GE CF34-8C1

Service difficulty reports · 1,415

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 = 'CF348C1'
  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 SWIA202163832None · broken*RH ENGINE UPPER TRANSCOWL INNER €ŒZ€? STIFFENER HAS BROKEN FREE OF THE ATTACHING FASTENERS (MARKED) (C CHECK RO 1/16/2022) PERFORMED REPAIR TO CRACK INNER PERFORATED SKIN AROUND FASTENER HOLES UNDER Z-STIFFENER. REF. AND COMPLIED WITH ALL STEPS OF REO Nov 8, 2021 · N770SK · Cndair CL600* · Engine Exhaust SystemSDR SWIA202163833None · worn*RH ENGINE LOWER TRANSCOWL THUMB LATCH STOP PADS (2EA), ON THE INNER SIDE OF COMBING ARE WORN (MARKED) (C CHECK RO 1/16/2022) R/H ENGINE LOWER TRANSCOWL HAS BEEN REPAIRED REF REO# 670-54-21-1207, REV A, DATED 8/27/15. SEE CONTINUATION SHEET FOR DETAILS. CNov 8, 2021 · N770SK · Cndair CL600* · Powerplant SystemSDR SWIA202163851None · chafed*RH ENGINE UPPER FAN COWL DOOR INNER LOWER €ŒZ€? STIFFENER CHAFFED (MARKED) (C CHECK RO 1/16/2022) INSTALLED R/H ENGINE UPR FAN COWL DOOR INNER LWR NEW €ŒZ€? STIFFENER REF. CRJ700 SRM 51-42-06-001-001-A01Nov 8, 2021 · N770SK · Cndair CL600* · Powerplant SystemSDR SWIA202163865None · seizedRH AFT CORE COWL OUTBD MOUNT BOLT IS SEIZED. (C CHECK RO 1/16/2022) REMOVED SEIZED OTBD MOUNT BOLT FROM R/H AFT CORE COWL USING SLIDE HAMMER, SOCKET AND "C" CLAMP.Nov 8, 2021 · N770SK · Cndair CL600* · Engine Exhaust SystemSDR SWIA202163871None · damaged*RIGHT ENGINE NOSE COWL LIPSKIN HAS EROSION DAMAGE AROUND ITS CIRCUMFERENCE. (C CHECK RO 1/16/2022) REMOVED AND INSTALLED THE NEW FROM STOCK RH ENGINE INLET COWL ASSY REF CRJ-700 AMM 71-61-01-000-801-A01 & 71-61-01-400-801-A01. LEAK CHECK, OPEARATIONAL CHENov 3, 2021 · N770SK · Cndair CL600* · Engine Cowl FlapsSDR SWIA202163590None · wornLT UPPER TRANSCOWL, Z ANGLE FASTENERS MISSING AND DISBONDED. (C CHECK RO 1/04/2021) ACCOMPLISHED REPAIR TO DAMAGED INNER PERFORATED SKIN ON LH UPPER TRANSCOWL AND INSTALLED MISSING FASTENERS. REF. AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1487 REV --, Oct 27, 2021 · N716SK · Cndair CL600* · Engine Exhaust SystemSDR SWIA202163591None · crackedLT LOWER TRANSCOWL, OUTER SKIN AROUND FORWARD LATCH APPEARS CRACKED. (C CHECK RO 1/04/2021) REPAIRED CRACK DAMAGE AT LT LOWER TRANSCOWL OUTER SKIN AROUND FWD LATCH REF REO 670-54-21-1486 REV--, DATED 2021-12-03. NO ADDITIONAL DEFECTS NOTED. SEE CONTINUE CAOct 27, 2021 · N716SK · Cndair CL600* · Engine Exhaust SystemSDR SWIA202163586None · worn* THE LH ENGINE CORE COWL€™S UPPER INBOARD TRANSCOWL SLIDER NYLON INSERT HAS 2 SHEARED ATTACH SCREWS. (C CHECK RO 1/04/2021) REPAIRED LH ENGINE CORE COWL UPPER INBOARD TRANSCOWL SLIDER NYLON INSERT ATTACH SCREWS REF. REO 670-78-30-921 REV. B DATED: 2014-0Oct 24, 2021 · N716SK · Cndair CL600* · Engine Exhaust SystemSDR SWIA202163562None · cracked* THE RH ENGINE'S UPPER TRANSCOWL HAS A SUSPECTED CRACK ON THE OUTBOARD SIDE, AT THE FWD TRANSCOWL LATCH ATTACH SCREW. (MARKED WITH RED GREASE PENCIL) (C CHECK RO 1/04/2021) REPAIRED R/H UPPER TRANSCOWL INNER AND OUTER SKIN CRACKS REF MHIRJ REO 670-54-21-1Oct 11, 2021 · N716SK · Cndair CL600* · Engine Exhaust SystemSDR SWIA202163230None · misaligned* THE RH ENGINE K FRAME ATTACHMENT LOWER FWD BUSHING IS MIGRATED. (C CHECK RO 12-19-21) REMOVED AND REPLACED K-FRAME REF CRJ 700 AMM 78-36-01-000-801-A01 AND CRJ 700 AMM 78-37-01-400-801-A01.Oct 4, 2021 · N606SK · Cndair CL600* · Engine (Turbine/Turboprop)SDR REXA2021100700788Yoke · chafedR/H ENGINE FWD MOUNT YOKE CHAFFED ON TOP SIDE - COMPLIED WITH STEP M SECTION 7.1 OF GREO 670-71-21-057 REV---DATED 2013-09-13. WVAC EMP STAMP # 794 MTCSep 19, 2021 · N376CA · Cndair CL6002C10 · Engine Mount SectionSDR ICRR2021811001Pin · crackedTSN/TSO UNKNOWN CRACK INDICATED WAS DISCOVERED DURING LIQUID PENETRANT INSPECTION PER SPM 70-32-02Aug 11, 2021 · Turbine Engine Air Inlet SectionSDR SWIA2021091060832Stand Off · crackedDURING REMOVAL OF STANDOFF ON LEFT UPPER TRANSCOWL,A CRACK WAS FOUND ON UNDERLAYING STRUCTURE (C-CHECK RO 9/8/2021) REPAIRED CRACK ON UPPER LEFT TRANSCOWL BY COMPLYING WITH ALL STEPS OF REO 670-54-21-1463 REV-- DATED 2021-08-12, COMPLIED WITH TASK CARD Aug 4, 2021 · N705SK · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous StructureSDR SWIA2021081860359Structure · chafedRH LOWER TRANSCOWL SPIGOT HOLE CHAFED/WORN. (C-CHECK RO 8/16/2021) REPLACED DAMAGED RH LOWER TRANSCOWL SPIGOT HOLE/DOOR LATCH COAMING WITH NEW (P/N: CN624-2060-207) REF REO 670-54-21-1207, REV A DATED 2015-08-27. COMPLIED WITH ST 51-900-1002-SKY.Jul 27, 2021 · N755EV · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR SWIA2021081960417Skin · chafedRH UPPER TRANSCOWL OUTBOARD LEADING EDGE SKIN, INNER SURFACE UNDER LATCH DOUBLER IS CHAFFED. (C-CHECK RO 8/18/2021) REPAIRED RH UPPER TRANSCOWL OUTBOARD LEADING EDGE SKIN REF REO 670-54-21-1456 REV -A DATED 2021-08-12. COMPLIED WITH TASK CARD 51-900-10Jul 9, 2021 · N752EV · Cndair CL6002C10 · Nacelle/Pylon, Plate/SkinSDR SWIA2021091060883Beam · gouged*RIGHT ENGINE, LOWER TR FIXED STRUCTURE LATCH BEAM (OTBD) IS GOUGED NEAR THE LATCHES (MARKED). (C-CHECK RO 9/8/21) REPAIRED GOUGED DAMAGE ON RIGHT ENGINE, LOWER TR FIXED STRUCTURE LATCH BEAM NEAR LATCHES REF MHIRJ REO 670-54-22-041 REV -- DATED 2021-08-06Jul 8, 2021 · N705SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2021081860353Angle · crackedRH LOWER TRANSCOWL "Z" ANGLE DISBONDED. (C-CHECK RO 8/16/2021) RH UPPER TRANSCOWL Z ANGLE FOUND TO BE CRACKED. PERFORMED REPAIR TO RH UPPER TRANSCOWL "Z" ANGLE IAW ALL STEPS OF REO 670-54-21-1461 REV--, DATED 2021-08-02 AND CRJ700 SRM 51-42-13-001-001-AJul 3, 2021 · N755EV · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR SWIA2021081860354Structure · chafedLH UPPER TRANSCOWL SPIGOT HOLE CHAFED/WORN. (C-CHECK RO 8/16/2021) REMOVED DAMAGE AND INSTALLED NEW LH UPPER TRANSCOWL DOOR LATCH COAMING AND SPIGOT DOUBLER PER REO 670-54-21-1207 REV-A, DATED 2015-08-27. COMPLIED WITH ST 51-900-1002-SKYJul 3, 2021 · N755EV · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR SWIA2021081860355Angle · crackedLH UPPER TRANSCOWL "Z" ANGLE APPEARS TO BE DISBONDED. (C-CHECK RO 8/16/2021) LH UPPER TRANSCOWL Z ANGLE FOUND TO BE CRACKED. PERFORMED REPAIR TO LH UPPER TRANSCOWL "Z" ANGLE IAW ALL STEPS OF REO 670-54-21-1460 REV--, DATED 2021-08-02 AND CRJ700 SRM 51-4Jul 3, 2021 · N755EV · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR ICRR20217020001Pin · crackedTSN/TSO UNKNOWN CRACK INDICATION WAS DISCOVERED DURING LIQUID PENETRANT INSPECTION PER SPM 70-32-02Jul 2, 2021 · Turbine Engine Air Inlet SectionSDR ICRR20217020002Pin · crackedTSN/TSO UNKNOWN CRACK INDICATION WAS DISCOVERED DURING LIQUID PENETRANT INSPECTION PER SPM 70-32-02Jul 2, 2021 · Turbine Engine Air Inlet SectionSDR ICRR20217020003Pin · crackedTSN/TSO UNKNOWN CRACK INDICATION WAS DISCOVERED DURING LIQUID PENETRANT INSPECTION PER SPM 70-32-02Jul 2, 2021 · Turbine Engine Air Inlet SectionSDR SWIA2021091060841Stand Off · cracked* LEFT SIDE UPPER TRANS COWL STANDOFF HAS SUSPECT CRACK AT TOP FASTENER ON INBOARD END OF COWL. (C-CHECK RO 9/8/21) REMOVED AND REPLACED LH UPPER TRANSCOWL STANDOFF ON THE INBOARD END REF REO 670-54-21-971 REV A DATED 2017/05/11, CRJ700 SRM 51-42-14-001-0Jul 2, 2021 · N705SK · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous StructureSDR SWIA202158127Engine · odorAT 200€™ ON CLIMB OUT RECEIVED SMOKE AFT LAV WARNING MESSAGE, FOLLOWED BY AFT FLIGHT ATTENDANT EMERGENCY CALL CONFIRMING LIGHT SMOKE FROM THE LAV. RETURNED TO FIELD WHILE COMPLYING WITH QRH PROCEDURE OF OPENING APPLICABLE CIRCUIT BREAKERS. UPON LANDING FLIGHTMay 9, 2021 · N722EV · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR ICRR202103250001Pin · crackedA CRACK INDICATION WAS DISCOVERED DURING LIQUID PENETRANT INSPECTION PER SPM 70-32-02.Mar 25, 2021 · Turbine Engine Air Inlet SectionSDR VNAA202012181112Control Valve · abnormalRTO-TAKING OFF RWY 6 IN ERI AT 40KTS THE CREW RECEIVED A RT THRUST REVERSER UNSAFE AMBER MESSAGE AND ABORTED TAKEOFF. CREW RETURNED TO GATE.Dec 16, 2020 · N516AE · Cndair CL6002C10 · Engine Thrust ReverserSDR VNAA202011191111Warning Message · illuminatedREJECTED TAKEOFF FOR A RT THRUST REV UNSAFE CAUTION MESSAGE AT THE VERY BEGINNING OF THE TAKEOFF ROLL, LESS THAN 10 KNOTS. AIRCRAFT EXITED THE RUNWAY WITHOUT ISSUE AND RETURNED TO GATE WHERE MAINTENANCE HAS BEEN CALLED TO INSPECT AND TO POTENTIALLY DEFER THE Nov 18, 2020 · N516AE · Cndair CL6002C10 · Engine Thrust ReverserSDR VNAA2020041611102Pressure Switch · failedAFTER T/O DURING CLIMB THE CREW RECEIVED A L/H ENGINE OIL WARNING MESSAGE. CREW LEVELED OFF AT 4000 AND ALL INDICATIONS ON OIL PRESSURE NORMAL. CREW DECLARED EMERGENCY AND RETURNED TO TLH WITHOUT INCIDENT. MX R/R L ENGINE OIL PRESSURE SWITCH IAW CRJ 700 AMM AApr 15, 2020 · N509AE · Cndair CL6002C10 · Engine Oil PressureSDR N6WA20200211001Engine · odorFA CALLED IMMEDIATELY AIRBORNE SMELLING BURNING SMELL. VERIFIED BURNING SMELL WAS DUE TO PREVIOUS ENGINE WASH. PERFORMED ENGINE RUN IAW CRJ-AMM-72-00-00. NO BURNING SMELL NOTED.Feb 10, 2020 · N656CA · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR MASA2020011500021Warning Light · illuminated#2 ENGINE OIL PRESSURE WARNING IN FLIGHT / ENGINE SHUTDOWNJan 15, 2020 · N504MJ · Cndair CL6002C10 · Engine Oil PressureSDR SWIA2020021848697Vane · crackedL/H ENGINE LOWER CASCADE VANE HAS SUSPECT CRACK. (MARKED) (C-CHECK) RO 2/14/2020 REPLACED LH ENG LOWER CASCADE REF CRJ700 AMM. OPS CHECKS GOODJan 10, 2020 · N730SK · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR N6WA201912110503Transcowl · crackedRH LOWER TR HAS 2 CRACKED BRACKETS. R&R RH LOWER TRANS COWLDec 5, 2019 · N502GJ · Cndair CL600* · Engine Thrust ReverserSDR MASA2019112112151Fadec · unknownCREW DIERTED & DECLARED AN EMERGENCY FOR LH FADEC CAUTION MSG IN FLIGHT. PLACED ON MEL.Nov 21, 2019 · N515MJ · Cndair CL6002C10 · Fuel Controlling SystemSDR MASA2019112112152Fadec · unknownCREW DIERTED & DECLARED AN EMERGENCY FOR A LH ENGINE DEGRADED IN FLT FOR 2 SECS. PLACED FADEC ON MEL.Nov 21, 2019 · N515MJ · Cndair CL6002C10 · Fuel Controlling SystemSDR V0XR20190613001Skin · crackedWHILE PERFORMING SERVICE BULLETIN 670BA-54-007. #1 PYLON FS1088.20 - 1098. DURING HFEC OPEN HOLE INSPECTION OF LOWER CHORD. #5 FASTENER HOLE WAS FOUND TO BE CRACKED. CRACK INDICATION WAS EMITTING FROM 4:30 POSITION AND .010 IN LENGTH. ORIGINAL FASTENER SIZE WAJun 13, 2019 · N810SK · Bombdr CL6002D15 · Wing, Nacelle/Pylon Attach FittingsSDR SWIA2019052945873Engine · malfunctionedAFT LAV SMOKE WARNING MESSAGE ON ROTATE. RETURN TO FIELD. (FLT#3136) FO: 05/13/2019 CLOSED REMOVED AND REPLACED LEFT ENGINE IAW AMM.May 12, 2019 · N754EV · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR MASA2019043011835Compressor · odorSMOKE IN LAVATORY MESSAGE IN FLIGHT. PERFORMED RH ENG COMPRESSOR RINSEApr 30, 2019 · N507MJ · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR CA190410018Pcu · failed(CAN) ESTABLISHED ON THE ILS36R AT 1000FT, MANUAL CONTROL, WE NOTICED THE PLANE WAS ROLLING ON THE RIGHT AND AT THE SAME TIME 2 CAUTION MESSAGES APPEARED ON THE ED1 : IB FLT SPOILERS AND IB SPOILERONS. WE HAVE DECIDED TO GO AROUND TO SORT THE PROBLEM OUT. THENApr 8, 2019 · Cndair CL6002C10 · Drag Control SystemSDR CA190403015Skin · corroded(CAN) CORROSION AREAS ON LHS AFT UPPER WING PLANK (DWG: CC670-10042 REF) AND AFT LOWER WING PLANK (DWG: CC670-10043 REF) AT OUTBOARD TRAILING EDGE FAIRING (56LAT) ATTACHMENT LAND (DWG: CC670-10235 REF) BETWEEN WS353.00-WS398.00. (TC# 20190403015)Apr 3, 2019 · Cndair CL6002C10 · Wing, Plate/SkinSDR CA190403016Skin · corroded(CAN) MULTIPLE BLENDED CORROSION AREAS TO AFT UPPER WING PLANK (DWG: CC670-10042, REF) BETWEEN WS353.00 - WS387.50, RHS. MINIMUM REMAINING THICKNESS IS 4.53MM [0.I78 ] OUT OF 0.200 +/-0.005 NOMINAL, REF, AND 2.25MM [0.089 ] OUT OF 0.100 +/-0.005 NOMINAL,Mar 27, 2019 · Cndair CL6002C10 · Wing, Plate/SkinSDR CA190620013Line · corroded(CAN) BOMBARDIER HAS OPENED A NEW CAW PROJECT RJ-CA-28-0022 TO FURTHER INVESTIGATE IF THESE FINDINGS HAVE CAUSED AN UNACCEPTABLE DEGRADATION OF LIGHTNING STRIKE PROTECTION IN THE WING TANKS. FOLLOWING THE DASH 8 FINDING OF CORRODED OR BLACKENED FUEL COUPLINGSMar 26, 2019 · Cndair CL6002C10 · Aircraft Fuel SystemSDR CA190320015Windshield · cracked(CAN) A/C DIVERTED DUE TO A CRACKED RH WINDSHIELD.Mar 11, 2019 · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA2018110645246Engine · smokeUPON LANDING WE WERE NOTIFIED BY TOWER WE HAD SMOKE BILLOWING FROM LEFT ENGINE. (FLT 3256) FO: 11/06/2018 WORK IN PROGRESS.Nov 4, 2018 · N730SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SWIA2018111645246Engine · smokeUPON LANDING WE WERE NOTIFIED BY TOWER WE HAD SMOKE BILLOWING FROM LEFT ENGINE. (FLT#3256) FO: 11/06/2018 CLOSED REMOVED AND REPLACED LT ENG OBV AND FUEL SUPPLY LINES IAW AMM. OPS CHECK GOOD, LEAK CHECK GOOD.Nov 4, 2018 · N730SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SWIA2018110545242Engine · damagedDAMAGE FOUND ON THE LH ENGINE THAT NEEDS TO BE REPAIRED. (C-CHECK) RO: 11/1/2018. DENT REPAIRED REF REO 670-54-21-1310. COMPLIED WITH 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**)Sep 19, 2018 · N730EV · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR CA180510011Indicator · false activation(CAN) BLANK OUT ISI & STALL FAIL CAUTION, RUD LIMIT FAULT STATUS MSG APPEARED. ISI CB TRIPPED/RESET. OPS BACK TO NORMAL. A/C RETURN TO SERVICE. HOWEVER, THE FAULT RETURNED IN FLIGHT, A/C DIVERTED BACK TO AIRPORT FOR LANDING. CORRECTIVE ACTION: ISI REPLACEDMay 9, 2018 · Cndair CL6002C10 · Independent InstrumentsSDR CA190731023Engine · power loss(CAN) ADG AUTO-DEPLOY IN FLIGHT, CREW REPORTED INTERMITTENT POWER LOSS JUST BEFORE ADG DEPLOYMENT (FLICKERED). BOTH MAIN GENERATORS CAME BACK ON-LINE AND PLANE LANDED WITHOUT FURTHER INCIDENT, BCA CONFIRMS IT IS NOT AN ENGINE FAILURE OR DUAL FAILURE BUT BOTH Mar 12, 2018 · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR VNAA2018030111101Warning Message · false activationTHE CREW RECEIVED A BLEED DUCT WARNING MESSAGE DURING FLIGHT AND DIVERTED AND DECLARED AN EMERGENCY. MAINTENANCE PERFORMED OPS TEST OF BLEED-AIR DETECTION AND WARNING SYSTEM NO DEFECTS NOTED. PERFORMED LEAK TEST OF BLEED-AIR DISTRIBUTION NO DEFECTS NOTED.Mar 1, 2018 · N512AE · Cndair CL6002C10 · Engine Bleed Air SystemSDR MASA2017101612702Transmitter · inoperativeNR 1 ENGINE HAD NO OIL PRESSURE. REPLACED OIL PRESS TRANSMITTER, OPS CHECKED NORMAL, NO FURTHER DEFECTS NOTEDOct 16, 2017 · N515MJ · Cndair CL6002C10 · Engine Oil Indicating SystemSDR SIMA20171008002Rotor · shearedWHILE ACCOMPLISHING W/C 72-009 PG 5, BORESCOPE PROCEDURES, FOUND ONE STAGE 1 HP TURBINE ROTOR BLADE SHEARED. REMOVED AND REPLACED THE LT ENGINE IAW WORK CARDS 71-001 AND 71-002. OPS CHECKED GOOD. NO LEAKS NOTED.Oct 8, 2017 · N523AE · Cndair CL6002C10 · Turbine Section
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