CFM International CFM56-5B8/P series
Service difficulty reports · 67
Newest first. General aviation reporting is voluntary.
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 = 'CFM565B8P' 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.
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 = 'CFM565B8P' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ANCF2016011202Engine · bird ingestionDURING TAKEOFF RNWY 34, SKCC ENG NR 2 HAD THE STRIKE, N1 INCREASED UP TO 4,7 VIB WHILE N2 VIB REMAINED UNCHANGED. PARAMETERS WERE LOOKED IN QRH PAGE 70,09A & NOT EXCEED THOSE VLVS. IAW AMM 05-51-19-200-601A INSPECTION OF THE ENG AFTER A BIRD STRIKE OR SLUSH SDR ANCF2015081101Engine · bird ingestionBIRD STRIKE ON ENG 2 DURING TAKEOFF. IAW AMM 72-21-00-210-009 GENERAL CONDITION OF THE FAN ROTOR BLADE ITEM 4-A-1-H WAS FOUND ROTOR BLADE NR 5 DEEP 4.54" & LARGE 101 MM BETWEEN LIMITS. IAW AMM 72-21-00-210-009 GENERAL CONDITION OF THE FAN ROTOR BLADE
ITEM 4SDR ANCF2015072601Hmu · malfunctionedDURING ENG 1 START, THE ENG 1 IGNITION B FAULT APPEARS ON ECAM. NEW START PROGRESS WAS PRESENTED WITH ING AB. THE ENG REACHED 50% N2 & REMAINED HUNG START. AT 3RD START APPEARS ENG STALL, THEN WAS PERFORMED ON MANUAL ENG START & APPEAR ENG 1 FAIL ALL PARAMESDR ANCF2015071301Starter · malfunctionedDURING ENG 1 START WHEN MASTER SWITCH TO NR N 2 MOVEMENT, BLEED PRESS NORMAL, START VLV OPEN. IAW AMM 80-11-10 PB 401 THE STARTER WAS REPLACED, O TEST WAS PERFORMED SATISFACTORY PN 3505582-27, SN OFF YG439040-H & SN ON Y6336238-AC.SDR ANCF2015021101Bleed Valve · faultyENGINE 1 COMPRESSOR ARE DISPLAY ON ECAM DESCENT, A STRONG NOISE ON ENG 1, STALL ON ECAM FOLLOWED BY ENG 1 STALL ON ECAM FOLLOWED BY ENG 1 COMPRESSOR VANE DURING THE REST. OF THE FLIGHT, WE HAD 2 COMPRESSOR STALL EVENTS. IAW AMM 75-31-50-000 400-A THE BLEED VSDR ANCF2013042900158Unknown · smokeDURING INITIAL CLIMB, ACCORDING TO THE F/A THERE WAS SMOKE WITH ELECTRICAL ODOR AND THE SAME CONDITION WAS REPORTED BY THE CABIN CREW AFTER ENGINE SHUTDOWN IAW AMM TASK 21-61-00-710-001A. THE OPS TEST OF PACKS 1 AND 2 WERE PERFORMED DURING TWENY FIVE MINUTES SDR F3LA2012020700705Engine · making metalABORTED TAKEOFF. UNUSUAL VIBRATION NOTED ON START OF NR 2 ENGINE DURING TAXI. NO ECAMS NOTED. ON APPLICATION OF TAKE OFF THRUST, A LOUD COMPRESSOR STALL, FLAMES NOTED BY TOWER FROM ENGINE REAR. ECAM FOR NR 2 OIL FILTER CLOGGED. IMMEDIATELY SECURED NR 2 ENSDR EE4Y20110002Skin · crackedENGINE NR 1 & NR 2, ENGINE PYLON, PRECOOLER FAIRING SKIN WITH CRACKS (ID ACCESS PANEL NR 413DL & NR 423DL). THE SKIN CRACKS REQUIRE A MAJOR REPAIR.SDR F3LA2010100600524Connector · misinstalledC-CHECK: NON ROUTINE N0033, EMERGENCY EXIT LIGHT AT ROW 13ABC INOP. FOUND CONNECTOR AT LIGHT ASSEMBLY TO BE INPROPERLY CONNECTED. RE-SEATED CONNECTOR IAW AIRBUS A318 AMM 33-51-19-400-003 SUBTASK 33-51-19-420-052 STEP A(1)(A)(B). OPS CHECK GOOD IAW AMM 33-51-00SDR F3LA2010100600525Fitting · gougedC-CHECK: NON ROUTINE N0124; FWD CARGO LOWER FWD CORNER SEALING SECTION FITTING GOUGED .1250 IN X .2500 IN X .040 INCH. R & R FWD LOWER SEALING SECTION FITTING IAW SRM 51-72-11, PAGE 1.SDR F3LA2010100600526Power Supply · no testC-CHECK: NON ROUTINE N0607; NUMEROUS EMERGENCY PATH LIGHTS INOP ON SEATS AND CEILING PANELS. PERFORMED OPS TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-059A. EMERGENCY POWER SUPPLY UNIT 10WL FAILED SYS TEST "BATT FAULT' LIGHT ILLUMINATED. R & R EPSU 10WL IAW SDR F3LA2010100600527Lens · crackedC-CHECK: NON ROUTINE N0610; EMERGENCY LIGHT ABOVE L-1 DOOR, THE LENS IS CRACKED. R & R EMERGENCY LIGHT ASSY IAW AMM 33-51-11-020-050B AND AMM 33-51-11-420-050A.SDR F3LA2010100600528Floor Panel · delaminatedC-CHECK: NON ROUTINE N0613; AFT CARGO FLOOR PANEL 161DF EDGE DELAMINATED AND EDGE FILLER DAMAGED 10 INCH. FABRICATED REPLACEDMENT FLOOR PANEL IAW MCG IRM 9701, REV G.SDR F3LA2010100600529Lens · crackedC-CHECK: NON ROUTINE N0616; L-1 ENTRY LOWER EXIT LIGHT, THE LENS IS ILLEGIBLE. R & R LENS ASSY ON L-1 DOOR LOWER EXIT LIGHT IAW AMM 33-51-13-400-001 PAGE 3 STEP A 3 AND AMM 33-51-13-020-050 STEP A(1)(A)(B).SDR F3LA2010090100490Bypass Valve · leakingAN EMERGENCY DECLARED WAS REPORTED BY THE PILOT. AIR TURN BACK, ECAS WARNING HYD GREEN ENG 1 PUMP LOW PRESSURE. FOUND NOSE GEAR DOOR BYPASS VALVE LEAKING. REPLACE NOSE GEAR DOOR BYPASS VALVE, REF AMM 32-31-15, PAGE BLOCK 401. OPS CHECK AND LEAK NORMAL WITH NSDR F3LA2010040700379Line · wornREFERENCE LOG PAGE, NR 535350, ITEM 1. ECAM HYD YELLOW LOW LEVEL INDICATION. FOUND DAMAGED HYD LINE IN NR 2 ENG PYLON. REPLACED LINE REF AMM 29-13-49-000-049 AND 29-13-49-400-049.SDR F3LA2010031000364Panel · delaminatedREFFERENCE NON ROUTINE NR N0072. DURING C4 S1 C-CHECK INSP NOTED AFT CARGO TRANSITION PANEL 151CH DELAMINATED. MX R & R AFT CARGO TRANSITION PANEL 151CH IAW AMM 53-42-14-400-001.SDR F3LA2010030300354Strip · corrodedREF NON ROUTINE NR N0249. DURING C4 S1 C CHECK INSP NOTED CORROSION ON L1 DOOR ENTRYWAY STRIP. MX R & R STRIP IAW WC CP053-12.SDR F3LA2010030300355Strip · corrodedDURING C4 SI C-CHECK INSP NOTED CORROSION ON THE R1 DOOR ENTRY WAY STRIP. MX R & R STRIP IAW WC CP053-12.SDR F3LA2010030900361Floor Panel · delaminatedDURING C4 S1 C-CHECK INSP NOTED AFT CARGO COMPARTMENT FLOOR PANEL 151AH DELAMINATED. MX FABRICATED REPLACEMENT PANEL IAW AIM 9701.SDR F3LA200800559Shear Plate · corrodedDURING C-CHECK INSP, NOTED CORROSION AROUND NUT CLIP HOLE APPROX 4.25 INCHES AFT OF FWD END ON RT SIDE FLOORBEAM ALONG Y1292 BETWEEN FR68 AND FR69. MAINTENANCE BLENDED AREA, FABRICATED FLANGE BUSHING AND INSTALLED IAW THE REQUIREMENTS OF ENGINEERING AUTHORIZASDR F3LA200800554Floor Panel · corrodedDURING C3 C-CHECK, INSP NOTED FLOOR PANEL 261FF HAS CORROSION ON LOWER SURFACE. MAINT REMOVED AND REPLACED FLOOR PANEL 261FF WITH A NEW PANEL AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)SDR F3LA200800555Blanking Plate · corrodedDURING C-CHECK INSP, NOTED R2 FWD GIRT BAR BLANKING PLATE HAS CORROSION. MAINT REMOVED AND REPLACED BLANKING PLATE WITH NEW ONE FROM STOCK AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)SDR F3LA200800523Floor Panel · damagedLINE MAINT NOTED THE AFT CARGO COMPARTMENT FLOOR PANEL 151CH WAS DAMAGED. MAINT REPAIRED FLOOR PANEL 151CH IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)SDR F3LA200800522Floor Panel · damagedLINE MAINT NOTED THE AFT CARGO COMPARTMENT FLOOR PANEL 151DH WAS DAMAGED. MAINT REPAIRED FLOOR PANEL 151DH IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)SDR F3LA200800521Floor Panel · damagedLINE MAINT NOTED THE AFT CARGO COMPARTMENT TRANSITION PANEL 151FH WAS DAMAGED. MAINT REPAIRED TRANSITION PANEL 151FH IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)SDR F3LA200800441Girt Bar · out of adjustDURING CLIMB OUT THE L2 AND R2 DOOR DISARMED AT 8500 FT AND REARMED DURING DESCENT AT 10000 FT. MAINT ADJUSTED GIRT BAR FITTINGS ON THE L2 AND R2 DOORS AND OPS AND RIG CHECKED GOOD IAW AMM 52-11-00-820-001, AMM 25-62-44-400-006 AND AMM 05-53-00-780-003. UPON CSDR F3LA200800424Floor Panel · corrodedDURING C-CHECK INSP NOTED FLOOR PANEL 261FF HAS CORROSION ON SURFACE. MAINT REMOVED AND REPLACED FLOOR PANEL 261FF IAW AMM 53-42-12-400-002. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)SDR F3LA200800425Floor Panel · corrodedDURING C-CHECK INSP, FLOOR PANEL 262FF HAS CORROSION ON SURFACE. MAINT REMOVED AND REPLACED FLOOR PANEL 262FF IAW AMM 53-42-12-400-002. UPON COMPLETION OF THE REPAIR, INSPECTED AND FOUND ACCEPTABLE. (B)SDR F3LA200800426Shear Plate · corrodedDURING C-CHECK INSP, NOTED CORROSION AROUND FAR RT NUTCLIP HOLE ON SHEAR PLATE ALONG FRAME 68 BETWEEN Y765 AND Y1292. MAINT REMOVED, FABRICATED AND INSTALLED SERVICEABLE SHEAR PLATE AT FRAME 68 BETWEEN Y765 AND Y1292 IAW DRAWING O53670099, SRM 51-21-11, SRM 51SDR F3LA200800427Floorbeam · corrodedDURING C-CHECK INSP NOTED FLOORBEAM Y1292 LT HAS CORROSION AT FIRST, SECOND AND THIRD NUTCLIP HOLES. MAINT REMOVED AND REPLACED FLOORBEAM IAW SRM 51-72-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)SDR F3LA200800421Shear Plate · corrodedDURING C-CHECK INSP NOTED CORROSION AROUND FAR RT NUTCLIP HOLE ON SHEAR PLATE ALONG FRAME 68 BETWEEN Y765 AND Y1292. MAINT REMOVED SHEAR CONNECTING PLATE, FABRICATED AND INSTALLED SHEAR CONNECTING PLATE IAW DRAWING D53670099 AND SRM 51-42-11. UPON COMPLETION OSDR F3LA200800422Floorbeam · corrodedDURING C-CHECK INSP NOTED FLOORBEAM Y1292 HAS CORROSION AT FWD OB NUTCLIP HOLE AT FRAME 66 JUST AFT OF LT LAVATORY. MAINT BLENDED CORROSION AND OVERSIZED HOLE, FABRICATED FLANGE BUSHING AND TREATED PRIMED AND PAINTED IAW EA A8-53R-30435 AND SRM 51-75-12. UPON SDR F3LA200800423Floorbeam · corrodedDURING C-CHECK INSP NOTED FLOOR BEAM Y1292 HAS CORROSION AT NUTCLIP HOLE AT FRAME 68 OB SIDE JUST FWD OF GALLEY. MAINT BLENDED CORROSION AND OVERSIZED HOLE, INSTALLED FLANGE BUSHING TREATED PRIMED AND PAINTED IAW EA A8-53R-30435 AND SRM 51-75-12. UPON COMPLETISDR F3LA200800420Blanking Plate · corrodedDURING C-CHECK INSP, NOTED GIRT BAR BLANKING PLATE ON R2 DOOR AFT HAS CORROSION. MAINT REMOVED AND REPLACED R2 DOOR GIRT BAR BLANKING PLATES IAW WORK CARD C250001-03. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)SDR F3LA200800419Plate · corrodedDURING C-CHECK INSP NOTED GIRT BAR BLANKING PLATE L2 AFT HAS CORROSION. MAINT REMOVED AND REPLACED CORRODED L2 AFT GIRT BAR BLANKING PLATES IAW WORK CARD C250001-03. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)SDR F3LA200800415Panel · damagedDURING C-CHECK INSP NOTED FWD CARGO PIT TRANSITION PANEL 131BF IS DAMAGED. MAINT REPAIRED FWD CARGO PIT TRANSITION PANEL 131BF IAW SRM 53-02-00 PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)SDR F3LA200800414Panel · damagedREFERENCE NON ROUTINE C046424. DURING C-CHECK INSPECTION NOTED FWD CARGO PIT TRANSITION PANEL 132DG IS DAMAGED. MAINT REPAIRED FWD CARGO PIT TRANSITION PANEL 132DG IAW SRM 53-02-00 PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUSDR F3LA200800385Servo Control · inoperativeDURING TAXI OUT, THE FLIGHT CREW RECEIVED A NOSE WHEEL STEERING FAULT AND LOSS OF STEERING. MAINT REMOVED AND REPLACED NLG STEERING SERVO CONTROL VALVE IAW AMM 32-51-51 PAGE BREAK 401. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE AND OPSDR F3LA200800382Lamp · burned outDURING A HEAVY MAINT CHECK INSP, NOTED ROWS 3 AND 11 AFT MOUNTED LAMP OF EMERGENCY LIGHT MOUNTED SEATS INOP. MAINT REMOVED AND REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-19 PAGE BREAK 401. UPON COMPLETION OF THE MAINT IT WAS INSPECTED, FOUNDSDR F3LA200800344Floor Panel · damagedDURING HEAVY SERVICE CHECK INSP, NOTED AFT CARGO COMPARTMENT FLOOR PANEL 151DH WAS DAMAGED. MAINT COMPLETED PERMANENT REPAIR ON PANEL 151DH IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)SDR F3LA200800130Unknown · smokeDURING LANDING ROLL OUT, THE FLIGHT CREW REPORTED WHITE/GRAY SMOKE AND ACRID ODOR IN THE COCKPIT AND PASSENGER CABIN. MAINTENANCE PERFORMED IDLE LEAK CHECK OF BOTH ENGINES IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 71-00-00-710-006 AND PERFORMED A CHECK OF THSDR F3LA200800077Cooling Fan · bindingDURING CRUISE, AT 35000, FLT CREW REPORTED LOUD NOISE AND VIBRATION FOLLOWED BY ACRID ODOR AND SMOKE IN COCKPIT. ECAM DISPLAYED BLOWER AND EXTRACTOR FAN FAULT. FLIGHT CREW DECLARED AN EMERGENCY, DIVERTED TO OKC AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANSDR F3LA200800072Actuator · leakingDURING CLIMB, THROUGH 15000 FEET, THE FLIGHT CREW RECEIVED AN ECAM WARNING INDICATING THE GREEN SYSTEM HYDRAULIC QUANTITY WAS LOST. THE FLIGHT CREW PERFORMED AN AIR TURNBACK AND AFFECTED AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THESDR F3LA200800027Hinge Fitting · damagedDURING C CHECK INSPECTION, THE CENTER HINGE ANTI-ROTATION LUG FOR THE LEFT NUMBER 4 SPOILER WAS FOUND DAMAGED. MAINTENANCE REMOVED THE DAMAGED ASSEMBLY AND PERFORMED A "MAJOR REPAIR" ON ACCORDANCE WITH THE REQUIREMENTS OF EA A8-57R-12379. UPON COMPLETION OF SDR F3LA200800029Hinge Bracket · damagedDURING C CHECK INSPECTION, THE CENTER HINGE ANTI-ROTATION BRACKET FOR THE LEFT NUMBER 2 SPOILER WAS FOUND DAMAGED. MAINTENANCE REMOVED THE DAMAGED ASSEMBLY AND PERFORMED A "MAJOR REPAIR" IN ACCORDANCE WITH THE REQUIREMENTS OF EA A8-57R-12381. UPON COMPLETIONSDR F3LA200800026Hinge Fitting · damagedDURING C CHECK INSPECTION, THE CENTER HINGE ANTI-ROTATION LUG FOR THE RIGHT NUMBER 4 SPOILER ACTUATOR BOLT WAS FOUND DAMAGED. MAINTENANCE REMOVED THE DAMAGED ASSEMBLY AND PERFORMED A "MAJOR REPAIR" IN ACCORDANCE WITH THE REQUIREMENTS OF EA A8-57R-12379. UPONSDR F3LA200800028Hinge Fitting · damagedDURING C CHECK INSPECTION, THE CENTER HINGE ANTI-ROTATION LUG FOR THE RIGHT NUMBER 3 SPOILER WAS FOUND DAMAGED. MAINTENANCE REMOVED THE DAMAGED ASSEMBLY AND PERFORMED A "MAJOR REPAIR" IN ACCORDANCE WITH THE REQUIREMENTS OF EA A8-57R-12379. UPON COMPLETION OFSDR F3LA200800030Hinge Fitting · damagedDURING C CHECK INSPECTION, THE CENTER HINGE ANTI-ROTATION LUG FOR THE LEFT NUMBER 3 SPOILER WAS FOUND DAMAGED. MAINTENANCE REMOVED THE DAMAGED ASSEMBLY AND PERFORMED A "MAJOR REPAIR" IN ACCORDANCE WITH THE REQUIREMENTS OF EA A8-57R-12379. UPON COMPLETION OF SDR F3LA200800031Pressure Switch · inoperativeDURING C CHECK AND FUNCTIONAL TEST, THE ALTITUDE PRESSURE SWITCH FAILED ITS FUNCTIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE ALTITUDE PRESSURE SWITCH IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 35-23-15 PB 401. FOLLOWING ITS INSTALLATION AND INSPECTION,
Back to CFM International CFM56-5B8/P series