# Service difficulty reports: GE CF34 series

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

Newest first. General aviation reporting is voluntary.

Page 1 of 28 · 1,368 reports

- [SDR ICRR202310180001](https://openairdocs.org/sdr/ICRR202310180001.md): Pin · cracked · Oct 18, 2023 · Engine (Turbine/Turboprop)
  > A CRACK INDICATION WAS DISCOVERED DURING FPI CF 34 PROCEDURE SPM 70-32-02
- [SDR ICRR202310180002](https://openairdocs.org/sdr/ICRR202310180002.md): Pin · cracked · Oct 18, 2023 · Engine (Turbine/Turboprop)
  > A CRACK INDICATION WAS DISCOVERED DURING FPI PER CF 34 PROCEDURE SPM 70-32-02.
- [SDR ICRR202310180003](https://openairdocs.org/sdr/ICRR202310180003.md): Pin · cracked · Oct 18, 2023 · Engine (Turbine/Turboprop)
  > A CRACK INDICATION WAS DISCOVERED DURING FPI PENETRANT INSPECTION SPM 70-32-02.
- [SDR ICRR202310060001](https://openairdocs.org/sdr/ICRR202310060001.md): Pin · cracked · Oct 6, 2023 · Main Rotor Blades
  > A CRACK WAS DISCOVERD DURING PENETRANT INSPECTION PER SPM 710-32-02
- [SDR ICRR202304250001](https://openairdocs.org/sdr/ICRR202304250001.md): Pin · cracked · Apr 25, 2023 · Engine (Turbine/Turboprop)
  > CRACK INDICATION DISCOVERED DURING LIQUID PENETRANT INSPECTION PER SPM 70-32-02. TSN/TSO UNKNOWN.
- [SDR AALA202209081644](https://openairdocs.org/sdr/AALA202209081644.md): Eec · inoperative · Sep 5, 2022 · N717AN · Boeing 777 · Fuel Control/Reciprocating Engines
  > AIRCRAFT WAS GROUNDED: RIGHT THRUST REVERSER APPEARED ON ENGINE INDICATING AND CREW ALERTING SYSTEM 3 TIMES IN THE AIR, TWICE ON THE GROUND. DIVERTED TO TUL. FOUND FAULTS TO BE CORRELATED WITH ELECTRONIC ENGINE CONTROL C1 R INDICATION ON STATUS MESSAGES. INSTA
- [SDR AALA202207266479](https://openairdocs.org/sdr/AALA202207266479.md): None · none · Jul 24, 2022 · N804AN · Boeing 737 · Engine (Turbine/Turboprop)
  > AIRCRAFT WAS GROUNDED: ABORTED TAKEOFF AT APPROXIMATELY 65 KNOTS DUE TO RIGHT ENGINE FAIL. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)
- [SDR R61A2022071500440](https://openairdocs.org/sdr/R61A2022071500440.md): Engine · vibration · Jul 11, 2022 · N650RW · Emb ERJ170100SE · Engine (Turbine/Turboprop)
  > ENGINE 2 LP VIBES 4.0. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. INSPECTED ENGINE 2 FAN BLADES, NO DEFECTS NOTED. PLACED ON DEFERRAL. CLEARED BY PERFORMING N1 VIBRATION WORKSCOPE JOBCARD.
- [SDR 2022F00278](https://openairdocs.org/sdr/2022F00278.md): None · unserviceable · Jul 6, 2022 · N957 · Boeing 7373B7 · Engine (Turbine/Turboprop)
  > ON JUNE 28TH, A/C N957AM SCHEDULED TO FLIGHT AM652 (GDL- ORD) PERFORMED AND AIR TURN BACK DUE TO ENGINE FAILURE DURING CLIMB, BIRDSTRIKE ON ENGINE #2 DAMAGED ON FAN BLADES AND FAN CASE WERE FOUND MAINLY, AS A CORRECTIVE ACTION THE ENGINE #2 WAS REPLACED AT GDL
- [SDR A6WA202206088189](https://openairdocs.org/sdr/A6WA202206088189.md): Oil System · warning message · Jun 8, 2022 · N444ZW · Cndair CL6002B19 · Engine Oil Cooler
  > AT CRUISE AT FL280, RECEIVED RT ENG OIL PSI WARNING MESSAGE. OIL PSI WAS FLUCTUATING IN THE GREEN BAND. C/W QRH. REDUCED POWER TO IDLE. DIVERTED TO ICT. AROUND 8,000FT, OIL PSI WENT INTO THE RED AND REMAINED THERE FOR THE REST OF THE FLIGHT. SHUT ENGINE D
- [SDR A6WA202205268214](https://openairdocs.org/sdr/A6WA202205268214.md): Bracket · cracked · May 26, 2022 · N444ZW · Cndair CL6002B19 · Engine Air Intake System
  > L/H #1 ENGINE BRACKET P/N:228-50020-805 CRACKED AT 7 O'CLOCK POSITION AND BRACKET P/N: 228-50020-161 CRACKED AT 11-12 O'CLOCK POSITON ON NOSE INLET ATTACH RING. L/H #1 ENGINE NOSE COWL ATTACH RING FLANGE HAS 2 EA ELONGATED HOLES AT 7 O'CLOCK POSITION AND BETW
- [SDR 2022FA0000154](https://openairdocs.org/sdr/2022FA0000154.md): Power Lever · loose · Mar 2, 2022 · N488CR · Cndair CL600* · Engine Controls
  > @1922.5HRS AND 321CY THROTTLE RESISTANCE FAILED APPLICABLE LIMITS PER THE MANUFACTURE MAINTENANCE MANUAL. AIRCRAFT WAS GROUNDED AND MAINTENANCE TEAM BEGAN TROUBLESHOOTING. PER THE MANUFACTURES FAULT ISOLATION AND TROUBLESHOOTING GUIDANCE FROM BOMBARDIER TECHNI
- [SDR 2022F00052](https://openairdocs.org/sdr/2022F00052.md): Manifold · cracked · Feb 25, 2022 · Aircraft Fuel System
  > A CRACK INDICATION WAS FOUND ON THE METAL PORTION OF THE MANIFOLD DURING FPI INSPECTION SPM 70-32-02.
- [SDR ICRR202109300001](https://openairdocs.org/sdr/ICRR202109300001.md): Pin · cracked · Sep 30, 2021 · Turbine Engine Air Inlet Section
  > CRACK INDICATION WAS DISCOVERED DURING LIQUID PENETRANT INSPECTION PER SPM 70-32-02. TSN/TSO UNKNOWN.
- [SDR ICRR202109300002](https://openairdocs.org/sdr/ICRR202109300002.md): Pin · cracked · Sep 30, 2021 · Turbine Engine Air Inlet Section
  > CRACK INDICATION DISCOVERED DURING LIQUID PENETRANT INSPECTION PER SPM 70-32-02. TSN/TSO UNKNOWN.
- [SDR ICRR202109300003](https://openairdocs.org/sdr/ICRR202109300003.md): Pin · cracked · Sep 30, 2021 · Turbine Engine Air Inlet Section
  > CRACK INDICATION DISCOVERED DURING LIQUID PENETRANT INSPECTION PER SPM 70-32-02. TSN/TSO UNKNOWN.
- [SDR ICRR2021811002](https://openairdocs.org/sdr/ICRR2021811002.md): Pin · cracked · Aug 11, 2021 · Turbine Engine Air Inlet Section
  > TSN/TSO UNKNOWN CRACK INDICATION WAS DISCOVERED DURING LIQUID PENETRANT INSPECTION PER SPM 70-32-02
- [SDR ICRR2021811003](https://openairdocs.org/sdr/ICRR2021811003.md): Pin · cracked · Aug 11, 2021 · Turbine Engine Air Inlet Section
  > TSN/TSO UNKNOWN CRACK INDICATION WAS DISCOVERED DURING LIQUID PENETRANT INSPECTION PER SPM 70-32-02
- [SDR ICRR2021811004](https://openairdocs.org/sdr/ICRR2021811004.md): Pin · cracked · Aug 11, 2021 · Turbine Engine Air Inlet Section
  > TSN/TSO UNKNOWN CRACK INDICATION WAS DISCOVERED DURING LIQUID PENETRANT INSPECTION PER SPM 70-32-02
- [SDR ICRR2021811005](https://openairdocs.org/sdr/ICRR2021811005.md): Pin · cracked · Aug 11, 2021 · Turbine Engine Air Inlet Section
  > TSN/TSO UNKNOWN CRACK INDICATION WAS DISCOVERED DURING LIQUID PENETRANT INSPECTION PER SPM 70-32-02
- [SDR ICRR2021811006](https://openairdocs.org/sdr/ICRR2021811006.md): Pin · cracked · Aug 11, 2021 · Engine (Turbine/Turboprop)
  > TSN/TSO UNKNOWN CRACK INDICATION WAS DISCOVERED DURING LIQUID PENETRANT INSPECTION PER SPM 70-32-02
- [SDR ICRR2021811007](https://openairdocs.org/sdr/ICRR2021811007.md): Pin · cracked · Aug 11, 2021 · Turbine Engine Air Inlet Section
  > TSN/TSO UNKNOWN CRACK INDICATION WAS DISCOVERED DURING LIQUID PENETRANT INSPECTION PER SPM 70-32-02
- [SDR ICRR2021811008](https://openairdocs.org/sdr/ICRR2021811008.md): Pin · cracked · Aug 11, 2021 · Turbine Engine Air Inlet Section
  > TSN/TSO UNKNOWN CRACK INDICATION WAS DISCOVERED DURING LIQUID PENETRANT INSPECTION PER SPM 70-32-02
- [SDR SWIA202156302](https://openairdocs.org/sdr/SWIA202156302.md): Nut · loose · Feb 17, 2021 · N920SW · Cndair CL6002B19 · Engine Thrust Reverser
  > RIGHT REV UNLOCKED IN FLIGHT, FLIGHT 5038 - FILED CLOSED. PLEASE REFERENCE AML 581409. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22323893 WITH THE FOLLOWING CORRECTIVE ACTION: BEFORE RIGGING THE RT ENGINE STOW MICRO SWITCH, FOUND THE JAM NUTS LOOSE CAUSI
- [SDR SWIA202155708](https://openairdocs.org/sdr/SWIA202155708.md): Engine · power loss · Jan 31, 2021 · N919SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > ON DEPARTURE, LOST POWER IN ENGINE 2. N2 VIB. COMPLIED WITH QRC AND QRH. RETURNED TO LAND FLIGHT 5431 - FILED CLOSED. INTERROGATED MDC. FOUND RT ENGINE TO HAVE HIGH N1 VIBE AND HIGH ITT. ITT WAS REPORTED THROUGH MDC TO BE 1076C FOR 3.7 SECONDS. PER AMM 71
- [SDR A6WA202101137518](https://openairdocs.org/sdr/A6WA202101137518.md): Pdu · malfunctioned · Jan 7, 2021 · N449AW · Cndair CL6002B19 · Engine Thrust Reverser
  > EN ROUTE, DURING CLIMB, THE FLIGHT EXPERIENCED A LT THRUST REVERSER UNLOCKED CAUTION MESSAGE. THE CREW COMPLIED WITH THE QRH, NOTIFIED DISPATCH, AND DIVERTED TO KSYR. AIRCRAFT REMOVED FROM SERVICE. PDU LOCK WILL NOT FULLY STOW R & R PDU, IAW AMM 78-30. OPE
- [SDR R61A2021013000129](https://openairdocs.org/sdr/R61A2021013000129.md): Access Panel · cracked · Jan 7, 2021 · N647RW · Emb ERJ170100SE · Turbine Engine Air Inlet Section
  > WHILE A/C WAS IN FOR HEAVY CHECK FOUND NR 2 ENGINE INLET COWL ANTI ICE EXHAUST PANEL (421DR) CRACKED. EXHAUST PANEL PN 14C0406001 REPAIRED, IAW ETD 2021-170-000730.
- [SDR A6WA202011167424](https://openairdocs.org/sdr/A6WA202011167424.md): Engine · overheated · Nov 15, 2020 · N444ZW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > CLIMBING THROUGH 7000 RH ENG ITT 888 FLASH RED AT N1 87% AFTER APPROXIMATELY 10 SEC HEARD BANG AND SHUTTER. A/C YAWED AS RH, ENG POWER REDUCED. ACCOMPLISHED ENG SHUTDOWN. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED R/H ENGINE S/N 872452 OFF WITH S/N 87230
- [SDR V0XD20202210001](https://openairdocs.org/sdr/V0XD20202210001.md): Skin · cracked · Oct 21, 2020 · N921FJ · Cndair CL6002D24 · Engine Thrust Reverser
  > LT ENGINE LOWER THRUST REVERSER SKIN AND COAMING CRACKED NEAR LATCH COVER DOOR. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 4092.
- [SDR SWIA202055058](https://openairdocs.org/sdr/SWIA202055058.md): Stiffener · chafed · Oct 20, 2020 · N609SK · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > LT ENGINE UPPER FAN COWL DOOR RIB STIFFENER CHAFED NEAR UPPER INBOARD THRUST REVERSER ACTUATOR, FLAGGED. C-CHECK RO 1/5/2021. BLENDED OUT CHAFE ON LT ENGINE UPPER FAN COWL DOOR RIB STIFFENER, NEAR UPPER INBOARD THRUST REVERSER ACTUATOR, RESTORED FINISH WITHI
- [SDR SWIA202055059](https://openairdocs.org/sdr/SWIA202055059.md): Stiffener · chafed · Oct 20, 2020 · N609SK · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > LT ENGINE LOWER FAN COWL DOOR RIB STIFFENER CHAFED NEAR LOWER INBOARD THRUST REVERSER ACTUATOR, FLAGGED. C-CHECK RO 1/5/2021. BLENDED AND RESTORED CHAFED AREA ON LT ENGINE LOWER FAN COWL DOOR RIB STIFFENER NEAR LOWER INBOARD THURST REVERSER ACTUATOR, REF REO
- [SDR SWIA202055054](https://openairdocs.org/sdr/SWIA202055054.md): Slider · gouged · Oct 17, 2020 · N609SK · Cndair CL6002C10 · Engine Thrust Reverser
  > THE LT LOWER TRANSCOWL INBOARD SLIDER IS GOUGED. C-CHECK RO 1/5/2021. BLENDED DAMAGE ON LT LOWER TRANSCOWL INBOARD SLIDER AND REPAIRED, PER REO AND WITHIN LIMITS REF REO. COMPLIED WITH SKYWEST TASK CARD.
- [SDR RU3A2020092500031](https://openairdocs.org/sdr/RU3A2020092500031.md): Unknown · unknown · Sep 25, 2020 · N85 · Cndair CL6002B16 · Engine (Turbine/Turboprop)
  > CLIMBING OUT AFTER LOW APPROACH, BOTH THROTTLES AT 85% N1, HEARD A CLUNK AND FELT A SMALL BUMP. ALL LEFT ENGINE INSTRUMENTS HIGH. ITT SHOWED ALL RED LIGHTS. NO FIRE INDICATIONS OR WARNING, BROUGHT LEFT ENGINE TO IDLE, N1 CAME BACK TO IDLE AND ITT STAYED A L
- [SDR SWIA202052761](https://openairdocs.org/sdr/SWIA202052761.md): Stiffener · cracked · Sep 9, 2020 · N707SK · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > LT UPPER TRANSCOWL IS CRACKED UNDER Z STIFFENER AREA COMMON TO LATCH DOOR COMBING. FOUND AFTER REMOVAL OF STIFFENER FOR FASTENER REPLACEMENT. C-CHECK RO 9/21/2020. REPAIRED LT UPPER TRANS COWL, REF MHIRJ REO.
- [SDR SWIA202052916](https://openairdocs.org/sdr/SWIA202052916.md): Nozzle · corroded · Aug 7, 2020 · N920EV · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > RT EXHAUST NOZZLE FAIRING HAS BOTH FASTENERS AND HARDWARE CORRODED IN SEVERAL LOCATIONS. C-CHECK RO 10/1/2020. REMOVED AND REPLACED FASTENERS AND HARDWARE IN SEVERAL LOCATIONS ON THE FIRE-WIRE COVER ASSEMBLY AND ATTACHING FIRE SENSING BRACKET WITH NEW SERVIC
- [SDR A6WA2020041347258](https://openairdocs.org/sdr/A6WA2020041347258.md): Oil System · low · Apr 12, 2020 · N457AW · Cndair CL6002B19 · Turbine Engine Oil System
  > TURBULENCE AP DISENGAGED AND RECIEVED RT OR LF ENGINE OIL LOW PRESS WARNING. CREW UNABLE TO DETERMINE LT OR RT ENGINE. NO EXCENDENCES FOUND IN MAIN DATA COMPUTER "AIRCRAFT REMOVED FROM SERVICE" INTERROGATED MDC NO EXCEEDANCE'S FOUND. RAN BOTH ENGINES WITH CR
- [SDR VNAA2020010311102](https://openairdocs.org/sdr/VNAA2020010311102.md): Duct · failed · Jan 3, 2020 · N702PS · Cndair CL6002C10 · Engine Anti-Icing System
  > ENROUTE TO DCA CREW REPORTED A RIGHT BLEED ANTI ICE DUCT WARNING MESSAGE. CREW DECLARED EMERGENCY. CREW LANDED IN DCA WITH NO ISSUES AND FIELD EMERGENCY EQUIPMENT DID NOT RESPOND. MX REMOVED AND REPLACED RH BLEED AIR SUPPLY DUCT IAW CRJ 700 AMM. OPS CHECK GOO
- [SDR SWIA2019071646061](https://openairdocs.org/sdr/SWIA2019071646061.md): Unknown · fire · Jul 16, 2019 · N445SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > DURING SECOND ENGINE START WE HAD A HOT START. GROUND CREW INDICATED ENGINE FIRE. AFTER MOTORING THE ENGINE, THE GROUND CREW STILL INDICATED ENGINE FIRE. WE ELECTED TO RUN THE EXPEDITED DEPLANING CHECKLIST WHICH INCLUDING ACTIVATING THE FIRE BOTTLES. FIRE CREW
- [SDR 2020FA0000070](https://openairdocs.org/sdr/2020FA0000070.md): Track · cracked · Jan 24, 2019 · N60JC · Cndair CL6002B16 · Engine Thrust Reverser
  > THIS IS THE SECOND CRACKED MAIN REVERSER TRACK THAT HAS CRACKED ON THIS AIRCRAFT. ONE ON THE LEFT ENGINE AND ONE ON THE RIGHT ENGINE. TOTAL TAXING AND LANDING CYCLES AROUND 15,000/20,000.
- [SDR SIMA2018073020007](https://openairdocs.org/sdr/SIMA2018073020007.md): Engine · failed · Jul 20, 2018 · N522AE · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > ON AP INTO ORD NR 1 ENG SHUTDOWN. FLT DECLARED EMRG. L OIL PRESS WARNING ON EICAS, SUBSEQUENT L ENGINE FAILURE. REMOVED AND REPLACED LT ENGINE IAW WC 71-00- AND 71-002. OPS CHECK AND LEAK CHECK GOOD.
- [SDR SIMA20170804002](https://openairdocs.org/sdr/SIMA20170804002.md): Pump · failed · Aug 4, 2017 · N255NN · Emb ERJ170200LR · Engine Fuel Pump
  > DURING TAKEOFF ROLL, AT ABOUT 90 KNOTS, 5 PERCENT N1 LOSS FOR ABOUT 2 SECONDS. FOLLOWED BY 5 PERCENT N1 INCREASE, ALL OTHER PARAMETERS REMAINED NORMAL REMOVED AND REPLACED THE NR 1 ENGINE FUEL PUMP IAW EMM 73-00-00, SPECIAL PROCEEDURE 002. PERFORMED OPS A
- [SDR A6WA2017071245090](https://openairdocs.org/sdr/A6WA2017071245090.md): Stiffener · cracked · Jul 10, 2017 · N409AW · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > RIGHT TAILPIPE HAS A CRACKED STIFFENER AT 9 O'CLOCK POSITION 2ND FROM LE
- [SDR SWIA201743256](https://openairdocs.org/sdr/SWIA201743256.md): Carbon Seal · leaking · May 1, 2017 · N866AS · Cndair CL6002B19 · Turbine Engine Oil System
  > SMOKE IN THE COCKPIT AND A SMOKE CARGO WARNING MESSAGE. DIVERTED. REMOVED AND REPLACED THE NR 1 CARBON SEAL. LEAK CHECKED AND OIL CONSUMPTION CHECKED GOOD.
- [SDR VNAA2017040900010](https://openairdocs.org/sdr/VNAA2017040900010.md): Carbon Seal · defective · Apr 9, 2017 · N260JS · Cndair CL6002B19 · Turbine Engine Oil System
  > RED RIGHT ENGINE OIL PRESSURE WARNING. REMOVED AND REPLACED THE ACCESSORY DRIVE GEARBOX’S CARBON SEAL ASSEMBLIES.
- [SDR YGJR2017012500001](https://openairdocs.org/sdr/YGJR2017012500001.md): Plug · backed out · Jan 24, 2017 · N549BA · Cndair CL6002B16 · Engine (Turbine/Turboprop)
  > WHILE COMPLYING WITH A VISUAL IDG OIL LEVEL CHECK ON THE NR 2 ENGINE, FOUND A DISLODGED BORESCOPE PORT PLUG LAYING IN THE LOWER ENGINE COWL. AFTER IDENTIFYING PROPER LOCATION OF DISLODGED BORESCOPE PORT PLUG, INSTALLED AS REQUIRED. REFERENCE SERVICE MANUAL S
- [SDR A6WA201744728](https://openairdocs.org/sdr/A6WA201744728.md): Engine · power loss · Jan 7, 2017 · N465AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > AT 31,000 FEET LOST 5% N1 ON RIGHT ENGINE WITH SLIGHT YAW. LASTED 2-3 SECONDS, THEN CONDITION CORRECTED ITSELF WITH NO INPUT FROM THE CREW. N1 WAS SET TO 85 % AT TIME OF ROLLBACK, AND SPEED SWITCHES WERE SELECTED ON. NO ABNORMAL CAUTIONS OR MESSAGES PRESENT DU
- [SDR ASOA201612273091](https://openairdocs.org/sdr/ASOA201612273091.md): Engine · power loss · Dec 27, 2016 · N741EV · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > THE CREW REPORTED DURING CLIMB BETWEEN 18000-21000 FT, THE LEFT ENGINE N1 ROLLED BACK FROM 86.7% TO 83.9% 5 TIMES. ALL OTHER ENGINE INDICATIONS WERE NORMAL. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE FADEC AND THE NR 1 ENGINE FUEL METTERING UNIT,AND T
- [SDR R61A201612090721](https://openairdocs.org/sdr/R61A201612090721.md): Bolt · missing · Dec 9, 2016 · N864RW · Emb ERJ170100SE · Engine (Turbine/Turboprop)
  > DURING FLIGHT, CREW RECEIVED AN NR 1 ENGINE CONTROL FAULT MESSAGE. CREW NOTED THE NR 1 ENGINE WAS STUCK IN IDLE POWER SETTING. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE VG ACTUATOR BOLT MISSING, INSTALLED A NEW ONE
- [SDR SWIA201642830](https://openairdocs.org/sdr/SWIA201642830.md): Check Valve · failed · Nov 14, 2016 · N461SW · Cndair CL6002B19 · Turbine Engine Oil System
  > LEFT ENGINE EXPERIENCED AN IN FLIGHT EMERGENCY SHUT DOWN DUE TO HIGH OIL TEMP (199 IN RED) INDICATION ON EICAS. ALL OTHER ENGINE INDICATIONS NORMAL. CREW FOLLOWED QRH UNABLE TO GET TEMP INTO AMBER RANGE & SHUTDOWN THE ENGINE. DECLARED EMERGENCY & DIVERTED.
- [SDR SWIA201642610](https://openairdocs.org/sdr/SWIA201642610.md): Nozzle · chafed · Sep 2, 2016 · N947SW · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > LEFT EXHAUST NOZZLE HAS SEVERE CHAFING ON FWD EDGE OF NOZZLE JUST AFT OF SEAL. INSTALLED NEW UPPER AND LOWER STIFFENER ON TO THE LEFT HAND EXHAUST NOZZLE FAIRING IAW CMM.

Next page: https://openairdocs.org/engine/ge-cf34-series/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 = 'CF34'
ORDER BY difficulty_date DESC
```

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

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