CFM International CFM56-5B5/P series
Service difficulty reports · 166
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 = 'CFM565B5P' 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 = 'CFM565B5P' 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 WX0A2024012631951Hmu · faultedENGINE 1 ROLLED BACK AT FL 370 IN CLEAR AIR AUTO IGNITION AND RE-LIGHT OCCURRED / PERFORMED TROUBLESHOOTING OF #1 ENGINE ROLLBACK IAW TSM 72-00-00-810-806-A. HMU FOUND BAD, REMOVED AND REPLACED PER IAW AMM 73-21-10-400-002, OPS AND LEAK CHECKS GOOD.SDR WX0A2020010373451Oil System · lowEMERGENCY DECLARED, NR 1 ENGINE LOW OIL QTY INDICATION. REMOVED & REPLACED THE NR 1 ENGINE.SDR F3LA201910240128Unknown · odorODOR EVENT AT CRUISE ALTITUDE STARTED SLIGHT AND GOT VERY STRONG ODOR. DID QRH PROCEDURE FOR ODOR IN FLIGHT, THIS DID NOT CHANGE INTENSITY OF ODOR. CORRECTIVE ACTION: PLACED ON TDI -T 1156114 FOR 60 A.C. DUE AT AC 9424 BY AUTHORITY EA# A0-21T-34386 (ENG #2 ISDR EE4Y2019040108585Inlet · crackedNR 1 ENGINE INLET COWL LIP SKIN AT 4 AND 12 O’CLOCK POSITION WITH TOOL MARKS AROUND FASTENERS HEAD.FOR CORRECTIVE ACTION SEE COOPESA NRI 4-86,ACTION TAKEN,PERFORMED PERMANENT REPAIR IAW COO-EO-2019-8117 R01 AND COLLINS AEROSPACE MESSAGE # CV19-01268 REV D.SDR F3LA2018041000321Mechanism · seizedDURING DESCENT AND RETARDING OF THROTTLES ENG-2 COMPRESSOR AND VANE ECAM APPEARED FOLLOWED BY COMPRESSOR STALL WHICH WAS FELT AND HEARD BY CREW. REMOVED AND REPLACED BLEED VALVE STOP MECHANISM REFERENCE AMM 75-31-20-400-002A. OPERATIONAL AND LEAK CHECK GOOD.SDR F3LA2018041000322Motor · seizedDURING DESCENT AND RETARDING OF THROTTLES ENG-2 COMPRESSOR AND VANE ECAM APPEARED FOLLOWED BY COMPRESSOR STALL WHICH WAS FELT AND HEARD BY CREW. REMOVED AND REPLACED VARIABLE BLEED VALVE FUEL GEAR MOTOR. REFERENCE AMM 75-31-20-400-002A. OPERATIONAL AND LEAK CHSDR F3LA2016062100051Engine · shutdownDURING CRUISE FLIGHT THE CREW NOTED, ECAM ENGINE 2 STALL WHICH WAS SOON FOLLOWED BY ENGINE 2 SHUTDOWN. THE CREW DECLARED EMERGENCY LANDING. MAINTENANCE R & R NR 2 ENGINE. REF WC MP71042-01 AND MP71042-02, REMOVAL AND INSTALLATION CARDS.
OPS CHECK GOOD.SDR WX0A2016042973141Acoustic Panel · crackedDURING DAILY CHECK WALK AROUND, DISCOVERED CRACKED ACOUSTIC PANEL AT 12 - 2 O'CLOCK POSITION ON NR 2 ENG. R & R ACOUSTIC PANEL AT 12 - 2 O'CLOCK POSITION IAW AMM 72-23-00. ALL IS GOOD.SDR F3LA2016032600014Engine · leakingAFTER TAKEOFF THE FLIGHT CREW RECEIVED A CARGO & LAVATORY SMOKE MSG. THE ACFT RETURNED TO THE FIELD & MX DISCOVERED OIL WETTING IN THE NR 2 ENG COMPRESSOR. MX REMOVED ENG SN 575632 & INSTALLED SERVICEABLE ENG 575640 IAW MPD TASK CARDS MP 71042-01, MP 71042-0SDR F3LA2015051101132Fuel Line · leakingNUMBER 2 ENG FUEL LEAK FROM MAIN FUEL SUPPLY LINE. R & R MAIN FUEL SUPPLY LINE IAW AMM 73-11-11 PAGE BLOCK 401. LEAK CHECKED GOOD. TORQUE WRENCH F9TAB3949C CALIBRATION DATE 10 15, LOG PAGE 896973.SDR F3LA2015041501130Duct · failedDISCREPANCY, ENG 2 FIRE, AIR TURN BACK 1839 Z. ENG 2 FIRE INDICATION ON TAKEOFF AFTER THRUST REDUCTION ON ENG 2 IAW ECAM. FIRE INDICATION CHANGED TO AMBER, ENG 2 SHUTDOWN. ENG 2 SHUTDOWN COMPLETED. FOUND HIGH PRESS BLEED DUCT BROKEN CAUSING ENG 2 FIRE INDISDR F3LA2014112401088Engine · malfunctionedAIRCRAFT DEPARTED & ENG 1 LOST OIL PRESS, OIL QTY WAS AT 0. CREW PERFORMED IN FLIGHT SHUTDOWN. EMER WAS DECLARED. ACFT ARRIVED WITHOUT FURTHER INCIDENT. ACFT ARRIVED WITH OIL TANK EMPTY. OIL WAS FOUND IN HOT STREAM OF EXHAUST PIPE, NO EVIDENCE OF OIL IN CSDR F3LA2014070101047Skin · debondedLT ELEVATOR THERMO GRAPHIC INSPECTION REVEALED INDICATIONS ON UPPER PANEL IRREGULAR IN SHAPE & BLACK IN COLOR. REPAIRED LT ELEVATOR UPPER SURFACE OF LIQUID INGRESS IAW SRM 55-20-00 PB201, SRM 55-21-11 PB201 & CMM 55-21-15-210-010-601. ACFT SCHEDULED BACK IN SDR F3LA2014052701040Idg · failedNUMBER 1 ENG GEN FAILED IN FLIGHT, UNABLE TO RESET. NR 2 ENG GEN FAILED IN FLIGHT, UNABLE TO RESET. REPLACED NR 1 ENG IDG IAW AMM 24-21-51 PB 401. OPERATIONS & LEAK CHECKED GOOD. R & R NR 2 ENG IDG IAW AMM 24-21-57 PB 401.SDR F3LA2013012400824Line · failedDURING CRUISE FLIGHT LOST GREEN SYSTEMS HYD; GREEN SYS HYD INOPERATIVE. FOUND BROKEN HYD LINE AT RT MLG DOOR ACTUATOR. R & R AFT HYD LINE ON RT MLG DOOR ACTUATOR. SERVICED GREEN HYD SYSTEM. LEAK AND OPS CHECKS NORMAL. REF 32-31-35 PB 401.SDR F3LA2013010300823Acm · malfunctionedAFTER LANDING, CABIN FILLED WITH SMOKE, DUCT TEMPS INCREASED TO OVER 110 DEGREES. MX DETERMINED THE NR 1 PACK TO BE OVERHEATING. RAN NR 1 PACK FOR 45 MINTUES. OPS CHECKED GOOD REF AMM 21-61-00-710-001A.SDR F3LA2012091700790Light · burned outC-CHECK: R2 DOOR "SLIDE ARMED" LIGHT DOES NOT ILLUMINATED DURING TEST. REMOVED SLIDE ARMED INDICATOR LIGHT ASSY IAW AMM 52-76-000-002-A. INSTALLED SERVICEABLE SLIDE ARMED LIGHT ASSY IAW AMM 52-73-21-400-002A. OPS CHECK GOOD IAW AMM 52-73-00-710-001-A.SDR F3LA2012091700792Sill · corrodedC-CHECK: R2 DOOR SILL BEAM CORRODED AROUND FASTENER HOLE AT FRAME 66. REPAIRED DOOR SILL BEAM WITH CUTOUT, FILLER AND SPLICE IAW SRM 53-41-14 PB201, PARA 5.A, FIG 201.SDR F3LA2012091700793Lamp · burned outC-CHECK: MAIN CABIN LT SEATS, ROW 13 HAS BURNED OUT LAMP FOR EMERGENCY EXIT LIGHT. R & R LAMP IAW AMM 33-51-19-420-052D. OPS CHECKED GOOD LAW AMM 33-51-00-71 0-00L-A.SDR F3LA2012083100782Actuator · intermittentACFT LEFT C-CHECK AFTER COMPLETE SET LANDING GEAR TIME, DEPARTED. NLG DID NOT LOCK UP, GEAR DOORS DID NOT CLOSE. ACFT WAS PREPPED FOR GEAR DOWN FERRY FLIGHT. FERRY FLIGHT DID NOT OCCUR. DISCREPANCY WAS WORKED AT AIRPORT, ADJUSTMENTS MADE, REF NR 43936. OCF USDR F3LA2012083100780Skin · dentedNR 1 ENGINE NOSE COWL INNER BARREL AT 9:00 POSITION HAS A DENT, REPAIRED IAW SRM 54-10-00, REPAIR 23, PARAGRAPH 2.A,B,C(1 -3), D, E(1 -2), F( 1-2), G AND H( 1-4).SDR F3LA2012081500777Ballast · failedODOR COMING FROM AFT CABIN. R & R BALLAST ASSY COVE LIGHT AT ROW 24 DEF. OPS CHECK GOOD, NO TROUBLE NOTED REF AMM 33-21-11, PAGE BLOCK 401.SDR F3LA2012003200728Blade · lack of lubeNR 1 ENGINE VIBRATION IN CLIMB OVER 4.0. VIBRATION WOULD FOLLOW THRUST. AIR TURN BACK. PERFORMED TSM TASKS 77-00-00-81 0-863-A AND 77-00-00-81 O-B64-A INCLUDING FAN BLADE LUBE REF AMM 72-21-00-210-004 AND COLD TRIM BALANCE REF AMM 71-00-00-750-001. MAXIMUM SDR F3LA2011052300652Pump · leakingPILOT REPORT YELLOW HYDRAULIC LOW RESERVOIR LEVEL. REMOVED AND REPLACED ENGINED NR2 HYDRAULIC PUMP DRIVER IAW AMM 29-13-51, PB 401, OPS CHECKS GOOD. FOUND SEVERAL LEAK YELLOW SYSTEM LINE TO PRESSURE SWITCH. REMOVED AND REPLACED LINE IAW AMM 28-23-11 LEAKED CHSDR F3LA2011022100606Stop · seizedACFT LOG PAGE 590497: AIR TURN BACK AT 01302. ECAM WARNING NR 2 ENGINE COMPRESSOR VANE (AIR RETURN. REPLACED NR 2 ENGINE MASTER BALLSCREW ACTUATOR STOP. REF AMM 75-31-50 PB 401, OPS CHECK NORMAL.SDR F3LA2010122900571Smoke Detector · faultyPILOT REPORT: LP 594710; AFT CARGO / LAV SMOKE DETECT FAULT. R & R THE AFT CARGO SMOKE DETECT UNIT (3WH) AND AFT LAV (E) DETECT UNIT. IAW AMM 26-46-15, PB 401. OPS TEST OK.SDR F3LA2010122000563Floor Panel · chafedC-CHECK: NON ROUTINE N0399; AFT CARGO PANEL 151VG AFT EDGE IS WORN THROUGH TOP PLY. AREA IS 10 SQ INCHES. DAMAGE IS OUT OF LIMITS. FABRICATED REPLACEMENT PANEL 151VG IAW MCG IRM 9701 REV G.SDR F3LA2010122000565Floorbeam · corrodedC-CHECK: NON ROUTINE N0436; LT FLOORBEAM, Y1292 AT FRAME 68L HAS A 2 SQ. INCHES OF CORROSION ON THE UPPER AND LOWER SIDERS. CORROSION IS OUT OF LIMITS. REPLACED FLOORBEAM, Y1292 BETWEEN FRAMES 68LT AND 69LT IAW SRM 51-72-11, PARA 6.SDR F3LA2010122000567Splice · corrodedC-CHECK: NON ROUTINE N0438; LT FLOORBEAM, Y1292 SPLICE COUPLING AT FRAME 66L HAS 2 INCHES OF CORROSION. CORROSION IS OUT OF LIMITS. REPLACED SPLICE COUPLING AT FRAME 66L IAW SRM 53-72-11, PARA 6.SDR F3LA2010122000570Plate · corrodedC-CHECK: NON ROUTINE N0596; FR69-70 SHEAR WEB PLATE HAS CORROSION AROUND FASTNER HOLES AND IS OLD CONFIGURATION. FOUND TO BE OUT OF LIMITS. REPLACED SHEAR WEB PLATE WITH NEW CONFIGURATION IAW EO AO-53EO-31434.SDR F3LA2010113000553Skin · crackedC-CHECK: NON ROUTINE N0178; NR2 ENGINE PYLON UPPER PANEL NR423DL HAS A 1 EACH CRACK ON THE INTERIOR SIDE AT THE CUT OUT ABOUT .25" IN LENGHT. IAW SRM 54-52-11, STOP DRILL CRACK ENDS AND WELDED IAW PMS 01-04-21.SDR F3LA2010113000554Skin · crackedC-CHECK: NON ROUTINE N0179; RT PYLON UPPER PANEL NR 423DL HAS A 4.0" CRACK AROUND LOUVERS AND ABOUT 1.0" IN LENGHT. IAW SRM 54-52-11 AND PMS 01-04-21, STOP DRILLED CRACK AND WELDED.SDR F3LA2010113000555Access Panel · crackedC-CHECK: NON ROUTINE N0565; LT PYLON ACCESS PANEL NR413DL CRACKED. IAW SRM 54-50-80 AND PMS 01-04-21, STOP DRILLED CRACK ENDS AND WELDED.SDR F3LA2010120200556Transition Panel · delaminatedC-CHECK: NON ROUTINE N0467; AFT CARGO COMPARTMENT LT TRANSITION PANEL NR 151DE HAS A 1.0" PUNTURE AND 3.0" SQUARE OF DELAMINATION. FABRICATED REPLEACEMENT PANEL IAW MCG IRM 9701, REV G.SDR F3LA2010111400549Actuator · out of rigACFT FLEW AT 5 TO 10 DEGREE LT WING DOWN ON AP, FL CTL SHOWED LT AILERON UP. FUEL BALANCE OK. ACFT WANTED TO FLY IN LT SLIP. FOUND RUDDER TRIM TO BE OUT RIG. REMOVED RUDDER TRIM ACTUATOR, PERFORM ZEROING PROCEDURE ON ACTUATOR. ADJUST ARTIFICIAL FEEL SPRING SDR F3LA2010103000533Floor Panel · delaminatedC-CHECK: NON ROUTINE N0573: AFT CARGO FLOOR PANEL 162EF HAS TOP SKIN DISBONDED FWD INBD CORNER. FABRICATED AND REPLACEMENT PANEL 162 EF IAW MCG IRM 9701 REV G.SDR 2010FA0001072Spool · unserviceableINCOMING FLUORESCENT PENETRANT INSP OF HPC 1-2 SPOOL REVEALED CRACK INDICATIONS IN 2 OF DOVE TAIL POSTS ALONG THE EDGE OF BEDDING MARK. ON 1 OF POST, THE CRACKING EXTENDS ACROSS BOTH THE FWD AND AFT FACES. CRACKING MEASURED AT 1.5 INCHES AND 0.375 INCHES. TSDR F3LA2010090100501Power Supply · inoperativeWHILE TROUBLESHOOTING EPSU REF. SWAPPED LT FWD EPSU INTO MID POSITION RESULTING IN ITS FAILURE. R & R LT FWD EPSU 10WL, OPS CHECKS NORMAL IAW AMM 33-51-38, PB 401.SDR F3LA2010090100497Power Supply · inoperativeLT SIDE AFT FACING EXIT ROW SIDE AND EXIT SIGN INOPERATIVE. R & R LT OVERWING EPSU. IAW AMM 33-51-38, PB 401.SDR F3LA2010090100493Seat Track · corrodedC-CHECK, NON ROUTINE N0567, AFT MAIN CABIN RT SEAT TRACK YR2 DOOR SILL TRAY AT FRAME 66-Y122 AT FRAME 68 HAS 2 AREAS OF CORROSION ON UPPER SURFACE. REMOVED CORROSION IAW SRN 51-74-00. BLEND OUT MEASURES 2.5 INCH X 1.5 INCH X .012 INCH AND 3 INCH X 1.5 INCH X .SDR F3LA2010090100495Sill · corrodedC-CHECK: NON ROUTINE N0590, R2 DOOR SILL TRAY AT FRAME 66 HAS 1 AREA OF CORROSION AROUND NUT PLATE HOLE. REMOVED CORROSION IAW SRM 51-74-00. OPENED HOLE TO .310, BLEND OUT MEASURES 1 INCH X 1.5 INCH X .020 WITHIN LIMITS IAW 53-00-14 FIG 102. REPROTECTED IAW SRSDR F3LA2010090100496Roll Pin · brokenC-CHECK: NON ROUTINE N0785. LT EMERGENCY EXIT SLIDE ARMING MECHANISM WILL NOT STAY IN ARMED POSITION. R & R SLIDE RELEASE MECHANISM SPRING PIN IAW AMM 52-21-11-000-003 AND AMM 52-11-420-051. PERFORMED SLIDE MECHANISM OPS CHECK IAW AMM 52-21-00-720-001. NO DEFESDR F3LA2010080800480Plate · corrodedREF NON-ROUTINECARD N0392, AFT CABIN RT SHEAR PLATE BETWEEN FRAMES 69 AND 70, HAS CORROSION THAT IS OUT OF LIMITS. R & R SHEAR PLATE AT AFT CABIN RT SIDE BETWEEN FRAMES 69 AND 70 IAW SRM 51-42-11 AND EO AO-53E0-31434.SDR F3LA2010080800482Floor Panel · damagedREF NON=ROUTINE N0691, FWD CARGO FLOOR PANEL 131AF BROKEN COTR APPROX 2.0 IN X 2.5 IN. ACFT IS IN C-CHECK. REPAIR DAMAGE AREA ON PANEL 131AF USING RESIN AND GLASS CLOTH PATCH METHOD IAW SRM 53-02-00, PARA 8B.SDR F3LA2010080800483Sill · corrodedMAIN CABIN FLOOR STRUCTURE LONGERON AT OTBD POSITION FRAME 66 HAS A 1 SQ IN ARE OF CORROSION REF NON-ROUTINE N0451. CUT OUT CORROSION AT NUTPLATE HOLE IAW SRM 53-42-14 PRINCIPLE 6 FABRICATED REPAIR ANGLES IAW SRM 53-42-14 PRINCIPLE 6 TREATED PRIMED AND TOP COOSDR F3LA2010080200477Engine · overservicedAIR TURN BACK DUE TO OIL TEMP TRENDING TOWARD EXCEEDANCE. REACHED 135 DEGREES CELCIUS MAXIMUM. PRECAUTIONARY RETURN BASED. ALSO ON ENGINE START, OIL PRESSURE REMAINED IN RED ARC UNTIL ABOUT 52.5 PERCENT N1. OIL QUANTITY INDICATED 20.5 QUARTS. FOUND NR 2 ENGINESDR F3LA2010080200476Valve · failedON CLIMBOUT NR 2 ENGINE OIL OVERTEMP. SHUTDOWN ENGINE NR 2 IAW ECAM. MAXIMUM NOTED OIL TEMP 160 DEGREES CELCIUS. MAXIMUM NOTED OIL PRESSURE WAS ABOUT 36 PSI, 10 PSI LOWER THAN ENGINE NR 1. R & R FUEL RETURN VALVE ASSY FOR NR 2 ENGINE. REF AMM 73-11-50 PAGE BLOSDR F3LA2010080300479Floor Support · corrodedREF HEAVY MX NON ROUTINE N0561. RT CABIN FLOOR AT FRAME 69 TO FRAME 70 SUPPORT EXTRUSION BELOW SHEAR PLATE IS CORRODED. R & R SUPPORT IAW SRM 51-72-11.SDR F3LA2010060400435Computer · malfunctionedPILOT REPORT REF LOG PAGE 524666 ITEMS 1 AND 2. SMOKE WARNING ACTUATED UPON LANDING. NO SMOKE NOTICED IN COCKPIT. BOTH BLOWER AND EXTRACT FAULTED AT SAME TIME ON THE VENTILLATION SYS. R & R AEVC COMPUTER.SDR F3LA2010052200422Sign · inoperativeREF HEAVY MX NON ROUTINE N0773. RT FWD LOWER EMERGENCY EXIT IDENTIFIER DOES NOT ILLUMINATE. R & R IDENTIFIER IAW AMM 33-51-13-000-001.
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