# Service difficulty reports: CFM International CFM56-5A3 series

A list on [CFM International CFM56-5A3 series](https://openairdocs.org/engine/cfm-international-cfm56-5a3-series.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 6 · 256 reports

- [SDR DALA2026083004887](https://openairdocs.org/sdr/DALA2026083004887.md): Engine · power loss · Aug 28, 2026 · N343NW · Airbus A320212 · Engine (Turbine/Turboprop)
  > RTO- DUE TO NR 1 ENGINE WOULD NOT MAKE T/O POWER WITH THRUST REVERSER FAULT AND THRUST LEVER DISAGREE. CREW REJECTED AT LOW SPEED. TROUBLESHOOTING IN PROGRESS. (LP: 9489017, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026072304302](https://openairdocs.org/sdr/DALA2026072304302.md): Alternator · detached · Jul 21, 2026 · N361NW · Airbus A320212 · Accessory Gearboxes
  > RETURNED TO DTW DUE TO LOSS OF NBR 2 ENGINE OIL QUANTITY AND PRESSURE. CREW SHUT ENGINE DOWN WHEN QUANTITY AND PRESSURE WENT TO ZERO. MTC FOUND ENGINE CONTROL ALTERNATOR DETACHED FROM AGB MOUNTING PAD. MAINTENANCE IN PROGRESS. (LP: 8844868. AIRCRAFT WAS GROU
- [SDR DALA2026072304308](https://openairdocs.org/sdr/DALA2026072304308.md): Blades · damaged · Jul 21, 2026 · N344NW · Airbus A320212 · Turbine Engine Compressor Section
  > BIRDSTRIKE NR 2 ENGINE SIGNIFICANT FAN BLADE DISTORTION. C/W AMM 05-51 BIRDSTRIKE INSPECTION, NO OTHER DAMAGE NOTED ON FUSELAGE. INSPECTED NR 2 ENG IAW AMM 72-00-00-200 -001-A. REMOVED BOROSCOPE PLUGS NR 1, 4, AND 8 IAW AMM 72-31 -00-290-001-A. REMOVED CRAN
- [SDR DALA2026060803417](https://openairdocs.org/sdr/DALA2026060803417.md): Blade · bird ingestion · Jun 8, 2026 · N362NW · Airbus A320212 · Turbine Engine Compressor Section
  > ON DEPT OUT OF HOU, BIRDSTRIKE ON RT ENG, HIGH VIB INDICATION ON ECAM MAX 8.8 N1, ENG CONT TO RUN WITH THRUST PULLED BACK. C/W BIRDSTRIKE INSP IAW 72-00. FOUND MULTIPLE BLADES DAMAGED BEYOND REPAIR, ACOUSTIC PANES DAMAGE & RUB STRIP OUT OF LIMITS PER 72-21. R
- [SDR DALA2026060703412](https://openairdocs.org/sdr/DALA2026060703412.md): Engine · making metal · Jun 5, 2026 · N361NW · Airbus A320212 · Engine (Turbine/Turboprop)
  > RETURNED TO MSP DUE TO REPORT OF #2 ENGINE EGT OVERLIMIT. METAL FOUND IN TAILPIPE, ENGINE CHANGE REQUIRED. (LP: 8940774, AIRCRAFT WAS GROUNDED.)
- [SDR DALA2026052703217](https://openairdocs.org/sdr/DALA2026052703217.md): Actuator · worn · May 27, 2026 · N374NW · Airbus A320212 · Compressor Bleed Control
  > ATO- DUE TO RIGHT ENGINE COMPRESSOR VANE FAULT. FOUND VBV MASTER BALLSCREW ACTUATOR WORN AND NOT FUNCTIONING. REPLACED ACTUATOR, MECHANICAL STOP, GEAR MOTOR AND POSITION SENSOR. (LP: 8881690) AIRCRAFT WAS GROUNDED
- [SDR DALA2026053103309](https://openairdocs.org/sdr/DALA2026053103309.md): Engine · no discrepancy · May 18, 2026 · N369NW · Airbus A320212 · Engine (Turbine/Turboprop)
  > ATO - BIRD STRIKE C/W QRH AND F/COM MAINTENANCE NOTIFIED. NORMAL ENGINE INDICATION DURING ENTIRE EVENT. NO ADVERSE ODORS IN CABIN OR COCKPIT. REMOVED BIRD REMAINS. PERFORMED BIRD STRIKE INSPECTION IAW A320 AMM 05-51. NO DAMAGE NOTED. (LP: 8330410, AIRCRAFT WA
- [SDR DALA2025110608081](https://openairdocs.org/sdr/DALA2025110608081.md): Ecu · faulted · Nov 5, 2025 · N359NW · Airbus A320212 · Fuel Control/Turbine Engines
  > UNCOMMAND ENGINE SHUT DOWN, RESET STARTING IAW MC ENG N1 HUNG. REMOVED AND REPLACED NR 1 ENG ECU IAW AMM 73-21, FADEC BITE TEST AND ENG RUN N1 READ 21%, OPS CHECKED GOOD, OK FOR SERVICE. (LP: 7991956)
- [SDR DALA2025102907909](https://openairdocs.org/sdr/DALA2025102907909.md): Engine · bird ingestion · Oct 29, 2025 · N352NW · Airbus A320212 · Engine (Turbine/Turboprop)
  > BIRD STRIKE IN #2 ENGINE ON FINAL APPROACH. NO ABNORMAL ENGINE INDICATIONS. ENGINE WAS AT LOW POWER. SMELLED LIKE FOOD COOKING IN OVEN ACCORDING TO FAS. LATER LATER SMELLED LIKE FRIED CHICKEN. PERFORMED AMM 05-51-14. CLEARED ENGINE OF DEBRIS REF A320 AMM 72-00
- [SDR DALA2025102307751](https://openairdocs.org/sdr/DALA2025102307751.md): Engine · bird ingestion · Oct 21, 2025 · N335NW · Airbus A320212 · Engine (Turbine/Turboprop)
  > ON WALKAROUND POST FLIGHT INSPECTION FOUND NR 1 ENGINE AD EVIDENCE OF A BIRD STRIKE INSIDE THE ENGINE COWLING, ALL ENGINE INDICATIONS NORMAL. C/A: CW AMM 05-51-14 INSPECTION, CLEANED DEBRIS, NO DAMAGE NOTED, DEFER BOROSCOPE INSPECTION ON MON. FOR 25 FLT HR OR
- [SDR DALA2025101607562](https://openairdocs.org/sdr/DALA2025101607562.md): Oil System · low pressure · Oct 15, 2025 · N336NW · Airbus A320212 · Engine Oil Pressure
  > RETURNED TO SLC DUE TO LEFT ENGINE LOW OIL PRESSURE AND ENGINE WAS SHUT DOWN. ENGINE CHANGE REQUIRED DUE TO ENGINE OPERATED BELOW AMM OIL PRESSURE LIMITS. (LP: 7404148)
- [SDR DALA2025072905706](https://openairdocs.org/sdr/DALA2025072905706.md): Warning Message · illuminated · Jul 29, 2025 · N345NW · Airbus A320212 · Turbine Engine Compressor Section
  > SHIP 3245 - IFSD/DIV - AIRCRAFT DIVERTED TO BUF DUE TO NR 2 ENGINE COMPRESSOR VANE MESSAGE ALONG WITH EGT OVER LIMIT. ENGINE CHANGE REQUIRED DUE TO EGT LIMITS EXCEEDED.
- [SDR DALA2025071505317](https://openairdocs.org/sdr/DALA2025071505317.md): Idg · damaged · Jul 14, 2025 · N369NW · Airbus A320212 · AC Generator-Alternator
  > SHIP 3269 - DIV - TO AUS DUE APU ON MEL AND #2 IDG OIL TEMPERATURE ABOVE 147 DEGREES. CORRECTIVE ACTION: REPLACEMENT OF IDG #2 IN PROGRESS. (LP: 7809135)
- [SDR DALA2025062904821](https://openairdocs.org/sdr/DALA2025062904821.md): Shaft · sheared · Jun 28, 2025 · N369NW · Airbus A320212 · Hydraulic Pump (Electric/Engine), Main
  > DECLARED EMERGENCY DUE TO HYDRAULIC G OVERHEAT WITH NO RESTORATION OF HYD G SYSTEM. REQUIRED USE OF L/G GRAVITY GEAR EXTN HANDCRANK. VERIFIED FREE FALL EXTENSION. REFERENCE ODI EVENT LOG 1050057. GREEN EDP SHAFT FOUND SHEARED. R/R SAME AND FILTERS. LK/OPS CK
- [SDR DALA2025061404500](https://openairdocs.org/sdr/DALA2025061404500.md): Oil Filter · clogged · Jun 14, 2025 · N364NW · Airbus A320212 · Engine Oil Distribution (Airframe Furnished)
  > SHIP 3264 DISC: ABORTED T/O @ 55-60 KTS FOR ENG #1 OIL FILTER CLOG. C/A: FOUND LUBE FILTER AND SCAVENGE FILTER LINE INCORRECTLY HOOKED UP. REINSTALLED LINE PER CFM 56-5A EM 71-00-01-440-014, REQUIRES LEAK AND OPS CK WIP 215635. PERFORMED GOOD ENGINE RUN/LEAK
- [SDR DALA2025061404502](https://openairdocs.org/sdr/DALA2025061404502.md): Oil Filter · clogged · Jun 13, 2025 · N364NW · Airbus A320212 · Engine Oil Distribution (Airframe Furnished)
  > SHIP 3264 DISC: ENG#1 OIL CLOGGED ECAM ON TAKEOFF REJECTED TAKEOFF AT 50KTS. C/A: NO FAULT DETECTED. C/W AMDS WORKCARD #7900-9201-01 FILTER OIL SCAVENGE & LUBE REPLACED, NO DEFECT OR DEBRIS NOTED. MASTER CHIPS DETECTORS NO DEBRIS. RESTORED A/C TO NORMAL. OPS &
- [SDR DALA2025050903591](https://openairdocs.org/sdr/DALA2025050903591.md): Blade · fod · May 5, 2025 · N373NW · Airbus A320212 · Turbine Engine Air Inlet Section
  > SHIP 3273 DISC: POSSIBLE BIRD INJESTION IN ENGINE #2 ON TAKEOFF FROM KBWI POSSIBLE BIRD STRIKE. BIRD FLEW BY WINDSCREEN THEN N1 VIB IMMEDIATELY CLIMBED TO 8.0 BUT QUICKLY DECREASED TO 4.1. ALL OTHER ENGINE PARAMETERS NORMAL ENG #2. C/A: PERFORMED BIRD STRIKE I
- [SDR DALA2025041702988](https://openairdocs.org/sdr/DALA2025041702988.md): Hydraulic Line · leaking · Apr 17, 2025 · N349NW · Airbus A320212 · Hydraulic System, Main
  > SHIP 3249 - MISC/DE - DUE TO LOSS OF ALL YELLOW HYD SYS FLUID. CORRECTIVE ACTION: FOUND #2 ENGINE, RH OUTBOARD THRUST REVERSER LOCK ACTUATOR RETURN LINE LEAK UNDER A CLAMP BLOCK. REPLACED #2 ENGINE LATCH RETURN PIPE. #2 ENGINE EDP REPLACED DUE TO HYDRAULIC LOS
- [SDR DALA2025022801555](https://openairdocs.org/sdr/DALA2025022801555.md): Blades · shingled · Feb 28, 2025 · N349NW · Airbus A320212 · Engine Ignition Analyzer System
  > N1 ON #1 ENGINE ON CLIMB OUT VARYING BETWEEN.9-4.4 QRH 7.80 COMPLIED WITH. CRUISE N1.9-3.9 ON DESCENT ON THRUST REDUCTION VIBES AS HIGH AS 9.9. THRUST REDUCED TO MAINTAIN BELOW 6.0 FOR DURATION OF FLIGHT. INSP. FAN BLADES PER A320 AMM 72-21. FOUND SHINGLED
- [SDR DALA2025021901234](https://openairdocs.org/sdr/DALA2025021901234.md): Engine · failed · Feb 19, 2025 · N341NW · Airbus A320212 · Engine (Turbine/Turboprop)
  > SHIP 3241 -IFSD- RIGHT ENGINE FAILURE/SHUTDOWN CREW DECLARING AN EMERGENCY. CORRECTIVE ACTION: METAL DEBRIS IN TAILPIPE, ENGINE CHANGE IN PROGRESS. (LP: 6883614)
- [SDR DALA2025021501164](https://openairdocs.org/sdr/DALA2025021501164.md): Ecu · faulted · Feb 13, 2025 · N348NW · Airbus A320212 · Fuel Controlling System
  > SHIP 3248 - DIV - TO ORD DUE TO ENG 2 EIU FAULT AND AIR BLEED ECAM MESSAGE, FOLLOWED BY CAB PR EXCESS CAB ALT AND AIR PACK 1 FAULT AND AIR PACK 2 FAULT. CORRECTIVE ACTION: REPLACED #2 ENGINE ECU. OK FOR SERVICE. (LP 6821996)
- [SDR DALA2025021301125](https://openairdocs.org/sdr/DALA2025021301125.md): Engine · power loss · Feb 11, 2025 · N342NW · Airbus A320212 · Engine (Turbine/Turboprop)
  > SHIP 3242 DISC: DURING CRUISE @FL370, ATC GAVE US A SPEED REDUCTION, AS THE ENGINES DECREASED THRUST WE NOTICED ENG #1 VIB @ 2.2, AIRFRAME VIBRATIONS ANS FA'S REPORTED A "LOUD BANG". C/A: T/S PER A320 TSM 73-00-00-810-866-A R/R ENG #1 IP CHECK VALVE. ENG RAN A
- [SDR DALA2025020100766](https://openairdocs.org/sdr/DALA2025020100766.md): Duct · contaminated · Jan 29, 2025 · N371NW · Airbus A320212 · Engine Bleed Air System
  > SHIP 3271 DISC: FLIGHT ATTS AND OFF DUTY PILOT DETECTED AN ELECTRICAL ODOR IN THE REAR OF THE A/C ON TO OUT OF ATL. THE ODOR QUICKLY DISSIPATED. C/A: T/S PER WC 0550-2002 AND 0550-2003. DECISION TABLE LEADS TO NO.2 ENG AS POSSIBLE SOURCE. INSPECTED NO.2 SPINNE
- [SDR DALA2025010400066](https://openairdocs.org/sdr/DALA2025010400066.md): Engine · making metal · Jan 2, 2025 · N365NW · Airbus A320212 · Engine (Turbine/Turboprop)
  > SHIP 3265 -ATB- RETURNED TO MSP DUE TO RIGHT ENGINE HIGH VIBES AND EGT RISE. DECLARING EMERGENCY. UPON ARRIVAL MTC FOUND METAL IN THE TAILPIPE. CORRECTIVE ACTION: ENGINE CHANGE REQUIRED. (LP: 6954016)
- [SDR DALA2024121511716](https://openairdocs.org/sdr/DALA2024121511716.md): O-Ring · failed · Dec 12, 2024 · N340NW · Airbus A320212 · Engine (Turbine/Turboprop)
  > ON FINAL APPROACH GOT SLIGHT DIRTY SOCK ODOR. FA'S REPORTED SAME ODOR IN CABIN, JUST PRIOR TO TOUCHDOWN. COCKPIT TEMP INCREASED TO 80 DEGREES, ON TAXI IN ODOR INCREASED. #1 PACK OUTLET TEMP INCREASED RADIPLY TO 55 DEGREES CELSIUS THEN DECREASED TO 5 DEGREES CE
- [SDR DALA2024091508990](https://openairdocs.org/sdr/DALA2024091508990.md): Idg · leaking · Sep 13, 2024 · N359NW · Airbus A320212 · AC Generator-Alternator
  > DUE TO #1 IDG FAILURE AND APU UNABLE TO START. REPLACED #1 IDG AND APU IGNITOR.
- [SDR DALA2024071207045](https://openairdocs.org/sdr/DALA2024071207045.md): Engine · failed · Jul 11, 2024 · N373NW · Airbus A320212 · Turbine Engine Compressor Section
  > SHIP 3273 - ATB/IFSD - RIGHT ENGINE FAILURE AFTER TAKEOFF. CORRECTIVE ACTION: MAINTENANCE FOUND METAL IN TAIL PIPE; ENGINE CHANGE REQUIRED. REMOVE AND REPLACED #2 ENGINE ON LOG 0435692. (LP; 5152018)
- [SDR DALA2024062106277](https://openairdocs.org/sdr/DALA2024062106277.md): Plug · missing · Jun 20, 2024 · N373NW · Airbus A320212 · Engine (Turbine/Turboprop)
  > SHIP 3273 DISC: DIV - RECEIVED ENG 1 FIRE INDICATION INFLIGHT, RAN QRH & ECAM WHEN THRUST LEVER PLACED AT IDLE WARNING WENT AWAY. LEFT ENGINE AT IDLE AND DIVERTED TO PIB. C/A: FOUND BOROSCOPE PLUG AT 6 O'CLOCK POSITION OFF. REINSTALLED PLUG PER A320 AMM 72-51.
- [SDR DALA2024061406074](https://openairdocs.org/sdr/DALA2024061406074.md): Line · chafed · Jun 13, 2024 · N353NW · Airbus A320212 · Hydraulic System, Main
  > SHIP 3253 - MISC/DE - DUE TO LOSS OF YELLOW HYDRAULIC SYSTEM (HYD Y RSVR LO LVL ECAM). CORRECTIVE ACTION: FOUND #2 ENGINE T/R LOCK ACTUATOR LINE DAMAGED (CHAFFED) AT THE CLAMP, R/R BOTH LINES UNDER SAME CLAMP. ALSO, R/R EDP DUE TO POSSIBLE CAVITATION. OPS CHEC
- [SDR DALA2024042904754](https://openairdocs.org/sdr/DALA2024042904754.md): Pump · failed · Apr 28, 2024 · N357NW · Airbus A320212 · Fuel Boost Pump
  > DIVERSION TO CVG DUE TO THE LEFT ENGINE ROLLED BACK. DESCENDED IN ALTITUDE AND THE LEFT ENGINE BEGAN TO PRODUCE DESIRED POWER. REPLACED FUEL PUMP, HMU, ECU AND 5TH STAGE CHECK VALVE. HPC AND LPT BORESCOPES PERFORMED WITH MINOR FINDINGS IN HPC, DAMAGE WAS BLE
- [SDR DALA2024042904753](https://openairdocs.org/sdr/DALA2024042904753.md): Warning Message · false activation · Apr 27, 2024 · N375NC · Airbus A320212 · Turbine Engine Oil System
  > SHIP 3275 -ATO- ABORTED ON T/O AT APPROX 75 KTS, NOTICED ECAM MSG "ENG 2 OIL FILTER CLOG" ON RIGHT ENGINE. CORRECTIVE ACTION: OIL CLOG MESSAGE WAS ON MEL. CHECKED MCDS AND DPI'S AS PRECAUTIONARY WITH NO FINDINGS. (LP: 5301389)
- [SDR DALA2024042304647](https://openairdocs.org/sdr/DALA2024042304647.md): Warning Message · illuminated · Apr 21, 2024 · N375NC · Airbus A320212 · Turbine Engine Oil System
  > SHIP 3275 -ATO- DISCONTINUED TAKEOFF AT 75 KNOTS DUE TO RIGHT ENGINE OIL FILTER CLOG MESSAGE. CORRECTIVE ACTION: MTC IN PROGRESS, FILTER AND MCD CHECKED AND FWD TO MEL.
- [SDR DALA2024040404090](https://openairdocs.org/sdr/DALA2024040404090.md): Engine · slow · Apr 1, 2024 · N377NW · Airbus A320211 · Engine (Turbine/Turboprop)
  > SHIP 3277 -RTO- REJECTED TAKEOFF AT 80KTS DUE TO RIGHT ENGINE REPORTED AS SLOW TO SPOOL. CREW DID ADMIT TO NOT ALLOWING ENGINES TO STABILIZE AT 40% PRIOR TO SETTING TOGO THRUST. CORRECTIVE ACTION: FLIGHT CREW GOT BACK IN LINE FOR TAKEOFF AND ALLOWED ENGINES TO
- [SDR DALA2024031403324](https://openairdocs.org/sdr/DALA2024031403324.md): Fcu · faulted · Mar 11, 2024 · N376NW · Airbus A320212 · Engine Fuel and Control
  > UNSATISFACTORY ACFT PERFORMANCE AT ALTITUDE. WITH MORE THAN 2000 FT BUFFER ACFT UNABLE TO CLIMB, UNABLE AT CRUISE OR TO MAINTAIN AIRSPEED 15 TO 20 KYS SLOW. ENG PARAMETERS SHOW NORMAL, PERFORMANCE REQTS UNSAT. ENG SLOW TO RESPOND TO REQUEST FOR PERFORMANCE.
- [SDR DALA2024022602586](https://openairdocs.org/sdr/DALA2024022602586.md): Fuel Filter · clogged · Feb 25, 2024 · N356NW · Airbus A320212 · Engine Fuel Distribution
  > SHIP 3256 -DIV- TO DFW DUE TO #1 ENGINE FUEL FILTER CLOG MESSAGE ON CLIMB AT 500' AGL. CORRECTIVE ACTION: REPLACED FILTER AND CONTINUED TO HRL.
- [SDR DALA2024021502253](https://openairdocs.org/sdr/DALA2024021502253.md): Anti-Ice Valve · faulted · Feb 13, 2024 · N363NW · Airbus A320212 · Engine Anti-Icing System
  > SHIP 3263 - ATB - DUE TO ANTI ICE ENG2 VALVE CLSD ECAM MESSAGE. CANNOT CONTINUE INTO ICING CONDITIONS. CORRECTIVE ACTION: R/R #2 ENGINE ANTI-ICE VALVE. NO HELP. ITEM PLACED ON MEL PROCEDURES C/W (LOCKED VALVE IN OPEN POSITION). (LP: 4897922)
- [SDR DALA2024020901768](https://openairdocs.org/sdr/DALA2024020901768.md): Oil System · leaking · Feb 5, 2024 · N358NW · Airbus A320212 · Turbine Engine Oil System
  > DHIP 3258 DISC: DESCENDING THROUGH 18,000, VERY STRONG DIRTY SOCK SMELL PRESENT IN FLIGHT DECK. GOT WORSE 12,000 - 8,000, DISSIPATED, THEN RETURNED DURING GLIDE SCOPE CAPTURE/ POWER ROLL BACK ON FINAL APPROACH. SMELL NOT PRESENT IN CABIN. REMOVED PLUGS S1 AND
- [SDR DALA2023012500613](https://openairdocs.org/sdr/DALA2023012500613.md): Hpc · contaminated · Jan 25, 2023 · N370NW · Airbus A320212 · Engine (Turbine/Turboprop)
  > DIVERTED TO JFK DUE TO ODOR IN THE CABIN. FOUND OIL IN THE RIGHT ENGINE HPC. R/R ENGINE PER DELTA WORK CARD 7100-9901-RT AND BURNED-OUT DUCTS. OK FOR SERVICE.
- [SDR DALA2022120607804](https://openairdocs.org/sdr/DALA2022120607804.md): Blades · damaged · Dec 3, 2022 · N377NW · Airbus A320211 · Turbine Engine Compressor Section
  > DIVERSION TO LAS DUE TO NR 1 ENGINE HIGH N1 VIBRATIONS, HIGH EGT, AND SUSPECTED STALL ON LEFT SIDE. MAINTENANCE FOUND EXTENSIVE LPT BLADE DAMAGE. ENGINE CHANGE CURRENTLY IN PROGRESS.
- [SDR DALA2022112807560](https://openairdocs.org/sdr/DALA2022112807560.md): Hmu · leaking · Nov 26, 2022 · N362NW · Airbus A320212 · Fuel Controlling System
  > SHIP 3262 -DIV/IFSD- DIVERTED TO ORD DUE TO #1 ENGINE FADEC FAULT AND ENGINE SHUTDOWN. CORRECTIVE ACTION: FOUND FUEL LEAK AT HMU REPLACED SAME. PERFORMED HIGH POWER RUN WITH NO LEAKS OR FAULTS. LP 9817534
- [SDR DALA2022061304125](https://openairdocs.org/sdr/DALA2022061304125.md): B-Nut · loose · Jun 13, 2022 · N362NW · Airbus A320212 · Engine Oil System (Airframe Furnished)
  > SHIP 3262 - ATB - FLIGHT CREW PERFORMED AIR TURNBACK TO JFK DUE TO LOSS OF THE #1 ENGINE OIL QUANTITY. CORRECTIVE ACTION: FOUND OIL SUPPLY LINE B-NUT LOOSE, TIGHTENED LINE AND ALSO REPLACED LPT SHAFT AND SEALS ON LOG PAGE 8599532. PERFORMED HIGH POWER RUN NO F
- [SDR DALA2022011000203](https://openairdocs.org/sdr/DALA2022011000203.md): Ecu · faulted · Jan 10, 2022 · N364NW · Airbus A320212 · Fuel Controlling System
  > SHIP 3264 ON APPROACH TO RWY 22 15 MILES FROM RWY RECEIVED ENG 2 THRUST LEVER DISAGREE. PERFORMED ECAM & QRH PROCEDURES. DECLARED EMERGENCY PRIOR TO LANDING 22. LANDING SUCCESSFUL. NO FURTHER ISSUES. CORRECTIVE ACTION: R/R ENG #2 ECU IAW A320 AMM 76-11. PERF E
- [SDR DALA2021100706140](https://openairdocs.org/sdr/DALA2021100706140.md): None · none · Oct 6, 2021 · N365NW · Airbus A320212 · Engine Mount Section
  > SHIP 3265 GOUGE ENGINE MOUNT FWD MATING FACE OF PYLON PYRAMID ON RH PYLON. CORRECTIVE ACTION: PERFORMED PERMANENT PER PRI 594262-14 REV.0 AND ER/A 594262-14 REV.ORIGINAL. (1974137)
- [SDR DALA2017100207249](https://openairdocs.org/sdr/DALA2017100207249.md): Engine · leaking · Sep 27, 2017 · N376NW · Airbus A320212 · Engine (Turbine/Turboprop)
  > OIL SMELL /FUME IN CABIN/COCKPIT, REMOVED INLET FOR NOSE CONE. FOUND OIL POOLING INSIDE. NR 1 ENGINE REMOVED & REPLACED ON LOG 233466.
- [SDR DALA2017090506630](https://openairdocs.org/sdr/DALA2017090506630.md): Engine · malfunctioned · Sep 1, 2017 · N314US · Airbus A320211 · Engine (Turbine/Turboprop)
  > FUME IN ATL DURING BOARDING, ODOR OF UNKNOWN ORIGIN IN THE CABIN. DEPLANED PAX. SMALL HYD LEFT HORIZONTAL STAB LEADING EDGE HYD PIPING WAS FOUND AND REPAIRED. APU REPLACED PRECAUTIONARY DUE TO EVIDENCE OF OIL INGESTION. OIL DE-CONTAMINATION PROCEDURE WAS ACC
- [SDR DALA2017050103530](https://openairdocs.org/sdr/DALA2017050103530.md): Engine · leaking · Apr 30, 2017 · N352NW · Airbus A320212 · Engine (Turbine/Turboprop)
  > CONDITION AIR STINKS, BORESCOPED HPC1 AND 2, DISCOVERED OIL ON ALL BLADES, PRESENCE OF OIL AT BOOSTER OUTLET. REPLACED POWERPLANT AND REPLACED LT AND RT CABIN AIR RECIRCULATION FILERS AND LEFT PACK OZONE FILTER.
- [SDR CA150202010](https://openairdocs.org/sdr/CA150202010.md): Engine · stalled · Feb 1, 2015 · Airbus A319114 · Engine (Turbine/Turboprop)
  > (CAN) INCIDENT DETAILS, AFTER LANDING & EXITING RUNWAY, NR 2 ENGINE STALLED. ENG 2 FADEC TEST CARRIED OUT, NIL FAULT. NIL EVIDENCE OF ANY DAMAGE IN INTAKE OR EXHAUST, AREA INSPECTED, NO ABNORMALITY. NR 2 ENGINE STARTED WITHOUT ANY FAULT, NIL NOTED IN PFR, C
- [SDR CA150120021](https://openairdocs.org/sdr/CA150120021.md): Ecu · failed · Jan 19, 2015 · Airbus A319114 · Fuel Controlling System
  > (CAN) AFTER DEPARTURE THE CREW RECEIVED A WARNING REGARDING A PROBLEM THE ENGINE THRUST CONTROL SYSTEM. AFTER CONSULTATION WITH MTCE THE CREW ELECTED TO DIVERT BACK TO DEPARTURE. THE FLIGHT RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. AIRCRAFT TAKEN OFFLINE
- [SDR CA141229004](https://openairdocs.org/sdr/CA141229004.md): Fmc · failed · Dec 28, 2014 · Airbus A319114 · Flight Controller
  > (CAN) AFTER DEPARTURE, EXPERIENCED NR 1 FMGC FAILURE, A PATCH WAS DONE WITH MOC AND CREW ELECTED TO RETURN TO DEPARTURE. FLIGHT LANDED. NR 1 FMGC WAS REPLACED AND OPS TESTED SERVICEABLE IAW AMM 22-83-34 PB 401.
- [SDR CA141229002](https://openairdocs.org/sdr/CA141229002.md): Module · failed · Dec 26, 2014 · Airbus A319114 · Electrical Power System Wiring
  > (CAN) ENROUTE, EXPERIENCED AN ACRID ELECTRICAL ODOR ON THE AIRCRAFT. UNABLE TO ISOLATE THE ORIGIN SO THE CREW ELECTED TO DIVERT. A EMERGENCY WAS DECLARED. INSPECTED ALL PANELS FOR SIGNS OF OVERHEAT OR BURNED COMPONENTS. WIRES INSPECTED FOR ARCHING OR BURN

Next page: https://openairdocs.org/engine/cfm-international-cfm56-5a3-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 = 'CFM565A3'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/cfm-international-cfm56-5a3-series/reports

---
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.