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 2006UALA01302Wire · inoperativeFOUND AFT CABIN EEL LIGHTS INOP FROM ROW 15 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT. REPLACED EEL TRACK CABLE.Jul 2, 2006 · N341UA · Boeing 737322 · Light System WiringSDR 2006UALA01307Angle · corrodedFOUND PASSENGER CABIN STA 260 TO STA 342 WL 208 RBL 54" TO RBL 60" Z ANGLE IS CORRODED IN SEVERAL AREAS CORROSION TASK NR C53-107 -02. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR ANGLE AND WEB.Jul 2, 2006 · N941UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA01308Odor · detectedFOUND ELECTRIC ODOR REPORTED FROM AFT F-A JUMPSEAT. UNDETERMINABLE. UNABLE TO DUPLICATE ELECTRICAL ODOR. REPLACED BOTH COALESCER BAGS.Jul 2, 2006 · N922UA · Boeing 737522 · Air Distribution SystemSDR 2006UALA01297Skin · dentedFOUND UPPER FUS EXT SKIN PREVIOUSLY INSTALLED RIVET DENTED THE SKIN BS 767 +4" S5R+4". MAJOR REPAIR, REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER.Jun 30, 2006 · N333UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2006UALA01298Skin · dentedFOUND UPPER FUSELAGE SKIN BS 845 S5R+7 PREVIOUSLY INSTALLED RIVET DENTED THE SKIN AND SKIN HAS TOOLING MARKS. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER.Jun 30, 2006 · N333UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2006UALA01299Skin · dentedFOUND UPPER FUS EXT SKIN BS 820 S5R+7.5" PREVIOUSLY INSTALLED RIVET SKIN IS DENTED AND HAS TOOLING MARK. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER.Jun 30, 2006 · N333UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2006UALA01300Skin · lightning strikeFOUND UPPER FUSELAGE SKIN BS 663 S5R+7" RIVET HAS LIGHTNING STRIKE. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER, TRIPLER AND FILLER.Jun 30, 2006 · N333UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR ASMF200606018Thrust Reverser · failedAIRCRAFT RETURNED TO PLATFORM (R ENGINE REVERSE) LIGHT TURNED ON AT P5. CAPTAIN PERFORMED 4 REVERSE CYCLES BUT FAIL CONTINUED. BITE TO EAU MODULE WAS PERFORMED AND REVERSE FAIL CODE APPEARED, THEREFORE, REVERSE WAS DEFERRED IAW MEL 78-1. DURING OVERNIGHT CHECKJun 28, 2006 · N997AM · Boeing 737* · Engine (Turbine/Turboprop)SDR 2006UALA01226Skin Panel · crackedSKIN APPEARS TO BE CRACKED ABOVE STRINGER ON LEFT SIDE OF FUSELAGE ABOVE AND AFT OF REPAIR SURROUNDING EMERGENCY EXIT LIGHT AFT OF WING TRAILING EDGE. REMOVED DAMAGE. ACCOMPLISHED DOUBLER-TRIPLER FILLER SKIN LAP REPAIR.Jun 22, 2006 · N377UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2006UALA01234Crease Beam · corrodedR2 DOOR CREASE BEAM ANGLE CORRODED FROM STA 947.5 TO STA 1006 BL 48R WL 208 ZONE 2414.Jun 22, 2006 · N936UA · Boeing 737522 · Fuselage Main, StructureSDR 2006UALA01232Wire · unknownAFT CABIN EEL LIGHTS INOP FROM ROW 15 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT.Jun 21, 2006 · N347UA · Boeing 737322 · Light System WiringSDR 2006UALA01233Lamp · inoperativeOFF WING EMERGENCY LIGHT AFT OF RT WING INOP. LAMP INOPERATIVE.Jun 21, 2006 · N347UA · Boeing 737322 · Emergency LightingSDR 2006UALA01211Bulkhead · crackedLT MLG WW BULKHEAD BEADED WEB PANEL IS CRACKED AT BS 665 LBL31 WL 202.Jun 20, 2006 · N339UA · Boeing 737322 · Fuselage Main, BulkheadSDR 2006UALA01212Crease Beam · corrodedFWD GALLEY DOOR CREASE BEAM CORRODED SEVERAL AREAS AT BS 294 - BS 360 RBL 55 - RBL 57 STR 17R.Jun 20, 2006 · N339UA · Boeing 737322 · Fuselage Main, StructureSDR 2006UALA01215Light · inoperativeEMERGENCY EXIT LIGHT STRIP AT AFT GALLEY FLOOR INOP.Jun 20, 2006 · N311UA · Boeing 737322 · Emergency LightingSDR 2006UALA01210Slide · disconnectedFWD SERVICE DOOR SLIDE FELL OUT. KNOWN CLAMSHELL CONTAINER HINGE ASSEMBLY ISSUE. REINSTALLED SLIDE PACK. AN ACTIVE COA CURRENTLY REPLACES THE HINGES AT 36 MONTH SLIDE OVERHAUL.Jun 19, 2006 · N933UA · Boeing 737522 · Escape SlideSDR 2006UALA01197Oil System · overheatedDIVERTED TO GJT DUE TO NR 1 ENGINE OIL TEMP. FUEL BYPASS VALVE FAILED. THE RESULT WAS THE COLD FUEL WAS BYPASSED AND NEVER WENT TO THE BAFFLES TO COOL THE HOT OIL. REPLACED MAIN OIL FULE HEAT EXCHANGER.Jun 17, 2006 · N922UA · Boeing 737522 · Turbine Engine Oil SystemSDR 2006UALA01192Intercostal · crackedCRACKS WERE FOUND AT THE INTERCOSTALS AT BS 294 NEAR STR 7L AND STR 10L.Jun 16, 2006 · N938UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA01193Skin · gougedFUSELAGE SKIN GOUGED AT FWD CARGO DOOR CUT-OUT AT ABOUT STR 23R.Jun 16, 2006 · N938UA · Boeing 737522 · Fuselage Main, Plate/SkinSDR 2006UALA01195Socket · corrodedEEL LIGHT OUTSIDE FWD SERVICE DOOR IS INOP.Jun 16, 2006 · N349UA · Boeing 737322 · Emergency LightingSDR 2006UALA01183Skin · damagedSKIN DAMAGE WAS FOUND BETWEEN STA 917 TO 939 BETWEEN STR 25L AND 26L.Jun 15, 2006 · N314UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2006UALA01184Skin · damagedSKIN DAMAGE WAS FOUND FROM STA 901 TO 919 BETWEEN STR 27L AND 26L.Jun 15, 2006 · N314UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2006UALA01188Skin · damagedAFT PIT DOOR CUTOUT, AFT SIDE AT S20R LAP, SKIN IS BLENDED BACK TO 15-32" (.468) AND BONDED DOUBLER TO .250.Jun 15, 2006 · N936UA · Boeing 737522 · Fuselage Main, Plate/SkinSDR 2006UALA01189Frame · crackedCABIN FRAME CRACKED OUT OF STRINGER PASS THROUGH CUTOUT BS 663, STR 2R.Jun 15, 2006 · N936UA · Boeing 737522 · Fuselage Main, FrameSDR UPS06847121O-Ring · damagedNR 3 ENG OIL PRESSURE DROPPED TO 15 PSI AND LIGHT ILLUMINATED THEN WENT OUT WITH OIL QTY DECREASING TO 8 QTS INITIALLY THEN CONTINUED TO 6 QTS. INFLIGHT ENG SHUT DOWN ACCOMPLISHED IAW CHECKLIST. WINDMILL TIME 25 MINUTES W/ POSITIVE OIL PRESSURE. PER PILOT RJun 14, 2006 · N700UP · Doug DC871F · Turbine Engine Oil SystemSDR ASMF200606007Engine · failedAIRCRAFT RETURNED TO PLATFORM, DURING RT ENGINE STARTING (REVERSE) LIGHT TURNED ON. DURING TRANSIT CHECK BOTH REVERSES WERE RESEATED IN STOW AND DEPLOY POSITION OF RT EDU AND FIM 78-31 PROCEDURE, TASK 801WAS PERFORMED, TESTED CORRECT. DEFERRED REPORT WAS CLOSEJun 14, 2006 · N853AM · Boeing 737* · Engine (Turbine/Turboprop)SDR SWAA062072Engine · malfunctionedAIR TURNBACK. ON DEPARTURE NR 2 ENGINE WOULD NOT ACCELERATE ABOVE 60 PERCENT N1, TURNING PMCS ON AND OFF MADE NO DIFFERENCE. REMOVED AND REPLACED ENGINE MEC PER MM.Jun 14, 2006 · N317WN · Boeing 7373Q8 · Fuel Controlling SystemSDR 2006UALA01181Frame · crackedLT FUSELAGE STA 380 AND 907 BETWEEN STRINGER 8L AND 9L AT STOW BIN RAIL SUPPORT, FASTENER HOLE HAS A CRACK ON THE FRAME.Jun 14, 2006 · N936UA · Boeing 737522 · Fuselage Main, FrameSDR 2006UALA01182Intercostal · crackedCRACKS WERE FOUND AT THE INTERCOSTAL WEBS AT BS 294 NEAR STR 7L AND 16L AND AT THE INTERCOSTAL CLIP BETWEEN STA 348-360 AT STR 11L.Jun 14, 2006 · N937UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA01209Cabin Pressure · failedAIRCRAFT LOST CABIN PRESSURE UPON DESCENT INTO DEN. DUE TO MULTIPLE SYMPTONS OF A POSSIBLE AIR GROUND ISSUE, M990 AND S105 WERE REPLACED.Jun 14, 2006 · N366UA · Boeing 737322 · Cabin Pressure Control SystemSDR 2006UALA01179Fitting · misdrilledAFT PIT BODY FRAME UPPER FITTING IS MISDRILLED AT FLOOR SUPPORT Z ANGLE INBOARD FASTENER BS 787, S25L-S26L, WL156.Jun 13, 2006 · N937UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA01180Skin · gougedAFT PIT DOOR CUTOUT EXTERNAL SKIN EDGE IS GOUGED BS 845 S21R-S23R.Jun 13, 2006 · N937UA · Boeing 737522 · Fuselage Main, Plate/SkinSDR 2006UALA01150Frame · bentAFT PIT, BS 827 BETWEEN STRINGERS 24L AND 25L FRAME BENT ON INNER FRAME RADIUS.Jun 12, 2006 · N936UA · Boeing 737522 · Fuselage Main, FrameSDR 2006UALA01151Attach Fitting · corrodedFOUND VERTICAL STAB ATTACH FITTINGS, AFT PRIMARY FITTINGS, RT AFT, RT FWD, LT AFT FITTING DRAG ANGLES CORRODED.Jun 12, 2006 · N937UA · Boeing 737522 · Fuselage, Stabilizer Attach FittingsSDR 2006UALA01140Attach Fitting · corrodedFOUND VERTICAL STAB BS 1088 LT AND RT PRIMARY FUSELAGE ATTACH FITTINGS CORRODED ON FWD AND AFT FACES.Jun 11, 2006 · N938UA · Boeing 737522 · Fuselage, Stabilizer Attach FittingsSDR 2006UALA01135Frame · crackedFOUND FWD CABIN FRAMES AT STA 400 AND 440 BETWEEN STR 8R AND 9R FRAME CRACKED.Jun 10, 2006 · N937UA · Boeing 737522 · Fuselage Main, FrameSDR 2006UALA01136Clip · crackedAFT PIT FLOOR KEEL BEAM IB CLIP IS CRACKED AT BS 727 AFT STR 27R WL 153.Jun 10, 2006 · N937UA · Boeing 737522 · Fuselage Main, KeelSDR 2006UALA01137Door Frame · crackedFOUND FWD GALLEY DOOR AFT LOWER STOP FRAME IS CRACKED OUT OF FASTENER HOLE IN 3 LOCATION MARKED.Jun 10, 2006 · N937UA · Boeing 737522 · Fuselage Main, StructureSDR 2006UALA01138Shear Tie · crackedFOUND CABIN BODY FRAME SHEAR TIE IS CRACKED BS 360 DIRECTLY BELOW STR 13L MARKED.Jun 10, 2006 · N937UA · Boeing 737522 · Fuselage Internal Mounting StructureSDR 2006UALA01139Frame · crackedFOUND PASSENGER CABIN OVERWING FRAME CHORD WEB AT BS 616R WL 202 CRACKED.Jun 10, 2006 · N937UA · Boeing 737522 · Fuselage Main, FrameSDR 2006UALA01132Skin · dentedFOUND FUSELAGE SKIN DENTED AT STA 927 BETWEEN STR 16R AND 17R.Jun 9, 2006 · N937UA · Boeing 737522 · Fuselage Main, Plate/SkinSDR 2006UALA01133Angle · corrodedFOUND FWD GALLEY DOOR LWR THRESHOLD INNER CHORD "L" ANGLE CORRODED AT STA 294 AND 328.Jun 9, 2006 · N938UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA01141Oil System · obstructedNR 1 ENGINE SHUTDOWN DUE TO LOW OIL PRESSURE, LOW OIL QUANTITY AND HIGH OIL TEMPERATURE. THE CAUSE WAS A RED PROTECTION CAP HAD NOT BEEN REMOVED AND BECAME LODGED IN A SUCTION PORT OF THE SCAVENGE VALVE. SERVICED OIL AND REPLACED LUBRICATION UNIT.Jun 9, 2006 · N305UA · Boeing 737322 · Turbine Engine Oil SystemSDR 2006UALA01003Light · inoperativeFOUND EXIT SIGN OVER DOOR 2R, AFT GALLEY CEILING EXIT SIGN, AND DOOR 2L SLIDE LIGHT INOP.May 24, 2006 · N398UA · Boeing 737322 · Emergency LightingSDR 2006UALA00998Skin · crackedFOUND AFT CARGO DOOR SN 1403 HAS A CRACK AT UPPER LEFT DOOR HANDLE CUTOUT.May 23, 2006 · N331UA · Boeing 737322 · Cargo/Baggage DoorsSDR 2006UALA00999Skin · crackedC1 AFT GALLEY DOOR UPPER HINGE CUTOUT CRACKED AT FWD UPPER CORNER STA 957 STR 14A, WL 253.May 23, 2006 · N332UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2006UALA00974Keelbeam · damagedRT WHEEL WELL KEELBEAM ATTACHED ANGLE HAD HOLE PREVIOUSLY DRILLED INTO AT BS 678.May 20, 2006 · N342UA · Boeing 737322 · Fuselage Main, KeelSDR AMTA200600346Warning Light · activatedNR 2 ENGINE CONTROL LIGHT CAME ON DURING ENGINE START. NO OTHER LIGHTS ASSOCIATED CAME ON. EEC BITE SHOWED MSG 75-20582. PERFORMED INIT EVAL IN FIM AND NO CURRENT OR RECENT FAULTS AFTER ACTUATORS TEST. CKD CONNECTORS AT EEC AND HMU AND RAN ENGINE TWICE, NOMay 20, 2006 · N319TZ · Boeing 73783N · Engine Indicating SystemSDR 2006UALA00971Crease Beam · corrodedFWD GALLEY DOOR CREASE BEAM INBD OF THRESHOLD FROM STA 294-340 HAS CORROSION.May 19, 2006 · N342UA · Boeing 737322 · Fuselage Main, StructureSDR 2006UALA00972Frame · crackedFWD GALLEY DOOR FWD AND AFT FRAMES CRACKED AT LOWER STOP FITTING MOUNT HOLE.May 19, 2006 · N342UA · Boeing 737322 · Cargo/Baggage Doors
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