GE CFM56 series

Service difficulty reports · 5,028

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 = 'CFM56'
  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 IXX2008F00011Landing Gear · malfunctionedDURING TAKEOFF, FLIGHT CREW WAS UNABLE TO RAISE GEAR HANDLE. FLIGHT CREW ACCOMPLISHED CHAPTER 3 PROCEDURES IN COCKPIT OPERATING MANUAL AND RAISED GEAR. GROUND CONTROL RELAY CIRCUIT BREAKER RELAYS WERE OPEN FOR FLIGHT AND RESET AFTER LANDING. AC LANDED UNEVEJul 11, 2008 · N604BX · Doug DC873F · Main Landing GearSDR IXX2008F00012Engine · fireDURING FLIGHT, NR 3 ENGINE FIRE WARNING LIGHT ILLUMINATED MOMENTARILY. FLIGHT CREW RETARDED THE THROTTLES AND SHUTDOWN THE ENGINE. THE FIRE LIGHT AND WARNING WENT OUT. APPROX 30 MINUTES LATER FIRE WARNING CAME BACK ON. FLIGHT CREW FIRED (1) BOTTLE AND AGENJul 11, 2008 · N603AL · Doug DC873F · Engine (Turbine/Turboprop)SDR IXX2008F00006Transducer · defectiveDURING CLIMB OUT, AT 240 KIAS WITH A 9 DEGREE PITCH NOSE UP STICK SHAKER CAME ON STEADY. IT CYCLED ON AND OFF RANDOMLY FOR 15 MINUTES UNTIL LANDING. STALL WARNING TEST SWITCH WAS TOGGLED WITH NO EFFECT. THE CREW LANDED WITH NO FURTHER INCIDENT. MAINTENANCEJul 10, 2008 · N821BX · Doug DC871F · Navigation SystemSDR IXX2008F00008Fire Warning · illuminatedDURING CRUISE, NR 2 FIRE WARNING CAME ON, THE CREW DISCHARGED BOTH FIRE BOTTLES AND SHUTDOWN NR (2) ENGINE. CREW LANDED WITHOUT INCIDENT. IN WORK. (K)Jul 8, 2008 · N820BX · Doug DC871F · Fire DetectionSDR 2008FA0000464Floorbeam · chafedDURING SCHEDULED INSP, FOUND CLIP NUTS CHAFING FLOORBEAM IN FWD CABIN BS 344, LBL 0 TO LBL 55. (K)Jul 7, 2008 · N304TZ · Boeing 73783N · Fuselage Main, Floor BeamSDR 2008FA0000465Floorbeam · corrodedDURING SCHEDULED INS, FUND FWD CABIN BS 344, LBL10, FLOORBEAM CORRODED. (K) SO 245010, NR27110Jul 7, 2008 · N304TZ · Boeing 73783N · Fuselage Main, Floor BeamSDR 2008FA0000462Floorbeam · corrodedDURING SCHEDULED INSP, FOUND CORROSION IN PAX CABIN FWD WET AREA ON FLOORBEAM AT BS 328, RBL 26 AFT SIDE OF BEAM FOUND TO BE BEYOND LIMITS. (K)Jul 4, 2008 · N304TZ · Boeing 73783N · Fuselage Main, Floor BeamSDR 2008FA0000461Floorbeam · corrodedDURING SCHEDULED INSP, FOUND CORROSION IN PAX CABIN FWD WET AREA ON FLOORBEAM AROUND FASTENERS AT BS 294 FROM RBL-2 TO RBL 43. SO NR 245010 NR 27077. (K)Jul 3, 2008 · N304TZ · Boeing 73783N · Fuselage Main, Floor BeamSDR 2008FA0000463Floorbeam · corrodedDURING SCHEDULED INSP, FOUND CORROSION IN PAX CABIN FWD WET AREA ON FLOORBEAM AT BS 328 FROM RBL 13 TO RBL 50. (K)Jul 3, 2008 · N304TZ · Boeing 73783N · Fuselage Main, Floor BeamSDR IXX2008F00002Indicator · inoperativeON TAKEOFF ROLL, CAPTAIN AIRSPEED DID NOT REGISTER 80 KNOTS (ANALOG NEEDLE AT ZERO, DIGITAL READOUT ERROR). CREW REJECTED TAKEOFF AT 80 KNOTS, THE CREW RETURNED TO BLOCKS WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED CAPTAIN MACH AIRSPEED INDICATOR OPERAJul 2, 2008 · N820BX · Doug DC871F · Airspeed/Mach IndicatorSDR IXX2008F00001Connector · dirtyDURING CRUISE, NR 2 ENGINE FIRE WARNING AND BELL CAME ON INTERMITTEN FOR 1-2 SECONDS. THE CREW ACCOMPLISHED, RAN CHECK LIST AND SHUTDOWN NR (2) ENGINE. THE FIRE BELL STOPPED AFTER FIRE HANDLE WAS MOVED TO FULL FWD POSITION. THE FIRE BOTTLES WERE NOT DISCHAJul 1, 2008 · N830BX · Doug DC871F · Turbine Engine System WiringSDR IXX2008F00003Fire Warning · intermittentDURING CRUISE, NR 2 ENGINE FIRE WARNING AND BELL INTERMITTENT FOR 1-2 SECONDS. THE CREW RAN CHECK LIST AND SHUT DOWN NR (2) ENGINE. THE FIRE BELL STOPPED AFTER FIRE HANDLE WAS MOVED TO FULL FWD POSITION. THE FIRE BOTTLES WERE NOT DISCHARGED. THE CREW LANDEJul 1, 2008 · N830BX · Doug DC871F · Fire DetectionSDR UPS08852737Rib · crackedINSPECTION TYPE-C2, AFT END OF RIB CRACKED IN RT HORIZ STAB L/E STA. XFS 47.5. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 5 1-3-02, 55-02-00 FIG 2.Jun 29, 2008 · N752UP · Doug DC871F · Horizontal Stabilizer, Spar/RibSDR ASAA0853109Oil System · lowBOTH ENGINE OIL QUANTITIES LOW NR 1 AT 13 NR 2 AT 14. SERVICED NR 1 ENG WITH 5QT OF OIL. SERVICED NR 2 ENG WITH 5 QT OF OIL.Jun 28, 2008 · N577AS · Boeing 737890 · Turbine Engine Oil SystemSDR ASAA0853106Oil System · lowNR 1 OIL AT 13 ADDED 4QTS OIL TO NR 1 AND 4QTS OIL TO NR 2.Jun 27, 2008 · N583AS · Boeing 737890 · Turbine Engine Oil SystemSDR IXX2008F00009Switch · brokenDURING CLIMB-OUT, OVER RIDE TOGGLE SWITCH BROKE OFF. AIRCRAFT RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED OVER RIDE SWITCH; OPS CHECK GOOD IAW UAL MM 74-20-36. (K)Jun 26, 2008 · N825BX · Doug DC871F · Electrical Power SystemSDR ASAA0853090Filter · dirtyLT ENG OIL FILTER POP OUT INDICATOR EXTENDED. REMOVED AND REPLACED LT ENG OIL SUPPLY FILTER PER MM79 21 03 000 802 F00. OPS AND LK CK GOOD. POP OUT IND CKS GOOD.Jun 25, 2008 · N570AS · Boeing 737890 · Turbine Engine Oil SystemSDR ASAA0853091Filter · dirtyRT ENG OIL FILTER POP OUT INDICATOR EXTENDED. DRAINED ENG OIL AND AGB PER 737 AMM 12 13 11. REMOVED AND REPLACED RT ENGINE OIL SUPPLY FILTER PER MM 79 21 00 802 FOO. OPS AND LEAK CHECK GOOD, POP OUT INDICATOR CKS GOOD. NO CONTAMINATION IN FILTER.Jun 25, 2008 · N570AS · Boeing 737890 · Turbine Engine Oil SystemSDR ASAA0853107Hydromech Unit · faultyENG NR 2 SHORT TERM FAULT MSG NO. FAULT CODE NR 73 20342. THE FMV POSITION SIGNAL OUT OF RANGE. PERFORMED TEST 12 ACTUATORS TEST CONFIRMED FAULT. VERIFIED ROTABLE COMPONENT MFG NR 442369 S/N NR 3219 REF IPC 73 21 10 01 ITEM 25T. REPLACED HMU REF MM 73 21Jun 23, 2008 · N584AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA0853034Oil System · lowNR 1 ENG QTY AT 13 NR 2 ENG QTY AT 15 SERVICED NR 1 ENG OIL TO FULL 5.5 QTS SERVICED NR 2 ENG TO FULL.Jun 4, 2008 · N583AS · Boeing 737890 · Turbine Engine Oil SystemSDR ASAA0853017Oil System · lowNR 1 ENGINE OIL IS AT 13 QTS SERVICED ENGINE OILS NR 1 ADDED 3 QTS, NR 2 ADDED 3.5 QTS APU ADDED 0.Jun 1, 2008 · N587AS · Boeing 737890 · Turbine Engine Oil SystemSDR ASAA0853016Oil System · lowNR ONE ENGINE OIL AT 13 QTS TOP OF DESCENT. NR TWO ENGINE OIL AT 14 QTS TOP OF DESCENT VERIFIED NR 1 AND NR 2 ENG OIL SERVICED TO 16 AND 17 QTS RESPECTIVELY. TOPPED OFF BOTH ENG OILS TO FULL. NR 1 ENG OIL ADDED 2.5 QTS, NR 2 ENG OIL ADDED 2.5 QTS, APU OIL AMay 30, 2008 · N570AS · Boeing 737890 · Turbine Engine Oil SystemSDR 2008UALA03068Skin · damagedFUSELAGE SKIN KINKED JUST BELOW STR 14L LAP JOINT, AFT OF STA 992. MAJOR REPAIR ACCOMPLISHED, REPLACED FUSELAGE SKIN.May 29, 2008 · N318UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR ASAA0853013Engine · oil consumptionNR 2 ENGINE HAS A HISTORY OF ABOVE NORMAL OIL CONSUMPTION PERFORM MM 71-71-00-200-801 VENTS AND DRAIN INSPECTION, PART POWER ENGINE RUN REQUIRED. ACCOMPLISHED TSR AND AMM 71 71 00. NO LEAKS NOTED.May 29, 2008 · N587AS · Boeing 737890 · Turbine Engine Oil SystemSDR 2008UALA03065Crease Beam · corrodedAFT GALLEY DOOR CUTOUT CREASE BEAM AT STR S- 17R CORRODED ON UPPER SURFACE FROM BS 967-986.5. MAJOR REPAIR ACCOMPLISHED: BLENDED CORROSION & FOUND BLEND OUT OF LIMITS. REMOVED AND REPLACED CREASE BEAM.May 28, 2008 · N399UA · Boeing 737322 · Fuselage Main, StructureSDR 2008UALA03066Angle · crackedBODY STATION 291.5 STRINGER S-12R WEB ANGLE CRACKED. MAJOR REPAIR ACCOMPLISHED, REMOVED AND REPLACED CRACKED ANGLE.May 28, 2008 · N399UA · Boeing 737322 · Fuselage Miscellaneous StructureSDR 2008UALA03067Skin · dentedUPPER LT FUSELAGE SKIN STA 904 S-14L IS DENTED. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED EXTERNAL DOUBLER, TRIPLER AND FILLER REPAIR.May 28, 2008 · N399UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2008UALA03040Floorbeam · corrodedCABIN FLOOR FRAME CAP CORRODED AROUND FASTENER HOLES BS 986 WL208 RBL 24"-37". MAJOR REPAIR ACCOMPLISHED, REMOVED UPPER "T" CAP. INSTALLED FLOORBEAM UPPER CAP SPLICE REPAIR.May 27, 2008 · N399UA · Boeing 737322 · Fuselage Main, Floor BeamSDR 2008UALA03041Skin · damagedRUDDER SN 100, LT LE SKIN HAS AREA OF DAMAGE 1 INCH ABOVE LOWER EDGE. MAJOR REPAIR ACCOMPLISHED, TAPER SANDED DAMAGED AREA. INSTALLED MULTIPLE LAYER COMPOSITE REPAIR.May 27, 2008 · N399UA · Boeing 737322 · Rudder, Plate/SkinSDR 2008UALA03048Shear Tie · crackedFWD ENTRY DOOR CUTOUT AFT SIDE SHEAR TIE IS CRACKED ON AFT SIDE AT BS 360 JUST BELOW STRINGER S-13L. MAJOR REPAIR ACCOMPLISHED, REPLACED SHEAR TIE WITH P/N 69-48204U505.May 27, 2008 · N399UA · Boeing 737322 · Fuselage Internal Mounting StructureSDR 2008UALA03052Skin · damagedSHEARED RIVET HEAD AFT OF E/E DOOR.May 27, 2008 · N905UA · Boeing 737522 · Fuselage Main, Plate/SkinSDR ASAA0852981Probe · dirtyNR 1 ENGINE EGT HOT DAY MARGIN HAS NOT RECOVERED TO EXPECTED LEVELS AFTER LAST COMPRESSOR WASH. ALL OTHER PARAMETERS ARE NORMAL. COMPLETED T C 78273000, NO FAULTS LOGGED. PRE CLEAN T49.5 S1 S4 106 61 67 128. AFTER CLEANED 62 32 35 78. DURING ENG RUN AFTMay 26, 2008 · N570AS · Boeing 737890 · Engine Temperature Indicating SystemSDR 2008UALA02851Wire · misinstalledWHEN EMERGENCY EXIT LIGHT SW IS SELECTED ' ON' THE 'ANTI-ICE' MASTER CAUTION IS ILLUMINATED INSTEAD OF 'OVERHEAD'. FOUND WIRES SWAPPED ON RIGHT SIX PACK. CORRECTED PER WDM33-18-21. SYSTEM OPS CHECK GOOD. AC OK FOR SERVICE.May 18, 2008 · N365UA · Boeing 737322 · Light System WiringSDR 2008UALA02862Stringer Clip · damagedFWD CARGO PIT STRINGER CLIP BENT AT BS 400 AND STRINGER S-24R. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED STRINGER CLIP AND REPLACED IT WITH NEW CLIP.May 18, 2008 · N399UA · Boeing 737322 · Fuselage Main, Attach FittingsSDR 2008UALA02863Stringer Clip · crackedFWD CARGO PIT STRINGER CLIP CRACKED AT BS 380 AND STRINGER S-22L. MAJOR REPAIR ACCOMPLISHED, REMOVED AND REPLACED DAMAGED STRINGER CLIP WITH NEW.May 18, 2008 · N399UA · Boeing 737322 · Fuselage Main, Attach FittingsSDR 2008UALA02864Stringer Clip · crackedFWD CARGO PIT STRINGER CLIP CRACKED AT BS 380 AND STRINGER S-21L. MAJOR REPAIR ACCOMPLISHED, REMOVED AND REPLACED DAMAGED STRINGER CLIP WITH NEW.May 18, 2008 · N399UA · Boeing 737322 · Fuselage Main, Attach FittingsSDR 2008UALA02865Strap · crackedTHE FOLLOWING CRACKS WERE AT VERTICAL STRAP STA 348 STR 16L, INTERCOSTAL CLIP STA 360 STR 11L, INTERCOSTAL CLIP STA 294.5 STR 11L AND INTERCOSTAL WEB STA 294.5 STR 11L.May 18, 2008 · N305UA · Boeing 737322 · Fuselage Miscellaneous StructureSDR 2008UALA02866Frame · damagedSTA 294.5 FRAME AT STR 11L HAS TOOLING MARK.May 18, 2008 · N305UA · Boeing 737322 · Fuselage Main, FrameSDR 2008UALA02867Oxygen System · lowCREW O2 INDICATES 1000PSI. May 18, 2008 · N386UA · Boeing 737322 · Crew Oxygen SystemSDR 2008UALA02848Door Frame · damagedFWD CARGO PIT DOOR CUTOUT FWD FRAME HAS DAMAGE UNDER LOWER STOP FITTING. MAJOR REPAIR ACCOMPLISHED: REPLACED FRAME.May 17, 2008 · N910UA · Boeing 737522 · Fuselage Main, StructureSDR 2008UALA02875Light · inoperativeEMERGENCY SLIDE LIGHT INOP DOOR 1L. RELAMPED.May 17, 2008 · N315UA · Boeing 737322 · Emergency LightingSDR 2008UALA02876Light · inoperativeEMERGENCY SLIDE LIGHT INOP DOOR 2R. RELAMPED.May 17, 2008 · N315UA · Boeing 737322 · Emergency LightingSDR 2008UALA02839Crease Beam · unknownFUSELAGE STR 17R CREASE BEAM NEEDS CUT AT BS 400. MAJOR REPAIR ACCOMPLISHED, FABRICATED REPAIR ANGLES AND INSTALLED NESTED ANGLE DOUBLER/TRIPLER REPAIR.May 16, 2008 · N910UA · Boeing 737522 · Fuselage Main, StructureSDR ASAA0852978Compressor · dirtyGE REMOTE DIAGNOSTICS NR 2 ENGINE TREND DATA CONTINUES TO SHOW A GREATER THAN NORMAL EGT MARGIN LOSS. ACCOMPLISH NR 2 ENGINE SINGLE ENGINE COMPRESSOR CLEANING IAW AMM SUPPLEMEMT 72-00-00 P710. ACCOMPLISHED COMPRESSOR WASH ON NR 2 ENG REF MM SUPP 72-00-00 PGMay 16, 2008 · N570AS · Boeing 737890 · Turbine Engine Compressor SectionSDR 2008UALA02799Skin · delaminatedLT OTBD FLAP INBD EDGE DELAMINATED 4 INCH BY 7 INCH. MOISTURE IS PRESENT. REPLACED LT OUTBOARD AFT FLAP AND OPS CHECKED REF MM 27-51-39-401. ACFT OK FOR SERVICE.May 15, 2008 · N927UA · Boeing 737522 · Trailing Edge FlapsSDR 2008UALA02781Wire · shortedBURNING ODOR NOTED THROUGHOUT THE ACFT. ODOR DISSIPATED WHEN RECIC FAN WAS TURNED OFF. AFTER EXTENSIVE TROUBLE SHOOTING AND PART REPLACEMENT REPAIRED WIRE W090-018-24 REF WD21-61-01 BETWEEN CABIN TEMP CONTROLLER AND CABIN TEMP SELECTOR. FOUND WIRE SHORTED TOMay 14, 2008 · N935UA · Boeing 737522 · Air Conditioning System WiringSDR 2008UALA02800Battery · dischargedMID CABIN EMERGENCY LIGHTING INOPERATIVE. REPLACED BATTERY AND OP CHK'D GOOD.May 14, 2008 · N910UA · Boeing 737522 · Emergency LightingSDR VQI2008F00001Wire Harness · damagedIN NORMAL CRUISE, THE AIRCRAFT EXPERIENCED AN UNCOMMANDED SHUTDOWN OF THE NR 1 ENGINE. ECAM ENG1 FADEC A FAULT OCCURRED WITH ASSOCIATED MESSAGES. THE CREW RESTARTED THE ENGINE AFTER FOLLOWING QRH PROCEDURES . A/C DIVERTED INTO PDX WITH NO FURTHER FAULTS NOTED.May 14, 2008 · N527VA · Airbus A319111 · Turbine Engine System WiringSDR 2008UALA02764Warning System · activatedRTFL DUE TO A WING/BODY OVERHEAT INDICATION. NORMAL LANDING. May 13, 2008 · N934UA · Boeing 737522 · Overheat DetectionSDR 2008UALA02706Clamp · looseRTFL DUE TO WING BODY OVERHEAT WARNING. FOUND PNEUMATIC LEAK JUST INBOARD OF NR 1 ENGINE PYLON AT CLAMP. REPLACED CLAMP.May 11, 2008 · N934UA · Boeing 737522 · Pneumatic Distribution System
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