CFM International CFM56-5A series

Service difficulty reports · 109

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Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DALA2015032502377Profile · crackedDURING 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 Mar 24, 2015 · N345NW · Airbus A320212 · Emergency ExitsSDR CA140627005Mechanism · mismanufactured(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 PRJun 20, 2014 · Airbus A319114 · Emergency EquipmentSDR CA140611004Smoke Detector · failed(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 FAUJun 11, 2014 · Airbus A319114 · Smoke DetectionSDR SOKF20140114001Interface Unit · faultyDURING 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 OPERATIOJan 13, 2014 · N991TA · Airbus A319112 · Landing Gear Retraction/Extension SystemSDR CA111019014B-Nut · failed(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 PROct 14, 2011 · Airbus A319114 · Hydraulic System, MainSDR CA110926002Computer · failed(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 ESep 24, 2011 · Airbus A319114 · Smoke DetectionSDR CA110725001Adiru · failedACFT 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-Jul 22, 2011 · Airbus A319114 · Attitude and Direction Data SystemSDR DALA1100083131Wire · shortedDURING 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.Jan 1, 2011 · N331NB · Airbus A319114 · Light System WiringSDR CA110104001Idg · failedDURING 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.Jan 1, 2011 · Airbus A319114 · AC Generation SystemSDR DALAFAR145SDR104Nut · missingUPON 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 SPONov 19, 2010 · Airbus A318111 · Turbine Engine Compressor SectionSDR F3LA2010110800535Thermostat · defectiveLOST 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.Nov 3, 2010 · N945FR · Airbus A319112 · Cabin Temperature Control SystemSDR DALA1026593120Light · inoperativeDURING A NON-ROUTINE CHECK, FOUND 1B EMERGENCY LIGHT INOPERATIVE. MAINT REPLACED 2 EMERGENCY LIGHT ASSY AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.Oct 13, 2010 · N320NB · Airbus A319114 · Emergency LightingSDR DALA1025953124Solenoid · failedDURING 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.Oct 7, 2010 · N324NB · Airbus A319114 · Passenger Oxygen SystemSDR CA101004008Seal · damagedON 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 90Oct 4, 2010 · Airbus A319114 · Cargo/Baggage DoorsSDR CA101004004Valve · failedAFTER 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.Oct 2, 2010 · Airbus A319114 · Hydraulic System, MainSDR DALA1024923129Floor Panel · damagedDURING L-CHECK FOUND DAMAGE TO AFT CARGO FLOOR PANEL 151 ZG. REPLACED FLOOR PANEL IAW DWG 3025-40532 & AMM 53-42-14, PAGE 401.Sep 30, 2010 · N329NB · Airbus A319114 · Fuselage Floor PanelSDR CA101001002Compressor · failedLAVATORY-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 COMSep 30, 2010 · Airbus A320* · Potable Water SystemSDR CA100929003Check Valve · failedSHORTLY 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.Sep 28, 2010 · Airbus A319114 · Hydraulic System, MainSDR DALA1022693101Skin · damagedDURING 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.Sep 14, 2010 · N301NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA1022703102Skin · dentedDURING 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.Sep 14, 2010 · N302NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA1022493131Wire · damagedDURING 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.Sep 12, 2010 · N331NB · Airbus A319114 · Light System WiringSDR DALA1022503135Connector · inoperativeDURING 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.Sep 12, 2010 · N335NB · Airbus A319113 · Light System WiringSDR DALA1022103102Door Frame · corrodedDURING 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 Sep 11, 2010 · N302NB · Airbus A319114 · Fuselage Main, StructureSDR DALA1022093101Door Frame · corrodedDURING 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 CYCLESSep 10, 2010 · N301NB · Airbus A319114 · Fuselage Main, StructureSDR DALA1022123102Floorbeam · corrodedDURING M-CHECK FOUND CORROSION ON CABIN FLOORBEAM AT +Y1292 FR68. REPAIRED IAW SRM 51-42-11, SRM 51-44-11.Sep 10, 2010 · N302NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA1021953102Floor Panel · delaminatedDURING M-CHECK FOUND CARGO FLOOR PANEL 131AF IS DELAMINATED. REPLACED FLOOR PANEL 161PF IAW DWG 3D25-40532.Sep 9, 2010 · N302NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1021963101Mount · gougedDURING 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.Sep 9, 2010 · N301NB · Airbus A319114 · Engine Mount SectionSDR DALA1021973101Mount · gougedDURING 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.Sep 9, 2010 · N301NB · Airbus A319114 · Engine Mount SectionSDR DALA1021743101Floor Support · corrodedDURING 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.Sep 8, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1021753101Floor Support · corrodedDURING 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.Sep 8, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1021723101Sill · corrodedDURING M-CHECK FOUND CORROSION ON AFT RT AFT DOOR SILL. REPAIRED IAW SRM 51-44-11, SRM 51-42-11.Sep 8, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1021763121Seat Track · damagedDURING LINE CHECK FOUND SEAT TRACK DAMAGE AT BS Y1292. REPAIRED IAW SRM 53-00-15 FIG 201.Sep 8, 2010 · N321NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR CA100913009Windshield · crackedLT WINDSHIELD CRACKED IN CRUISE - STARTED IN LOWER LT CORNER. ACFT DIVERTED, WINDSHIELD REPLACED. REFER ETQ SAFETY REPORT NR 12134. STRIP REPORT REQUESTED.Sep 7, 2010 · Airbus A319114 · Flight Compartment WindowsSDR DALA1021033210Floorboard · damagedFOUND FWD CARGO FLOORBOARDS DAMAGED BEYOND SRM LIMITS. R & R CARGO FLOORBOARDS 131AE AND 131EG IAW AMM 53-22-14.Sep 2, 2010 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA1021053102Seat Track · corrodedCABIN 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)Sep 1, 2010 · N302NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1020983102Floor Support · corrodedCABIN FLOOR LONGITUDINAL BEAM AT FR66 -Y765 HAS CORROSION. REMOVED SEAT TRACK -Y765 BETWEEN FR 66 TO 64. (NOT FR66 TO 68).Sep 1, 2010 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1020923101Floor Support · corrodedAFT 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 DRILLEAug 30, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1020933101Floor Support · corrodedAFT 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 SUPPOAug 30, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1020943101Seat Track · corrodedAFT 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 SEATAug 30, 2010 · N301NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1020913101Seat Track · corrodedFWD 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, BRAAug 29, 2010 · N301NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1020883101Seat Track · corrodedFWD 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 CABINAug 28, 2010 · N301NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1020893101Floor Support · corrodedAFT 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. Aug 28, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1020903102Floor Support · corrodedCABIN 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.Aug 28, 2010 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1020453101Floor Support · corrodedDURING M-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT BS +Y765 BETWEEN FR 66 & FR 69. REPAIRED IAW SRM 51-42-11, 51-44-11.Aug 25, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1019253114Wire · damagedDURING 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.Aug 11, 2010 · N314NB · Airbus A319114 · Light System WiringSDR CA100819011Safety Valve · shortedA 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 THAug 10, 2010 · Airbus A319114 · Landing Gear Retraction/Extension SystemSDR CA100804025Window · failedIN 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.Jul 23, 2010 · Airbus A319111 · Flight Compartment WindowsSDR DALA1012253123Battery Pack · inoperativeDURING 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.Jun 5, 2010 · N323NB · Airbus A319114 · Emergency LightingSDR DALA1010293102Wire Harness · inoperativeDURING 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.May 17, 2010 · N302NB · Airbus A319114 · Light System WiringSDR DALA109573152Wire · damagedDURING 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.May 8, 2010 · N352NB · Airbus A319114 · Light System Wiring
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