GE CFM56 series

Service difficulty reports · 5,028

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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"

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SDR DU4R0507003Skin · dentedDENT AND CREASE IN LOWER FUSELAGE SKIN AT BS 907 BETWEEN S-25R - S-26R.Jun 30, 2005 · N387UA · Boeing 737 · Fuselage Main, Plate/SkinSDR DU4R0507128Skin · crackedDL/H UPPER FUSELAGE SKIN S-7L HAS 1 EA. CHERRY MAX RIVET FS 420. S/O NR 134005, OPS NR 20347.Jun 30, 2005 · N387UA · Boeing 737 · Fuselage Main, Plate/SkinSDR DU4R0507130Skin · misrepairedFUSELAGE LT SIDE BS 927-945.5 S-19L- 20L HAS PREVIOUS REPAIR THAT ENDS ON A LAP SEAM.Jun 30, 2005 · N387UA · Boeing 737 · Fuselage Main, Plate/SkinSDR DU4R0507131Skin · misrepairedFUSELAGE RT SIDE BS 927-945.5 S-21R-22R HAS PREVIOUS REPAIR THAT ENDS ON A STRINGER.Jun 30, 2005 · N387UA · Boeing 737 · Fuselage Main, Plate/SkinSDR DU4R0507132Skin · dentedBS 1024, S-6L-S-7L HAS A DENT WIDTH 1.5 INCH X .070 DEPTH.Jun 30, 2005 · N387UA · Boeing 737 · Fuselage Main, Plate/SkinSDR IXXA05SMN136SSkin · damagedDURING ROUTINE C CHECK INSPECTION, RT OB FLAP FWD UPPER PLATING NON STANDARD REPAIRS (03 EA) AND WEAR DAMAGES BETWEEN STA XF 197.000 - XF 213.000PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1, SRM 57-7-1 FIG. 4 TR NR 57-94, EO SEMAN NR 2005912 DATE 06-18-05. REMJun 30, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN138SSkin · improperDURING ROUTINE C CHECK INSP, RT OB FLAP FWD UPPER PLATING NON STANDARD REPAIR AT STA XF 415.000. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1, SRM 57-7-1 FIG. 4 TR NR 57-94, EO SEMAN NR 2005914 DATE 06-18-05. REMOVED DAMAGED PLATING IAW SRM 51-1-21 PAGE 1. FJun 30, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN139SDoubler · corrodedDURING ROUTINE C CHECK INSPECTION, FUSELAGE EXTERIOR INTERNAL DOUBLER CORRODED , STA 35.000 - 70.000 BETWEEN L - 28 TO L 31. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1, SRM 53-3-1 FIG. 1, EO SEMAN NR 2005877 DATE 06-22-05. REMOVED CORROSION IAW SRJun 30, 2005 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN140SSkin · brokenDURING ROUTINE C CHECK INSPECTION, LT WING IB L/E UPPER SURFACE BROKEN, STA XFS 51.250 - 57.500. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 25, EO SEMAN NR 2005908 DATE 06-15-05. REMOVED DAMAGED AREA IAW SRM 57-2-1 FIG. 21. PERFORMED NDT INSPECTION IAW NDT SJun 30, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR USAA200506004Skin · cracked2.25 INCH CRACK FOUND AT 727E, S25R ON SKIN. INSTALLED DOUBLER IAW SRM 53-00-01 FIG. 229.Jun 29, 2005 · N511AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR IXXA05SMN121SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT. ACCESSORY COMPARTMENT FITTING CRACKED L-28R, STA 1766.000 REMOVED CRACKED FITTING IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 1. TORQUED IAJun 29, 2005 · N822BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA05SMN122SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT ACCESSORY COMPARTMENT BATHTUB FITTING, CRACKED STA 1690.000 L-34L. REMOVED CRACKED BATHTUB FITTING IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW BATHTUB FITTING IAW SRM 51-1-20Jun 29, 2005 · N822BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA05SMN123SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT ACCESSORY COMPARTMENT BATHTUB FITTING CRACKED, STA 1690.000 L - 30L. REMOVED CRACKED BATHTUB FITTING IAW SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING (ALCLAD 7075 T6 51) IAW DWG 4641324. PERFORMED HEAT TREATMENT IAW SRJun 29, 2005 · N822BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA05SMN124SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT ACCESSORY COMPARTMENT BATHTUB FITTING CRACKED, STA 1690.000 L-34R. REMOVED CRACKED BATHTUB FITTING IAW SRM 51-1-20D PAGE 21. FABRICATED NEW BATHTUB FITTING (ALCLAD 7075 T6 51) IAW DWG 4641324. PERFORMED HEAT TREATMENT IAJun 29, 2005 · N822BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA05SMN125SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, AFT ACCESSORY COMPARTMENT, L -34R CRACKED STA 1690.000. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1, SRM 53-5-1 FIG. 7, EO SEMAN NR 2005863 DATE 06-18-05. REMOVED CRACKED LONGERON SEGMENT + EXISTING SPLICES IAW SRM 51-1Jun 29, 2005 · N822BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA05SMN127SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, AFT. LWR. CARGO BILGE INTERIOR. NR 3 DOOR HOUSING LWR FITTING CORRODED (INTERNAL STRUCTURE), STA. 1215.000, L-31LREMOVED CORROSION IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE 2P. REMOVED CORRODED FITTIJun 29, 2005 · N822BX · Doug DC871F · Fuselage Main, Attach FittingsSDR 2005UALA00602Strip · missingAFT GALLEY EMERGENCY EEL STRIP IN FRONT OF CART STOWAGE COMPARTMENT MISSING. SUPPLEMENTAL DATA UPDATE EEL STRIP WAS MISSING AND WAS REPLACED.Jun 27, 2005 · N937UA · Boeing 737522 · Emergency LightingSDR 2005UALA00603Cable · damagedEMERGENCY EEL LIGHTS INOP FROM ROW 17 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT. SUPPLEMENTAL DATA UPDATE EEL CABLE WAS DAMAGED, REPLACED CABLE.Jun 27, 2005 · N309UA · Boeing 737322 · Light System WiringSDR IXXA05SMN115SSkin · nickedDURING ROUTINE C CHECK INSP, LT OB FLAP L/E NICKED, XF 226.000 (UPPER PART) PERFORMED MAJOR REPAIR, DWG NR ED 3987 DATE 06-20-05, EO. REMOVED FASTENERS IAW SRM. REMOVED DAMAGED PLATING SEGMENT IAW DWG ED 3987. PERFORMED NDT INSP IAW SPM. NO CRACK, CORROSION FJun 27, 2005 · N822BX · Doug DC871F · Wing, Plate/SkinSDR ASAA0540303Skin · delaminatedOKC - FOUND RT OB AFT FLAP DELAMINATED AT IB AFT CORNER.Jun 26, 2005 · N773AS · Boeing 7374Q8 · Trailing Edge FlapsSDR 2005UALA00598Attach Angle · crackedHORIZONTAL STAB CENTER SECTION CENTER LT SIDE 3 EACH BEAM ATTACHED ANGLES CRACKED, NR 1 UPPER FWD, NR 2 LOWER FWD AND NR3 LOWER AFT. REPLACED 3 EACH CRACKED FITTINGS REF SRM 51-40-02.Jun 25, 2005 · N340UA · Boeing 737322 · Horizontal Stabilizer Miscellaneous StructureSDR SB05071Light · shortedCLT MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT ROW 22 WAS SHORTED. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AND THE FUSE IN THE EMERGENCY LIGHT BATTERY PACK BETWEEN AFT GALLEYS. OPERATIONAL CHECK GOOD.Jun 16, 2005 · N511AU · Boeing 7373B7 · Emergency LightingSDR AU510002097Pump · leakingAPU FUEL PUMP LEAKING BEYOND LIMITS.Jun 11, 2005 · Boeing 7377Q8 · APU Engine Fuel and ControlSDR AU510002101Odor · detectedELECTRICAL BURNING ODOR IN CABIN IN AREA OF ROW 18. EXTENSIVE INVESTIGATION COULD FIND NO CAUSE FOR THE ODOR.Jun 11, 2005 · Boeing 737800* · Air Distribution SystemSDR AU510001832Wheel · wrong partINCORRECT PART NUMBER MAIN WHEEL FITTED TO LT MAIN LANDING GEAR NR 2 POSITION. WHEEL FITTED WAS PNO 277A6000-204 WHICH IS FOR FITMENT TO 737-800 SERIES AIRCRAFT. THE CORRECT P/N 277A6000-206 IS FITTED TO 737-700 SERIES. THE INCORRECT WHEEL IS A HIGH GROSS WJun 9, 2005 · Boeing 7377BX · Wheel/Ski/FloatSDR AU510001720Window · failedNR 4 RT FLIGHT COMPARTMENT WINDOW INNER PANE SHATTERED. WINDOW HEAT SYSTEM WAS FOUND TO BE SERVICEABLE.Jun 8, 2005 · Boeing 737800* · Flight Compartment WindowsSDR AU510001840Controller · faultyNR 2 CABIN PRESSURE CONTROLLER FAULTY.Jun 8, 2005 · Boeing 737800* · Cabin Pressure ControllerSDR AU510001557Bolt · dislodgedDOOR L1 UPPER GATE STUCK IN LOCKED POSITION DUE TO LOWER ROD ASSEMBLY BOLT DISLODGED IN THE TORQUE BOX ASSEMBLY. SUSPECT BOLT INSUFFICIENTLY TORQUED.Jun 7, 2005 · Boeing 737800* · Passenger/Crew DoorsSDR PIDA20050050Engine · bird ingestionINGESTED BIRD IN RIGHT ENGINE AT ROTATION. VIBRATION INDICATION 4.0 UNITS AT POWER REDUCTION. INSPECTED ENGINE PER MM 71-00-47. UNSHINGLED BLADES NR 20, 21, 22, 23, AND 24. ALL ENGINE PARAMETERS AND VIBRATION CHECKS NORMAL ON ENGINE RUN.Jun 6, 2005 · N380WL · Boeing 7373G7 · Engine (Turbine/Turboprop)SDR ASMF200506004Strut · leakingDURING OVERNIGHT SERVICE, WAS DETECTED AN HYDRAULIC LEAK IN SHOCK STRUT OF NOSE LANDING GEAR. THE SEALS WERE REPLACED BUT WHEN TAKING OUT THE PISTON, A BUSHING WAS DETECTED DAMAGED. THE SHOCK STRUT OF NOSE LANDING GEAR SEALS WERE REPLACED IAW MM 32-21-11, TESTJun 3, 2005 · N904AM · Boeing 737* · Main Landing Gear Strut/Axle/TruckSDR FX7A200500006Warning Light · illuminatedAPU FIRE WARNING SWITCH LIGHT ILLUMINATED AND FIRE WARNING. INDICATION AFTER TAKEOFF, SHUT DOWN APU AND PERFORMED FALCON AIR EMERGENCY PROCEDURES.Jun 2, 2005 · N371FA · Boeing 73733A · Fire DetectionSDR 103Seat Track · gougedCABIN RT OB SEAT TRACK HAS NUMEROUS GOUGES STA. 540 TO 727E. S/O 109001, N/R 22858May 27, 2005 · N312FL · Boeing 7373L9 · Fuselage, Seat/Cargo Attach FittingsSDR SB05064Light · inoperativeMAINTENANCE FOUND THE INTERIOR EMERGENCY EXIT LIGHT ASSEMBLY, FORWARD OF THE FORWARD SERVICE DOOR, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.May 26, 2005 · N515AU · Boeing 7373B7 · Emergency LightingSDR 2005UALA00480Skin · damagedRT AFT FUSELAGE SKIN REPLACEMENT NEEDS DOUBLER REMOVAL AND INSTALLATION AFTER AFT SKIN IS REPLACED. REMOVED THE DOUBLER, ACCOMPLISHED HFEC OF THE HOLES. FOUND NO CRACKS, FABRICATED AND INSTALLED STRUCTURAL FILLER, DOUBLER AND TRIPLER PER SRM 51-00-01.May 25, 2005 · N313UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2005UALA00473Odor · detectedACRID ELECTRICAL SMELL IN COCKPIT. NOT NOTED IN CABIN AND NO VISIBLE SMOKE. ELECTICAL SMELL IN FLIGHT DECK COULD ONLY BE SIMULATED WHEN TURNING ON WINDOW HEAT. REPLACED WINDOW HEAT SWITCH MODULE 69-37346-310 (MR30009). UNIT MR30009-9 WAS SENT TO SHOP 147. May 24, 2005 · N370UA · Boeing 737322 · Air Distribution SystemSDR 2005UALA00467Skin · punctured3-4 INCH DIAMETER HOLE PUNCTURED IN FUSELAGE SKIN ON RIGHT SIDE OF AIRCRAFT 6 FEET AFT OF RADOME AND 12 INCHES ABOVE NLG DOOR CUTOUT. SKIN IS ALSO DENTED 2 INCHES ABOVE PUNCTURE. THIS IS A MAJOR REPAIR INSTALLED DOUBLER AND TRIPLER PER SRM 53-10-01 FIG 211 DMay 20, 2005 · N383UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2005UALA00470Stringer · corrodedAFT PIT STA787+2 TO 787+4 STR 25L UPPER FLANGE IS EXFOLIATED LBL24-24. FABRICATED AND INSTALLED PARTS PER SRM 53-00-03.May 20, 2005 · N313UA · Boeing 737322 · Fuselage Main, Longeron/StringerSDR 99Skin · dentedNUMEROUS DENTS ON AFT CARGO DOOR SKIN AND CREASES ON THE REPAIR DOUBLER. S/O 269010, NR 22292May 19, 2005 · N953UA · Boeing 737522 · Cargo/Baggage DoorsSDR DL738050271Pneumatic System · contaminatedABORTED T/O FOR SMOKE IN COCKPIT AND CABIN. PERFORMED OIL CONTAMINATION REMOVAL FROM AIR COND AND PNUEM SYS. NO SMELL OF CONTAMINATION NOTED. RAN PACKS AND ENGS TO T/O. NO SMOKE NOTED.May 15, 2005 · N3742C · Boeing 737832 · Pneumatic Distribution SystemSDR SWAA051387Engine · making metalDURING SCHEDULED C4 CHECK, NR 1 ENGINE FWD SUMP CHIP DETECTOR HAD EXCESSIVE METAL DEBRIS. REMOVED AND REPLACED NR 1 ENGINE PER MM.May 12, 2005 · N318SW · Boeing 7373H4 · Engine (Turbine/Turboprop)SDR AU510002100Antenna · brokenNR 2 VHF ANTENNA BROKEN IN HALF. BROKEN SECTION MISSING. SUSPECT CAUSED BY FOD.May 11, 2005 · Boeing 73776N · VHF Communications SystemSDR AU510001548Bearing · failedHYDRAULIC SYSTEM `B` NR 1 ELECTRIC HYDRAULIC PUMP FAILED. NIL PRESSURE AND METAL CONTAMINATION. INVESTIGATION FOUND THE FAILURE WAS DUE TO FAILURE OF THE PRE-MOD SB 57186-29-291 TRUNNION NEEDLE BEARING P/N 21830.May 7, 2005 · Boeing 7377Q8 · Hydraulic Pump (Electric/Engine), MainSDR AU510001558Compressor Wheel · wrong partNR 2 ENGINE FAN BLADE PLATFORMS NR 1 AND NR 4 LOCATED OPPOSITE NR 13 AND NR 16 FAN BLADES WERE NOT CHANGED WHEN NR 13 AND NR 16 FAN BLADE PLATFORMS WERE CHANGED AS DIRECTED BY SB CFM56-7B-0353. NR 13 AND NR 16 FAN BLADE PLATFORMS WERE CHANGED TO P/N 340-001-8May 7, 2005 · Boeing 737800* · Turbine Engine Compressor SectionSDR SWAA051354Engine · making metalDURING SCHEDULED RON CHECK, NR 1 ENGINE FWD SUMP CHIP DETECTOR HAD EXCESSIVE METAL & PHENOLIC DEBRIS. REMOVED AND REPLACED NR 1 ENGINE PER MM.May 6, 2005 · N684WN · Boeing 7373T0 · Engine (Turbine/Turboprop)SDR 2005UALA00410Hinge Fitting · mismanufacturedUNABLE TO ADJUST GAP ON R1 DOOR. MAJOR REPAIR ACCOMPLISHED. REPLACED UPPER BODY HINGE FITTING HOUSING AND INSTALLED WEB REPAIR.May 5, 2005 · N311UA · Boeing 737322 · Fuselage, Door HingeSDR U30A200500003Structure · damagedDURING POST FLIGHT, DAILY INSPECTION, GROUND EQUIPMENT INDUCED DAMAGE WAS FOUND TO LOWER AFT CORNER OF L2 (LT AFT PAX/CREW ) DOOR. MAINTENANCE INSPECTED THE DOOR IAW SRM. MAINTENANCE ALSO PERFORMED A HFEC (HIGH FREQUENCY EDDY CURRENT) INSPECTION IN COMPLIANCEMay 5, 2005 · N260AV · Airbus A320214 · Passenger/Crew DoorsSDR DHL2005809003O-Ring · leaking1+ 12 HR INTO FLT NR 1 ENG LOST OIL QUANTITY WITH RESULT OF LOW OIL PRESS PERFORMED ABNORMAL PROCEDURE AND ENG SHUT DOWN. REPLACED O-RING AT STARTER CASE. PER DC-8 M/M 80-10-02 OPS CHECK NORMAL ON RUNS PER JRH CH 13, P/N M83248-1-160.May 4, 2005 · N809DH · Doug DC873F · Turbine Engine Oil SystemSDR 2005UALA00407Floorbeam · corrodedAFT CABIN FLOORBEAM CORROSION STA 947 LBL 15 TO 44. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION, FABRICATED REPAIR ANGLE AND INSTALLED.May 4, 2005 · N312UA · Boeing 737322 · Fuselage Internal Mounting StructureSDR 2005UALA00408Frame · crackedFUSELAGE FRAME IS CRACKED AT STA 616 BELOW STR 17R. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE AND INSTALLED ANGLE DOUBLER.May 4, 2005 · N314UA · Boeing 737322 · Fuselage Main, FrameSDR 2005UALA00403Connector · burnedACCOMPLISHING TEST OF CROSSFEED VALVE, FOUND VALVE INOP AND ELECTRICAL CONNECTOR TO VALVE BURNED. FUEL CROSSFEED VALVE LIGHT ILLUMINATED BRIGHT IN ALL SWITCH POSITIONS. REPLACED FUEL CROSSFEED VALVE MOTOR ACTUATOR ASSEMBLY V39 AND CONNECTOR D792. REMOVED ACMay 2, 2005 · N383UA · Boeing 737322 · Fuel Transfer Valve
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