CFM International CFM56-3B2

Service difficulty reports · 635

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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 = 'CFM563B2'
  ORDER BY difficulty_date DESC"

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SDR USAASB08116Compressor · leakingON TAKEOFF FROM ORD, EN ROUTE TO CLT, CREW REPORTED A STRONG ODOR WITH SMOKE DETECTORS SOUNDING OFF. NO VISUAL INDICATION OF SMOKE WAS NOTED. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT CLT. CLT MAINTENANCE FOUND OIL RESIDUE IN APU DISTRIBUTION DUCT. CLEANEDNov 23, 2008 · N430US · Boeing 7374B7 · Turbine Engine Compressor SectionSDR DU4R2008203Floorbeam · corrodedS/O 312001 N/R 28019, CORROSION AT CABIN FLOORBEAM UPPER CHORD UPPER SURFACE BS 360 LBL 15 TO RBL 15 W/L 201.May 11, 2008 · N742VA · Boeing 737448 · Fuselage Main, Floor BeamSDR DU4R2008194Structure · corrodedS/O 312001 OPS NR 24701, CORROSION OUT OF LIMITS ON L-1 DOOR LOWER INNER CHORD AT BS 328, LBL 58 TO LBL 60.May 5, 2008 · N742VA · Boeing 737448 · Passenger/Crew DoorsSDR DU4R2008197Frame · crackedS/O 312001 OPS NR27954 - FLIGHT COMPARTMENT HAS CRACK AT MAIN FRAME BS 188 - 196 LT FLOOR LEVEL (CRACK AT RADIUS) OB CHORD W/L 208.May 5, 2008 · N742VA · Boeing 737448 · Fuselage Main, FrameSDR DU4R2008198Frame · crackedS/O 312001 OPS NR 27955 - FLIGHT COMPARTMENT HAS CRACK AT SHEAR WEB FRAME BS 188 - 196 LT FLOOR LEVEL (CRACK EMANATING AT EDGE CUT OUT).May 5, 2008 · N742VA · Boeing 737448 · Fuselage Main, FrameSDR DU4R2008200Floorbeam · corrodedS/O 312001 N/R 24703 - CORROSION ON TOP OF FLOORBOARD IN GOUGE BS 312 LBL 52 TO LBL 8, AND NUMEROUS PLACES AT RBL 0 TO RBL-54.May 2, 2008 · N742VA · Boeing 737448 · Fuselage Main, Floor BeamSDR DU4R2008201Floorbeam · corrodedS/O 312001 N/R 24738 - CORROSION ON UPPER SURFACE OF FLOOR SUPPORT BEAM BS 328 RBL 16 - RBL 60.May 2, 2008 · N742VA · Boeing 737448 · Fuselage Main, Floor BeamSDR SWAA082193Engine · shutdownINFLIGHT SHUTDOWN/DIVERSION. NR 2 ENGINE FAILED DURING CLIMB THRU 33,000 FT. NO ABNORMAL INDICATIONS ON ANY ENGINE INSTRUMENT. FUEL WAS BEING TRANSFERRED FROM NR 1 TANK TO NR 2 TANK WHEN ENGINE FAILURE OCCURRED. PERFORMED VISUAL CHECK OF NR 2 ENGINE FUEL COApr 23, 2008 · N304SW · Boeing 7373H4 · Engine (Turbine/Turboprop)SDR SWAA081703Engine · failedDECLARED EMERGENCY / INFLIGHT SHUTDOWN / AIR TURNBACK. CLIMBING OUT OF DAL NR 1 ENGINE FAILED. REMOVED AND REPLACED NR 1 ENGINE PER MT.Mar 29, 2008 · N408WN · Boeing 7377H4 · Engine (Turbine/Turboprop)SDR SWAA080224Engine · malfunctionedAIR TURNBACK / DECLARED EMERGENCY / INFLIGHT SHUTDOWN. NR 1 ENGINE FAILURE ON CLIMBOUT OF SMF, NOTICED BURNING BIRD RESIDUE SMELL. POSSIBLY AS A RESULT OF BIRD STRIKE OR FROM PREVIOUS FLIGHT. APPROX 4500' MSL NR 1 ENGINE MADE LOUD BANGING NOISE. REMOVED ANJan 7, 2008 · N340LV · Boeing 7373K2 · Engine (Turbine/Turboprop)SDR GAIA07018OPApu · flamed outDURING CLIMBOUT, THE APU FLAMMED OUT AT FL 320. AND EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DEPARTURE. AN UNEVENTFUL LANDING WAS MADE. NOTE: NR 1 GENERATOR ON DMI. PERFORMED APU INSPECTION, NO DEFECTS NOTED. OPS CHECKED GOOD. AIRCRAFT RETURNEOct 30, 2007 · N108KH · Boeing 7373Y0 · APU Core EngineSDR SWAA073943Engine · making metalINFLIGHT SHTDOWN / DIVERSION / DECLARED EMERGENCY. VIBRATION NR 2 ENGINE FOLLOWED BY LOSS OF OIL QUANTITY AND PRESSURE. INSPECTED CHIP DETECTORS, FOUND FOD IN MIDDLE DETECTOR. REMOVED AND REPLACED NR 2 ENGINE PER MT.Aug 8, 2007 · N706SW · Boeing 7377H4 · Engine (Turbine/Turboprop)SDR SB07029Module · faultyIAD FLT1724, ON DESCENT, CREW REPORTED THERE WAS NO INDICATION OF GEAR EXTENSION (RED OR GREEN LIGHTS) WHEN LANDING GEAR HANDLE WAS PUT IN THE DOWN POSITION. CREW PERFORMED QUICK REFERENCE HANDBOOK PROCEDURES AND EXTENDED THE GEAR MANUALLY. STILL NO LIGHTS. FLApr 17, 2007 · N434US · Boeing 7374B7 · Flight Compartment LightingSDR SB07027Light · inoperativeMAINTENANCE REPORTED THE EMERGENCY LIGHT ON SEAT 20C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.Apr 12, 2007 · N405US · Boeing 737401 · Emergency LightingSDR CA070114002Bolt · cracked(CAN) ENGINE WAS INDUCTED INTO SHOP FOR SCHEDULED MAINTENANCE. DURING THE SHOP VISIT THE FAN DISK WAS REMOVED FROM THE FAN ASSEMBLY AND ROUTED FOR OVERHAUL. THE DISK ATTACH BOLTS (QTY 30) WERE ROUTED FOR NDT INSPECTION. FPI DETECTED ONE FAN DISK ATTACH BOLT WJan 12, 2007 · Turbine Engine Compressor SectionSDR AWXA200602126Skin · crackedMAJOR REPAIR - NR 4018731, FUSELAGE EXTERIOR SKIN CRACKED BETWEEN 2 EXISTING REPAIRS, AFT OF EMERGENCY EXIT LIGHT, BS 727E, S23R. REPAIRED FUSELAGE EXTERIOR SKIN CRACKED BETWEEN 2 EXISTING REPAIRS, AFT OF EMERGENCY EXIT LIGHT, BS 727E, S23R IAW SRM 53-00-01Dec 28, 2006 · N309AW · Boeing 7373G7 · Fuselage Main, Plate/SkinSDR SWAA065024Mechanism · faultyON TAKEOFF NR 1 ENGINE UNABLE TO MAINTAIN CLIMB N1 WITH NR 1 POWER LEVER FULL FORWARD. FOUND VBV NOT CLOSING ALL THE WAY. REMOVED AND REPLACED VBV MECHANISM AND VBV MOTOR PER MM.Dec 20, 2006 · N340LV · Boeing 7373K2 · Compressor Bleed ValveSDR USAA061454Skin · crackedSKIN AT STA 23R BETWEEN STA 727D AND 727E JUST AFT OF LIGHT. CUT OUT CRACK, FABRICATED DOUBLERS IAW SRM 53-00-01 DEFECT SIZE: .75 INCH.Dec 19, 2006 · N433US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAASB06112Splice · faultyPILOT REPORTED THE INTERIOR EMERGENCY LIGHTS AT SEATS 4C AND 8C WERE INOPERATIVE. MAINTENANCE SPLICED CONNECTION, FORWARD AND AFT, AT SEAT ROW 4 ABC. RELAMPED BOTH LIGHTS. OPERATIONAL CHECK GOOD.Nov 10, 2006 · N406US · Boeing 737401 · Light System WiringSDR AWXA200601851Intercostal · crackedMAJOR REPAIR - C-16 CHECK - NR 5935073, CRACKED INTERCOSTAL, BS 344 - BS 360, BL 0, WL 208. REPAIRED CRACKED INTERCOSTAL, BS 344 - BS 360, BL 0, WL 208 IAW SRM 51-70-11.Oct 25, 2006 · N311AW · Boeing 7373G7 · Fuselage Miscellaneous StructureSDR AWXA200601853Attach Angle · corrodedMAJOR REPAIR- C-16 CHECK - NR 5935066, CORROSION ON THE L2 DOOR CUT OUT SCUFF PLATE ATTACH ANGLE, BS 980, S17L. REPLACED THE L2 DOOR CUT OUT SCUFF PLATE ATTACH ANGLE, BS 980, S17L IAW SRM 51-40-02.Oct 25, 2006 · N311AW · Boeing 7373G7 · Fuselage Main, Attach FittingsSDR AWXA200601788Stringer Clip · crackedC-19 CHECK - NR 5928339, STRINGER TIE CLIP CRACKED, BS 727D, S22L. REPLACED STRINGER TIE CLIP, BS 727D, S22L IAW SRM 51-40-02, FIGURES 8 AND 12.Oct 20, 2006 · N313AW · Boeing 7373S3 · Fuselage Main, Attach FittingsSDR AWXA200601789Stringer Clip · crackedC-19 CHECK - NR 5928340, STRINGER TIE CLIP CRACKED, BS 727D, S23L. REPLACED STRINGER TIE CLIP, BS 727D, S23L IAW SRM 51-40-02, FIGURES 8 AND 12.Oct 20, 2006 · N313AW · Boeing 7373S3 · Fuselage Main, Attach FittingsSDR AWXA200601790Stringer Clip · crackedC-19 CHECK - NR 5928341, STRINGER TIE CLIP CRACKED, BS 727D, S24L. REPLACED STRINGER TIE CLIP, BS 727D, S24L IAW SRM 51-40-02, FIGURES 8 AND 12.Oct 20, 2006 · N313AW · Boeing 7373S3 · Fuselage Main, Attach FittingsSDR AWXA200601852Door Frame · corrodedMAJOR REPAIR - C-16 CHECK - NR 5935507, CORROSION ON THE L1 DOOR CUT OUT INNER CHORD, BS 310 - BS 345, LBL 70, WL 208. REPLACED THE L1 DOOR CUT OUT INNER CHORD, BS 310 - BS 345, LBL 70, WL 208 IAW SRM 51-40-02.Oct 18, 2006 · N311AW · Boeing 7373G7 · Fuselage Main, StructureSDR AWXA200601858Floorbeam · corrodedMAJOR REPAIR-C-16 CHECK - NR 5935515, CORROSION ON MAIN CABIN FLOORBEAM, BS 986, LBL 55. REPAIRED MAIN CABIN FLOORBEAM, BS 986, LBL 55 IAW AWA ER 03-5311-06296-TH1.Oct 18, 2006 · N311AW · Boeing 7373G7 · Fuselage Main, Floor BeamSDR AWXA200601854Floorbeam · corrodedMAJOR REPAIR - C-16 CHECK - NR 5935405, CORROSION ON MAIN CABIN FLOORBEAM, BS 986, RBL 27 - RBL 51.5, WL 208. REPAIRED MAIN CABIN FLOORBEAM, BS 986, RBL 27 - RBL 51.5, WL 208 IAW AWA ER 03-5311-06296-TH1.Oct 17, 2006 · N311AW · Boeing 7373G7 · Fuselage Main, Floor BeamSDR AWXA200601857Shear Web · corrodedMAJOR REPAIR-C-16 CHECK - NR 5935406, CORROSION ON RT AFT LAV AND GALLEY AREA FLOOR SHEAR WEB, BS 1014 - BS 1016, RBL 40, WL 208. REPLACED RT AFT LAV AND GALLEY AREA FLOOR SHEAR WEB, BS 1014- BS 1016, RBL 40, WL 208 IAW SRM 51-40-02.Oct 17, 2006 · N311AW · Boeing 7373G7 · Fuselage Miscellaneous StructureSDR AWXA200601711Skin · crackedMAJOR REPAIR-4DAY CHECK-NR 4057772, RT FUSELAGE AFT OF AFT CARGO DOOR HAS A CRACK (MARKED) AT STA 867 AND STR 23R. INSTALLED REPAIR DOUBLER RT FUSELAGE AFT OF AFT CARGO DOOR STA 867 STR 23R IAW SRM 53-00-01-2R 31 FIG 201 SHT 32.Oct 8, 2006 · N312AW · Boeing 7373S3 · Fuselage Main, Plate/SkinSDR AWXA200601712Skin · crackedPHX-MAJOR REPAIR-4DAY CHECK-NR 4057770, LT FUSELAGE AFT OF WTB AT LWR LAP SEAM HAS A CRACK AT STA 774 STR 25L AT LAP JOINT. REPAIRED LT FUSELAGE AFT OF WTB LAP SEAM STA774 STR25L IN REF TO SRM53-00-01-2R FIG201.Oct 8, 2006 · N312AW · Boeing 7373S3 · Fuselage Main, Plate/SkinSDR AWXA200601713Skin · crackedPHX-MAJOR REPAIR-4DAY CHECK-NR 4057771, LT FUSELAGE AFT OF WTB 8 IN. AFT OF PREVIOUS CRACK HAS ANOTHER CRACK AT STA 782 STR. 25L AT LAP JOINT. REPAIRED LT FUSELAGE AFT OF WTB AT LWR LAP SEAM STA 782 STR.25L IN REF TO SRM53-00-01 2R FIG201. SEE AWXA200601712 FOct 8, 2006 · N312AW · Boeing 7373S3 · Fuselage Main, Plate/SkinSDR AWXA200601714Wire · brokenPHX - EEL - DURING ROUTINE MAINTENANCE IT WAS DISCOVERED THAT ROW 13 EMERGENCY PATH LIGHT HAS BROKEN WIRE AT SPLICE. MX REPAIRED THE WIRE AT ROW 13 EMERGENCY ESCAPE PATH LIGHTS, OPS CHECK WAS GOOD.Oct 6, 2006 · N308AW · Boeing 7373G7 · Light System WiringSDR AWXA200601761Angle · crackedCRACKED FLOOR STABILIZER UPPER ATTACH ANGLE, BS 500D- BS 520, BL 0. REPLACED FLOOR STABILIZER UPPER ATTACH ANGLE, BS 500D - BS 520, BL 0 IAW SRM 51-40-02-0G FIG 8 AND 51-40-02, FIGS 12 AND 14.Oct 6, 2006 · N313AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200601760Crease Beam · corrodedCRACK AT LT CREASE BEAM SHEAR WEB, BS 617.5, LBL 64.53, WL 208.1. REPLACED LT CREASE BEAM SHEAR WEB, BS 617.5, LBL 64.53, WL 208.1 IAW SRM 51-40-02-0G PAR 4 PG 1 AND 2 FIGURES 3, 6, 7 AND 8 AND DWG 65-47973 SHEETS 6 AND 57.Oct 5, 2006 · N313AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200601759Frame · corrodedCORROSION ON AFT CARGO COMPARTMENT FRAME, BS 827 BETWEEN LBL 3.00 AND RBL 3.00. REPAIRED AFT CARGO COMPARTMENT FRAME, BS 827 BETWEEN LBL 3.00 AND RBL 3.00 IAW SRM 53-00-07-2R 5 FIG 201.Oct 3, 2006 · N313AW · Boeing 7373S3 · Fuselage Main, FrameSDR AWXA200601762Skin · debondedNR 4 SPOILER UPPER SURFACE HAS A DISBONDED AREA 55 INCHES FROM OB END. REPAIRED NR 4 SPOILER UPPER SURFACE IAW SRM 51-70-10-2R4, REPAIR 4, FIGURE 201.Oct 2, 2006 · N313AW · Boeing 7373S3 · SpoilersSDR AWXA200601786Stringer · crackedC-19 CHECK - NR 5931682, RT STRINGER 18A CRACKED, BS 727 AT IB FASTENER. REPAIRED RT STRINGER 18A, BS 727 IAW AWA ER 03-5314-06287-ES1.Oct 1, 2006 · N313AW · Boeing 7373S3 · Fuselage Main, Longeron/StringerSDR COOSDR060034Ballast · overheatedPAX CABIN LIGHT BALLAST OVERHEATED BURNING INSULATION BLANKET AT BS 328, STR 1. (K)Aug 25, 2006 · N161LF · Boeing 7377Q8 · Passenger Compartment LightingSDR 2006FA0000733Tube · damaged(REF: MDR NR MDR002/06) STRIP OF CORE ASSEMBLY NOTED FRETTAGE DAMAGE TO 3 LOCATIONS ON THE NR 3 POSITION FUEL NOZZLE DRAIN TUBE. THE DEEPEST WAS TO A DEPTH OF .016 INCH. THE ROUTE CAUSE OF THE FRETTAGE HAD BEEN DETERMINED AS CONTACT WITH RIVETS ON THE DEFLEJun 7, 2006 · Boeing 737300 · Turbine Engine Combustion SectionSDR SB06040Engine · failedPHL - FLT1447 - ON CLIMB-OUT FROM PHL, AT 12,000 FT, THE NR 2 ENGINE LOST THRUST AND WENT TO IDLE. PARTIAL THRUST CAME BACK BUT DECREASED AGAIN ON APPROACH. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT PHL. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND Apr 21, 2006 · N425US · Boeing 737401 · Engine (Turbine/Turboprop)SDR AWXA200600565Blades · damagedFLT CREW REPORTED THAT ON DESCENT HEARD A LOUD THUMPING WITH VIBRATION, WERE ABLE TO STOPPED THIS BY RETARDING THE NR 1 THROTTLE. F/A REPORTED FLAMES COMING OUT OF THE NR 1 ENG TAIL PIPE. CREW REQUESTED A PRIORITY LANDING. LANDED IN IAH W/O FURTHER EVENT. Mar 23, 2006 · N315AW · Boeing 7373S3 · Turbine Engine Compressor SectionSDR USAA060378Rib · crackedFOUND CRACKED LOWER AFT LEG OF WBL 135.5 RIB. REMOVED DAMAGE, INSTALLED SHIMS AND REPAIR PARTS IAW EA 97418, DEFECT SIZE: 1.25 INCH.Mar 1, 2006 · N778AU · Boeing 7374B7 · Wing, Rib/BulkheadSDR USAA060386Intercostal · crackedAD 2005-20-03 INSP/REPAIR OF INTERCOSTALS FOUND CRACK COMMON TO MAIN ENTRY DOOR. REMOVED AND REPLACED CRACKED INTERCOSTAL WEB AND STRAP WITH FABRICATED PARTS IAW SRM 53-10-04 REPAIR DEFECT SIZE: .25.Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA060385Frame · crackedFOUND CRACK STA 807 BETWEEN S8L-9L AT OVERHEAD BIN LOWER ATTACH POINT. REMOVED AND REPLACED FRAME SUPPORT BRACKETS IAW TR 53-10-20C, DEFECT SIZE: 1 INCH.Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA060384Frame · crackedFOUND CRACK AT FRAME STA 827 BETWEEN S8L. FABRICATED FRAME REPAIR ANGLES AND INSTALLED PER T/R 53-10-20C, DEFECT SIZE: .125 INCH.Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA060383Bracket · crackedFOUND CRACKED PSU RAIL BRACKET AT RT BODY STA 480. REMOVED AND REPLACED PSU RAIL BRACKET WITH FABRICATED IAW TR 53-10-20C, DEFECT SIZE: .250 INCH.Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA060382Frame · crackedFOUND FRAME CRACKED LT BODY STA 480. REMOVED AND REPLACED PSU BRACKET WITH FABRICATED PARTS IAW TR 53-10-20C, DEFECT SIZE: .250 INCH.Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA060381Stringer · dentedFOUND DENT STA 550 S3R. REMOVED DAMAGED SECTION, SPLICED IN NEW STRINGER IAW SRM 53-00-03, DEFECT SIZE: 1.00 INCH.Mar 1, 2006 · N778AU · Boeing 7374B7 · Fuselage Main, Longeron/StringerSDR USAA060379Rib · crackedFOUND CRACK WBL 135.5 LOWER AFT LEG OF RIB. FABRICATED AND INSTALLED NEW T-SECTION IAW EA 97417, DEFECT SIZE: 1.5 INCH.Mar 1, 2006 · N778AU · Boeing 7374B7 · Wing, Rib/BulkheadSDR USAA060389Angle · corrodedFOUND CORROSION ON TRANSITION ANGLE STA 767-790 AT NUT PLATES. REMOVED CORROSION AND INSTALLED REPAIR PARTS IAW SRM 51-10-02, DEFECT SIZE: .250".Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
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