# Service difficulty reports: GE CF34-3A1

A list on [GE CF34-3A1](https://openairdocs.org/engine/ge-cf34-3a1.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 28 · 1,372 reports

- [SDR CA190801004](https://openairdocs.org/sdr/CA190801004.md): Brake Disc · disintegrated · Jul 25, 2019 · Cndair CL6002B16 · Landing Gear Brake System
  > (CAN) WHEN TECHNICIAN TOW THE A/C INTO THE HANGAR, HE SAW BLACK POWDER ON THE GROUND. THE TECHNICIAN FOUND MAIN WHEEL BRAKE ASSY #3 OUTER STATOR & ROTOR DAMAGED. THE BRAKE AND THE WHEEL ASSEMBLIES WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. BRAKE SYSTE
- [SDR SWIA2019071946078](https://openairdocs.org/sdr/SWIA2019071946078.md): Engine · failed · Jul 17, 2019 · N868CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > LEFT ENGINE FAILURE DURING CLIMB OUT. DECLARED EMERGENCY, COMPLETED QRH, SHUTDOWN LEFT ENGINE IN FLIGHT. (FLT#3780) FO: 07/19/2019 CLOSED REMOVED AND REPLACED LT ENGINE IAW AMM. OPS AND LEAK CHECKS GOOD.
- [SDR CA190815007](https://openairdocs.org/sdr/CA190815007.md): Landing Gear · malfunctioned · Jul 9, 2019 · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > (CAN) NOSE GEAR DID NOT RETRACT AFTER SELECTING GEAR UP ON TAKE OFF. NOSE LANDING GEAR DOWN WHEN WHEN GEAR DISAGREE WARNING MESSAGE OCCURRED MSG OCCURRED 28 SECONDS AFTER THE HANDLE REMAINED UP AND THE QRH ACTIONED A MANUAL EXTENSION WAS PERFORMED AND THE GEA
- [SDR CA190620001](https://openairdocs.org/sdr/CA190620001.md): Autopilot Sys · faulted · Jun 15, 2019 · Cndair CL6002B19 · Auto Flight System
  > (CAN) FLT CREW EXPERIENCED AN UNCOMMANDED YAW MOTION, FULL DEFLECTION NOSE RIGHT WITH AP ON WHILE CRUISING AT MACH 0.74. MAINTENANCE ACTION: PERFORMED OPS TEST OF THE RUDDER CONTROL SYS AND RUDDER TRIM SYS WITH NO DEFECTS NOTED IAW AMM 27-21-00-710-801 & 802
- [SDR CA190529003](https://openairdocs.org/sdr/CA190529003.md): Director · faulted · May 25, 2019 · Cndair CL6002B19 · Central Display
  > (CAN) DISPLAY COOL CAUTION MESSAGE. RAN QRH DIDN`T RESOLVE ISSUE,REMOVED AND REPLACED DISPLAY COOL LOW FLOW EXHAUST SENSOR. (TC# 20190529003)
- [SDR CA190527016](https://openairdocs.org/sdr/CA190527016.md): Fairing · damaged · May 15, 2019 · Cndair CL6002B19 · Wing Main, Frame Structure
  > (CAN) LEFT WINGLET FAIRING DAMAGED DURING FLIGHT DESCENDING THROUGH 14000 FEET. MOST OF THE FAIRING WAS RIPPED OFF IN FLIGHT ALONG WITH THE LIGHTNING PROTECTION KIT. (TC# 20190527016)
- [SDR CA190521026](https://openairdocs.org/sdr/CA190521026.md): Skin · cracked · May 13, 2019 · Cndair CL6002B19 · Passenger/Crew Doors
  > (CAN) DURING INSPECTION OF THE PASSENGER DOOR INNER SKIN WE HAVE NOTICED 2-OFF CRACKS. (TC# 20190521026)
- [SDR CA190522004](https://openairdocs.org/sdr/CA190522004.md): Skin · corroded · May 3, 2019 · Cndair CL6002B19 · Passenger/Crew Doors
  > (CAN) PAX DOOR INNER SKIN BLENDED TO REMOVE SURFACE CORROSION UNDER CLOSING PLATE REF 601R318059. (TC# 20190522004)
- [SDR CA190522001](https://openairdocs.org/sdr/CA190522001.md): Tire · failed · May 2, 2019 · Cndair CL6002B19 · Tire
  > (CAN) ABORTED TAKEOFF AT APPROXIMATELY 90 KTS DUE TO A BURST TIRE. UPON INSPECTION #3 AND #4 MAIN TIRES WERE BURST. NOTHING WAS HIT ON THE RUNWAY DURING THE TAKEOFF ATTEMPT. CORRECTIVE ACTION: REPLACED #3 AND #4 MAIN WHEEL ASSY (TC# 20190522001)
- [SDR CA190522005](https://openairdocs.org/sdr/CA190522005.md): Skin · corroded · May 2, 2019 · Cndair CL6002B19 · Passenger/Crew Doors
  > (CAN) PAX DOOR INNER SKIN BLENDED UNDER ACCESS PANEL 832ER (TC# 20190522005)
- [SDR CA190522009](https://openairdocs.org/sdr/CA190522009.md): Panel · cracked · May 2, 2019 · Cndair CL6002B19 · Passenger/Crew Doors
  > (CAN) PAX DOOR AFT SIDE PANEL CORROSION AND CRACK. CORROSION HAS BEEN BLENDED IN SEVERAL AREAS. 1EA AREA IS DOWN TO.028 MIN. REMAINING. MAT. THK. SRM ALLOWS.029. ALSO 1EA SMALL CRACK AT BOTTOM EDGE OF PANEL ADJACENT TO THE ASSIST MOTOR PULLEY MOUNT.
- [SDR CA190425026](https://openairdocs.org/sdr/CA190425026.md): Frame · corroded · Apr 20, 2019 · Cndair CL6002B19 · Fuselage Main, Frame
  > (CAN) FRAME AT FS319 BLENDED TO REMOVE CORROSION BETWEEN STGR 25L AND 26L. (TC# 20190425026)
- [SDR CA190425027](https://openairdocs.org/sdr/CA190425027.md): Splice Strap · corroded · Apr 20, 2019 · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > (CAN) FS333 SPLICE STRAP BLENDED TO REMOVE SURFACE CORROSION BETWEEN STGR 25L AND 26L, FWD AND AFT OF THE FRAME AT FS333. (TC# 20190425027)
- [SDR CA190405014](https://openairdocs.org/sdr/CA190405014.md): Bpsu · failed · Apr 3, 2019 · Cndair CL6002B19 · Trailing Edge Flap Control System
  > (CAN) FLAP FAIL ON DEPARTURE, FLAPS AT 0, LEVER AT 0. COMPLIED WITH QRH. REPLACED FLAP BRAKE POSITION SENSOR UNIT (BPSU) (SEE ALSO FAA SDR #2019090100924/SWIA201904035713) (TC# 20190405014)
- [SDR CA190403010](https://openairdocs.org/sdr/CA190403010.md): Floorbeam · corroded · Apr 1, 2019 · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > (CAN) 1-OFF CORROSION DAMAGE TO FLOOR BEAM OUTBOARD FLANGE DIMENSIONS POST BLEND OUT ARE AS FOLLOWS: 0 1.625`L X 1.090`W X 0.035` MIN. REMAINING THK (0.060` NOM THK, REF) (TC# 20190403010)
- [SDR CA190322012](https://openairdocs.org/sdr/CA190322012.md): Intercostal · corroded · Mar 13, 2019 · Cndair CL6002B19 · Passenger/Crew Doors
  > (CAN) OPERATOR REPORTS CORROSION DAMAGE TO PAX DOOR INTERCOSTAL (TC# 20190322012)
- [SDR CA190227008](https://openairdocs.org/sdr/CA190227008.md): Pressure Switch · failed · Feb 21, 2019 · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > (CAN) RIGHT WING ANTI ICE CAUTION MESSAGE ON CLIMB OUT (SEE ALSO FAA SDR #2019081703527/SWIA2019022145537) (TC# 20190227008)
- [SDR CA190225008](https://openairdocs.org/sdr/CA190225008.md): Windshield · cracked · Feb 19, 2019 · Cndair CL6002B19 · Flight Compartment Windows
  > (CAN) UPON DESCENT, WINDSHIELD CRACKED (TC# 20190225008)
- [SDR CA190220017](https://openairdocs.org/sdr/CA190220017.md): Stator Vane · worn · Feb 15, 2019 · Cndair CL600* · Turbine Engine Compressor Section
  > (CAN) ENGINE ASSY P/N 6078T7G01, WAS INSTALLED. AT 12054:22 ENGINE HOURS, 11860 CYCLES, AS A PREVENTIVE ACTION, A SPECIAL DETAILED INSPECTION OF COMPRESSOR VARIABLE VANE SPINDLE AXIAL MOVEMENT HAS BEEN PERFORMED USING GUIDELINES AND LIMITS FROM GE HEAVY MAINT
- [SDR CA180404014](https://openairdocs.org/sdr/CA180404014.md): Gearbox · damaged · Apr 1, 2018 · Cndair CL6002B19 · Power Lever
  > (CAN) AIR TURNBACK, N1, N2 AND ITT FLUCTUATION ON CLIMB OUT. CORRECTIVE ACTION: REMOVED AND REPLACED RT THROTTLE GEAR BOX. PERFORMED IDLE SPEED CHECK. PERFORMED POWER ASSURANCE CHECK. OPS CHECKS GOOD. (TC# 20180404014)
- [SDR SWIA201642426](https://openairdocs.org/sdr/SWIA201642426.md): Engine · failed · Aug 7, 2016 · N783CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > DURING APP BASE LEG RIGHT ENGINE N1 FLUCTUATED AND NOTABLE A/C ENGINE VIBRATION @ 58 N1. VIBRATION STOPPED. DECLARED EMERGENCY WITH ATC. ON TAXI IN ENG TEMP WENT TO MAX TEMP OIL PRESSURE ZERO SHUT ENG DOWN. R&R THE RT ENGINE IAW AMM. OPS CHECK AND LEAK CH
- [SDR SWIA201641901](https://openairdocs.org/sdr/SWIA201641901.md): Engine · flamed out · Feb 19, 2016 · N498CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE FLAMED OUT AFTER TAKEOFF. ATTEMPTED TO RELIGHT ENGINE, UNSUCCESSFUL. CREW DECLARED AN EMERGENCY AND DIVERTED. CABIN WAS BRACED AND THE ACFT LANDED SAFELY. TAXIED TO THE GATE UNDER ITS OWN POWER. R & R RT ENGINE ASSY. OPS CHECKS AND LEAK CHECKS
- [SDR VNAA2016021900022](https://openairdocs.org/sdr/VNAA2016021900022.md): Carbon Seal · leaking · Feb 19, 2016 · N258PS · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > CREW REPORTED RECEIVING A RT ENGINE OIL PRESSURE MESSAGE DURING CRUISE AT FL310. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE NR 6 CARBON SEAL AND PERFORMED CHECKS IAW THE AM
- [SDR VNAA2016021900023](https://openairdocs.org/sdr/VNAA2016021900023.md): Carbon Seal · leaking · Feb 19, 2016 · N258PS · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > CREW REPORTED RECEIVING A RT ENGINE OIL PRESSURE MESSAGE DURING CRUISE AT FL310. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE NR 7 CARBON SEAL AND PERFORMED CHECKS IAW THE A
- [SDR CA160126009](https://openairdocs.org/sdr/CA160126009.md): Skin · cracked · Jan 24, 2016 · Cndair CL6002B19 · Wing, Plate/Skin
  > (CAN) LEFT WING LOWER PLANK 601R10045-11 DRAIN HOLE AT WS 85.5 BETWEEN S-14 AND S-15 HAS TWO (2) EACH CRACKS. THE FORWARD CRACK EMANATES FROM THE EDGE OF THE DRAIN HOLE TO THE FORWARD AND MEASURES 0.4 INCHES LONG. THE AFT CRACK EMANATES FROM THE EDGE OF THE DR
- [SDR CA160120016](https://openairdocs.org/sdr/CA160120016.md): Indicator · malfunctioned · Jan 18, 2016 · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > (CAN) DURING APPROACH GGN7336 CREW REPORTED FLAPS FAILURE TO ATC. WEATHER AT THE TIME INCLUDED LIGHT SNOW SHOWERS. CREW ELECTED TO CONTINUE TO DESTINATION AND PERFORM A FLAPLESS LANDING IN CYYZ AND DECLARE AN EMERGENCY IN ORDER TO HAVE EMERGENCY VEHICLES ON ST
- [SDR CA160121013](https://openairdocs.org/sdr/CA160121013.md): Flap System · failed · Jan 18, 2016 · Cndair CL6002B19 · Trailing Edge Flap Control System
  > (CAN) FLAPS FAIL AT 2 DURING APPROACH, QRM ACTIONED, MOC ADVISED. CARRIED OUT RESET OF FLAP SKEW DETECTION SYSTEM CARRIED OUT. LUBRICATION CARRIED OUT. OPERATIONAL TEST CARRIED OUT. OPERATIONAL TEST SKEW DETECTION SYSTEM.
- [SDR CA160121014](https://openairdocs.org/sdr/CA160121014.md): Flap System · warning message · Jan 18, 2016 · Cndair CL6002B19 · Trailing Edge Flap Control System
  > (CAN) FLAP FAIL MESSAGE ON LANDING, FLAP 0 LANDING CONDUCTED AS PER QRM CARRIED OUT LUBRICATION CARRIED OUT REMOVAL OF FLEX DRIVE SHAFTS CARRIED OUT LUBRICATION OF FLEX DRIVE SHAFTS CARRIED OUT OPERATIONAL TEST OF FLAPS.
- [SDR CA151221009](https://openairdocs.org/sdr/CA151221009.md): Control Lever · corroded · Dec 21, 2015 · Cndair CL6002B19 · Elevator Control System
  > (CAN) ELEVATOR JAM DUE TO CORRODED ELEVATOR CONTROL LEVERS. SOME OF THE MOVING PARTS IN THIS MECHANISM WERE FOUND STUCK DUE TO CORROSION AND THE ELEVATOR COULD NOT MOVE.
- [SDR CA151123008](https://openairdocs.org/sdr/CA151123008.md): Rotor · failed · Nov 23, 2015 · Cndair CL6002B16 · Brake
  > (CAN) AFTER LANDING, THE PILOT REPORTED RT INBD BRAKE JAM DURING TAXI. THE TECH FOUND 1 OF THE BRAKE ROTORS DESTROYED. THE UNIT WAS INSTALLED LAST WEEK AND OPERATED FOR JUST 53 CYCLES.
- [SDR CA151113003](https://openairdocs.org/sdr/CA151113003.md): Harness · damaged · Nov 11, 2015 · Cndair CL6002B19 · Landing Gear Steering System
  > (CAN) ON TAKEOFF ROLL F/O HAD NO DIRECTIONAL CONTROL, ABORTED TO, THE TERM NO DIRECTIONAL CONTROL MEANT THEY LOST NOSE WHEEL STEERING. REPLACED THE NOSE WHEEL STEERING HARNESS.
- [SDR CA151026002](https://openairdocs.org/sdr/CA151026002.md): Shield · worn · Oct 22, 2015 · Cndair CL6002B19 · Passenger/Crew Doors
  > (CAN) ON INVESTIGATION OF THE DOOR LOCKING SYS CAUTION MESSAGE ON THE EICAS, IT WAS NOTED THAT THE HINGE SHIELDS ON THE RAILING WERE NOT STAYING INSIDE THE RAILING WHEN THE DOOR WAS CLOSED. THE HINGE SHIELDS ARE IN A POSITION THAT IF THE DOOR WAS TO OPEN AND
- [SDR CA150916012](https://openairdocs.org/sdr/CA150916012.md): Fitting · cracked · Sep 15, 2015 · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > (CAN) COCKPIT WINDSHIELD CENTER POST LT LOWER FITTING CRACK DAMAGE.
- [SDR CA150908007](https://openairdocs.org/sdr/CA150908007.md): Skin · cracked · Sep 3, 2015 · Cndair CL6002B19 · Wing, Plate/Skin
  > (CAN) RT LOWER WING PLANK IS CRACKED AT WS148.019 AFT EDGE. CRACK WAS DISCOVERED WHILE PERFORMING S/B 601R-57-031 FOR THE INSPECTION OF THE LOWER WING PLANKS IN THE AREA OF THE JACK POINT FITTINGS.
- [SDR CA150809002](https://openairdocs.org/sdr/CA150809002.md): Priority Valve · failed · Aug 6, 2015 · Cndair CL6002B19 · Hydraulic System, Main
  > (CAN) AFTER T/O NOSE GEAR WOULD NOT COME UP. RECEIVED A GEAR DISAGREE WARNING MSG THEN NOSE GEAR RETRACTED ON ITS OWN AFTER A FEW MORE SECONDS.
- [SDR CA150730013](https://openairdocs.org/sdr/CA150730013.md): Tire · separated · Jul 29, 2015 · Cndair CL6002B16 · Tire
  > (CAN) AFTER LANDING, FLIGHT CREW DURING WALK AROUND INSPECTION NOTICED THAT NR 3 TIRE WAS MISSING A STRIP OF RUBBER, APPROXIMATELY 18" LONG X 4" WIDE. TIRE PRESSURE WAS VERIFIED, AT HOME BASE THE SAME DAY.
- [SDR CA150728009](https://openairdocs.org/sdr/CA150728009.md): Selector Valve · failed · Jul 24, 2015 · Cndair CL6002B19 · Landing Gear Selector
  > (CAN) ON LANDING APPROACH COMING INTO THE AIRPORT, UPON LANDING GEAR SELECTED DOWN IT WAS INDICATED THAT THERE WAS A PROBLEM WITH THE NOSE GEAR. THE PILOTS FLEW A GO AROUND AND DECLARED AN EMERGENCY, THE GEAR CAME DOWN SUCCESSFULLY WHEN THE ALTERNATE EXTENSION
- [SDR CA150724002](https://openairdocs.org/sdr/CA150724002.md): Handle · failed · Jul 20, 2015 · Cndair CL6002B19 · Landing Gear Selector
  > (CAN) AFTER MLG SYSTEM COMPONENT REPLACEMENT, ROUTINE GEAR SWINGS WERE CARRIED OUT ON AIRCRAFT. DURING ALTERNATE EXTENSION FUNCTION TEST, IT WAS DISCOVERED THAT THE ALTERNATE EXTENSION CONTROL HANDLE ASSEMBLY DID NOT OPERATE CORRECTLY. THE CONTROL HANDLE WAS B
- [SDR CA150713017](https://openairdocs.org/sdr/CA150713017.md): Actuator · failed · Jul 2, 2015 · Cndair CL6002B19 · Landing Gear Actuator
  > (CAN) ON APPROACH GEAR DISAGREE W, UPON LG EXTENSION SELECTION WITH RT MLG UNLOCKED INDICATION. LG RECYCLED & ALL DOWN LOCKED INDICATIONS OK. REPLACED RT MLG SIDE STAY ACTUATOR. ACFT RTS.
- [SDR CA150602017](https://openairdocs.org/sdr/CA150602017.md): Quick Disconnect · disconnected · May 31, 2015 · Cndair CL6002B19 · Nose/Tail Landing Gear
  > (CAN) DURING LANDING GEAR RETRACTION FOLLOWING MESSAGES APPEARED: NOSE DOOR OPEN GEAR DISAGREE WOW INPUT CAUTION MSG WOW OUTPUT FAIL THE CAPTAIN MADE THE EMERGENCY PROCEDUCE: GEAR DOWN IN EMERGENCY, AND EVERYTHING OK. AFTER LANDING, APPEARS NO STEERING MSG AN
- [SDR CA150519027](https://openairdocs.org/sdr/CA150519027.md): Disk · disintegrated · May 16, 2015 · Cndair CL6002B16 · Landing Gear Brake System
  > (CAN) UPON LANDING, 2 ROTATING DISKS OF NR 4 BRAKE ASSEMBLY HAVE DISINTEGRATED INTO FRAGMENTS. MAINTENANCE PERSONEL REPLACED THE ASSY TO CORRECT THE SITUATION AND REPLACED THE BRAKE CONTROL VALVES AND THE AFFECTED WHEEL ASSY AS PREVENTIVE MAINTENANCE.
- [SDR CA150312002](https://openairdocs.org/sdr/CA150312002.md): Line · worn · Mar 12, 2015 · Cndair CL6002B19 · Aircraft Fuel Distribution System
  > (CAN) DURING INSPECTION, FULE LINES IN THE LT WING TANK AT BS, LBL 22.50 DAMAGE TO PIPE ASSY AND RIB SUPPORT STRUCTURE WAS FOUND. WHILE IN AN UNLOADED CONDITION THE PIPE ASSY AND THE RIB SUPPORT STRUCTURE THERE IS APPROXIMATELY.5" OF CLEARANCE. THE PIPE ASS
- [SDR CA150112010](https://openairdocs.org/sdr/CA150112010.md): Transmitter · failed · Jan 7, 2015 · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > (CAN) IAS HI SPEED Q POPPED OUT AND THE ACFT STARTED TO CLIMB. FLAPS WERE MOVING UNCOMMANDED WITH FLAP HANDLE AT 0,FROM 0-2,0-8, 0-20. HYD 2B AND 3B CAUTION MSGS. AFTER APPROX. 3 CYCLES OF FLAP EXTENSION INDICATION FLAPS DEGRADED STATUS MSG APPEARED. FLAP P
- [SDR CA141215012](https://openairdocs.org/sdr/CA141215012.md): Wire · chafed · Nov 28, 2014 · Cndair CL6002B16 · Instrument System Wiring
  > (CAN) AFTER TOUCHDOWN, THE RIGHT THRUST REVERSER DEPLOYED WHEN COMMANDED BUT THE CREW WAS UNABLE TO STOW IT. ON THE SAME TIME, NO LIGHTS WERE SHOWN ON T/R CONTROL PANEL (UNSAFE, ARMED, REVERSER UNLOCKED) ON THE LEFT THRUST REVERSER. THE MAINTENANCE PERSONNEL
- [SDR CA141008018](https://openairdocs.org/sdr/CA141008018.md): Throttle Cable · broken · Oct 4, 2014 · Cndair CL6002B19 · Power Lever
  > (CAN) LOSS OF CONTROL OF LEFT THROTTLE ON CLIMB OUT. MAINTENANCE FOUND LEFT THROTTLE CABLE TO THROTTLE GEAR BOX BROKEN.
- [SDR VNAA2014083000019](https://openairdocs.org/sdr/VNAA2014083000019.md): Skin · dented · Aug 30, 2014 · N228PS · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > DURING SCHEDULED MAINTENANCE, THE RT ENGINE TRANSLATING COWL HAD TWO DENTS. REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR CA140821003](https://openairdocs.org/sdr/CA140821003.md): Proximity Switch · failed · Aug 19, 2014 · Cndair CL6002B16 · Landing Gear Position and Warning
  > (CAN) AT TAKEOFF, CREW SELECTED GEAR UP. THE MAIN GEAR RETRACTED AS NORMAL BUT THE NOSE GEAR FAILED TO RETRACT. INDICATIONS SHOWED NOSE GEAR STILL DOWN AND LOCKED. CREW SELECTED GEAR DOWN ALL GEAR EXTENDED AND INDICATED DOWN AND LOCKED. THE ACFT LANDED WITH
- [SDR CA160219006](https://openairdocs.org/sdr/CA160219006.md): Floor Skin · cracked · Jul 29, 2014 · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > (CAN) FOUND CRACKS LOCATED ON PRESSURE FLOOR STRUCTURE BS 461.5 BETWEEN RBL 9 AND LBL 9
- [SDR SWIA2014062338265](https://openairdocs.org/sdr/SWIA2014062338265.md): Bushing · galled · Jun 21, 2014 · N779CA · Cndair CL6002B19 · Engine Mount Section
  > LEFT ENGINE, YOKE MOUNT LINK BUSHINGS ARE GALLED. R & R LT ENGINE YOKE LINK IAW AMM.
- [SDR SWIA2014062338266](https://openairdocs.org/sdr/SWIA2014062338266.md): Pin · scored · Jun 21, 2014 · N779CA · Cndair CL6002B19 · Engine Mount Section
  > LEFT ENGINE, YOKE MOUNT PINS AND BOLTS SCORED. R & R LT ENGINE FWD YOKE MOUNT PINS AND BOLTS IAW AMM.

Next page: https://openairdocs.org/engine/ge-cf34-3a1/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 = 'CF343A1'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cf34-3a1/reports

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