, BOTH THRUST LEVERS WERE RETARDED TO IDLE. THE RT ENGINE FLAMEDOUT. THE CREW ELECTED TO CONTINUE WITH THE APPROACH SINGLE ENGINE. THE CUSTOMER IS REQUESTING TROUBLESHOOTING GUIDE LINES. ACFT WAS 5.5 HRS INTO FLIGHT LEG, STARTING DESCENT
- [SDR CA120321004](https://openairdocs.org/sdr/CA120321004.md): Actuator · failed · Mar 19, 2012 · Cndair CL6002B16 · Trailing Edge Flap Actuator
  > (CAN) AFTER TAKE OFF THE FLAP FAIL AT 20 DEGREES DOWN, THE AIPLANE FLEW TO DESTINATION WITH THE FLAPS AT 20 DEGREES AND LANDED WITHOUT INCIDENT.
- [SDR CA120127001](https://openairdocs.org/sdr/CA120127001.md): Window · cracked · Jan 23, 2012 · Cndair CL600* · Flight Compartment Windows
  > (CAN) IN CRUISE THE PILIOT SUDDENLY SEE THAT THE LT SIDE WIDOW CRACKED, WENT FROM 24,000 TO 13,000 WITHOUT PANIC SLOWLY TO MAKE SURE THAT THE WINDOW DOESN`T BREAK AS A SAFETY PRECAUTION AND BECAUSE HE WAS GOING TO THE THE HOME BASE HE DIDN`T HAVE TO CANCEL HI
- [SDR CA120104009](https://openairdocs.org/sdr/CA120104009.md): Line · leaking · Jan 4, 2012 · Cndair CL6002B19 · Hydraulic System, Main
  > (CAN) HYDRAULIC NR 3 LOSS CAUSING AN EMERGENCY GEAR EXTENSION. THE HYDRAULIC LEAK WAS LOCATED ON ACMP 3 A HOSE PUMP PRESS LINE.
- [SDR CA110328003](https://openairdocs.org/sdr/CA110328003.md): Strut · binding · Mar 27, 2011 · Cndair CL600* · Nose/Tail Landing Gear Strut/Axle
  > (CAN) DURING AN APPROACH IN CYUY MARCH 27 2011,THE NLG REFUSE TO DESCENT.THEY DID THE EMERGENCY LANDING GEAR PROCEDURE AND IT DIDN`T WORK.THEY HAD IN THE COCKPIT AN INDICATION OF NLG IN TRANSIT AND WOW INPUT FAIL.SO WITH THE MTCE THEY PRESUME THAT THE GEAR W
- [SDR CA110112009](https://openairdocs.org/sdr/CA110112009.md): Support Beam · cracked · Dec 17, 2010 · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > THIS SDR SHOULD HAVE BEEN ISSUED IN JULY 2010 WHEN DISCOVERED. MISTAKENLY OMITTED. DURING EXCHANGE OF AN APU, THE TECHNICIAN NOTICE A CRACK ON THE UPPER WEB, AFT WEB AJ RGL 9.5 AND UPPER ATLBL 9.5 ENG SUPPORT BEAM FS 640. TEMPORARY REPAIR WAS DONE IAW RE 0
- [SDR 2010FA0000201](https://openairdocs.org/sdr/2010FA0000201.md): Frame · cracked · Feb 5, 2010 · N500PG · Cndair CL6002A12 · Fuselage Main, Frame
  > FWD FUSELAGE FRAME AT FS235 ABOVE FLOOR, PILOTS AND COPILOTS SIDE, FOUND CRACKED. DURING 240 MONTH INSP.
- [SDR CA091216003](https://openairdocs.org/sdr/CA091216003.md): Fuel Control · malfunctioned · Nov 9, 2009 · Fuel Control/Turbine Engines
  > (CAN) THE ENGINE WAS IN FLIGHT AT 9000 FT WHEN A REQUEST WAS MADE TO AIR TRAFFIC TO INCREASE TO NEXT ALTITUDE. AFTER THE REQUEST WAS GRANTED, THE PILOT ADVANCED THE THROTTLE TO ACHIEVE SPEED AND ALTITUDE. AT THIS TIME, AN ENGINE FLAMEOUT OCCURED. THE PILOT WA
- [SDR CA090529001](https://openairdocs.org/sdr/CA090529001.md): Cable · worn · May 24, 2009 · Cndair CL6013A · Fuel Controlling System
  > (CAN) DURING APPROACH THE CREW EXPERIENCED MULTIPLE COMPRESSOR STALLS ON THE LT ENG. THEY CARRIED OUT THE APPROACH WITH THAT ENGINE AT IDLE. AT ONE POINT, THE ITT STARTED RISING AND THE CREW ELECTED TO SHUTDOWN THE ENGINE FOR THE REMAINING OF THE APPROACH. THE
- [SDR CA090525006](https://openairdocs.org/sdr/CA090525006.md): Cowling · departed · Feb 26, 2009 · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > (CAN) OPERATOR REPORTED THE FOLLOWING TO MFG: DURING A PASSENGER FLIGHT THE LT UPPER ENGINE COWL ACCESS PANEL (PN 228-50080-801) DEPARTED THE ACFT DURING FLIGHT. THE INCIDENT PANEL WAS REMOVED FOR MX ON THE THRUST REVERSER THE NIGHT PRIOR TO THE INCIDENT FLIGH
- [SDR 2008FA0000358](https://openairdocs.org/sdr/2008FA0000358.md): Control Box · failed · May 19, 2008 · N779AZ · Cndair CL6002B16 · Trailing Edge Flap Control System
  > CREW REPORTED FLAP FAILURE DURING APPROACH APPROXIMATELY 8 HOURS AFTER INSTALLATION. RESET SYSTEM AND FLAPS WORKED FINE. FLEW AIRCRAFT HOME AND NO DISCREPANCIES. UNABLE TO DUPLICATE PROBLEM UNTIL SEVERAL WEEKS LATER DURING MAINTENANCE RUN. FLAPS WOULD IMMEDIAT
- [SDR CA070403005](https://openairdocs.org/sdr/CA070403005.md): Water Heater · odor · Mar 31, 2007 · Cndair CL6013A · Wash Water System
  > (CAN) WHILE EN ROUTE, A BURNING ODOR WAS NOTICED BY THE CREW AND PASSENGERS. NO SMOKE WAS APPARENT IN THE CABIN OR COCKPIT. THEN SEARCHED THE LAVATORY AND BAGGAGE COMPARTMENT. A TRACE OF SMOKE WAS FOUND IN THE BAGGAGE COMPARTMENT. A QUICK VISUAL INSPECTION
- [SDR 2007FA0000298](https://openairdocs.org/sdr/2007FA0000298.md): Inverter · shorted · Mar 20, 2007 · N5PG · Gulstm GVSPG550 · Electrical Power System
  > WHEN TURNING MAIN BATTERY SWITCHES ON, MECHANIC HEARD A LOUD POPPING SOUND, FOLLOWED BY THE AROMA OF SMOKE IN THE ENTRANCE AREA OF THE AIRCRAFT. THE FLOORBOARD WAS REMOVED AND FOUND THAT WATER FROM THE FORWARD LAVATORY AREA HAD BEEN RUNNING ONTO THE TOP OF TH
- [SDR CA070125001](https://openairdocs.org/sdr/CA070125001.md): Actuator · inoperative · Jan 25, 2007 · Cndair CL6012A12 · Landing Gear Actuator
  > (CAN) RT MAIN LANDING GEAR UNLOCK INDICATION APPROX. 15 - 20 MIN. AFTER ARRIVAL, NO PUMP, NO GEAR COMMAND, LOCK PARTIALLY MOVED TO UNLOCK POSITION. RETRACTING ACTUATOR REPLACED AND AC RETURNED TO SERVICE.
- [SDR CA061227006](https://openairdocs.org/sdr/CA061227006.md): Windshield · broken · Dec 27, 2006 · Cndair CL6013A · Flight Compartment Windows
  > (CAN) RT WINDSHIELD FACE PLY BROKEN IN FLIGHT. APPROX. 7000 INCH ON APPROACH. FOD INSPECTION CARRIED OUT ON ENGINE INTAKE AND WINDSHIELD REPLACED. A/C HOURS; 6836 A/C CYCLES; 7326 (TC NR 20061227006)
- [SDR CA061218015](https://openairdocs.org/sdr/CA061218015.md): Pump · damaged · Dec 18, 2006 · Cndair CL6013A · Hydraulic Pump (Electric/Engine), Main
  > (CAN) LOST OF NR 3 SYSTEM HYDRAULIC FLUID IN FLIGHT. THE NR 3B PUMP HAS FAILED ON FLANGE GASKET. THE PUMP HAS BEEN REPLACED AND A\C RETURNED TO SERVICE. A/C HOURS: 6816:27 A/C CYCLES; 7302 (TC NR 20061218015)
- [SDR CA061208001](https://openairdocs.org/sdr/CA061208001.md): Actuator · cracked · Dec 6, 2006 · Cndair CL6013A · Trailing Edge Flap Actuator
  > (CAN) DURING SCHEDULE LUBRICATION OF THE FLAP ACTUATORS, THE TECHNICIAN NOTICED GREASE WAS OOZING OUT OF A CRACKED WELD ON THE HOUSING OF THE LT OB FLAP ACTUATOR JACK SCREW. (TC NR 20061208001)
- [SDR CA061116003](https://openairdocs.org/sdr/CA061116003.md): Bulkhead · cracked · Nov 16, 2006 · Cndair CL600* · Wing, Rib/Bulkhead
  > (CAN) BULKHEAD STRUCTURE AT STATION 559.00 CRACKED ON TWO AILERON MIXER (P/N 600-91154-5) ATTACHMENTS BOLTS. A/C HOURS:25688 A/C CYCLES:30488
- [SDR CA061103011](https://openairdocs.org/sdr/CA061103011.md): Control Unit · failed · Nov 2, 2006 · Cndair CL600* · Trailing Edge Flap Control System
  > (CAN) DURING TAKE OFF FLAP FAIL DURING FLAP RETRACTION, A/C RETURN TO TERMINAL.BREAKER RESET AS PER OPERATING MANUAL NR 1 ABNORMAL PROCEDURE SECTION 10 P 3-4. A/C RETURN TO SERVICE,NO FURTHER SNAG.TWO MORE TAKE -OFF WERE CARRIED OUT FOLLOWING THAT INCIDENT,
- [SDR CA061010005](https://openairdocs.org/sdr/CA061010005.md): Flap System · malfunctioned · Oct 9, 2006 · Cndair CL6012A12 · Trailing Edge Flap Control System
  > (CAN) FLAP FAIL BETWEEN 20 DEGREES TO 0 DEGREE DURING RETRACTION OF THE FLAPS AT TAKEOFF, FLAPS RESET ON GROUND IAW OPERATING MANUAL NR 1 ABNORMAL PROCEDURE SECTION 10 P3-4. A/C RETURN TO SERVICE. NO SNAG. FLAP FAIL BETWEEN 20 DEGREES TO 0 DEGREE DURING RET
- [SDR CA060918001](https://openairdocs.org/sdr/CA060918001.md): Flap System · malfunctioned · Sep 18, 2006 · Cndair CL6012A12 · Trailing Edge Flap Control System
  > (CAN) FLAP FAILED ON TAKEOFF, A/C RETURNED AND LANDED SAFELY AT QB MAIN BASE, BREAKER WAS RESET IAW OPERATING MANUAL, COULDN`T DUPLICATED THE SNAG. A/C DID ONE FLIGHT AND RETURN TO BASE WITHOUT ANY SNAG.
- [SDR CA060828001](https://openairdocs.org/sdr/CA060828001.md): Pump · broken · Aug 28, 2006 · Cndair CL6012A12 · Engine Fuel Pump
  > (CAN) LT MAIN AND SCAVENGE EJECTOR FAILURE (MOTIVE FLOW FAILURE). FUEL PUMP SHAFT FOUND BROKEN. FUEL PUMP REPLACED AND AIRCRAFT RETURNED TO SERVICE. A/C HOURS; 25194:25 CYCLES; 29896 (TC NR 20060828001)
- [SDR CA060712003](https://openairdocs.org/sdr/CA060712003.md): Feeder Cable · arced · Jul 2, 2006 · Cndair CL6013A · Electrical Power System Wiring
  > (CAN) RT GEN TRIPPED OFFLINE DURING APPROACH. GEN OFF ANNUNCIATOR CAME ON, PWR AUTO TRANSFERED FROM GEN 1. NO LOSS OF PWR ON ANY AC BUSES. AC FERRIED WITH GENERATOR 2 SELECTED OFF. ON 3RD ENGINE RUN, PROBLEM WAS DUPLICATED. PROBLEM WAS ISOLATED TO A WIRING PRO
- [SDR CA060428002](https://openairdocs.org/sdr/CA060428002.md): Transformer · inoperative · Apr 28, 2006 · Cndair CL6012A12 · Attitude Gyro and Indicating System
  > (CAN) LOSS OF NR 1 MASI, NR 1 ALTIMETER, FDR, NR 1 ADI PITCH AND ROLL INFO, COMPASS INFO, NR 1 ESSENTIAL BUS AND LOSS 26 VAC. CAUSE OF FAULT FOUND TO BE BROKEN WIRES AT T2XD POST NR 3. TRANSFORMER LOCATED ON BACK OF C/B PANEL C. (TC NR 20060428002)
- [SDR DJFA2005143](https://openairdocs.org/sdr/DJFA2005143.md): Engine · overserviced · Sep 26, 2005 · N699CW · Cndair CL6002B16 · Turbine Engine Oil System
  > KAPA - KSMO - WHILE CLIMBING THROUGH 15,000 FEET, THE NR 2 ENGINE OIL TEMPERATURE BEGAN TO RISE INTO THE AMBER BAND. WHEN POWER WAS REDUCED THE OIL TEMPERATURE CONTINUED TO RISE INTO THE RED BAND. ENGINE POWER WAS REDUCED TO IDLE. AN EMERGENCY WAS DECLARED
- [SDR CA050920004](https://openairdocs.org/sdr/CA050920004.md): Wire · overheated · Sep 13, 2005 · Cndair CL6002B16 · Turbine Engine System Wiring
  > (CAN) POST FLIGHT INSPECTION REVEALED EVIDENCE OF OVERHEAT CONDITION FOUND AT 6 O'CLOCK POSITION AT THE COMBUSTOR SECTION FWD FRAME WHEN COWLINGS OPENED TO INVESTIGATE IDG FAILURE. MAINTENANCE PERSONNEL FOUND LOCALIZED AREA WITH OVERHEATED WIRE AND FUEL MANIF
- [SDR UG82005F00006](https://openairdocs.org/sdr/UG82005F00006.md): Warning Light · illuminated · Aug 15, 2005 · N241FB · Cndair CL6002B16 · Landing Gear Position and Warning
  > (REF CNTRL NR PA05003) THERE WAS NOT GREEN (DOWN AND LOCKED) INDICATION ON THE NOSE GEAR. THERE WAS ALSO NO RED (UNSAFE) INDICATION. THE CREW WENT THROUGH THE REQUIRED CHECKLIST AND DECLARED AN EMERGENCY TO TOWER. (K)
- [SDR UG82005F00010](https://openairdocs.org/sdr/UG82005F00010.md): Indicator · defective · Aug 15, 2005 · N241FB · Cndair CL6002B16 · Landing Gear Position and Warning
  > ( REF: PA 05-003) THERE WAS NO GREEN DOWN AND LOCKED INDICATION ON THE NOSE GEAR. THERE WAS ALSO NO RED UNSAFE INDICATION. THE CREW WENT THROUGH THE REQUIRED CHECKLIST AND DECLARED AN EMERGENCY TO KDAL TOWER. THERE WERE MULTIPLE FAILURES IN THE GEAR INDICAT
- [SDR 2005FA0001071](https://openairdocs.org/sdr/2005FA0001071.md): Tire · separated · Jun 19, 2005 · N241FB · Cndair CL6002B16 · Tire
  > (REF: PA05002) VIBRATION NOTED AT ROTATION SPEED. FLIGHT CREW RETURNED TO POINT OF ORIGIN AND LANDED UNEVENTFULLY. NR 4 TIRE TREAD SEPARATED. THE NR 4 MAIN WHEEL AND TIRE ASSY WERE CHANGED IAW MM. THE AC WAS THEN FERRIED TO A MAINTENANCE BASE TO REPAIR THE
- [SDR CA050324002](https://openairdocs.org/sdr/CA050324002.md): Sensor · inoperative · Jan 2, 2005 · Cndair CL6002B16 · Landing Gear Position and Warning
  > (CAN) ON JANUARY 02, 2005, AFTER TAKE OFF THE LANDING GEAR WERE SELECTED UP (RETRACT). LANDING GEAR REMAINED ON EXTENDED POSITION. AIRCRAFT RETURNED TO DEPARTURE AND LANDED SAFELY WITH NO INCIDENCE. POST FLIGHT INSPECTION REVEALED NO MECHANICAL DAMAGE. LT AND
- [SDR CA041223003](https://openairdocs.org/sdr/CA041223003.md): Engine · malfunctioned · Dec 23, 2004 · Cndair CL6013A · Engine (Turbine/Turboprop)
  > (CAN) UNCOMMANDDED ACCELERATION ON THE LT ENGINE ON TAKE OFF AROUND + 7 PERCENT ABOVE RETURN TO NORMAL 40 SECONDS LATER.
- [SDR DJFA2004032](https://openairdocs.org/sdr/DJFA2004032.md): Engine · malfunctioned · Nov 12, 2004 · N699CW · Cndair CL6002B16 · Engine (Turbine/Turboprop)
  > CREW REPORTED, THAT DURING CLIMB WHILE EN ROUTE FROM KBRO TO KATL CLIMB POWER WAS NOT ACHIEVED. THE NR 1 ENGINE POWER WAS 2 PERCENT LOWER THAN REQUIRED. AIRCRAFT DIVERTED TO KDAL. MAINTENANCE SWAPPED THE P2 AND T2 PROBES BETWEEN THE LEFT AND RIGHT ENGINES A
- [SDR ASOA04576](https://openairdocs.org/sdr/ASOA04576.md): Scavenge Pump · clogged · Aug 8, 2004 · N922EV · Cndair CL6002B19 · Turbine Engine Oil System
  > DURING CRUISE FROM AEX-DFW, AT APPROXIMATELY 22,000 FT WHILE FERRYING THE AIRCRAFT TO DFW THE CREW RECEIVED A RT ENGINE OIL PRESSURE WARNING. THE QRH WAS COMPLIED WITH AND THE CREW WAS ABLE TO MAINTAIN ADEQUATE THRUST TO MAINTAIN LEVEL FLIGHT AT 22,000 FT. T

Next page: https://openairdocs.org/engine/ge-cf34-3a/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 = 'CF343A'
ORDER BY difficulty_date DESC
```

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

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