# Service difficulty reports: GE CF34-8C5B1

A list on [GE CF34-8C5B1](https://openairdocs.org/engine/ge-cf34-8c5b1.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 9 · 418 reports

- [SDR N6WA2026100101](https://openairdocs.org/sdr/N6WA2026100101.md): Engine · vibration · Sep 30, 2026 · N549GJ · Cndair CL6002C11 · Engine (Turbine/Turboprop)
  > R ENG HIGH VIBE AT 1.8-2.0 MILS - UNSCHED LANDING AT STL, PERFORM HIGH TORQUE PIN INSPECT WITH IN 15FC PER AMM 72-21-02. COMPLIED WITH FAN BLADE SHAKE IAW AMM 72-21-02, NO DEFECTS NOTED. COMPLIED WITH ENG HIBE CHECK. HIGHEST VIBE AT 0.3. IAW AMM 71-00-00-720
- [SDR VNAA2026082123301](https://openairdocs.org/sdr/VNAA2026082123301.md): Pin · failed · Aug 21, 2026 · N500AE · Cndair CL6002C10 · Turbine Engine Compressor Section
  > RT ENGINE HIGH VIBE IN FLIGHT. REMOVED AND REPLACED RH FAN BLADE PINS IAW CRJ7 AMM 72-21-02-000/400-801-A01-PSA.
- [SDR N6WA2026080503](https://openairdocs.org/sdr/N6WA2026080503.md): Anti-Ice Valve · warning message · Aug 1, 2026 · N580GJ · Cndair CL6002C11 · Engine Anti-Icing System
  > LEFT COWL ANTI-ICE CAUTION MSG IN FLIGHT(B1-039268/ L COWL A/ICE SOV/ SOV SW POSITION MISMATCH). DEFERRED COWL ANTI-ICE VALVE ON OCN 70102844 PER MEL 30-22-01 CAT C. CORRECT PRIOR TO 08/12/2026. AUTHORIZED BY MXC.
- [SDR N6WA2026070804](https://openairdocs.org/sdr/N6WA2026070804.md): Clamp · loose · Jul 6, 2026 · N538GJ · Cndair CL6002C11 · Engine Bleed Air System
  > R BLEED DUCT WARNING AT FL 270. R & R ALL WORN OUT & LOOSE FITTING P-CLAMPS ON BLEED AIR LEAK AIR DETECTION LOOP IN AFT EQUIPMENT BAY IAW CRJ 550 AMM 36-21-01, 36-21-03 & 36-21-00. PERFORMED OPS CHECK IAW CRJ 550 AMM 36-21-00-710-801-A01, OPS CHK SATISFACTORY
- [SDR SWIA2026060776666](https://openairdocs.org/sdr/SWIA2026060776666.md): Thrust Shaft · gouged · Jun 7, 2026 · N632SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > LEFT ENG AFT THRUST SHAFT HAS SMALL GOUGING ON SURFACE THAT SLIDES INTO THRUST FITTING. REMOVED AND REPLACED LT ENGINE AFT THRUST SHAFT IN REFERENCE TO AMM 71-22-01. SEE CP 32395243 FOR ENGINE CHANGE TASK CARD.TORQUE WRENCH INFORMATION: S/N: 0304100422 DATE
- [SDR SWIA2026031477510](https://openairdocs.org/sdr/SWIA2026031477510.md): Skin · punctured · Mar 14, 2026 · N611SK · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > PUNCTURE DAMAGE ON UPPER FAN COWL DOOR. REPAIRED DAMAGE ON UPPER FAN COWL DOOR OUTER SKIN IAW REO 670-54-14-1342, REV -.
- [SDR SWIA2026031477512](https://openairdocs.org/sdr/SWIA2026031477512.md): Thrust Shaft · loose · Mar 14, 2026 · N611SK · Cndair CL6002C10 · Engine Mount Section
  > BEFORE REMOVING HI-LOKS ON LT & RT ENGINES AFT MOUNT, AFT SIDE OF THRUST SHAFT HOLE STARTED TO SPIN. CONFIRMED LT & RT ENGINE AFT MOUNT THRUST AFT FASTENERS HOLES ARE WITHIN LIMITS. DURING INVESTIGATION NOTED HOLE 4 RT LWR HOLE TO HAVE DAMAGE IN COUNTER BOR
- [SDR SWIA2026031477514](https://openairdocs.org/sdr/SWIA2026031477514.md): Anchor Nut · mechanic error · Mar 14, 2026 · N611SK · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > MISSED DRILLED ANCHOR NUT ON LH ENGINE UPPR FWD TORQUE BOX BEAM FAN COWL ATTACHMENT HN00301025 MARKED HN00301025 C-CHECK RO 09302026FABRICATED AND INSTALLED REPAIR FITTING TO THE LH ENGINE UPPER TRUST REVERSER REF REO 670-54-22-166 REV -- 2026-07-22 AND REO 6
- [SDR SWIA2026022477507](https://openairdocs.org/sdr/SWIA2026022477507.md): Door · gouged · Feb 24, 2026 · N611SK · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > GOUGE ON INTERIOR AND PROTRUDING DENT ON EXTERIOR ON LOWER RT FAN COWL DOOR, 8 O`CLOCK. PERFORMED A CUT OUT OF DAMAGE IAW SRM 54-14-00-201-001-A01, FABRICATED, LOCATED, DRILLED, AND INSTALLED DOUBLER IAW SRM 54-14-00-201-001-A01, SRM 54-14-00-201-001-A01.
- [SDR SWIA2026021977505](https://openairdocs.org/sdr/SWIA2026021977505.md): Coaming · chafed · Feb 19, 2026 · N611SK · Cndair CL6002C10 · Engine Thrust Reverser
  > RT UPPER TRANCCOWL INNER COAMING IS CHAFED FWD LATCH. COMPLIED WITH REPAIR OF THE RT UPPER TRANCCOWL INNER COAMING IAW REO 670-54-21-1812, REV-.
- [SDR SWIA2026021977506](https://openairdocs.org/sdr/SWIA2026021977506.md): Stiffener · gouged · Feb 19, 2026 · N611SK · Cndair CL6002C10 · Engine Thrust Reverser
  > RT UPPER TRANSCOWL ZED STIFFENER IS GOUGED. REPAIRED RT UPPER TRANSCOWL IAW REO 670-54-21-1810 REV -.
- [SDR SWIA2026021977508](https://openairdocs.org/sdr/SWIA2026021977508.md): Coaming · cracked · Feb 19, 2026 · N611SK · Cndair CL6002C10 · Engine Thrust Reverser
  > LH UPPER TRANSCOWL INNER COAMING IS CRACKED. REPAIRED WITH NEW LH UPPER TRANSCOWL INNER COAMING IAW REO 670-54-21-1803 REV --
- [SDR SWIA2026021977511](https://openairdocs.org/sdr/SWIA2026021977511.md): Stand Off · cracked · Feb 19, 2026 · N611SK · Cndair CL6002C10 · Engine Thrust Reverser
  > LT UPPER TRANSCOWL OTBD A BRACKET STANDOFF SUSPECTED CRACKED. LT UPPER TRANSCOWL OTBD A BRACKET WAS REMOVED AND REPLACED IAW REO 670-54-21-971, REV -B,
- [SDR SWIA2026021977513](https://openairdocs.org/sdr/SWIA2026021977513.md): Stiffener · loose · Feb 19, 2026 · N611SK · Cndair CL6002C10 · Engine Thrust Reverser
  > LEFT LOWER TRANSCOWL ZEE STIFFENER RIVETS ARE PULLED LOOSE. REPAIRED INNER SKIN UNDER ZEE STIFFENER ON LH LOWER TRANSCOWL REF REO 670-54-21-1806 REV --, 2026-03-09 COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
- [SDR VNAA2026020811901](https://openairdocs.org/sdr/VNAA2026020811901.md): Compressor · stalled · Feb 4, 2026 · N705PS · Cndair CL6002C10 · Turbine Engine Compressor Section
  > COMPRESSOR STALL AT ROTATION RT ENGINE. REMOVED & REPLACED RT ENGINE ASSEMBLY IAW AMM 71-00-00-400-801-A02-PSA. OPS & LEAK CHECK GOOD AT THIS TIME.
- [SDR SWIA20251223017](https://openairdocs.org/sdr/SWIA20251223017.md): Engine · failed · Dec 17, 2025 · N797SK · Cndair CL6002C10 · Engine Oil Quantity
  > RIGHT ENGINE OIL PRESSURE WARNING MESSAGE IN FLIGHT. LEAD TO LOSS OF ENGINE INFLIGHT HAD TO RETURN TO TUS SINGLE ENGINE LANDING. (FLIGHT 6088) REPLACED RT ENGINE WITH SERVICABLE ENGINE IAW AMM 71-00-00-400-801-A02. OPS CHECKED GOOD. LEAK CHECKED GOOD. COMPL
- [SDR N6WA2025091801](https://openairdocs.org/sdr/N6WA2025091801.md): Cascade · damaged · Sep 16, 2025 · N501GJ · Cndair CL6002C11 · Engine (Turbine/Turboprop)
  > RIGHT ENGINE, NR 2 UPPER OTBD CASCADE DAMAGED. REMOVED AND REPLACED RT ENGINE UPPER OTBD CASCADE IAW AMM 78-34-01
- [SDR VNAA2025041511103](https://openairdocs.org/sdr/VNAA2025041511103.md): Bleed Valve · torn · Apr 14, 2025 · N527EA · Cndair CL6002C10 · Compressor Bleed Valve
  > L BLEED DUCT WARNING MSG WHILE CLIMBING THROUGH FL 210 / FOUND INSULATION MUFF FOR THE CROSS BLEED VALVE TORN. REMOVED AND REPLACED INSULATION MUFF IAW CRJ-700 AMM 36-13-15-400-801 AND 36-21-00-910-801. OPS TEST AND LEAK TEST GOOD. L BLEED DUCT WARNING MSG DID
- [SDR VNAA20250329012](https://openairdocs.org/sdr/VNAA20250329012.md): Exhaust Cone · dented · Jan 26, 2025 · N539EA · Bombdr CL6002D15 · Engine Collector/Tailpipe/Nozzle
  > DENT ON EXHAUST NOZZLE BTW 9-10 O'CLOCK POSITION AT RH ENGINE. DENT ON EXHAUST NOZZLE BTW 9-10 O'CLOCK POSITION AT RH ENGINE WAS REPAIRED PER REO 670-51-00-085 REV.-A AND PER REO 670-54-15-933 REV - -
- [SDR VNAA2024121711101](https://openairdocs.org/sdr/VNAA2024121711101.md): Engine · fumes · Oct 26, 2024 · N505AE · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > ON DESCENT, THE FLIGHT CREW REPORTED FUMES IN COCKPIT IN FLIGHT, SMELLING OF TIRES AND OCCASIONAL BURNING. THE LOCATION OF THE FUMES WAS IN THE COCKPIT AND FORWARD JUMP SEAT AREA. THE CAPTAIN WAS EVALUATED BY PARAMEDICS DUE TO THE HEADACHE THAT FORMED FROM THE
- [SDR VNAA202409270001](https://openairdocs.org/sdr/VNAA202409270001.md): Duct · gouged · Sep 27, 2024 · N708PS · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > RIGHT HAND ENGINE LOWER C-DUCT LEADING EDGE CHAFFED AND GOUGED. COMPLETE: COMPLIED WITH ALL THE STEPS OF REO 670-54-23-1272 REV -- DATED 2024-08-27. ENSURED BLEND OUT WAS PERFORMED TO A SMOOTH CONTOUR, ENSURED COMPLETE DAMAGE REMOVAL, ENSURED DID NOT EXCEED R
- [SDR SWIA2024060400528](https://openairdocs.org/sdr/SWIA2024060400528.md): Engine · odor · May 28, 2024 · N784SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > STRONG FUEL ODOR OBSERVED IN CABIN DURING DESCENT AND LANDING. GROUND CABIN OBSERVED WHITE/BLUE SMOKE COMING FROM LEFT ENGINE AS AIRCRAFT APPROACHED THE GATE WITH BOTH ENGINES RUNNING. SMOKE DECREASED IN INTENSITY AFTER ENGINE WAS SHUT DOWN, BUT WHITE SMOKE CO
- [SDR N6WA2022091901](https://openairdocs.org/sdr/N6WA2022091901.md): Engine · vibration · Sep 14, 2022 · N573GJ · Cndair CL6002C10 · Engine Ignition Analyzer
  > ENG 2 VIB N1 AMBER RANGE (1.9). R AND R FAN BLADE PINS AND BUMPERS IAW CRJ 550 AMM 72-21-02, PERFORMED ENGINE RUNS AT IDLE AND 1.0MIL OBSERVED, RUN AT TOGA 3.7 -3.8 OBSERVED N1 VIBRATION. ENGINE RUNS AND BALANCE TRIM IAW AMM 71-00-00. OPS AND N1 VIBE CHECK GOO
- [SDR N6WA2022053002](https://openairdocs.org/sdr/N6WA2022053002.md): Engine · failed · May 29, 2022 · N541GJ · Cndair CL600* · Fuel Control/Reciprocating Engines
  > LEFT ENGINE SHOWS NO N1 DURING START.PERFORMED TWO ENGINE STARTS IAW CRJ 550 AMM 71-00-00. OPS CHECK GOOD. NO L ENG DEGRADED CAUTION MESSAGE PRESENT
- [SDR VNAA202205091111](https://openairdocs.org/sdr/VNAA202205091111.md): Engine · shutdown · May 6, 2022 · N540EG · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > WHILE ON BASE TO FINAL INTO GRR, THE LEFT ENGINE FAILED AND SHUTDOWN, CAPTAIN VERIFIED THEY DID NOT SHUT THE ENGINE. DUE TO THE PHASE OF FLIGHT (LANDING), THEY CONTINUED ON WITH THE APPROACH AND THE CAPTAIN HAD THE FO CALL BACK TO THE FA TO ASK IF THEY SAW ANY
- [SDR SWIA202266002](https://openairdocs.org/sdr/SWIA202266002.md): Coaming · cracked · May 5, 2022 · N607SK · Cndair CL6002C10 · Engine Thrust Reverser
  > UPON REMOVAL OF THE LEFTHAND ENGINE UPPER TRANSCOWL COAMING AND STIFFENER FOUND INTERNAL STRUCTURE SECTION MISSING AND CRACKED (C-CHECK RO 7/8/2022) PERMENANTLY REPAIRED L/H UPPER TRANSCOWL INTERNAL STRUCTURE UNDER STIFFNER REF MHIRJ REO 670-54-21-1537
- [SDR SWIA202266001](https://openairdocs.org/sdr/SWIA202266001.md): None · gouged · May 4, 2022 · N607SK · Cndair CL6002C10 · Engine Exhaust System
  > DOUBLER GOUGED ON LEFTHAND ENGINE UPPER TRANSCOWL (C-CHECK RO 7/8/2022) DOUBLER GOUGED ON LEFTHAND ENGINE UPPER TRANSCOWL REPAIRED REF REO# 670-54-21-1207, REV A, DATED 8/27/15 AND FULLY COMPLIED W/SKYCARD 51-900-1002-SKY.
- [SDR SWIA202266000](https://openairdocs.org/sdr/SWIA202266000.md): Latch · chafed · May 3, 2022 · N607SK · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > LEFT ENG. LOWER TRANS COWL HAS CHAFFING ON THE LEADING EDGE NEAR THE 1ST LATCH. (MARKED) (C-CHECK RO 7/8/2022) REMOVED AND REPLACED CHAFED LATCH DOOR COAMING P/N CN624-2061-205. REF AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1207 FIGURE 6, REV A, DATE
- [SDR VNAA202203241111](https://openairdocs.org/sdr/VNAA202203241111.md): Engine · vibration · Mar 22, 2022 · N536EA · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > 5206/22MAR CLT-LFT TAIL 536 ENGINE VIBE WARNING, FOLLOWED QRH, UNABLE TO CLIMB FURTHER. RETURNING TO CLT. EMERGENCY DECLARED 0235Z ENGINE VIBE WENT UP TO 2.0 LANDED OVERWEIGHT, BUT WITHOUT FURTHER/OTHER ISSUE 70.4 - 70 LANDING WEIGHT. L ENGINE VIB WENT TO 2.0
- [SDR VNAA202202021111](https://openairdocs.org/sdr/VNAA202202021111.md): Bleed Valve · broken · Jan 31, 2022 · N545PB · Cndair CL6002C10 · Compressor Bleed Valve
  > DIVERSION TO CHO DUE TO FUEL LEAK ENROUTE. FLIGHT WAS ABLE TO LAND SAFELY IN CHO. UPON ARRIVAL INTO CHO, THE CREW NOTICED SMOKE COMING OUT OF THE RIGHT ENG. THEY DECIDED TO DEPLANE ON THE TAXIWAY AND CALL FIRE DEPARTMENT OVER. NO INJURIES WERE REPORTED AND ALL
- [SDR VNAA202201271111](https://openairdocs.org/sdr/VNAA202201271111.md): Compressor · fod · Jan 25, 2022 · N532EA · Cndair CL6002C10 · Fuel Controlling System
  > TAKING OFF OUT OF DCA THE RH ENGINE DID NOT ACHIEVE TAKEOFF POWER SO THE TAKEOFF WAS ABORTED. RH ENG LOW PWR ON TAKE OFF ROLL HIGH SPEED ABORT. REMOVED AND REPLACED FUEL METERING UNIT IAW 73-21-03-000/400-801-A01. OPS AND LEAK CHECK OF THE FMU GOOD AT THIS TI
- [SDR V0XD20220127003](https://openairdocs.org/sdr/V0XD20220127003.md): Housing · gouged · Jan 6, 2022 · N525AE · Cndair CL6002C10 · Engine Cowling System
  > R/H ENG LOWER COWLING AFT LATCH HOUSING UNDER PANEL 443 AR HAS A GOUGED. CORRECTIVE ACTION: BLENDED TO SMOOTH PROFILE GOUGED AREA AT AFT LATCH HOUSING UNDER PANEL 443 AR IAW CRJ 700 A.E # 22-C7-54-062.
- [SDR N6WA2021120201](https://openairdocs.org/sdr/N6WA2021120201.md): Check Valve · damaged · Dec 1, 2021 · N523GJ · Cndair CL600* · Powerplant System
  > RH ENGINE FLAMEOUT. PERFORMED CRJ FIM 72-00-00-810-805 FOR RT ENG FLAMEOUT, PERFORMED BOROSCOPE OF COMBUSTION HPT & LPT IAW CRJ 550 AMM 72-44-00 & 72-51-01 & 72-56-00 WITH NO DEFECTS FOUND. PERFORMED DVI OF BLEED ECS SYSTEM AND FOUND SIXTH STAGE CHECK VALVE DA
- [SDR VNAA202111301111](https://openairdocs.org/sdr/VNAA202111301111.md): Transmitter · unserviceable · Nov 30, 2021 · N531EG · Cndair CL6002C10 · Engine Oil Indicating System
  > IN FLIGHT AT APPROX 8000FT, WE NOTICED RH OIL PRESS INDICATION OF ZERO, RAN QRC/QRH FOR NON MSG LOW OIL PRESSURE. OIL PRESSURE REMAINED AT ZERO, OIL TEMP INCREASING QRH DROVE US TO TO SHUT DOWN RH ENGINE; DID NOT RECEIVED THE RH ENG OIL PRESSURE WARNING MSG, O
- [SDR SWIA202163691](https://openairdocs.org/sdr/SWIA202163691.md): None · shifted · Nov 30, 2021 · N796SK · Cndair CL600* · Engine Exhaust System
  > DURING INSTALL OF THE R/H UPPER TRANSCOWL, FOUND OUTBOARD SLIDER TRACK INSERT TO HAVE SHIFTED FORWARD. (C CHECK RO 01-05-2022) REMOVED AND REPLACED R/H UPER TRANSCOWL OUTBOARD TRACK INSERT IAW CRJ 700 78-33-05-960-801-A02
- [SDR N6WA202108030101](https://openairdocs.org/sdr/N6WA202108030101.md): Bleed Valve · leaking · Aug 1, 2021 · N514MJ · Cndair CL600* · Compressor Bleed Valve
  > FUEL LEAK LH ENGINE. R&R OBV VALVE ON #1 ENG IAW CRJ 550 AMM 75-31-01. OPS CHECK GOOD AT THIS TIME. NO LEAKS NOTED AT THIS TIME.
- [SDR N6WA2020122601](https://openairdocs.org/sdr/N6WA2020122601.md): Engine · flamed out · Dec 26, 2020 · N508GJ · Cndair CL600* · Engine (Turbine/Turboprop)
  > RT ENGINE FLAME OUT TWICE IN FLIGHT. PERFORMED INSPECTION OF RT ENGINE FOR ITT EXCEEDANCE MESSAGE ON EICAS, IAW CRJ FIM TASK 72-00-00 REFER TO LOG PG 494489 DISCREPANCY FOR WORK DONE. R & R NR 2 ENGINE, IAW CRJ550 AMM 71-00-00
- [SDR SWIA202054912](https://openairdocs.org/sdr/SWIA202054912.md): Slider · gouged · Nov 17, 2020 · N787SK · Cndair CL6002C10 · Engine Thrust Reverser
  > LEFT ENGINE TRANSLATING COWL SLIDER INBOARD GOUGED. C-CHECK RO 12/28/2020. REPAIRED LT T/R UPPER INBOARD SLIDER, REF REO. ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD.
- [SDR N6WA2020110601](https://openairdocs.org/sdr/N6WA2020110601.md): Transcowl · cracked · Nov 6, 2020 · N540GJ · Cndair CL600* · Engine Thrust Reverser
  > RT LOWER T/R EXTRUSION CRACKED ON INBOARD SIDE. REMOVED AND REPLACED RT LOWER TRANS COWL, IAW CRJ 700 AMM 78-33-01. PERFORMED OPERATIONS CHECK, NO DEFECTS FOUND.
- [SDR SWIA202052574](https://openairdocs.org/sdr/SWIA202052574.md): Latch · worn · Aug 10, 2020 · N784SK · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > THUMB LATCH TAB ON RIGHT LOWER TRANS COWL WORN, MARKED. C-CHECK RO 9/20/2020. REPLACED RT LOWER TRANSCOWL LATCH DOOR COAMING, PER REO SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2019111246761](https://openairdocs.org/sdr/SWIA2019111246761.md): Engine · malfunctioned · Nov 12, 2019 · N780SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > WHILE SETTING THRUST FOR TAKEOFF, THE ENGINE NEVER SPOOLED UP PAST 56% N1, EVEN WHEN INSIDE THE CLIMB DETENT. ABORTED TAKEOFF, COMPLIED WITH REJECTED TAKEOFF QRH PROCEDURE, AND RETURNED TO GATE. FLIGHT # 5341 CLOSED VERIFIED ABORTED TAKE-OFF INSPECTION NOT
- [SDR SWIA2019101846547](https://openairdocs.org/sdr/SWIA2019101846547.md): Engine · contaminated · Oct 17, 2019 · N764SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > RECEIVED SMOKE AFT AFT WARNING MESSAGE. COMPLETED QRH AND RETURNED TO FIELD. FLIGHT ATTENDANTS AND PILOTS NOTICED FUMES BUT NO SMOKE IN CABIN (FLT#3210) CLOSED AFTER SOME INVESTIGATION, FOUND THE A #1 ENGINE COMPRESSOR WASH WAS COMPLETED THE PREVIOUS NIGHT P
- [SDR VNAA2019092511101](https://openairdocs.org/sdr/VNAA2019092511101.md): Blade · damaged · Sep 25, 2019 · N719PS · Cndair CL6002C10 · Turbine Engine Compressor Section
  > DURING TAKE OFF FROM RUNWAY 36R AT 100 KNOTS THE CREW BELIEVED THEY BLEW A TIRE AND REJECTED THE TAKE OFF. THE AIRCRAFT TAXIED BACK TO THE GATE UNDER IT'S OWN POWER. MX INSPECTED AND FOUND DAMAGE TO RT ENGINE FAN BLADES. BORESCOPE INSPECTION REVEALED ENGINE
- [SDR SIMA2019082219006](https://openairdocs.org/sdr/SIMA2019082219006.md): Indication Sys · unknown · Aug 19, 2019 · N536EA · Cndair CL6002C10 · Engine Oil Temperature
  > AT LEVEL OFF 13,000' 0 LEFT OIL TEMP WENT AMBER AND RED. WENT IDLE, TEMP WENT BACK AMBER, THEN WENT 147-149 AFTER 10 MIN TEMP STAYED 135 TO 137. TAXI, TAFF, CLIMB NORMAL OPS. CHECKED IAW FIM 79-30-00-810-810 RAR #1 ENGINE OIL LEVEL/OIL TEMPERATURE SENSOR IA
- [SDR 19EA201910075121](https://openairdocs.org/sdr/19EA201910075121.md): Engine · seized · May 12, 2019 · N24EA · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > ENGINE WOULD NOT START. DISCOVERED ENGINE PHYSICALLY WOULD NOT ROTATE. SENT TO ENGINE SHOP FOR EVALUATION
- [SDR CA190522014](https://openairdocs.org/sdr/CA190522014.md): Engine · contaminated · May 11, 2019 · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > (CAN) AFT LAV SMOKE WARNING MESSAGE ON ROTATION FOUND EVIDENCE OF OIL COKING ON STAGE 3 STATOR PLATFORM AND ON THE LEADING EDGE OF 5TH STAGE ROTOR DURING BOROSCOPE OF LEFT ENGINE. R/R LEFT ENGINE. (TC# 20190522014)
- [SDR SWIA2019050645828](https://openairdocs.org/sdr/SWIA2019050645828.md): Pin · defective · May 6, 2019 · N774SK · Cndair CL6002C10 · Turbine Engine Compressor Section
  > ENGINE 1 N1 VIBRATION. AT CRUISE, MOVED THROTTLES FROM CLIMB TO CRUISE RANGE. N1 VIBRATION INCREASED TO 2.1 WITH NOTICEABLE VIBRATION CHANGE AND SOUND. CONTINUED TO DECREASE POWER UNTIL VIBRATION IN NORMAL RANGE. ENGINE VIBRATION WOULD THEN INCREASE AGAIN INTO
- [SDR N6WA2019012602](https://openairdocs.org/sdr/N6WA2019012602.md): Engine · fire · Jan 26, 2019 · N167GJ · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > RT ENG FIRE INFLIGHT.
- [SDR N6WA20190205601](https://openairdocs.org/sdr/N6WA20190205601.md): Engine · fire · Jan 26, 2019 · N167GJ · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > RIGHT ENGINE FIRE IN FLIGHT. REMOVED AND REPLACED RIGHT ENGINE IAW CRJ700 AMM 71-00-00. AIRCRAFT RELEASED 1/31/2019
- [SDR SIMA2018121211003](https://openairdocs.org/sdr/SIMA2018121211003.md): Compressor · contaminated · Dec 11, 2018 · N531EG · Cndair CL6002C10 · Turbine Engine Compressor Section
  > DURING CLIMB THROUGH APPROXIMATELY 9,000FT VMC AIRCRAFT CLEAN CONFIG NO ICING. M.W. FOR AFT LAV SMOKE ILLUMINATED. PAX AND CREW NOTICED ODOR. ALERT EXTINGUISHED AFTER APPROXIMATELY 1 MINUTE OR SO. ODOR LIKENED TO BURNING EXHAUST. LDG WT UNDER 64,000 #'S.-C/A-N

Next page: https://openairdocs.org/engine/ge-cf34-8c5b1/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 = 'CF348C5B1'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cf34-8c5b1/reports

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