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

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

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 109 reports

- [SDR DALA2015032502377](https://openairdocs.org/sdr/DALA2015032502377.md): Profile · cracked · Mar 24, 2015 · N345NW · Airbus A320212 · Emergency Exits
  > DURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR RT LOAD TRANSMITTING PROFILE LOCATED EXIT HATCHES 843 IN PASSENGER CABIN. ATTACH THE FORM 5100-3201, SSI 522102-01-1. REPLACED LOAD TRANSMITTING PROFILE LOCATED EXIT HATCHES 843 EMERGENCY EXIT DOOR AS IAW
- [SDR CA140627005](https://openairdocs.org/sdr/CA140627005.md): Mechanism · mismanufactured · Jun 20, 2014 · Airbus A319114 · Emergency Equipment
  > (CAN) GIRT BAR TRIGGER POSITION REF F, TRIGGER DEVIATIONS FROM DWG REF G, SB A320-53-1289, REF H, GIRT BAR ATTACHMENT FITTING CONFIGURATION REF I, GIRT BAR EXPLODED VIEW THE GIRT BARS INSTALLED ON OVERWATER ACFT ARE DESIGNED TO BE RETRACTABLE, ENSURING THE PR
- [SDR CA140611004](https://openairdocs.org/sdr/CA140611004.md): Smoke Detector · failed · Jun 11, 2014 · Airbus A319114 · Smoke Detection
  > (CAN) FLIGHT REPORTED AN "AVIONICS SMOKE ECAM" MESSAGE WITH SMOKE NOT VISUALLY CONFIRMED AND COULD NOT DETERMINE IF WARNING WAS VALID. CREW ELECTED TO DO A PRECAUTIONARY DIVERSION TO THE CLOSEST AIRPORT AND LANDED WITHOUT FURTHER INCIDENT. AVIONICS SMOKE FAU
- [SDR SOKF20140114001](https://openairdocs.org/sdr/SOKF20140114001.md): Interface Unit · faulty · Jan 13, 2014 · N991TA · Airbus A319112 · Landing Gear Retraction/Extension System
  > DURING TAKEOFF AT MROC THE LG DID NOT RETRACT & LG DOORS DID NOT CLOSE CORRECTLY. LG LGCIU 1 FAULT & LG SYS DISAGREE APPEARED ON ECAM. R & R LGCIU IAW AMM 32-41-71. PERFORMED TEST IAW AMM 32-69-00-740-001 OK NORMAL. THE AIRCRAFT RETURNED TO NORMAL OPERATIO
- [SDR CA111019014](https://openairdocs.org/sdr/CA111019014.md): B-Nut · failed · Oct 14, 2011 · Airbus A319114 · Hydraulic System, Main
  > (CAN) CREW ADVISED FLIGHT DISPATCH THAT THEY HAD A "YELLOW HYDRAULIC" FAILURE AND REQUIRED A PATCH TO MOC. PATCH WAS COMPLETED, FLIGHT CONTINUED, ATC WAS ADVISED AND TRUCKS WERE CALLED OUT AS A PRECAUTION. FOUND NR 2 ENGINE HYD PRESSURE LINE B-NUT LEAKING PR
- [SDR CA110926002](https://openairdocs.org/sdr/CA110926002.md): Computer · failed · Sep 24, 2011 · Airbus A319114 · Smoke Detection
  > (CAN) AFTER TAKEOFF CREW RECEIVED SMOKE INIDICATION IN AVIONICS BAY. FLIGHT DECLARED EMERGENCY RETURNED AND LANDED OVERWEIGHT. NO SMOKE OR ODOR FOUND DURING INVESTIGATION. ECAM 26-00 AVIONICS SMOKE WITH CFDS NO AEVC DATA AT 1215 GMT INDICATED, NO FAULT ON E
- [SDR CA110725001](https://openairdocs.org/sdr/CA110725001.md): Adiru · failed · Jul 22, 2011 · Airbus A319114 · Attitude and Direction Data System
  > ACFT WAS DISPATCHED WITH NR 3 ADR INOPERATIVE. AFTER DEPARTURE IN THE CLIMB, THE FLIGHT EXPERIENCED A FAILURE OF THE NR1 ADR AND ELECTED TO RETURN. NO EMERGENCY WAS DECLARED. THERE WAS NO ADVERSE PASSENGER REACTION OBSERVED REPLACED ADIRU 1 IAW AMM TASK 34-
- [SDR DALA1100083131](https://openairdocs.org/sdr/DALA1100083131.md): Wire · shorted · Jan 1, 2011 · N331NB · Airbus A319114 · Light System Wiring
  > DURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT SEAT 2A INOPERATIVE. MX RECONNECTED SHORTED WIRE AT SEAT AND PERFORMED FUNCTIONAL CHECK. CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.
- [SDR CA110104001](https://openairdocs.org/sdr/CA110104001.md): Idg · failed · Jan 1, 2011 · Airbus A319114 · AC Generation System
  > DURING CRUISE ELECTRICAL TRANSIENT OCCURRED CAUSING LOSS OF FAC NR 1, ALL DISPLAYS EXCEPT F/O PFD WAS LOST FOR ABOUT 5 SECONDS. TSM 24-20-00-810-806/814 CARRIED OUT, NO FAULT FOUND. REPLACED IDG AS PER AMM 24-21-51-400-040.
- [SDR DALAFAR145SDR104](https://openairdocs.org/sdr/DALAFAR145SDR104.md): Nut · missing · Nov 19, 2010 · Airbus A318111 · Turbine Engine Compressor Section
  > UPON DISASSEMBLY OF THE ROTOR STACK, SHOP NOTICED 48 NUTS OUT OF 60 MISSING FROM THE STACK WHICH HOLDS THE LLPS TOGETHER. THE LLPS AND HARDWARE INVOLVED ARE AS FOLLOWS: 1-2 SPOOL PN 1558M31G07, SN GWNOEW92, STAGE 3 HPC DISK PN 2116M23P01, SN XALG9478, 4-9 SPO
- [SDR F3LA2010110800535](https://openairdocs.org/sdr/F3LA2010110800535.md): Thermostat · defective · Nov 3, 2010 · N945FR · Airbus A319112 · Cabin Temperature Control System
  > LOST BLEED NR1 AT 36,000 CAUSING CABIN PRESSURE EXCESS CABIN ALTITUDE. EMERGENCY WAS DECLARE AND DECENTED TO 10,000. FOUND THERMOSTAT DEFECTIVE, R & R THE THERMOSTAT IAW AMM 36-11-43-PB401. OPS CHECK GOOD.
- [SDR DALA1026593120](https://openairdocs.org/sdr/DALA1026593120.md): Light · inoperative · Oct 13, 2010 · N320NB · Airbus A319114 · Emergency Lighting
  > DURING A NON-ROUTINE CHECK, FOUND 1B EMERGENCY LIGHT INOPERATIVE. MAINT REPLACED 2 EMERGENCY LIGHT ASSY AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.
- [SDR DALA1025953124](https://openairdocs.org/sdr/DALA1025953124.md): Solenoid · failed · Oct 7, 2010 · N324NB · Airbus A319114 · Passenger Oxygen System
  > DURING A NON ROUTINE CHECK, THE OXYGEN CONTAINER FAILED A DROP TEST AT ROW 4 LT. MX REPLACED SOLENOID IN OXYGEN CONTAINER AND FUNCTIONAL TEST WAS NORMAL.
- [SDR CA101004008](https://openairdocs.org/sdr/CA101004008.md): Seal · damaged · Oct 4, 2010 · Airbus A319114 · Cargo/Baggage Doors
  > ON DEPARTURE CREW RECOGNIZED A HIGH RATE OF CLIMB IN CABIN PRESSURIZATION. CREW STOPPED THE CLIMB AND DESCENDED TO FL150 FOR DURATION OF FLIGHT. CABIN PRESSURE CONTROLLER NR 1 REPLACED AND TESTED IAW AMM 21-31-34 PB401. OUTFLOW VALVE WAS ALSO REPLACED (PN 90
- [SDR CA101004004](https://openairdocs.org/sdr/CA101004004.md): Valve · failed · Oct 2, 2010 · Airbus A319114 · Hydraulic System, Main
  > AFTER TAKEOFF POWER WAS APPLIED THE CREW REJECTED TAKEOFF DUE TO A LOSS OF THE YELLOW HYD SYS PRESSURE. THE ACFT RETURNED TO THE GATE. EMERG BRAKE DUAL DISTRIBUTION VALVE REPLACED IAW AMM 32-43-14-400 CHECKS SERV.
- [SDR DALA1024923129](https://openairdocs.org/sdr/DALA1024923129.md): Floor Panel · damaged · Sep 30, 2010 · N329NB · Airbus A319114 · Fuselage Floor Panel
  > DURING L-CHECK FOUND DAMAGE TO AFT CARGO FLOOR PANEL 151 ZG. REPLACED FLOOR PANEL IAW DWG 3025-40532 & AMM 53-42-14, PAGE 401.
- [SDR CA101001002](https://openairdocs.org/sdr/CA101001002.md): Compressor · failed · Sep 30, 2010 · Airbus A320* · Potable Water System
  > LAVATORY-E WAS REPORTED TO HAVE WATER CONTINUOUSLY RUNNING FROM THE SINK FAUCET. THE WATER COMPRESSOR C/B WAS PULLED FROM THE AFT GALLEY CEILING PANEL 2001VU. A QUICK INSP OF THE WATER COMPRESSOR WAS ALSO CARRIED OUT, AND EXTENSIVE DAMAGE WAS FOUND ON THE COM
- [SDR CA100929003](https://openairdocs.org/sdr/CA100929003.md): Check Valve · failed · Sep 28, 2010 · Airbus A319114 · Hydraulic System, Main
  > SHORTLY AFTER TAKEOFF, THE CREW REPORTED A YELLOW HYD SYS OVERHEAT AND AFTER DISCUSSION WITH MX AND SOC IT WAS DECIDED TO RETURN THE ACFT TO AIRPORT OF DEPARTURE.
- [SDR DALA1022693101](https://openairdocs.org/sdr/DALA1022693101.md): Skin · damaged · Sep 14, 2010 · N301NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > DURING M-CHECK FOUND R2 DOOR LOWER CUT OUT EXTERNAL SKIN HAD 8 EA ELONGATED HOLES. REPAIRED IAW SRM 51-90-00, SRM 51-10-01, SRM 51-10-08 & ERA 484908-14.
- [SDR DALA1022703102](https://openairdocs.org/sdr/DALA1022703102.md): Skin · dented · Sep 14, 2010 · N302NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > DURING M-CHECK FOUND DENT ON FUSELAGE SKIN BETWEEN FRAMES 24-25 STRINGER 42R TO STRINGER 41R. REPAIRED IAW SRM 53-21-11, SRM 51-75-15 & SRM 51-42-11. REPAIR MUST BE INSPECTED AT 60,000 FLIGHT CYCLES IAW SRI 53-21-11.
- [SDR DALA1022493131](https://openairdocs.org/sdr/DALA1022493131.md): Wire · damaged · Sep 12, 2010 · N331NB · Airbus A319114 · Light System Wiring
  > DURING A NON ROUTINE CHECK, FOUND EMERGENCY SEAT LIGHT AT ROW 12L AND 20L INOPERATIVE. MX REPAIRED WIRING AT SEAT ROW 12L AND 20L. FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.
- [SDR DALA1022503135](https://openairdocs.org/sdr/DALA1022503135.md): Connector · inoperative · Sep 12, 2010 · N335NB · Airbus A319113 · Light System Wiring
  > DURING A NON ROUTINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHT AT ROW 7C INOPERATIVE. MX INSTALLED NEW CONNECTOR AT SEAT HARNESS. FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.
- [SDR DALA1022103102](https://openairdocs.org/sdr/DALA1022103102.md): Door Frame · corroded · Sep 11, 2010 · N302NB · Airbus A319114 · Fuselage Main, Structure
  > DURING M-CHECK FOUND CORROSION ON DOOR R1 DOOR FRAME 20 AT CABIN FLOOR LINE. REPAIRED IAW NTM 51-10-08, NTM 51-10-02. INDENTIFIED REPAIR AS ENGINEERING APPROVED TIME LIMITED REPAIR IAW ERA 484247-14 SECTION I. INSP TO BE ACCOMPLISHED EVERY 500 FLIGHT CYCLES
- [SDR DALA1022093101](https://openairdocs.org/sdr/DALA1022093101.md): Door Frame · corroded · Sep 10, 2010 · N301NB · Airbus A319114 · Fuselage Main, Structure
  > DURING M-CHECK FOUND CORROSION ON DOOR R1 DOOR FRAME 20 AT CABIN FLOOR LINE. REPAIRED IAW NTM 51-10-08, NTM 51-10-02. INDENTIFIED REPAIR AS ENGINEERING APPROVED TIME LIMITED REPAIR IAW ERA 484247-14, SECTION I. INSP TO BE ACCOMPLISHED EVERY 500 FLIGHT CYCLES
- [SDR DALA1022123102](https://openairdocs.org/sdr/DALA1022123102.md): Floorbeam · corroded · Sep 10, 2010 · N302NB · Airbus A319114 · Fuselage Main, Floor Beam
  > DURING M-CHECK FOUND CORROSION ON CABIN FLOORBEAM AT +Y1292 FR68. REPAIRED IAW SRM 51-42-11, SRM 51-44-11.
- [SDR DALA1021953102](https://openairdocs.org/sdr/DALA1021953102.md): Floor Panel · delaminated · Sep 9, 2010 · N302NB · Airbus A319114 · Fuselage Floor Panel
  > DURING M-CHECK FOUND CARGO FLOOR PANEL 131AF IS DELAMINATED. REPLACED FLOOR PANEL 161PF IAW DWG 3D25-40532.
- [SDR DALA1021963101](https://openairdocs.org/sdr/DALA1021963101.md): Mount · gouged · Sep 9, 2010 · N301NB · Airbus A319114 · Engine Mount Section
  > DURING M-CHECK FOUND GOUGE IN NR 1 PYLON AFT ENGINE MOUNT INBD SIDE ADJACENT TO SAFETY WIRE HOLE FOR AFT MOUNT BOLT. REPAIRED IAW ERA 484227-14 SECTION I, SECTION II REQUIRES APPROVAL OF REPAIR WITHIN 6 MONTHS.
- [SDR DALA1021973101](https://openairdocs.org/sdr/DALA1021973101.md): Mount · gouged · Sep 9, 2010 · N301NB · Airbus A319114 · Engine Mount Section
  > DURING M-CHECK FOUND GOUGES IN NR 1 PYLON ENGINE MOUNT OTBD SIDE ADJACENT TO SAFETY WIRE HOLE FOR AFT MOUNT BOLT. REPAIRED IAW ERA 484227-14 SECTION I, SECTION II REQUIRES APPROVAL OF REPAIR WITHIN 6 MONTHS.
- [SDR DALA1021743101](https://openairdocs.org/sdr/DALA1021743101.md): Floor Support · corroded · Sep 8, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > DURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT -Y1292 BETWEEN FR 67 & FR 68. REPAIRED IAW SRM 51-44-11, SRM 51-42-11 & TRM 53-21-01.
- [SDR DALA1021753101](https://openairdocs.org/sdr/DALA1021753101.md): Floor Support · corroded · Sep 8, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > DURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT AT Y1292 BETWEEN FR 66- FR 68. REPAIRED IAW SRM 51-44-11, SRM 51-42-11 & TRM 53-21-01.
- [SDR DALA1021723101](https://openairdocs.org/sdr/DALA1021723101.md): Sill · corroded · Sep 8, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > DURING M-CHECK FOUND CORROSION ON AFT RT AFT DOOR SILL. REPAIRED IAW SRM 51-44-11, SRM 51-42-11.
- [SDR DALA1021763121](https://openairdocs.org/sdr/DALA1021763121.md): Seat Track · damaged · Sep 8, 2010 · N321NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > DURING LINE CHECK FOUND SEAT TRACK DAMAGE AT BS Y1292. REPAIRED IAW SRM 53-00-15 FIG 201.
- [SDR CA100913009](https://openairdocs.org/sdr/CA100913009.md): Windshield · cracked · Sep 7, 2010 · Airbus A319114 · Flight Compartment Windows
  > LT WINDSHIELD CRACKED IN CRUISE - STARTED IN LOWER LT CORNER. ACFT DIVERTED, WINDSHIELD REPLACED. REFER ETQ SAFETY REPORT NR 12134. STRIP REPORT REQUESTED.
- [SDR DALA1021033210](https://openairdocs.org/sdr/DALA1021033210.md): Floorboard · damaged · Sep 2, 2010 · N310NW · Airbus A320211 · Fuselage Floor Panel
  > FOUND FWD CARGO FLOORBOARDS DAMAGED BEYOND SRM LIMITS. R & R CARGO FLOORBOARDS 131AE AND 131EG IAW AMM 53-22-14.
- [SDR DALA1021053102](https://openairdocs.org/sdr/DALA1021053102.md): Seat Track · corroded · Sep 1, 2010 · N302NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR LONGITUDINAL BEAM AT FR66 -Y765 HAS CORROSION. LOG PAGE NR 0264321. REMOVED SEAT TRACK -Y765 BETWEEN FR 66 TO 64. (NOT FR66 TO 68)
- [SDR DALA1020983102](https://openairdocs.org/sdr/DALA1020983102.md): Floor Support · corroded · Sep 1, 2010 · N302NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CABIN FLOOR LONGITUDINAL BEAM AT FR66 -Y765 HAS CORROSION. REMOVED SEAT TRACK -Y765 BETWEEN FR 66 TO 64. (NOT FR66 TO 68).
- [SDR DALA1020923101](https://openairdocs.org/sdr/DALA1020923101.md): Floor Support · corroded · Aug 30, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > AFT CABIN UTILITY AREA BETWEEN FR66 & FR68 FLOOR SUPPORT Y+1292 HAS CORROSION. CHECKED LIMITS AT BLENDED OUT AREA, DIMENSIONS L=2.100" W=1.100" D=0.055" ORIG MAT THICKNESS 0.157 FOUND TO BE OUT OF LIMITS IAW SRM TRM 53-41-15 FIG 1. REMOVED, LOCATED, AND DRILLE
- [SDR DALA1020933101](https://openairdocs.org/sdr/DALA1020933101.md): Floor Support · corroded · Aug 30, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > AFT CABIN UTILITY AREA BETWEEN FR68 & FR69 FLOOR SUPPORT Y+1292 HAS CORROSION. CHECKED LIMITS AT BLENDED OUT AREA, DIMENSIONS L=1.500" W=1.300" D=0.075" ORIG MAT THICKNESS 0.157" FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15 FIG 1. LOCATED AND DRILLED FLOOR SUPPO
- [SDR DALA1020943101](https://openairdocs.org/sdr/DALA1020943101.md): Seat Track · corroded · Aug 30, 2010 · N301NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CABIN UTILITY AREA FR66 SEAT TRACK Y+1292 HAS CORROSION. CHECKED LIMITS AT BLENDED OUT AREA, DIMENSIONS L=1.740" W=1.360" D=0.070" ORIG MAT THICKNESS 0.157 FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15 FIG 1. LOCATED & DRILLED IAW SRM 51-44-11. INSTALLED SEAT
- [SDR DALA1020913101](https://openairdocs.org/sdr/DALA1020913101.md): Seat Track · corroded · Aug 29, 2010 · N301NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN, FR16 TO FR20, SEAT TRACK -Y254 CORRODED AT 2 AREAS. BLENDED OUT CORROSION AREA IAW SRM 51-74-00 FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15. REMOVED DAMAGED SEAT TRACK & BRACKETS (12) IAW SRM 51-42-11. LOCATED, DRILLED, AND INSTALLED NEW BEAM, BRA
- [SDR DALA1020883101](https://openairdocs.org/sdr/DALA1020883101.md): Seat Track · corroded · Aug 28, 2010 · N301NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN, FR20 DUMMY RAIL AT -Y189 CORRODED THRU T-CHORD OF SEAT TRACK. REMOVED DUMMY RAIL AT FR20 Y-189 IAW SRM 51-42-11 REMOVED CORROSION IAW SRM 51-74-00 BLENDED THE AREA L=2" W=1.5" D=.015 FOUND TO BE OUT OF LIMITS IAW SRM 53-41-15 INSTALLED NEW FWD CABIN
- [SDR DALA1020893101](https://openairdocs.org/sdr/DALA1020893101.md): Floor Support · corroded · Aug 28, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > AFT CABIN UTILITY AREA BETWEEN FR 66 & FR 70 FLOOR SUPPORT Y-765 HAS CORROSION. BLENDED OUT CORRODED AREA IAW SRM 51-74-00 DIMENSION L=1.900" W=1.020" D=.065" MAX ALLOWEDD=.027 ORIGINAL MATL.THICKNESS.157 FOUND TO BE OUT OF LIMITS IAW SRM TRM 53-41-15 FIG I.
- [SDR DALA1020903102](https://openairdocs.org/sdr/DALA1020903102.md): Floor Support · corroded · Aug 28, 2010 · N302NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CABIN FLOOR LONGITUDINAL BEAM AT FR 66, Y512 HAS CORROSION. REMOVED DAMAGED FLOORBEAM AT FR 66, Y512 DAMAGED AREA DIM ARE W=0.50" D=0.24" L=1.5" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. INSTALLED NEW FLOORBEAM IAW SRM 51-42-11 & PAINTED IAW SRM 51-75-12.
- [SDR DALA1020453101](https://openairdocs.org/sdr/DALA1020453101.md): Floor Support · corroded · Aug 25, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > DURING M-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT BS +Y765 BETWEEN FR 66 & FR 69. REPAIRED IAW SRM 51-42-11, 51-44-11.
- [SDR DALA1019253114](https://openairdocs.org/sdr/DALA1019253114.md): Wire · damaged · Aug 11, 2010 · N314NB · Airbus A319114 · Light System Wiring
  > DURING A NON-ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 11 INOP. REPAIRED WIRE AND PERFORMED FUNCTIONAL CHECK. CHECK WAS NORMAL AND ACFT RETURNED TO SERVICE.
- [SDR CA100819011](https://openairdocs.org/sdr/CA100819011.md): Safety Valve · shorted · Aug 10, 2010 · Airbus A319114 · Landing Gear Retraction/Extension System
  > A SHORT IN THE LANDING GEAR HYD SAFETY VALVE CAUSED THE TRIPPING OR CIRCUIT BREAKERS LGCIU SYS 1 AND LGCIU SYS 1 GRD SUP. THE FAILURE CONDITION OF THE LANDING GEAR SAFETY VALVE CAUSING THE TRIPPING OF THE CIRCUIT BREAKERS AUTOMATICALLY FORCED THE ACFT INTO TH
- [SDR CA100804025](https://openairdocs.org/sdr/CA100804025.md): Window · failed · Jul 23, 2010 · Airbus A319111 · Flight Compartment Windows
  > IN CRUISE, CAPT`S REAR FIXED WINDOW SHATTERED. THE CREW FOLLOWED THE QRH AND DESCENDED TO FL230 JUST PRIOR TO TOD. ATC WAS ADVISED, NO EMERGENCY WAS DECLARED.
- [SDR DALA1012253123](https://openairdocs.org/sdr/DALA1012253123.md): Battery Pack · inoperative · Jun 5, 2010 · N323NB · Airbus A319114 · Emergency Lighting
  > DURING A NON ROUTINE CHECK, EMERGENCY LIGHT ON FAP MESSAGE EPSU LOAD FAIL AT FWD LT. REPLACED BATTERY PACK AND FUNCTIONAL TEST WAS NORMAL. ACFT RETURNED TO SERVICE.
- [SDR DALA1010293102](https://openairdocs.org/sdr/DALA1010293102.md): Wire Harness · inoperative · May 17, 2010 · N302NB · Airbus A319114 · Light System Wiring
  > DURING A NON ROUTINE CHECK, MX FOUND SEAT 5C EMERGENCY LIGHT INOPERATIVE. FOUND WIRE PULLED FROM INBD CONNECTOR OF HARNESS. REPLACED HARNESS AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.
- [SDR DALA109573152](https://openairdocs.org/sdr/DALA109573152.md): Wire · damaged · May 8, 2010 · N352NB · Airbus A319114 · Light System Wiring
  > DURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 5C INOPERATIVE. MX REPAIRED WIRE AND OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.

Next page: https://openairdocs.org/engine/cfm-international-cfm56-5a-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 = 'CFM565A'
ORDER BY difficulty_date DESC
```

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

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