# Service difficulty reports: GE CF34-10E6

A list on [GE CF34-10E6](https://openairdocs.org/engine/ge-cf34-10e6.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 140 reports

- [SDR EE4Y2025FA0000667](https://openairdocs.org/sdr/EE4Y2025FA0000667.md): Skin · worn · Sep 27, 2025 · N247JB · Emb ERJ190100IGW · Engine Thrust Reverser
  > DURING THE INSPECTION WAS FOUND ON ENGINE NR 2 OUTBD THRUST REVERSER TRANSLATING COWL, EXTERNAL SKIN WITH WORN AT 1 O’CLOCK POSITION. DUE TI THIS, WAS REPORTED AND REPAIRED TO BOWDEN (ENGINEERING SOLUTIONS PTY LDT) WITH THE ENGINEERING ORDER ESE-ERJ190-78-006
- [SDR YENA2023010300005](https://openairdocs.org/sdr/YENA2023010300005.md): Engine · failed · Dec 31, 2022 · N192JB · Emb ERJ190100LR · Engine (Turbine/Turboprop)
  > FLT 1882, IAH-JFK. RIGHT ENGINE FAILED WITH WEIGHT ON WHEELS UPON TOUCHDOWN RT ITT WAS ALSO EXCEEDENCE, ITEM C/W PER WO #1226080 EC E22-1068-01.
- [SDR YENA202301040011](https://openairdocs.org/sdr/YENA202301040011.md): Pressure Switch · faulted · Dec 26, 2022 · N258JB · Emb ERJ190100IGW · Engine Bleed Air System
  > FLT 726, BWI - BOS. AIRCRAFT PERFORMED AN AIR TURN BACK TO BWI, BLEED 1 OVERPRESSURE MSG APPEARED ON CLIMB AFTER TAKEOFF. RAN QRH PROCD, MSG RETURNED. DISPATCH ADVISED RETURN TO BWI; ACCOMPLISHED FIM TASK 36 14 00 810 867A. REMOVED AND REPLACED LH BLEED OVER
- [SDR YENA2022111801136](https://openairdocs.org/sdr/YENA2022111801136.md): Anti-Ice System · faulted · Nov 16, 2022 · N329JB · Emb ERJ190100IGW · Engine Anti-Icing System
  > FLT # 2041, CROSS BLEED FAIL IN FLIGHT COULD NOT RESET ENCOUNTERED ICING + SYSTEM COULD NOT FUNCTION W ONE BLEED AND NO BLEED; PERFORMED OPS CHECK OF CROSS BLEED SYSTEM OPS CHECK GOOD REF FIM 36-10-00
- [SDR YENA2022072900727](https://openairdocs.org/sdr/YENA2022072900727.md): Engine · failed · Jul 5, 2022 · N328JB · Emb ERJ190100IGW · Turbine Engine Air Inlet Section
  > DURING HEAVY MAINTENANCE: ENG ITT EXCEEDANCE ON TAKEOFF OVER 1020 DEGREES CELSIUS FOR 2 MINUTES; REF TOMX N/R 00001 WO 2023 EVALUATION OF THE EXCEEDANCE WAS PERFORMED PER EMB-190 FIM 72-00-00-810-801-A, PER EMB-190 FIM 72-00-00-810-805-A, PER CF34-10E LMM SUB
- [SDR YENA202201201038](https://openairdocs.org/sdr/YENA202201201038.md): Fmu · failed · Jan 18, 2022 · N351JB · Emb ERJ190100IGW · Fuel Controlling System
  > FLT # 716,BUF-BOS.(EMERGENCY DECLARED). DURING CLIMB AT APPROX 12000FT ENGINE 1 BEGAN SURGING BETWEEN 56% - 79% N1. UPON LEVEL OFF AT 19,000 FEET, THE SURGE STOPPED. ONCE WE BEGAN DECENT IT SURGED ONE MORE TIME, THEN WAS NORMAL THROUGHOUT LANDING ROLL.; SEE
- [SDR YENA2022011900031](https://openairdocs.org/sdr/YENA2022011900031.md): Transmitter · failed · Jan 15, 2022 · N355JB · Emb ERJ190100IGW · Engine Oil Indicating System
  > FLT # 1704, CTG-FLL(DIVERTED TO MBJ). IN FLT # 1 OIL PRESSURE INDICATION AMBER AT PSI SLOWLY BLEED DOWN TO 0 IN LESS THAN FEW MINUTES. ENGINE VIBRATION MEER 1.3=1.4 STEADY UNITL SHUTDOWN, FOLLOWED QRH PROCEDURE 6-25 FOR ENG OIL PRESSURE ABNORMAL INDICATION AN
- [SDR YENA2021100700660](https://openairdocs.org/sdr/YENA2021100700660.md): Engine · faulted · Oct 5, 2021 · N267JB · Emb ERJ190100IGW · Engine (Turbine/Turboprop)
  > FLT# 1355, BOS-DCA (RETURNED BACK BOS). ENG 1 CONTROL FAULT ITT INDICATION WENT AMBER AND FUEL FLOW WAS 500PPHABOVE #2 DURING CLIMB. ENGINE WOULD NOT MAKE CLIMB 1 THRUST WITHIN ITT LIMITS; R & R # 1 ENGINE IAW AMM 71-00-01
- [SDR 3CEY20210817001](https://openairdocs.org/sdr/3CEY20210817001.md): Retaining Ring · deformed · Aug 13, 2021 · Emb ERJ190200LR · Turbine Engine Compressor Section
  > QUICK TURN HPC TOP CASE REPAIR IAW 72-00-00 SP001 AND 72-00-00 SP110 CONDUCTED. DURING THE AFFECTED HPC STG2 & 3 BLADES REMOVAL WE NOTED THE STG2 FWD BLADE RETAINER LUG WEAR AND TIGHT CONDITION. FURTER EXAMINATION REVEALED THAT BLADE RETAINER PN 2031M31G01 HAS
- [SDR AALA2019123059001](https://openairdocs.org/sdr/AALA2019123059001.md): Starter · failed · Dec 24, 2019 · N951UW · Emb ERJ190100IGW · Engine Starter
  > AIRCRAFT WAS GROUNDED, NR 2 ENGINE NO LIGHT OFF DURING START. GROUND PERSONAL REPORTED SPARKS FROM ENGINE. REPLACED THE STARTER IAW AMM 80-10-03.
- [SDR AALA2019112759023](https://openairdocs.org/sdr/AALA2019112759023.md): Bleed Valve · unreliable · Nov 24, 2019 · N955UW · Emb ERJ190100IGW · Compressor Bleed Valve
  > AIRCRAFT WAS GROUNDED: PILOT REPORTS WITH ICING CONDITIONS AND APPARENT WEAK BLD ON #1 WE DIVERTED TO CLT AFTER DECLARING EMERGENCY PRIOR TO DESCENT. MAINTENANCE REMOVED AND REPLACED #1 ENG PRSOV IAW AMM 36-11-01 & NAPR SHUTOFF VALVE IAW AMM 36-11-03. ALL OPS
- [SDR AALA2019060549017](https://openairdocs.org/sdr/AALA2019060549017.md): Blade · fod · Jun 3, 2019 · N947UW · Emb ERJ190100IGW · Turbine Engine Compressor Section
  > AIRCRAFT WAS GROUNDED: PILOT REPORTS BIRD INGESTED IN LEFT ENGINE ON TAKEOFF. ITT INCREASED SLIGHTLY COULD SMELL IT IN CABIN. MAINTENANCE ACCOMPLISHED CARD 43L00005001 BIRD STRIKE INSP.FOUND #1 ENG OGV BASE DAMAGE 3 BLADES @ 9 O'CLOCK POSITION. MAINTENANCE REP
- [SDR RJEF20190402001](https://openairdocs.org/sdr/RJEF20190402001.md): Acm · odor · Mar 30, 2019 · N988TA · Emb ERJ190100IGW · Cabin Cooling System
  > DURING TAXI OF FLIGHT TAI310 (SAL-MIA), WAS FELT SMOKE ODOR IN CABIN, THE AIRCRAFT RETURNED TO THE GATE FOR MAINTENANCE. MAINTENANCE PERSONNEL PERFORMED FAULT ANALYSIS IN ACCORDANCE WITH FIM 21-20-00-810-801-A, REPLACED THE AIR CYCLE MACHINE (P/N 1000700-5, S
- [SDR RJEF20190311001](https://openairdocs.org/sdr/RJEF20190311001.md): Control Valve · unserviceable · Mar 7, 2019 · N937TA · Emb ERJ190100IGW · Cabin Cooling System
  > DURING CLIMB OF FLIGHT TAI441 (DFW-SAL) THE AIRCRAFT HAD MALFUNCTIONING OF AIR CONDITIONING SYSTEM AND RETURNED TO DFW FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING AT DFW THE PILOT REPORTED: 1)"CABIN TEMPERATURE (COCKPIT) INDICATION OSCILLATES FROM 3 TO 17C. C
- [SDR RJEF20181211001](https://openairdocs.org/sdr/RJEF20181211001.md): Anti-Ice Valve · failed · Dec 8, 2018 · N988TA · Emb ERJ190100IGW · Engine Anti-Icing System
  > DURING TAXIING OF FLIGHT TA441 FROM DFW TO SAL, THE AIRCRAFT HAD FAILURE OF ENGINE 1 ANTI-ICE AND RETURNED TO THE GATE FOR MAINTENANCE. THE FAILURE IS DEFERRABLE AS PER MEL 30-21-01 BUT DUE TO RESTICTION ABOUT OPERATIONS ON FORECASTED ICING CONDITION THE AIRCR
- [SDR AALA201810119009](https://openairdocs.org/sdr/AALA201810119009.md): Bleed Valve · defective · Oct 8, 2018 · N948UW · Emb ERJ190100IGW · Compressor Bleed Valve
  > BLEED 2 SURGING 5 - 75 PSI. CABIN ALTITUDE RATE +600 TO -800 FPM. STOPPED CLIMB AT FL-210. BLEED SURGE CONTINUED THROUGHOUT FINAL APPROACH. THE AIRCRAFT WAS GROUNDED. REPLACED RIGHT ENGINE BLEED PRESSURE VALVE IAW AMM 36-11-03. LEAK CHECK AND ENGINE RUN CH
- [SDR 5TTY2018091500001](https://openairdocs.org/sdr/5TTY2018091500001.md): Warning System · activated · Sep 8, 2018 · N938TA · Emb ERJ190100IGW · Pneumatic Indicating System
  > DURING TAI-440 FLIGHT FROM SAL TO IAH, THE AIRCRAFT WAS TURNED BACK IN FLIGHT DUE BLEED 1 OVERPRESS EICAS WARNING MESSAGE IN CLIMB FLIGHT PHASE. AFTER LANDING WITH NO INCIDENT, THE BLEED SYSTEM ON ENGINE 1 WAS DEFERRED AND AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR RJEF20180814001](https://openairdocs.org/sdr/RJEF20180814001.md): Warning Message · illuminated · Aug 13, 2018 · N987TA · Emb ERJ190100IGW · AC Generator-Alternator
  > DURING TAXI THE PILOT REPORTED A IDG 2 OFF BUSS, AND AN IDG 2 OIL WARNINGS, THE IDG WAS DISCONNECTED IAW CHECKLIST.
- [SDR RJEF20180803001](https://openairdocs.org/sdr/RJEF20180803001.md): Interface Unit · failed · Jul 31, 2018 · N986TA · Emb ERJ190100IGW · Navigation System
  > PRIOR TO DEPARTURE, THE PILOT REPORTED THAT THE NAVCOM2 FAILED. APPR2 NOT AVAILABLE AND AURAL WARNING SYSTEM FAULT. THE AIRCRAFT WAS HELD ON GROUND. MAINTENANCE PERSONNEL PERFORMED FAULT ANALYSIS IAW FIM 34-61-00-810-838-A, REPLACED THE NETWORK INTERFACE MOD
- [SDR RJEF20180506001](https://openairdocs.org/sdr/RJEF20180506001.md): Control Panel · malfunctioned · May 31, 2018 · N936TA · Emb ERJ190100IGW · Hydraulic System, Main
  > AFTER ENGINES STARTING FOR FLIGHT, THE PILOT REPORTED THE HYD PUMP DID NOT AUTO ON EICAS, THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PERFORMED A FAULT ANALYSIS IAW FIM 29-10-00-810-803-A, REPLACED THE HYDRAULIC CONTROL PANEL IAW AMM 29-10-01-000-801-A,
- [SDR SOKF201710310001](https://openairdocs.org/sdr/SOKF201710310001.md): Controller · malfunctioned · Oct 28, 2017 · N986TA · Emb ERJ190100IGW · Cabin Pressure Controller
  > DURING FLIGHT FROM SAL TO PTY THE AIRCRAFT DIVERT TO MGA DUE TO EICAS MESSAGE CAB ALT HI EMERGENCY DESCEND MEMORY ITEM. AT MGA STATION PERFORMED TASK CARD IAW AMM 21.31.01 REMOVAL AND REPLACED CPCS AND PERFORMED OPERATIONAL TEST IAW AMM 21.30.00.720.801.A WAS
- [SDR SOKF20171024009](https://openairdocs.org/sdr/SOKF20171024009.md): Warning Message · illuminated · Oct 20, 2017 · N986TA · Emb ERJ190100IGW · Central Warning
  > DURING CLIMB, NEAR FL 206, THE AIRCRAFT RETURN TO DEPARTURE, DUE TO EICAS MESSAGE IN ICE CONDITIONS, STALL PROT ICE SPEED, THEM DURING QRH ACTIONS EICAS MESSAGE BLEED 1 FAIL AFTER FEW SECONDS, BLEED 2 FAIL AND THEN CABIN ALT HI EICAS MESSAGE AND EMERGENCY D
- [SDR YENA201710080824](https://openairdocs.org/sdr/YENA201710080824.md): Bleed Valve · failed · Oct 8, 2017 · N348JB · Emb ERJ190100IGW · Compressor Bleed Valve
  > RETURN TO FIELD. NR 2 BLEED LEAK. FOLLOWED QRH, LEAK MESSAGE EXTINGUISHED. TROUBLESHOT IAW FIM 36-11-00-810-837. RT ENGINE HIGH STAGE BLEED VALVE LEAKING. R & R THE BLEED VALVE IAW AMM 36-11-01. PERFORMED ENGINE RUNS IAW AMM 71-00-01. NO CURRENT FAULTS. AC
- [SDR YENA201710050820](https://openairdocs.org/sdr/YENA201710050820.md): Engine · odor · Oct 5, 2017 · N316JB · Emb ERJ190100IGW · Engine (Turbine/Turboprop)
  > NR 2 ENGINE BLEED PRODUCED A DIRTY SOCK ODOR, REPORTED BY THE FLIGHT ATTENDANT AND CREW MEMBERS. ON LANDING, FA REPORTED THE ODOR AGAIN DURING DESCENT. R & R THE NR 2 ENGINE IAW AMM 71-00-01.
- [SDR RJEF20171005001](https://openairdocs.org/sdr/RJEF20171005001.md): Actuator · faulty · Sep 29, 2017 · N989TA · Emb ERJ190100IGW · Leading Edge Slat Position Indicating System
  > AFTER TAKE OFF, THE SLAT FAILED TO RETRACT, RETURNED TO DEPARTURE. AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED THE SLAT FAILED DURING RETRACTION AFTER TAKE OFF. MAINTENANCE PERFORMED FAULT ANALYSIS IAW FIM 27-81-00-810-805-A, FOUND ONE ATTACHMENT BOLT OF
- [SDR YENA201709080759](https://openairdocs.org/sdr/YENA201709080759.md): Engine · contaminated · Sep 8, 2017 · N329JB · Emb ERJ190100IGW · Engine (Turbine/Turboprop)
  > STRONG PUNGENT AND NOXIOUS ODOR EXPERIENCED BY FLIGHT CREW DURING TAKEOFF AND CLIMBOUT. EXPERIENCED STRONG ODORS IN FWD.GALLEY THROUGH MID CABIN. CONFIRMED ODOR PRESENCE AT ROW 14 BRIEFLY. NO VISIBLE HAZE OR SMOKE PRESENT IN COCKPIT OR CABIN. ODORS GRADUALLY D
- [SDR SOKF20172305006](https://openairdocs.org/sdr/SOKF20172305006.md): Warning System · false activation · May 21, 2017 · N938TA · Emb ERJ190100IGW · Landing Gear Brake System
  > DURING T/O FROM SAL TO PTY, RTO DO TO MSG ON EICAS(AFTER RTO BRAKES OVERHEAT) 100KTS 4 BRAKE TEMP REACH 400°C. AS PER AMM 05-50-12-200-801-A WAS COMPLETED INSPECTION AFTER RTO AND BRAKE OVERHEAT MSG ON EICAS AND NO DAMAGES WAS FOUND, ALL NORMAL IAW FIM 32-47-0
- [SDR YENA201705160373](https://openairdocs.org/sdr/YENA201705160373.md): Engine · contaminated · May 16, 2017 · N229JB · Emb ERJ190100IGW · Engine (Turbine/Turboprop)
  > RETURN TO FIELD DUE TO A DIRTY SOCK ODOR DURING TAKEOFF. THE ACFT DID NOT PRESSURIZE. OUTFLOW VALVE WAS FULL OPEN. PERFORMED FIM TASK 21-20-00. VERIFIED THE NR 1 ENGINE COMP WASH WAS PERFORMED. PERFORMED DECONTAMINATION ON PNEUMATIC SYS WITH ENGINE IAW AMM
- [SDR AALA201705099009](https://openairdocs.org/sdr/AALA201705099009.md): Oil System · overserviced · May 8, 2017 · N963UW · Emb ERJ190100IGW · Turbine Engine Oil System
  > AIRCRAFT WAS GROUNDED. IMMEDIATELY AFTER TAKEOFF STRONG ELECTRICAL BURNING SMELL WITH NO VISIBLE SMOKE. FLIGHT RETURNED TO FIELD AND DECLARED AN EMERGENCY. LEFT HAND ENGINE OIL OVERSERVICED. DRAINED OIL TO PROPER LEVEL.
- [SDR SOKF20171904005](https://openairdocs.org/sdr/SOKF20171904005.md): Pressure Switch · failed · Apr 17, 2017 · N986TA · Emb ERJ190100IGW · Landing Gear Brake System
  > DURING CRUISE FLIGHT, THE AIRCRAFT HAD AN EICAS WARNING MESSAGE FOR THE PARKING BRAKE NOT RELEASED. PERFORMED FIM 32-41-00-810-852-A. REMOVED AND REPLACED THE PARKING BRAKE PRESSURE SWITCH SYS NR 2 IAW AMM 32-44-09, TESTED NORMAL IAW AMM 32-44-09-720-801-A
- [SDR YENA201703210205](https://openairdocs.org/sdr/YENA201703210205.md): Engine · multiple fail · Mar 21, 2017 · N197JB · Emb ERJ190100IGW · Engine (Turbine/Turboprop)
  > AIRCRAFT DEPARTED AND DURING CLIMBOUT ENCOUNTERED A NR 1 ENGINE ROLLBACK WITH SEVERAL FAULT MESSAGES. RETURN TO FIELD, R & R THENR 1 ENGINE.
- [SDR AALA201612079005](https://openairdocs.org/sdr/AALA201612079005.md): Engine · vibration · Dec 6, 2016 · N953UW · Emb ERJ190100IGW · Engine (Turbine/Turboprop)
  > AIRCRAFT WAS GROUNDED. FUMES AFTER TAKEOFF WITH SLIGHT ENGINE VIBRATION, SUSPECT NR 1 ENGINE. DIVERTED TO PHL DUE TO ODOR IN CABIN. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT INCIDENT. ACCOMPLISHED CABIN AIR QUALITY JOB CARD 43L00021001 AND CF34-1
- [SDR YENA201611221018](https://openairdocs.org/sdr/YENA201611221018.md): Engine · stalled · Nov 22, 2016 · N292JB · Emb ERJ190100IGW · Engine (Turbine/Turboprop)
  > DURING CLIMB, THE CREW REPORTED THE NR 2 ENGINE HAD A COMPRESSOR STALL. THE ENGINE WAS SHUT DOWN IAW THE QRH. THE CREW DECLARED AN EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. PERFORMED A VISUAL INSPECTION OF THE RT ENGINE. NO DAMAGE NOTED PERFORMED AMM
- [SDR SOKF20161005009](https://openairdocs.org/sdr/SOKF20161005009.md): Lever · damaged · Oct 2, 2016 · N987TA · Emb ERJ190100IGW · Landing Gear Selector
  > DURING FLIGHT FROM SAL TO SAP THE AIRCRAFT RETURN TO DEPARTURE DUE GEAR LEVER CAN NOT BE MOVED UP DURING FLIGHT. PERFORMED FIM 32.33.00.810.802.A, REMOVED AND REPLACED THE MLG CONTROL LEVER IAW AMM 32-33-01 AND CHECHED IAW AMM 32-33-00-710-801.A AND AMM 32-3
- [SDR SOKF20160906007](https://openairdocs.org/sdr/SOKF20160906007.md): Control Lever · damaged · Sep 4, 2016 · N987TA · Emb ERJ190100IGW · Landing Gear Selector
  > AFTER TAKEOFF, THE AIRCRAFT RETURN TO DEPARTURE DUE TO EICAS MSG LANDING GEAR LEVER DID NOT WORK PROPERLY IN THE UP POSITION DURING TAKEOFF. PERFORMED FIM TASK CARD 32-33-00-810-802-A AND WAS R & R LANDING GEAR CONTROL LEVER IAW AMM 32-33-01. PERFORMED OPS
- [SDR AALA201607189004](https://openairdocs.org/sdr/AALA201607189004.md): Engine · odor · Jul 16, 2016 · N957UW · Emb ERJ190100IGW · Engine (Turbine/Turboprop)
  > ACFT WAS GROUNDED, FLIGHT CREW REPORTED RECEIVING A LAV SMOKE EICAS ON TAKEOFF AT 500' AGL, EICAS WENT OUT WITH POWER REDUCTION AND A SMOKE ODOR IN THE CABIN. AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED SAFELY WITHOUT FURTHER
- [SDR YENA20160611549](https://openairdocs.org/sdr/YENA20160611549.md): Wire Harness · damaged · Jun 11, 2016 · N183JB · Emb ERJ190100IGW · Turbine Engine System Wiring
  > AIR RETURN. PILOT REPORTED ENGINE NR 1 HAS A N-1 VIBRATION OF 4.0 AMBER THROUGH FL 270. FLUCTUATED BETWEEN 3.4-4.0 IN CLIMB TO FL360. AT FL360 ENGINE VIBE 4.0 AMBER AN NOT ABLE TO REDUCE VIBE WITH THRUST LEVER CHANGE. LP VIBE SPIKE. HP VIBE NORMAL.; FOUND
- [SDR YENA20160606544](https://openairdocs.org/sdr/YENA20160606544.md): Engine · vibration · Jun 6, 2016 · N184JB · Emb ERJ190100IGW · Engine (Turbine/Turboprop)
  > FLIGHT CREW REPORTED HIGH ENGINE VIBRATION ON DEPARTURE. ACFT DIVERTED DUE TO HIGH VIBRATION AND ENGINE EXCEEDANCE ON NR 1 ENGINE. NR 1 ENGINE R & R.
- [SDR SOKF20160607003](https://openairdocs.org/sdr/SOKF20160607003.md): Acm · malfunctioned · Jun 4, 2016 · N986TA · Emb ERJ190200IGW · Cabin Cooling System
  > DURING CLIMB, AIRCRAFT RETURNED TO DEPARTURE DUE TO CABIN SMOKE ODOR, AT STATION. PERFORMED FIM 21.20.00.810.800A, AND FOUND ACM 1 DAMAGED. R & R THE ACM 1 IAW AMM 21.51.05 AND PERFORMED OPS CHECK IAW AMM 21.51.00.710.801A, OK NORMAL. THE ACFT RETURN TO NORM
- [SDR RJEF201605300001](https://openairdocs.org/sdr/RJEF201605300001.md): Warning Message · false activation · May 30, 2016 · N983TA · Emb ERJ190100IGW · Aircraft Fuel System
  > DURING TAKEOFF OF THE ACFT, THE EICAS MSG, FUEL LOW PRESS, WAS DISPLAYED. THEREFORE, A REJECT TAKEOFF PROCEDURE WAS PERFORMED. ONCE THE ACFT WAS AT THE GATE, THE DEFUEL SOV, PREVIOUSLY DEFERRED, WAS INSPECTED TO ASSURE ITS CLOSED POSITION. THE ACFT WAS RETU
- [SDR YENA20160425353](https://openairdocs.org/sdr/YENA20160425353.md): Engine · making metal · Apr 25, 2016 · N296JB · Emb ERJ190100IGW · Engine (Turbine/Turboprop)
  > DIVERTED, CREW REPORTED ENGINE NR 1 WAS EXPERIENCING HIGH VIBRATIONS AFTER TAKEOFF. CREW ALSO REPORTED EGT WAS 60 DEGREES HOTTER AND FUEL FLOW WAS 400 LBS INCREASED COMPARED TO ENGINE NR 2. INITIAL INSPECTION AND ENGINE WALK AROUND WAS PERFORMED. FOUND METAL
- [SDR AALA201604189009](https://openairdocs.org/sdr/AALA201604189009.md): Pressure Switch · defective · Apr 16, 2016 · N947UW · Emb ERJ190100IGW · Fuel Pressure Sensor
  > DIVERTED & ACFT WAS GNDED. IN FLIGHT EICAS MSG, FUEL FEED 2 FAULT. REPLACED NR 2 ENG FUEL LOW PRESS SWITCH IAW AMM 73-31-01 & EMM 71-00-73-450-801. A SATISFACTORY OPERATIONAL & LEAK CHECK WAS ACCOMPLISHED.
- [SDR AALA201603289008](https://openairdocs.org/sdr/AALA201603289008.md): Engine · odor · Mar 26, 2016 · N950UW · Emb ERJ190100IGW · Engine (Turbine/Turboprop)
  > RETURNED, ACFT WAS GNDED. RT AFTER ROTATION, THE CREW NOTED A STRONG SMELL OF BURNING OIL & HAD SMOKE IN THE COCKPIT. THE CREW OXYGEN MASKS WERE USED IN THE COCKPIT ONLY SINCE THERE WAS NO SMOKE & ONLY AN ODOR IN THE CABIN. DECLARED AN EMER & THE ACT RETURN
- [SDR YENA20151219662](https://openairdocs.org/sdr/YENA20151219662.md): Fadec · inoperative · Dec 19, 2015 · N183JB · Emb ERJ190100IGW · Fuel Controlling System
  > FLIGHT RETURNED TO GATE. ENGINE NR 1 FAIL ON TAXI OUT. R & R 1 ENGINE FADEC. OPS CHECK GOOD. RAN NR 1 ENGINE 2 TIMES. NO DEFECTS NOTED. OK FOR SERVICE
- [SDR RJEF20151125001](https://openairdocs.org/sdr/RJEF20151125001.md): Bleed Valve · malfunctioned · Nov 22, 2015 · N983TA · Emb ERJ190100IGW · Compressor Bleed Valve
  > DURING FLIGHT, THE PILOT REPORTED THAT BLEED 1 PRESSURE OSCILLATES BETWEEN 4 AND 60 PSI; BLEED 2 PRESSURE OSCILLATES BETWEEN 10 AND 55 PSI. DUE THAT SITUATION THE ACFT RETURNED TO DEPARTURE FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING, THE ACFT WAS HELD ON GR
- [SDR RJEF20151125002](https://openairdocs.org/sdr/RJEF20151125002.md): Module · damaged · Nov 22, 2015 · N985TA · Emb ERJ190100IGW · Engine Air Intake System
  > AFTER ARRIVAL, THE PILOT REPORTED BIRD STRIKE ON ENGINE 2 NACELLE. IT WAS PERFORMED INSPECTION AFTER BIRD STRIKE IAW AMM 05-50-02-200-801-A, FOUND A DENT OUT OF LIMITS FOR ACFT OPERATION ON THE AIR INLET MODULE 2, THE AIR INLET MODULE WAS REPLACED IAW AMM 71-
- [SDR RJEF20150728001](https://openairdocs.org/sdr/RJEF20150728001.md): Warning System · false activation · Jul 28, 2015 · N989TA · Emb ERJ190100IGW · Navigation System
  > PREVIOUS TO DISPATCH OF FLIGHT TA-367, THE PILOT IN COMMAND REPORTED, EICAS MSG, NAV COM 1 WAS FAILED. IT WAS PERFORMED A FAULT ANALYSIS IAW FIM 34-02-01-810-804-A & REPLACED THE NIM 1 IAW AMM 34-02-000-801-A34-02-400-801-A. PERFORMED OPERATIONAL TEST WITH N
- [SDR AALA201506259003](https://openairdocs.org/sdr/AALA201506259003.md): Engine · malfunctioned · Jun 22, 2015 · N955UW · Emb ERJ190100IGW · Engine (Turbine/Turboprop)
  > FLIGHT 2135 EN-ROUTE, DIRTY SOCK SMELL ON TAKEOFF. ONLY COULD BE SMELLED IN FLIGHT DECK. FLIGHT ATTENDANT DID NOT SMELL ANYTHING ON MAIN CABIN. PACKS 1 & 2 ON, ENG BLEED ON, APU WAS OFF. AT REDUCTION OF POWER 1000 FEET SMELL WENT AWAY. THE FLIGHT RETURNED
- [SDR SOKF20150617002](https://openairdocs.org/sdr/SOKF20150617002.md): Duct · damaged · Jun 14, 2015 · N935TA · Emb ERJ190200IGW · Air Distribution System
  > DURING CLIMB, THE ACFT RETURNED DUE SMOKE ODOR IN PAX CABIN. FIM 21-20-00-801-810-A WAS PERFORMED SMOKE & OR ABNORMAL SMELL IN PAX CABIN & OR COCKPIT & FOUND CABIN SUPPLY DUCT FROM RECIRCULATION SYS DAMAGED. FIM 21-20-00-810-801-A COMPONENTS OF GALLEY AREA &
- [SDR RJEF20150528001](https://openairdocs.org/sdr/RJEF20150528001.md): Engine · leaking · May 28, 2015 · N984TA · Emb ERJ190100IGW · Engine Oil Indicating System
  > DURING THE CLIMB, THE PILOT REPORTED NR 1 ENGINE OIL LEVEL & LOW PRESSURE INDICATIONS. RETURNED, AND AFTER A SAFE LANDING, PILOT REPORTED A NR 1 ENGINE EXCEEDANCE EICAS INDICATION AFTER LANDING. FOUND AN OIL LEAK FROM THE NR 1 ENGINE FWD SUMP BEING THE CAUS

Next page: https://openairdocs.org/engine/ge-cf34-10e6/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 = 'CF3410E6'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cf34-10e6/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.