# Service difficulty reports: CFM International CFM56-5A5 series

A list on [CFM International CFM56-5A5 series](https://openairdocs.org/engine/cfm-international-cfm56-5a5-series.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 178 reports

- [SDR DALA2026102605859](https://openairdocs.org/sdr/DALA2026102605859.md): Engine · vibration · Oct 25, 2026 · N314NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > DECLARED AN EMERGENCY AND DIVERTED TO BWI DUE TO RIGHT ENGINE HIGH VIBRATION. INSPECTION PERFORMED BORESCOPE OF LPT WITH NO FINDINGS. PERFORMED FAN LUBE AND FAN TRIM BALANCE. COMPLETED WORK CARD 0550-2004. (LP: 9454672, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026101005578](https://openairdocs.org/sdr/DALA2026101005578.md): Engine · bird ingestion · Oct 8, 2026 · N353NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > ON T/O ROLL POSSIBLE BIRD INGESTION ON RT ENGINE. HIGH VIBRATION MESSAGE ON ROTATION & CLIMB. N1 AS HIGH AS 9.0 IN CRUISE N1 VIB AROUND 5.2. PERFORM BIRD STRIKE INSPECTION IAW AMM 72-00-00-200-001-001-A. FOUND NR 2 ENGINE WITH FAN BLADE DAMAGE. INSTALLED PE
- [SDR DALA2026092405335](https://openairdocs.org/sdr/DALA2026092405335.md): Blades · dented · Sep 21, 2026 · N327NB · Airbus A319114 · Turbine Engine Air Inlet Section
  > FOUND TWO BLADES DENTED ON NR 2 ENG. FOUND BLADES 29 AND 30 DENTS TO BE OUT OF LIMITS IAW AMM 72 -21-00-320-001-Q, DAMAGE EXCEEDS A DEPTH OF 1 INCH IN SECTION D INTO SECTION C. REROMVED SPINNER FRONT & REAR CONE IAW AMM 72-21 REMOVED AND REPLACED THE FAN B
- [SDR DALA2026091805197](https://openairdocs.org/sdr/DALA2026091805197.md): Engine · vibration · Sep 18, 2026 · N336NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > ATB- RETURNED TO AUS DUE TO ENGINE 1 VIBES ABOVE 4.0. CREW ALSO REPORTED FEELING A PULSE. MTC REPORTED HIGHEST N1 VIBE OBSERVED ON NUMBER ONE ENGINE WAS 4.2 UNITS. C/W FAN LUBE PER WORK CARD 7221-9601-01. C/W VIBE SURVEY PER AMM 71-00, N1 VIBES WITHIN LIMITS
- [SDR DALA2026092105243](https://openairdocs.org/sdr/DALA2026092105243.md): Engine · power loss · Sep 18, 2026 · N336NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > RTO - RIGHT ENG DID NOT SPOOL UP AS FAST AS THE LEFT ENGINE. NR 1 ENG REACHED 80% N1 WHILE END #2 WAS MUCH SLOWER. PERFORMED TSM 71-00-00-810-807-A, ENG SLOW TO ACCEL; PERFORMED A319 AMM 73-21-60-740-028-A, CORRECT FAULTS OF ENG SCHED MAINT RPTS; NO FAULTS RE
- [SDR DALA2026070603916](https://openairdocs.org/sdr/DALA2026070603916.md): Engine · no discrepancy · Jul 5, 2026 · N355NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > ATB, #2 ENG OVER LIMIT ON TAKEOFF. REMOVED CRANKPAD AND S17 BOROSCOPE PLUG ON NR 2 ENG PER A319 AMM 72-00. C/W OVERTEMP BSI ON #2 ENG PER A319 AMM 72-00 -00-200-003-A. NO DEFECTS NOTED. REINSTALLED CRANKPAD AND S17 BOROSCOPE PLUG ON #2 ENG PER A319 AMM 72-00.
- [SDR DALA2026070103869](https://openairdocs.org/sdr/DALA2026070103869.md): Drain Mast · missing · Jun 25, 2026 · N360NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE ARRIVED WITH DRAIN MAST MISSING. INSTALLED NR 2 ENGINE DRAIN MAST IAW AMM 71-71-42. (LP: 8906834, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026040802238](https://openairdocs.org/sdr/DALA2026040802238.md): Engine · no discrepancy · Apr 7, 2026 · N362NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > SUCKED UP PLASTIC BAG IN NR 2 ENGINE PRIOR TO TAKE OFF ON RWY. INSPECTED NR 2 ENG IAW AMM 72-00. NO DAMAGE OR DEFECT WAS NOTED. ACFT OK FOR SVC. IAW AMM 05-51-19-200-001-A. MCC NOTIFIED. INSPECTED NR 2 ENG IAW AMM 05-51-19-200-001-A. NO DAMAGE OR DEFECT WAS N
- [SDR DALA2026040602163](https://openairdocs.org/sdr/DALA2026040602163.md): Engine · faulted · Apr 4, 2026 · N349NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > REJECT TAKEOFF DUE TO ASYMMETRICAL POWER AND GATE RETURN FOR SIGNIFICANT LAG BETWEEN ENG & 2 ENG 1 LAGS 4 SEC TO ENG 2. INSPECTED PS3 LINE IAW AMM 72-00. PERFORMED ACCEL CHKD IAW AMM 71-00710-010-A ACCEL TIME OF 6.0 SECOND WITH IN LIMIT OF 7.5 AMM LIMIT. RUN
- [SDR DALA2026033002091](https://openairdocs.org/sdr/DALA2026033002091.md): Pump · faulted · Mar 29, 2026 · N371NB · Airbus A319114 · Hydraulic Pump (Electric/Engine), Main
  > ATO AT 70 KNOTS DUE TO HYD G ENG 1 PUMP LOW PRESSURE ECAM WARNING. REPLACED THE NR 1 ENGINE EDP PUMP (1030GK) AND PRESSURE SWITCH (1074GK). OPS CHECKED GOOD. (LP: 8863450)
- [SDR DALA2026032301930](https://openairdocs.org/sdr/DALA2026032301930.md): Generator · faulted · Mar 22, 2026 · N334NB · Airbus A319114 · AC Generator-Alternator
  > DUE TO LOSS OF BOTH ENGINE GENERATORS (ELEC GEN 1 FAULT AND ELEC GEN 2 FAULT ECAM WARNINGS), RAT DEPLOYED, AND APU GENERATOR RUNNING, #2 GENERATOR RECOVERED. CORRECTIVE ACTION: FOUND IDG #1 OVERSERVICED IN THE RED BAND. MAINTENANCE STILL IN PROGRESS. (LP: 8427
- [SDR DALA2026022701383](https://openairdocs.org/sdr/DALA2026022701383.md): Tailpipe · fire · Feb 25, 2026 · N337NB · Airbus A319114 · Engine Collector/Tailpipe/Nozzle
  > AT THE GATE, START WITH GND CART SUPPLYING AIR, RAMP PERSONNEL REPORTED POSSIBLE TAILPIPE FIRE NR 1 ENG. ALL SIGNS OF FLAME WENT OUT UPON ENGINE GETTING TO IDLE. NO CREW INTERACTION OR COCKPIT INDICATIONS WERE REPORTED. T/S PER AMM 71-00-00-869-001A, ANY FLA
- [SDR DALA2026012600553](https://openairdocs.org/sdr/DALA2026012600553.md): Hmu · failed · Jan 22, 2026 · N361NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > OBSERVED LARGE FLAMES EXITING NR 2 ROTOR ON START. TOWER CAM VERIFIED. NO COCKPIT/ECAM INDICATIONS. SHUTDOWN NR 2 AND TOWED BACK IN. R & R NR 2 ENGINE HMU IAW AMM 73-21. PERFORMED ENGINE IDLE LEAK CHECK. LEAK CHECKS GOOD. (LP: 8056744)
- [SDR DALA2026011200259](https://openairdocs.org/sdr/DALA2026011200259.md): Engine · fire · Jan 11, 2026 · N361NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > ON NR 2 ENGINE START, GROUND ADVISED FIRE & THAT THEY OBSERVED FLAMES COMING FROM THE ENGINE. T/S IAW TSM 72-00-00-810-801-A. NO DISCREPANCIES NOTED. NO 30-DAY HISTORY
- [SDR DALA2026011200260](https://openairdocs.org/sdr/DALA2026011200260.md): Engine · no discrepancy · Jan 10, 2026 · N317NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > UPON TOUCHDOWN, TOWER OBSERVED A FIRE OUT THE AFT END OF THE AIRCRAFT. ONCE EXITING THE RUNWAY THEY STATED IT WAS OUT. THERE WERE INDICATIONS INSIDE THE COCKPIT AND ALL ENGINE PARAMETERS WERE NORMAL. THERE WERE NO SMOKE OR FUMES PRESENT. T/S PER TSM 72-00-00-
- [SDR DALA2025120408855](https://openairdocs.org/sdr/DALA2025120408855.md): Engine · odor · Dec 3, 2025 · N317NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > DIRTY SOCK SMELL ON DESCENT. BECAME WORSE WITH APU BLEED ON IN GATE AREA. REMOVED AND REPLACED THE NR 2 ENGINE IAW AMM 7101. (8080650)
- [SDR DALA2025112108515](https://openairdocs.org/sdr/DALA2025112108515.md): Shaft · sheared · Nov 20, 2025 · N348NB · Airbus A319114 · Hydraulic Pump (Electric/Engine), Main
  > SHIP 3148 - DIV - TO PIT DUE TO LOSS OF THE GREEN SYSTEM HYDRAULIC PRESSURE. FOUND LT ENGINE HYDRAULIC PUMP SHAFT SHEARED. REPLACED LT ENGINE PUMP AND PTU. (LP 8013960, 8013958)
- [SDR DALA2025092206911](https://openairdocs.org/sdr/DALA2025092206911.md): Switch · leaking · Sep 20, 2025 · N301NB · Airbus A319114 · Hydraulic System, Main
  > HYD - DECLARED EMERGENCY DUE TO GREEN HYDRAULIC SYSTEM QUANTITY LOSS (HYD G RSVR LO LVL ECAM WARNING). FOUND SOLENOID SWITCH ON THE GREEN EDP LEAKING. REPLACED GREEN HYDRAULIC EDP. OPS CHECK GOOD. (LP 7820938)
- [SDR DALA2025090906649](https://openairdocs.org/sdr/DALA2025090906649.md): Engine · faulted · Sep 8, 2025 · N328NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE SHOWS HIGH FUMES FROM TAIL PIPE (BLUE). PERFORMED OIL SERVICE TO ENG 2 ADDED 5 QTS, PERFORMED DVI ON ENG 2 FOR OIL LEAKS EVIDENCES, NO FOUND. (7273398).
- [SDR DALA2025080805955](https://openairdocs.org/sdr/DALA2025080805955.md): Engine · odor · Aug 7, 2025 · N361NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > DIRTY SOCK SMELL NOTICED ON TAKEOFF ROLL AND EARLY CLIMB OUT. REMOVED AND REPLACED NR 1 ENGINE IAW AMDS 7100-9901-LT.
- [SDR DALA2025071605350](https://openairdocs.org/sdr/DALA2025071605350.md): Cable · sheared · Jul 16, 2025 · N361NB · Airbus A319114 · Engine Pressure Ratio (EPR)
  > SHIP 3161-ATB-RETURNED TO BIS DUE TO RIGHT ENGINE EGT OVER LIMIT. EMERGENCY WAS DECLARED. EGT LIMIT WAS NOT REACHED. MTC FOUND VBV INTERCONNECTING CABLE SHEARED AT NUMBER 9 POSITION VBV DOOR. REPLACED MASTER ACTUATOR, STOP MECHANISM, MOTOR, AND SHAFT. MIP.
- [SDR DALA2025053104192](https://openairdocs.org/sdr/DALA2025053104192.md): Hmu · failed · May 30, 2025 · N344NB · Airbus A319114 · Fuel Controlling System
  > SHIP 3144 -ATO- REJECTED TAKEOFF AT 30KTS DUE TO AN ENGINE #2 FAIL MESSAGE WITH ASSOCIATED ENGINE ROLL BACK. REPLACED HMU, PERFORMED HIGH POWER RUN CHECKS OK. (LP 7384562)
- [SDR DALA2025052303990](https://openairdocs.org/sdr/DALA2025052303990.md): Compressor · damaged · May 23, 2025 · N366NB · Airbus A319114 · Turbine Engine Compressor Section
  > SHIP 3166 - ATB- DECLARED AN EMERGENCY AND RETURNED TO IAH DUE TO RIGHT ENGINE COMPRESSOR STALL. CORRECTIVE ACTION: MULTIPLE HPC BLADES FOUND DAMAGED ON BORESCOPE INSPECTION. REPLACED NBR 2 ENGINE. (LP 7251270)
- [SDR DALA2025050103357](https://openairdocs.org/sdr/DALA2025050103357.md): Engine · power loss · Apr 30, 2025 · N329NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > SHIP 3129 -RTO- DISCONTINUED TAKE OFF @ 40KTS DUE TO #2 ENGINE WOULD NOT STABILIZE. CORRECTIVE ACTION: REPLACED ECU AND RAN ENGINE TO POWER, NO INDICATION ISSUES. (LP: 6989630)
- [SDR DALA2025040702620](https://openairdocs.org/sdr/DALA2025040702620.md): Bleed Valve · overheated · Apr 5, 2025 · N359NB · Airbus A319114 · Compressor Bleed Valve
  > SHIP 3159 - DIV - TO DEN DUE TO DUAL BLEED FAULT (AIR ENG 1 BLEED FAULT AND AIR ENG 2 BLEED FAULT). WAS ABLE TO RECOVER #1 ENGINE BLEED, PRESSURIZATION AND PACKS WORKING AS SHOULD. UNABLE TO CONTINUE DUE TO ENROUTE WEATHER. CORRECTIVE ACTION: REPLACED FAN AIR
- [SDR DALA2025032002105](https://openairdocs.org/sdr/DALA2025032002105.md): Hmu · faulted · Mar 17, 2025 · N336NB · Airbus A319114 · Fuel Controlling System
  > SHIP 3136 -DIV- DIVERTED TO PHL DUE TO RIGHT ENGINE COMPRESSOR STALL. ENGINE THROTTLE WAS NOT PULLED BACK AND ENGINE RESUMED NORMAL POWER. COMPLETED REQUIRED BOROSCOPE WITH NO ABNORMALITIES FOUND AND REPLACED HMU. (LP: 6826498)
- [SDR DALA2025022301384](https://openairdocs.org/sdr/DALA2025022301384.md): Anti-Ice Valve · inoperative · Feb 22, 2025 · N362NB · Airbus A319114 · Air Intake Anti/De-Ice System
  > SHIP 3162 DISC: SMOKE IN COCKPIT AT THE GATE IN KHOU. ON EXTERNAL POWER ONLY. APU AND ENGINES OFF. TURNED OFF ALL ELECTRICAL POWER AND SMOKE DISSAPATED. NO ECAM OR POPPED CIRCUIT BREAKERS. C/A: T/S SMOKE/FUME EVENT, DURING T/S FOUND C/B W10 #2 ENG ANTIICE POPE
- [SDR DALA2024110210585](https://openairdocs.org/sdr/DALA2024110210585.md): Bleed Air Sys · leaking · Nov 1, 2024 · N321NB · Airbus A319114 · Pneumatic Distribution System
  > SHIP 3121 - ATB - DUE TO AIR ENG 2 BLEED LEAK ECAM MESSAGE. UNABLE TO CONTINUE DUE TO WEATHER IN MSP. CORRECTIVE ACTION: FOUND LEAKS ON TLT, TCT, AND PRV. REPLACED PYLON OVERHEAT SENSING ELEMENT. FAN CONTROL THERMOSTAT, BLEED PRESSURE REGULATOR VALVE CONTROL,
- [SDR DALA2024093009562](https://openairdocs.org/sdr/DALA2024093009562.md): Mount · gouged · Sep 27, 2024 · N332NB · Airbus A319114 · Engine Mount Section
  > SHIP 3132 DURING M-CHECK AT BFM INSPECTION FOUND A GOUGE ON FWD ENGINE MOUNT AT THE # 3 GUIDE PIN HOLE LOCATION. CORRECTIVE ACTION: THE DAMAGE HAS BEEN BLENDED PER 51-73-00. (0579671)
- [SDR DALA2024090508740](https://openairdocs.org/sdr/DALA2024090508740.md): Idg · faulted · Sep 2, 2024 · N326NB · Airbus A319114 · AC Generator-Alternator
  > SHIP 3126 - ATO - AT THROTTLE UP DUE TO IDG 2 LOW OIL PRESSURE MESSAGE. CORRECTIVE ACTION: DEFERRED IDG 2 PER MEL. LATER REPLACED NBR 2 ENGINE IDG 4000XU. (LP 5713626)
- [SDR DALA2024022102369](https://openairdocs.org/sdr/DALA2024022102369.md): Valve · leaking · Feb 19, 2024 · N345NB · Airbus A319114 · Engine Fuel Distribution
  > SHIP 3145 -DIV- FLIGHT DIVERTED TO DTW DUE TO SUSPECTED FUEL OVER BURN. CORRECTIVE ACTION: FOUND UNION ON FUEL RETURN VALVE LEAKING ON LEFT ENGINE. REPLACED O-RING AND LEAK CHECKED. (LP 0209373)
- [SDR DALA2023032602312](https://openairdocs.org/sdr/DALA2023032602312.md): Unknown · unknown · Mar 24, 2023 · N364NB · Airbus A319114 · Hydraulic System, Main
  > SHIP 3164 - ATB - DUE TO LOSS OF GREEN SYSTEM HYDRAULICS. CORRECTIVE ACTION: FOUND LH MAIN GEAR LOCK STAY ACTUATOR INBOARD HYDRAULIC HOSE CAME APART AT SWAGE FITTING. REPLACED HOSE, PTU, FILTERS AND ENGINE HYDRAULIC PUMP. (LP 9395052)
- [SDR DALA2022122208288](https://openairdocs.org/sdr/DALA2022122208288.md): Latch · unlatched · Dec 19, 2022 · N359NB · Airbus A319114 · Engine Thrust Reverser
  > SHIP 3159 - IFSD/ATB - DUE TO ENG 2 THRUST REVERSER UNLOCKED MESSAGE. CORRECTIVE ACTION: FOUND ENG 2 UPPER OUTBOARD BLOCKER DOOR POPPING OPEN DURING DVI. REPLACED DOOR LATCH AND STOW SWITCH. P/N ON/OFF 321-400-502-0 SN ON:2323 SN OFF: 3082 PN ON C24742000-3 SN
- [SDR DALA2022101706707](https://openairdocs.org/sdr/DALA2022101706707.md): Compressor · stalled · Oct 15, 2022 · N317NB · Airbus A319114 · Turbine Engine Compressor Section
  > SHIP 3117 - ATO- DISCONTINUED TAKEOFF FOR RIGHT ENGINE COMPRESSOR STALL. MTC FOUND METAL DEBRIS IN THE TAIL PIPE. CORRECTIVE ACTION: REMOVED AND REPLACED # 2 ENGINE.(9730832)
- [SDR DALA2022050603186](https://openairdocs.org/sdr/DALA2022050603186.md): Ecu · faulty · May 5, 2022 · N370NB · Airbus A300* · Power Lever
  > SHIP 3170 -EMERGENCY DECLARED- FLIGHT CREW DECLARED AN EMERGENCY DUE TO LEFT ENGINE THRUST LEVER DISAGREE ECAM MESSAGE. CORRECTIVE ACTION: MAINTENANCE PERFORMED TROUBLESHOOTING PER TSM, REPLACED ECU PER A319 AMM 73-21-60. ALL CHECKS GOOD. NO PRIOR 30 DAY HISTO
- [SDR DALA2021081304668](https://openairdocs.org/sdr/DALA2021081304668.md): Engine · slow · Aug 9, 2021 · N335NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > SHIP 3135 - LOW SPEED REJECTED T/O DUE TO SLOW #1 ENG ADVANCING TO TOGA. CORRECTIVE ACTION: PERFORMED ACCEL CHECKS ON #1 AND #2 ENG'S IAW A319 AMM 71-00-00-710-010-A WITH GEN'S AND BLEED'S ON 1 AND 2 ACCEL WITH IN 4 SEC. WITH GEN'S AND BLEED'S OFF 1 AND 2 ACCE
- [SDR DALA2021072004088](https://openairdocs.org/sdr/DALA2021072004088.md): Engine · making metal · Jul 18, 2021 · N339NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > SHIP 3139 -DIV- DIVERSION DUE TO #2 ENGINE EGT OVER LIMIT ECAM MESSAGE WITH ASSOCIATED STALL AND VIBE. FOUND METAL IN THE TAILPIPE. CORRECTIVE ACTION: REMOVED #2 ENGINE PER AMDS WC 7100-9901RT. (7855264)
- [SDR DALA2021052502892](https://openairdocs.org/sdr/DALA2021052502892.md): Eec · malfunctioned · May 23, 2021 · N357NB · Airbus A319114 · Fuel Controlling System
  > SHIP 3157 -DIV- CREW EXPERIENCED ENG FADEC FAULT WITH ASSOCIATED FUEL CONTROL FAULT MESSAGE ON LEFT ENGINE. QRH STATES "AVOID RAPID THRUST CHANGES" OR ENGINE MAY RESPOND SLOWER THAN EXPECTED. OPERATIONAL DECISION TO DIVERT TO SLC. CORRECTIVE ACTION: REPLACED L
- [SDR DALA2021051202686](https://openairdocs.org/sdr/DALA2021051202686.md): Bleed Valve · not reported · May 11, 2021 · N336NB · Airbus A319114 · Pneumatic Distribution System
  > SHIP 3136 - REMOVE THE LT VALVE, BLEED, HIGH PRESSURE UNSERVICEABLE FOR ROUTE TO SHOP. CORRECTIVE ACTION: REMOVED LT HIGH PRESSURE BLEED VALVE PER A319 AMM 36-11 FOR SHOP ROUTING.(1805862)
- [SDR DALA2021051202687](https://openairdocs.org/sdr/DALA2021051202687.md): Valve · unserviceable · May 11, 2021 · N336NB · Airbus A319114 · Pneumatic Distribution System
  > SHIP 3136 - REMOVE THE VALVE, PNEUMATIC LOW PRESSURE CHECK UNSERVICEABLE FOR ROUTING TO PRIME SHOP FOR REPAIR. CORRECTIVE ACTION: PART REMOVED AS PER AMDS WORK CARD 7100.(1805877)
- [SDR DALA2021051202688](https://openairdocs.org/sdr/DALA2021051202688.md): Valve · unserviceable · May 11, 2021 · N336NB · Airbus A319114 · Pneumatic Distribution System
  > SHIP 3136 - REMOVE THE LT VALVE, BLEED HIGH PRESSURE UNSERVICEABLE FOR ROUTE TO SHOP. CORRECTIVE ACTION: REMOVED LT HIGH PRESSURE BLEED VALVE PER A319 AMM 36-11.(1805985)
- [SDR DALA2021051102657](https://openairdocs.org/sdr/DALA2021051102657.md): Ecu · faulted · May 10, 2021 · N336NB · Airbus A319114 · Fuel Controlling System
  > SHIP 3136 NBR 1 ENG COMPRESSOR STALLED IN FLIGHT. CORRECTIVE ACTION: PERFORMED VISUAL INSP OF VBV SYS, IP CHECK VALVE, VSV AND FOD INSP PER A319 TSM 7300. RR NBR 1 ENG ECU PER AB TSM 7300. (7317459)
- [SDR DALA2021051102655](https://openairdocs.org/sdr/DALA2021051102655.md): Hmu · failed · May 9, 2021 · N336NB · Airbus A319114 · Fuel Controlling System
  > SHIP 3136 DIV TO CVG DUE TO NO 2 ENGINE COMPRESSOR STALL. QRH FOLLOWED AND ENGINE PARAMETERS ARE NORMAL. CORRECTIVE ACTION: REPLACED RIGHT ENGINE IP CHECK VALVE, HMU AND ECU PER A319 AMM. (7317454)
- [SDR DALA2020121104053](https://openairdocs.org/sdr/DALA2020121104053.md): Latch · damaged · Dec 9, 2020 · N369NB · Airbus A319114 · Engine Thrust Reverser
  > DIV-TO BOI FOR ENGINE 1 REVERSER UNLOCKED ECAM MESSAGE. CREW SHUT THE ENGINE DOWN. NO BUFFETING REPORTED. CORRECTIVE ACTION: LOCKED OUT REVERSER AND DEFERRED, PER MEL (12/10 SEA). PERFORMED T/R TEST MULTIPLE TIMES, NO FAULTS. REMOVED AND REPLACED BLOCKER
- [SDR DALA2020120303958](https://openairdocs.org/sdr/DALA2020120303958.md): Cap · missing · Dec 2, 2020 · N366NB · Airbus A319114 · Turbine Engine Oil System
  > FOUND NR 2 ENGINE OIL CAP MISSING. CORRECTIVE ACTION: INSTALLED SERVICEABLE CAP ASSEMBLY LEAK CHECK NORMAL. OK FOR SERVICE.
- [SDR DALA2020113003916](https://openairdocs.org/sdr/DALA2020113003916.md): Hydraulic System · overserviced · Nov 27, 2020 · N319NB · Airbus A319114 · Hydraulic System, Main
  > DIRTY SOCK SMELL AT IDLE POWER ON DOWNWARD/BASE INTO ATL. CONFIRMED W/FA DISSIPATED ONCE ENGINES SPOOLED BACK UP. DID NOT SMELL AT HIGHER ALTITUDES ON DESCENT. CORRECTIVE ACTION: OPERATED BOTH ENGINES. PACKS AND APU, DETECTED SLIGHT ODOR WHILE RUNNING NR 1
- [SDR DALA2020111103675](https://openairdocs.org/sdr/DALA2020111103675.md): Support Bracket · cracked · Nov 9, 2020 · N369NB · Airbus A319114 · Turbine Engine Combustion Section
  > CRACK SUPPORT BRACKET COMBUSTION SECTION LOCATED 5 O'CLOCK POSITION ENGINE 1. CORRECTIVE ACTION: REPAIRED SUPPORT BRACKET COMBUSTION SECTION LOCATED 5 O'CLOCK POSITION ENGINE 1, AS PER ERA 564620-14MA REV ORIGINAL SECTION 1.
- [SDR DALA2020092803189](https://openairdocs.org/sdr/DALA2020092803189.md): Engine · failed · Sep 25, 2020 · N320NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > ATB/DE DECLARED EMERGENCY AND PERFORMED ATB DUE TO NUMBER 1 ENGINE FAILURE. A/C RETURNED WITH OUT FURTHER INCIDENT. MAINTENANCE FOUND DEBRIS IN THE TAILPIPE AND THE ENGINE WILL NOT TURN. CORRECTIVE ACTION: FOUND LEFT ENGINE TURBINE AND TAIL CONE DAMAGE WIT
- [SDR DALA2020010300041](https://openairdocs.org/sdr/DALA2020010300041.md): Housing · leaking · Jan 3, 2020 · N322NB · Airbus A319114 · Turbine Engine Accessory Drive
  > SHIP 3122 - DIV - TO JFK DUE NUMBER 2 ENGINE OIL QUANTITY INDICATING 2 QTS, WITH NO ENGINE PERFORMANCE ISSUES. CORRECTIVE ACTION: MAINTENANCE FOUND OIL LEAKING FROM RADIAL DRIVE SHAFT HOUSING. ENGINE REPLACEMENT IN PROGRESS.
- [SDR DALA2019122007473](https://openairdocs.org/sdr/DALA2019122007473.md): Skin · cracked · Dec 19, 2019 · N346NB · Airbus A319114 · Nacelle/Pylon, Plate/Skin
  > CRACK INTERNAL SKIN INBOARD FAN COWL AFT AREA ON ENGINE 1 LOG-PAGE UPDATED. REPLACED FAN COWL ENG #1 I/B P/N 238-0302-513 S/N CU102 SERVICEABLE CONDITION THE INSTALLATION IS TO BE ACCOMPLISHED ON AMDS CARD 7832-2010-1R.

Next page: https://openairdocs.org/engine/cfm-international-cfm56-5a5-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 = 'CFM565A5'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/cfm-international-cfm56-5a5-series/reports

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