# Service difficulty reports: CFM International CFM56-5B6 series

A list on [CFM International CFM56-5B6 series](https://openairdocs.org/engine/cfm-international-cfm56-5b6-series.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 6 · 280 reports

- [SDR AALA202609064238](https://openairdocs.org/sdr/AALA202609064238.md): Duct · disconnected · Sep 1, 2026 · N9013A · Airbus A319115 · Engine (Turbine/Turboprop)
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY DECLARED & ACFT RETURNED TO PHL DUE THE FLT CREW REPORTING ON TAKEOFF ENG 2 HAD A VERY SLOW SPOOL UP MORE SO THAN NORMAL & ON TAKEOFF AT 500 FT HAD ENG 2 FIRE ECAM. FLT CREW RAN ECAM & WHEN THRUST LEVER BROUGHT TO IDLE ECAM
- [SDR AALA202607066305](https://openairdocs.org/sdr/AALA202607066305.md): Duct · blown · Jul 1, 2026 · N8009T · Airbus A319115 · Fire Detection
  > AIRCRAFT GROUNDED: AN EMERGENCY DECLARED & ACFT RETURNED TO MIA DUE TO FLT CREW REPORTED THAT AT V1, LT ENG FIRE FAULT CAME ON TWICE. FLT CREW ACCOMP CHKLST & SHUT ENGINE DOWN. AFTER ENGINE SHUT DOWN, THE FAULT WENT AWAY. FLT CREW INFORMED BY THE FLIGHT ATTEN
- [SDR AALA202601107690](https://openairdocs.org/sdr/AALA202601107690.md): Seal · leaking · Jan 6, 2026 · N9010R · Airbus A319115 · Turbine Engine Oil System
  > AIRCRAFT WAS GROUNDED: FAIRLY RAPID DECREASE NUMBER 1 ENGINE OIL QUANTITY IN CRUISE FLIGHT LEVEL 360. REDUCED THRUST ON NUMBER 1 WHEN OIL QUANTITY REACHED 4QTS AND DIVERTED TO KMIA. PERFORMED A PRECAUTIONARY SHUTDOWN ENGINE ONE WHEN OIL QUANTITY REACHED 3QTS.
- [SDR QEMY20250905001](https://openairdocs.org/sdr/QEMY20250905001.md): Hub · cracked · Sep 3, 2025 · Turbine Engine Air Inlet Section
  > DURING INCOMING INSPECTION AT GE WALES, DEFECTS ON THE FAN FRAME HAVE BEEN NOTED. INNER HUB OF FAN FRAME FOUND CRACKED ON SURFACE L FLANGE IN 2 OFF LOCATIONS. IN BOTH LOCATIONS THE CRACK HAS FULL PENETRATION THROUGH THE FLANGE. DR #02238550 WAS REJECTED BY THE
- [SDR AALA202410244078](https://openairdocs.org/sdr/AALA202410244078.md): Engine · stalled · Oct 23, 2024 · N9010R · Airbus A319115 · Turbine Engine Compressor Section
  > AIRCRAFT WAS GROUNDED: DURING DESCENT INTO PIT, GOT ENG 2 COMPRESSOR VANE ECAM. CLEARED ON ITS OWN THEN CAME BACK ABOUT 30 SECS LATER. SHORTLY AFTERWHILE DESCENDING THROUGH 28000 FEET GOT AN ENG STALL ECAM AND WECOULD HEAR THE POPPING FROM THE ENGINE. WENT
- [SDR AALA202410284078](https://openairdocs.org/sdr/AALA202410284078.md): Motor · inoperative · Oct 23, 2024 · N9010R · Airbus A319115 · Compressor Bleed Valve
  > AIRCRAFT WAS GROUNDED: DURING DESCENT INTO PIT, GOT ENG 2 COMPRESSOR VANE ECAM. CLEARED ON ITS OWN THEN CAME BACK ABOUT 30 SECS LATER. SHORTLY AFTERWHILE DESCENDING THROUGH 28000 FEET GOT AN ENG STALL ECAM AND WECOULD HEAR THE POPPING FROM THE ENGINE. WENT
- [SDR AALA202401180715](https://openairdocs.org/sdr/AALA202401180715.md): Engine · stalled · Jan 17, 2024 · N778XF · Airbus A319112 · Engine (Turbine/Turboprop)
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED COMMING INTO ORD. IN LEVEL CRUISE AT FL 370 ENGINE 1 AND ENGINE 2 STALL. OAT -64C, CLEAN AIR. FLIGHT CREW FOLLOWED QRH AND ECAM PROCEDURE, DESCENDED TO FL 270 AND ENGINE PARAMETERS RETURNED TO NORMAL. THE AIRCRA
- [SDR AALA202106299013](https://openairdocs.org/sdr/AALA202106299013.md): Engine · stalled · Jun 27, 2021 · N763US · Airbus A319112 · Engine (Turbine/Turboprop)
  > AIRCRAFT WAS GROUNDED: ENGINE #2 HAD TWO COMPRESSOR STALLS. VACATING FL 360 TO DESCEND TO FL 350, SMOOTH AIR, AUTO THRUST ON, ECAM ENGINE 2 STALL, SELF RECOVERED. ACCOMPLISHED VARIABLE BLEED VALVE LUBRICATION AND ENGINE WASH PER AMM 75-31-00-640-801-A, AMM
- [SDR AALA202102239012](https://openairdocs.org/sdr/AALA202102239012.md): Fuel Filter · clogged · Feb 19, 2021 · N9011P · Airbus A319115 · Engine Fuel Distribution
  > AIRCRAFT WAS GROUNDED: ENGINE 2 FUEL FILTER CLOG ECAM MESSAGE. REPLACED NR 2 ENGINE FUEL FILTER ELEMENT PER AMM 73-11-10-400-004-A (AALA202102239012) AND THE NR 2 ENGINE DIFFERENTIAL PRESSURE SWITCH PER AMM 73-34-15-400-041-A. (AALA202102239013) A SATISFACTO
- [SDR AALA202102239013](https://openairdocs.org/sdr/AALA202102239013.md): Pressure Switch · faulted · Feb 19, 2021 · N9011P · Airbus A319115 · Engine Fuel Distribution
  > AIRCRAFT WAS GROUNDED: ENGINE 2 FUEL FILTER CLOG ECAM MESSAGE. REPLACED NR 2 ENGINE FUEL FILTER ELEMENT PER AMM 73-11-10-400-004-A (AALA202102239012) AND THE NR 2 ENGINE DIFFERENTIAL PRESSURE SWITCH PER AMM 73-34-15-400-041-A. (AALA202102239013) A SATISFACTO
- [SDR AALA202012249009](https://openairdocs.org/sdr/AALA202012249009.md): Valve · leaking · Dec 23, 2020 · N9004F · Airbus A319115 · Engine Fuel and Control
  > AIRCRAFT WAS GROUNDED. ON TAKEOFF TOWER AND ANOTHER AIRCRAFT REPORTED LEFT ENGINE LEAKING FUEL (NO LEAK INDICATED IN THE AIR). AN EMERGENCY WAS DECLARED AND RETURNED TO PHL WHERE THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. REPLACED THE HPTACC VALVE
- [SDR AALA202011169003](https://openairdocs.org/sdr/AALA202011169003.md): Warning Message · false activation · Nov 15, 2020 · N760US · Airbus A319112 · Engine Thrust Reverser
  > AIRCRAFT WAS GROUNDED. REJECTED TAKEOFF AT APPROXIMATELY 40 KNOTS, ENGINE NR 1 THRUST REVERSER LOCK ELECTRONIC CENTRALIZED AIRCRAFT MONITOR FAULT. ACCOMPLISHED TROUBLESHOOTING, PER TSM 78-31-00-810-863-A. NO FAULTS NOTED. PERFORMED A SATISFACTORY OPERATI
- [SDR AALA202010209016](https://openairdocs.org/sdr/AALA202010209016.md): Check Valve · out of tolerance · Oct 18, 2020 · N740UW · Airbus A319112 · Pneumatic Distribution System
  > AIRCRAFT WAS GROUNDED. AT CRUISE, FL 280, WITH REDUCTION OF POWER, RECEIVED MULTIPLE (2) COMPRESSOR/ENGINE STALLS WITH SELF RECOVERY. MOMENTARY ECAM (LEFT ENGINE) THAT SELF CLEARED. ACCOMPLISHED BORESCOPE ON NR 1 ENGINE WITH NO DEFECTS NOTED. MAINTENANCE F
- [SDR AALA202003169004](https://openairdocs.org/sdr/AALA202003169004.md): Fuel · clogged · Mar 11, 2020 · N9011P · Airbus A319115 · Engine Fuel Pump
  > AIRCRAFT GROUNDED - ENG NO.2 FUEL FILTER CLOG, MSG ON FINAL APPROACH. REMOVED AND REPLACED NO. 2 ENGINE FUEL PUMP PER AMM 73-11-10 AND MCM 73-94-11, OPERATIONAL CHECK AND LEAK CHECK OK.
- [SDR AALA2020022099016](https://openairdocs.org/sdr/AALA2020022099016.md): Sensor · faulty · Feb 18, 2020 · N712US · Airbus A319112 · Fuel Controlling System
  > AIRCRAFT WAS GROUNDED: ON ENGINE RUNUP FOR TAKEOFF WITH BOTH ENGINES AT 50% N1, THRUST LEVERS PLACED IN TOGA LEFT ENGINE EXTREMELY SLOW TO RUNUP. ASSYMETRIC THRUST CREATED REJECT ON RUNWAY. MAX AIRSPEED 50 KTS. ACCOMP;ISED TSM TASK 71-00-00-810-807-A AND TSM T
- [SDR AALA202002109043](https://openairdocs.org/sdr/AALA202002109043.md): Warning Message · false activation · Feb 6, 2020 · N9002U · Airbus A319115 · Engine (Turbine/Turboprop)
  > AIRCRAFT NOT GROUNDED: COMPRESSOR STALL / ENG 1 STALL MSG DURING REV THRUST OK AFTER POWER REDUCTION. ACCOMPLISHED TSM 73-00-00-810-865-A ENG 1 STALL. AFTER THAT, PERFORMED #1 ENGINE POWER ASSURANCE CHECK CARD NO 71-95-01, NO DISCREPANCIES NOTED.
- [SDR ASAA2020010231741](https://openairdocs.org/sdr/ASAA2020010231741.md): Engine · failed · Dec 29, 2019 · N525VA · Airbus A319112 · Engine (Turbine/Turboprop)
  > PRIOR TO TOP OF DESCENT, N1 ROLL BACK AND ENG 2 STALL ECAM. ENGINE RECOVERED TO CRUISE POWER BUT N@ VIBE INCREASED TO ABOUT 4.5 AS WE WERE IN QRH FOR ENG 2 STALL VIBE ON N2 UP TO 9.9 ENG 2 THEN FLAMED OUT AND FLAMES EXITED TAILPIPE. PROCEEDED TO SHUT ENG 2 D
- [SDR AALA201910189013](https://openairdocs.org/sdr/AALA201910189013.md): Blade · damaged · Oct 17, 2019 · N4005X · Airbus A319115 · Turbine Engine Compressor Section
  > AIRCRAFT WAS GROUNDED: PILOT REPORTS AT CRUISE ECAM ENG 1 E10 FAULT ANNUNCIATED WITH ENGINE 1 FIRE LIGHT FLASHING, FAULT LIGHT ASSOCIATED AUTOTHURST ECAM MESSAGES FAULT WENT AWAY AFTER 3 MIN (THIS EVENT OCCURED TWICE). MAINTENANCE FOUND EVIDENCE OF A BIRDSTRIK
- [SDR CA190809013](https://openairdocs.org/sdr/CA190809013.md): O-Ring · leaking · Aug 8, 2019 · Airbus A319112 · Hydraulic System, Main
  > (CAN) HYDRAULIC LEAK SUSPECTED BY CREW INFLIGHT. LEAK CONFIRMED AFTER ARRIVAL. RESOLUTION O RING ON PTU MFLD. (YELLOW) HYD. RETURN LINE FOUND LEAKING. O RING REPLACED PER AMM STD.PRACTICES. LEAK CHECK OK PER AMM 29-10-00-200-025A. (TC# 20190809013)
- [SDR AALA201901059002](https://openairdocs.org/sdr/AALA201901059002.md): Engine · malfunctioned · Jan 4, 2019 · N747UW · Airbus A319112 · Turbine Engine Compressor Section
  > AIRCRAFT WAS GROUNDED: CLIMBING THROUGH 30,000, 2 BANGS HEARD AND ECAM MESSAGE DISPLAYED COMPRESSOR STALL NR 2 ENGINE. EMERGENCY DECLARED AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED #2 ENGINE AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
- [SDR ASAA2018052024715](https://openairdocs.org/sdr/ASAA2018052024715.md): Apu · overserviced · May 20, 2018 · N527VA · Airbus A319112 · APU Oil System
  > STRONG ODOR RETURNED ON DESCENT. SMELLED LIKE OIL DROPPING ON SOMETHING HOT. MOST NOTICEABLE IN CENTER CABIN. ACFT GROUNDED. TROUBLESHOT AND FOUND A APU BLEED FAULT IAW TSM 25-00-00-810-823. RAN ENGINES AND APU BLEED OFF WITH NO OCCURENCE OF ODORS. FOUND
- [SDR CA180423013](https://openairdocs.org/sdr/CA180423013.md): Software · failed · Apr 22, 2018 · Airbus A319112 · Engine Controls
  > (CAN) WHILE POSITIONING INTO TAKE-OFF POSITION NR 2 ENGINE FLAMED OUT. FLIGHT RETURNED TO GATE FOR INVESTIGATION. RESOLUTION, AS PER AMM 72-00-00-200-026A NR 2 ENG PS3 FLEX SENSE LINE REPLACED, AS PER AMM 73-21-60-420-052-A. NR 2 ENG ECU REPLACED AND TESTED
- [SDR CA180314007](https://openairdocs.org/sdr/CA180314007.md): Fan · failed · Mar 12, 2018 · Airbus A319112 · Air Distribution Fan
  > (CAN) SMOKE IN COCKPIT. FLIGHT DIVERTED. RESOLUTION EXTRACT FAN 18HQ REPLACED, IAW AMM 21-26-51 PB401. OPERATIONAL TEST, AS PER AMM 21-26-00-710-001-A. (TC# 20180314007)
- [SDR AALA201802089026](https://openairdocs.org/sdr/AALA201802089026.md): Engine · malfunctioned · Feb 7, 2018 · N4005X · Airbus A319115 · Engine (Turbine/Turboprop)
  > REJECTED TAKE OFF FOR ASYMETRIC THRUST. LEFT ENGINE SPOOLED UP. RIGHT ENGINE LAGGED, MINOR SKID RESULTED. INSPECTED THE LEFT AND RIGHT MLG WHEEL AND BRAKES IAW AMM 32-11-00. NO DEFECT NOTED. PREFORMED ENGINE RUN WITH CREW TO POWER. ALL CHECKED GOOD IAW A
- [SDR AALA201712159044](https://openairdocs.org/sdr/AALA201712159044.md): Fuel Filter · clogged · Dec 14, 2017 · N9015D · Airbus A319115 · Engine Fuel Distribution
  > AIRCRAFT WAS GROUNDED. FLIGHT RETURNED TO MIA ON ACCOUNT OF A #2 ENGINE FUEL FILTER CLOG MESSAGE ON ECAM. EMERGENCY WAS DECLARED AND FLIGHT LANDED SAFELY WITHOUT FURTHER INCIDENT. REPLACED #2 ENGINE FUEL FILTER ELEMENT, ACCOMPLISED A SATISFACTORY OPERATIONAL C
- [SDR AALA20171214013](https://openairdocs.org/sdr/AALA20171214013.md): Filter · clogged · Dec 14, 2017 · N9015D · Airbus A319115 · Engine Fuel Distribution
  > AIRCRAFT WAS GROUNDED. DURING CRUISE, ECAM MESSAGE FOR THE NR 2 ENGINE FUEL FILTER CLOG MESSAGE ILLUMINATED. AIR RETURN BACK TO DEPARTURE. MAINTENANCE REPLACED THE FUEL FILTER ELEMENT IAW 73-11-10 AND PERFORMED SUCCESSFUL OPS CHECK.
- [SDR AALA201707119003](https://openairdocs.org/sdr/AALA201707119003.md): Engine · malfunctioned · Jul 6, 2017 · N9004F · Airbus A319115 · Engine (Turbine/Turboprop)
  > ABRUPT YAW ON TAKEOFF PRIOR TO 80 KNOTS. SYMMETRIC ENGINE INDICATIONS. REJECTED TAKEOFF AND RETURNED TO GATE. ACCOMPLISHED FURTHER RESEARCH AND FOUND NO ADDITIONAL INFORMATION.
- [SDR AALA20161211003](https://openairdocs.org/sdr/AALA20161211003.md): Fadec · malfunctioned · Dec 11, 2016 · N9018E · Airbus A319115 · Fuel Control/Turbine Engines
  > AIRCRAFT WAS GROUNDED. DEN, AIR INTERRUPT, DFW-EGE. EMERGENCY DECLARED. LANDING UNEVENTFUL. DURING CRUISE ECAM ALERTED "ENG NR 1 FUEL CTL FAULT". MAINTENANCE ACCOMPLISHED NR 1 ENGINE FADEC RESET IAW TSM 73-29-00. PERFORMED ENGINE NR 1 RUN WITH NO FAULTS NOTED
- [SDR VQIA2017081000044](https://openairdocs.org/sdr/VQIA2017081000044.md): Hmu · failed · Sep 23, 2016 · N528VA · Airbus A319112 · Fuel Controlling System
  > NR 1 ENGINE N1 VERY SLOW TO RESPOND, 70% SPLIT IN FLIGHT AT 3000 FT. IN FLIGHT LEFT N1 DROPPED FROM 70% TO IDLE, RIGHT N1 REMAINED AT 70%. R & R NR 1 ENGINE HMU IAW AMM 73-21-10. NO FURTHER ISSUES REPORTED ON SUBSEQUENT FLIGHTS.
- [SDR VQI2016F00030](https://openairdocs.org/sdr/VQI2016F00030.md): Wire · chafed · Aug 3, 2016 · N528VA · Airbus A319112 · Fire Protection System Wiring
  > DURING PREFLIGHT, HAD THE FOLLOWING WRITEUP: ENGINE 1 FIRE BOTTLE SQUIB, NR 1 NOT TESTING. R & R ENGINE 1 BOTTLE 1 SQUIB IAW AMM 26-21-41. OPS CHECK NO GOOD. ITEM REMAINS OPEN. REMOVED CONNECTOR PLUG FROM SQUIB FIRE BOTTLE 1 AND 2 ON ENGINE 1 AND CHECK VOL
- [SDR AALA201604099010](https://openairdocs.org/sdr/AALA201604099010.md): Control Unit · defective · Apr 8, 2016 · N714US · Airbus A319112 · Power Lever
  > AIRCRAFT WAS GNDED. ENG 1 THRUST LEVER DISAGREEMENT. ENG 1 STUCK AT IDLE THRUST. REPLACED NR 1 ENG THROTTLE CONTROL UNIT IAW AMM 76-11-19-400-042-A.
- [SDR AALA201603219006](https://openairdocs.org/sdr/AALA201603219006.md): Starter · defective · Mar 20, 2016 · N749US · Airbus A319112 · APU Start/Ignition System
  > AIRCRAFT WAS NOT GNDED. APU AUTO SHUTDOWN IN FLIGHT, FOLLOWED BY SMELL IN THE CABIN. REPLACED APU STARTER IAW AMM 49-42-51-400-0065-A. ACCOMPLISHED A SATISFACTORY LEAK & OPERATIONAL CHECK WITH NO ODORS BEING DETECTED.
- [SDR CA160321002](https://openairdocs.org/sdr/CA160321002.md): Warning Message · false activation · Mar 20, 2016 · Airbus A319112 · Ground Proximity System
  > (CAN) GPWS WARNING 15NM NW YDF VOR AT 3800 FT/250 KTS. TERRAIN, TERRAIN, THEN 10 SECONDS LATER TERRAIN,TERRAIN, PULL-UP. ASR TO FOLLOW. RESOLUTION FOCA CARD RETRIEVED AND DFDR DOWNLOAD C/O IAW MOCR.
- [SDR AALA201603159016](https://openairdocs.org/sdr/AALA201603159016.md): Engine · odor · Mar 11, 2016 · N760US · Airbus A319112 · Engine (Turbine/Turboprop)
  > AIRCRAFT WAS GNDED. INBD FLIGHT ATTENDANT REPORTED NOXIOUS CHEMICAL ODOR THROUGHOUT CABIN ON LANDING. REPLACED NR 2 ENG IAW JC 26L40071001.
- [SDR CA160128003](https://openairdocs.org/sdr/CA160128003.md): Safety Valve · failed · Jan 27, 2016 · Airbus A319112 · Pressure Regulator/Outflow Valve
  > (CAN) APPROXIMATELY 1HR INTO FLIGHT CREW REPORTED CABIN PRESSURE VALVE NOT CLOSING. CABIN PRESSURE ABOVE NORMAL. CREW PATCHED TO MOC VIA DISPATCH AND DECISION MADE TO DIVERT BACK TO THE AIRPORT. RESOLUTION SAFETY VALVES 6HL AND 7 HL REPLACED IAW AMM 21-31-5
- [SDR AALA201512299001](https://openairdocs.org/sdr/AALA201512299001.md): Engine · failed · Dec 28, 2015 · N737US · Airbus A319112 · Engine (Turbine/Turboprop)
  > AIRCRAFT WAS GNDED. ENG NR 1 STALL ECAM 2 TIMES. NO FLUCTUATIONS N1, N2, EGT NORMAL. FLIGHT LEVEL 370 WITH THRUST REDUCTION. NR 1 ENG FAILED BORESCOPE & WAS REPLACED IAW TASK CARD 26L40071001.
- [SDR CA151224004](https://openairdocs.org/sdr/CA151224004.md): Idg · failed · Dec 24, 2015 · Airbus A319112 · AC Generator-Alternator
  > (CAN) CREW RECEIVED AN IDG LOW OIL PRESSURE MESSAGE. MOC WAS CONSULTED AND RECOMMENDED CONTINUING TO DESTINATION WHERE THE GENERATOR COULD BE LOOKED AT FOR A POSSIBLE FIX OR DISPATCH UNDER MEL. CAPTAIN DETERMINED THAT BEST COURSE OF ACTION WAS TO RETURN TO DEP
- [SDR CA151208004](https://openairdocs.org/sdr/CA151208004.md): Hose · leaking · Dec 4, 2015 · Airbus A319112 · Hydraulic System, Main
  > (CAN) APPROXIMATELY 1 HR AFTER DEPARTURE THE CREW REPORTED A GREEN HYDRAULIC SYSTEM LOW PRESSURE INDICATION AND RETURNED TO AIRPORT. NO EMERGENCY WAS DECLARED AND LANDING WEIGHT WAS BELOW MAXIMUM. HYD LINE REPLACED ON NR 1 ENGINE. LEAK CHECK CARRIED OUT. N
- [SDR CA151202003](https://openairdocs.org/sdr/CA151202003.md): Hose · leaking · Dec 1, 2015 · Airbus A319112 · Hydraulic System, Main
  > (CAN) CREW REPORTED LOSING ALL YELLOW HYD SYS FLUID ABOUT 1 HR OUT OF FLL. AN EMERGENCY WAS NOT DECLARED AND A NORMAL LANDING WAS CARRIED OUT. MAINTENANCE CONTROL WAS ADVISED AND ARE INVESTIGATING. RESOLUTION FOUND LINE FROM PRESSURE SWITCH 3074GD LEAKING.
- [SDR CA151204010](https://openairdocs.org/sdr/CA151204010.md): Spool · failed · Nov 28, 2015 · Airbus A319112 · Turbine Engine Compressor Section
  > (CAN) ON SEPTEMBER 25, 2015 A CFM56 ENGINE WAS REMOVED FROM SERVICE DUE TO HPT DISK CYCLE LIMIT. AFTER INDUCTION INTO THE ENGINE SHOP THE ENGINE WAS DISASSEMBLED AS REQUIRED BY THE WORK SCOPE. DURING ROUTINE NDT INSPECTION THE HPC 1.-2. STAGE SPOOL WAS FOUND W
- [SDR CA151026004](https://openairdocs.org/sdr/CA151026004.md): Filter · dirty · Oct 25, 2015 · Airbus A319112 · Air Distribution System
  > (CAN) THE CAPTAIN REPORTED A FUMED EVENT THAT WAS APPARENTLY NOTICEABLE BY THE PASSENGERS AND CABIN CREW. THE EVENT OCCURRED IN THE LATTER STAGES OF THE FINAL APPROACH TO FLL, BELOW 500FT. THE ACFT HAS BEEN TEMPORARILY REMOVED FROM SERVICE PENDING MAINTENANC
- [SDR CA151013005](https://openairdocs.org/sdr/CA151013005.md): Hydraulic Line · leaking · Oct 12, 2015 · Airbus A319112 · Hydraulic System, Main
  > (CAN) GREEN HYDRAULIC SYS FAILURE ENROUTE. DIVERTED FOR MAINTENANCE. RESOLUTION FOUND LT ENGINE T/R ISOLATION VALVE HYD LINE LEAKING IN THE PYLON REPLACED HYD LINE IAW AMM 20-21-12 PB201.
- [SDR CA150922001](https://openairdocs.org/sdr/CA150922001.md): Fan · failed · Sep 21, 2015 · Airbus A319112 · Air Distribution Fan
  > (CAN) ON THE CLIMB OUT AT FL330, AN ELECTRICAL ODOR BEGAN EMANATING IN THE CABIN FOLLOWED BY AN ECAM MESSAGE IN THE FLIGHT DECK, VENT EXTRACT FAULT. THE CREW DECLARED AN EMERGENCY AND CARRIED OUT AN AIRBORNE RETURN TO AIRPORT. A NORMAL LANDING WAS CARRIED OUT
- [SDR CA150915003](https://openairdocs.org/sdr/CA150915003.md): Computer · malfunctioned · Sep 13, 2015 · Airbus A319112 · Central Warning
  > (CAN) ELECTRIC DC ESS BUS FAULT ON ECAM IN FLT. RESOLUTION: FOUND C/B "F05" FIN "12WV" " SDAC 1&2 28VDC ESS. BUS" AT 49VU TRIPPED. T/S C/O WITH REF. TO WD 31-54-27 P2, SHEET 2. SDAC 1 & SDAC, NR 2 REPLACED IAW AMM 31-55-34, PB 401. MSG CLEARED AFTER C/B RESE
- [SDR CA150825012](https://openairdocs.org/sdr/CA150825012.md): Controller · failed · Aug 24, 2015 · Airbus A319112 · Cabin Pressure Controller
  > (CAN) PRESSURIZATION ISSUES, DIVERTING TO LAND, DESCENDED TO F100. NO FURTHER INFORMATION AT THIS TIME. RESOLUTION R & R CPC NR 2 IAW AMM 21-31-34-000-001. REPLACE CABIN PRESSURE CONTROLLER OPS TEST PASS IAW AMM 21-31-00-710-002-A. ACFT OK FOR SERVICE.
- [SDR CA150623001](https://openairdocs.org/sdr/CA150623001.md): Valve · failed · Jun 22, 2015 · Airbus A319112 · Engine Fuel Distribution
  > (CAN) APPROX 45 MINUTES AFTER DEPARTURE THE CREW REPORTED A FUEL FLOW PROBLEM & NR 2 ENG STALL. FLIGHT RETURNED TO DEPARTURE AIRPORT & LANDED AT MAXIMUM LANDING WEIGHT. THE ENG WAS NOT SHUTDOWN & NO EMER WAS DECLARED. RESOLUTION REPLACED FUEL RETURN VLV IAW
- [SDR CA150605006](https://openairdocs.org/sdr/CA150605006.md): Starter · failed · Jun 5, 2015 · Airbus A319112 · Engine Starter
  > (CAN) AFTER PUSH, DURING START UP, SMOKE EMANATED FROM THE NR 2 ENGINE. THE START WAS ABORTED AND THE ACFT RETURNED TO THE GATE. MAINTENANCE CONTROL ADVISED. RESOLUTION NR 2 ENGINE STARTER REPLACED IAW AMM 80-11-10 FADEC MOTORING TESTS NORMAL ENGINE START C
- [SDR CA150504002](https://openairdocs.org/sdr/CA150504002.md): Hose · leaking · May 3, 2015 · Airbus A319112 · Fuel Heater
  > (CAN) DURING THE BOARDING PROCESS, A LEAK OCCURRED IN THE NR 2 ENGINE AREA RESULTING IN A PUDDLE 10X10 FEET. ERS RESPONDED FOR THE CLEAN UP. PASSENGERS WERE DEPLANED AS A PRECAUTION. RESOLUTION FOUND HEATER RETURN HOSE LEAKING NR HMU CONECTION, RESEATED CO
- [SDR SOKF20141125001](https://openairdocs.org/sdr/SOKF20141125001.md): Engine · bird ingestion · Nov 24, 2014 · N991TA · Airbus A319112 · Engine (Turbine/Turboprop)
  > DURING CLIMB FORM SJO TO SAL THE ENGINE NR 1 DAMAGED DUE BIRD STRIKE. ENGINE NR 1 WAS REMOVED AND REPLACED IAW AMM 71-00-00 AND OPERATIONAL AND LEAK TESTED IAW AMM 71-00-00-710-008 OK NORMAL. THE AIRCRAFT RETURNED TO NORMAL OPERATION.
- [SDR CA141020006](https://openairdocs.org/sdr/CA141020006.md): Cooling Fan · worn · Oct 20, 2014 · Airbus A319112 · Air Distribution Fan
  > (CAN) ON START UP A GRINDING SOUND FOLLOWED BY AN ODOR OCCURRED. SHORTLY AFTER STARTUP, SMELL DISSIPATED AND THE FLIGHT DEPARTED. APPROXIMATELY 1 HOUR INTO THE FLIGHT THE GRINDING SOUND RETURNED ALONG WITH THE ODOR. AFTER CONSULTATION WITH MOC THE FLIGHT WA

Next page: https://openairdocs.org/engine/cfm-international-cfm56-5b6-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 = 'CFM565B6'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/cfm-international-cfm56-5b6-series/reports

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