GE CF34-8C5B1

Service difficulty reports · 418

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR N6WA2026100101Engine · vibrationR 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 71-00-00-720Sep 30, 2026 · N549GJ · Cndair CL6002C11 · Engine (Turbine/Turboprop)SDR VNAA2026082123301Pin · failedRT ENGINE HIGH VIBE IN FLIGHT. REMOVED AND REPLACED RH FAN BLADE PINS IAW CRJ7 AMM 72-21-02-000/400-801-A01-PSA.Aug 21, 2026 · N500AE · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR N6WA2026080503Anti-Ice Valve · warning messageLEFT 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.Aug 1, 2026 · N580GJ · Cndair CL6002C11 · Engine Anti-Icing SystemSDR N6WA2026070804Clamp · looseR 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 SATISFACTORYJul 6, 2026 · N538GJ · Cndair CL6002C11 · Engine Bleed Air SystemSDR SWIA2026060776666Thrust Shaft · gougedLEFT 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 Jun 7, 2026 · N632SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SWIA2026031477510Skin · puncturedPUNCTURE DAMAGE ON UPPER FAN COWL DOOR. REPAIRED DAMAGE ON UPPER FAN COWL DOOR OUTER SKIN IAW REO 670-54-14-1342, REV -.Mar 14, 2026 · N611SK · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR SWIA2026031477512Thrust Shaft · looseBEFORE 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 BORMar 14, 2026 · N611SK · Cndair CL6002C10 · Engine Mount SectionSDR SWIA2026031477514Anchor Nut · mechanic errorMISSED 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 6Mar 14, 2026 · N611SK · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR SWIA2026022477507Door · gougedGOUGE 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.Feb 24, 2026 · N611SK · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR SWIA2026021977505Coaming · chafedRT 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-.Feb 19, 2026 · N611SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2026021977506Stiffener · gougedRT UPPER TRANSCOWL ZED STIFFENER IS GOUGED. REPAIRED RT UPPER TRANSCOWL IAW REO 670-54-21-1810 REV -.Feb 19, 2026 · N611SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2026021977508Coaming · crackedLH UPPER TRANSCOWL INNER COAMING IS CRACKED. REPAIRED WITH NEW LH UPPER TRANSCOWL INNER COAMING IAW REO 670-54-21-1803 REV --Feb 19, 2026 · N611SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2026021977511Stand Off · crackedLT 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,Feb 19, 2026 · N611SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2026021977513Stiffener · looseLEFT 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-SKYFeb 19, 2026 · N611SK · Cndair CL6002C10 · Engine Thrust ReverserSDR VNAA2026020811901Compressor · stalledCOMPRESSOR 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.Feb 4, 2026 · N705PS · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR SWIA20251223017Engine · failedRIGHT 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. COMPLDec 17, 2025 · N797SK · Cndair CL6002C10 · Engine Oil QuantitySDR N6WA2025091801Cascade · damagedRIGHT ENGINE, NR 2 UPPER OTBD CASCADE DAMAGED. REMOVED AND REPLACED RT ENGINE UPPER OTBD CASCADE IAW AMM 78-34-01Sep 16, 2025 · N501GJ · Cndair CL6002C11 · Engine (Turbine/Turboprop)SDR VNAA2025041511103Bleed Valve · tornL 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 DIDApr 14, 2025 · N527EA · Cndair CL6002C10 · Compressor Bleed ValveSDR VNAA20250329012Exhaust Cone · dentedDENT 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 - -Jan 26, 2025 · N539EA · Bombdr CL6002D15 · Engine Collector/Tailpipe/NozzleSDR VNAA2024121711101Engine · fumesON 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 THEOct 26, 2024 · N505AE · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR VNAA202409270001Duct · gougedRIGHT 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 RSep 27, 2024 · N708PS · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SWIA2024060400528Engine · odorSTRONG 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 COMay 28, 2024 · N784SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR N6WA2022091901Engine · vibrationENG 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 GOOSep 14, 2022 · N573GJ · Cndair CL6002C10 · Engine Ignition AnalyzerSDR N6WA2022053002Engine · failedLEFT 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 PRESENTMay 29, 2022 · N541GJ · Cndair CL600* · Fuel Control/Reciprocating EnginesSDR VNAA202205091111Engine · shutdownWHILE 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 ANYMay 6, 2022 · N540EG · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SWIA202266002Coaming · crackedUPON 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 670-54-21-1537May 5, 2022 · N607SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA202266001None · gougedDOUBLER 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.May 4, 2022 · N607SK · Cndair CL6002C10 · Engine Exhaust SystemSDR SWIA202266000Latch · chafedLEFT 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, DATEMay 3, 2022 · N607SK · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR VNAA202203241111Engine · vibration5206/22MAR 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 2.0Mar 22, 2022 · N536EA · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR VNAA202202021111Bleed Valve · brokenDIVERSION 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 ALLJan 31, 2022 · N545PB · Cndair CL6002C10 · Compressor Bleed ValveSDR VNAA202201271111Compressor · fodTAKING 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 TIJan 25, 2022 · N532EA · Cndair CL6002C10 · Fuel Controlling SystemSDR V0XD20220127003Housing · gougedR/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.Jan 6, 2022 · N525AE · Cndair CL6002C10 · Engine Cowling SystemSDR N6WA2021120201Check Valve · damagedRH 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 DADec 1, 2021 · N523GJ · Cndair CL600* · Powerplant SystemSDR VNAA202111301111Transmitter · unserviceableIN 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, ONov 30, 2021 · N531EG · Cndair CL6002C10 · Engine Oil Indicating SystemSDR SWIA202163691None · shiftedDURING 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-A02Nov 30, 2021 · N796SK · Cndair CL600* · Engine Exhaust SystemSDR N6WA202108030101Bleed Valve · leakingFUEL 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.Aug 1, 2021 · N514MJ · Cndair CL600* · Compressor Bleed ValveSDR N6WA2020122601Engine · flamed outRT 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 71-00-00Dec 26, 2020 · N508GJ · Cndair CL600* · Engine (Turbine/Turboprop)SDR SWIA202054912Slider · gougedLEFT 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.Nov 17, 2020 · N787SK · Cndair CL6002C10 · Engine Thrust ReverserSDR N6WA2020110601Transcowl · crackedRT 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.Nov 6, 2020 · N540GJ · Cndair CL600* · Engine Thrust ReverserSDR SWIA202052574Latch · wornTHUMB 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.Aug 10, 2020 · N784SK · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR SWIA2019111246761Engine · malfunctionedWHILE 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 Nov 12, 2019 · N780SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SWIA2019101846547Engine · contaminatedRECEIVED 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 POct 17, 2019 · N764SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR VNAA2019092511101Blade · damagedDURING 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 ENGINESep 25, 2019 · N719PS · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR SIMA2019082219006Indication Sys · unknownAT 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 IAAug 19, 2019 · N536EA · Cndair CL6002C10 · Engine Oil TemperatureSDR 19EA201910075121Engine · seizedENGINE WOULD NOT START. DISCOVERED ENGINE PHYSICALLY WOULD NOT ROTATE. SENT TO ENGINE SHOP FOR EVALUATIONMay 12, 2019 · N24EA · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR CA190522014Engine · contaminated(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)May 11, 2019 · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SWIA2019050645828Pin · defectiveENGINE 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 INTOMay 6, 2019 · N774SK · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR N6WA2019012602Engine · fireRT ENG FIRE INFLIGHT.Jan 26, 2019 · N167GJ · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR N6WA20190205601Engine · fireRIGHT ENGINE FIRE IN FLIGHT. REMOVED AND REPLACED RIGHT ENGINE IAW CRJ700 AMM 71-00-00. AIRCRAFT RELEASED 1/31/2019Jan 26, 2019 · N167GJ · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SIMA2018121211003Compressor · contaminatedDURING 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-NDec 11, 2018 · N531EG · Cndair CL6002C10 · Turbine Engine Compressor Section
Back to GE CF34-8C5B1