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.
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
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 IXXA05SMN216SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE LONGERON 17R CRACKED 1, STA 1786.000. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, EO SEMAN NR 20051286 DATED 09-27-05. REMOVED CRACKED LONGERON IAW SRM 53-5-1 FIG 7 (SHEET 1) ITEM B SRM 51-2-0 FIG 5 (SHEET 37).SDR IXXA05SMN217SLongeron · crackedDURING ROUTINE C-CHECK INSPECTION, AFT FUSELAGE LONGERON 17L CRACKED 1, STA 1786.000PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, EO SEMAN NR 20051285 DATED 09-27-05. REMOVED CRACKED LONGERON IAW SRM 51-1-20D. FABRICATED NEW LONGERON (EXTRUSION P/N S1616757) ISDR AALA20050622Oil System · contaminatedJFK INFLIGHT T1558/26 SEPT - LEFT ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. PERFORMED REQUIRED SHUTDOWN AND DIVERTED TO JFK. FOUND METAL IN OIL FILTER AND CHIP DETECTORS. CHANGED NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR 2005UALA01043Cabin Pressure · malfunctionedUNABLE TO HOLD PRESSURIZATION. REPLACED OVERHEAD CABIN PRESSURE SELECTOR REF MM21-31-25 AND CABIN PRESSURE CONTROLLER REF MM21-31-21 AND ACCOMPLISHED SYSTEM OPS TEST PER MM21-31-00 ALL CK OK. ALSO PRESSURIZED A-C MANUALLY UP TO 3.5 DIFFERENTIAL ALL CK OK.SDR 2005UALA01032Frame · crackedMID CABIN FRAME IS CRACKED AT FASTENER HOLE AT STA 727B NEAR STR 8L. ACCOMPLISHED A REPAIR PER MM 53-10-84, FABRICATED ANGLE, FILLER AND SUPPORT AND INSTALLED PER MM.SDR 2005UALA01038Light · tornEMERGENCY EXIT LIGHTING STRIP TORN NEAR AFT GALLEY. SUPPLEMENTAL DATA UPDATE, REPLACED LIGHT STRIP.SDR 2005UALA01040Fire Warning · will not testDURING PREFLT TEST, FIRE BELL DOES NOT RING ON ENG APU TEST OR CARGO TEST.SDR 2005UALA01025Skin · dentedAFT PIT DOOR EXTERIOR SKIN HAS DENTS. DAMAGE REMOVED, MANUFACTURED AND INSTALLED REPAIR PER SRM.SDR 2005UALA01026Crease Beam · corrodedAFT CABIN FLOOR STA 962 TO STA 1006 WL 208 RBL 54 RT CREASE BEAM CORRODED. REMOVED DAMAGE CREASE BEAM INNER CORD. MATCH DRILLED AND INSTALLED NEW CORD REF SRM 51-40-0 2.SDR 2005UALA01027Stringer Splice · crackedAFT CABIN CROWN STRINGER SPLICE IS CRACKED AT STA 907 STR 4R. REMOVED DAMAGED STRINGER SPLICE. ACCOMP HFEC INSPECTION ON EXISTING STRINGER SECTIONS. NO CRACKS FOUND. DRILLED UP NEW STRINGER SPLICE CHANNEL PN 65-51698-2 AND INSTALLED. REF SRM 51-40-02.SDR 2005UALA01028Frame · crackedAFT CABIN FRAME IS CRACKED AT STA 907 NEAR STR 8L. FABRICATED AND INSTALLED REPAIR PARTS WITH REF TO MM 53-10-84. FABRICATED NEW RAIL SUPPORT BRACKET.SDR 2005UALA01029Frame · crackedAFT CABIN FRAME IS CRACKED AT STA 787 NEAR STR 8L MARKED. FABRICATED ANGLE,FILLER & SUPPORT BRACKET PER MM 53-10-84 AND INSTALLED.SDR 2005UALA01030Frame · crackedAFT CABIN STA 867 FRAME IS CRACKED NEAR STR 8L. FABRICATED AND INSTALLED REPAIR PARTS WITH REF. TO MM CHAPT 53-10-84. FABRICATED NEW RAIL SUPPORT BRACKET.SDR 2005UALA01031Frame · crackedAFT CABIN FRAME IS CRACKED AT STA 827 NEAR STR 8L MARKED. FABRICATED AND INSTALLED ANGLE, FILLER AND SUPPORT PER MM 53-10-84SDR IXXA05SMN185SRivet · incorrectDURING ROUTINE C CHECK INSP, FUSELAGE BELLY, STA FS 76.000 L-35. 75R. UPGRADE REPAIR DOUBLER TO INCORP A MINIMUM OF 3 ROWS OF RIVETS. PERFORMED REPAIR IAW NR 05446 DATED 10-05-05, DWG NR ED-4058 DATED 09-27-05, EO NR 20051191 DATED 10-05-05. REMOVED EXISTINGSDR IXXA05SMN186SRivet · improperDURING ROUTINE C CHECK INSPECTION, FWD LOWER FUSELAGE BELLY, STA FS 173.000 L-35.5R. UPGRADE EXTERNAL REPAIR DOUBLER TO INCORPORATE A MINIMUM OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR, REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21. REMOVED DAMAGED SECTIOSDR IXXA05SMN191SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, VERT STAB DELAMINATED SKIN ON RUDDER TAB. REMOVED DAMAGED SECTION PLUS FABRICATED DOUBLER (AL2024T3 0.012) IAW SRM 55-2-2 PARA 2. BONDED CORE PLUS DOUBLER WITH HYSOL IAW SRM 51-1-9. REFER TO NR 2801 FOR WEIGHT.SDR IXXA05SMN192SDoor · crackedDURING ROUTINE C CHECK INSPECTION, LT WING NR 2 ALT TANK 506B ACCESS DOOR CRACKED. REMOVED AND REPLACED CRACKED ACCESS DOOR NR 506 B (NR 2 ALT TANK) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE) REFER TO JC 99116 FOR LEAK CHECK.SDR IXXA05SMN193SSkin · crackedDURING ROUTINE C CHECK INSPECTION, LT WING. UPPER SKIN AROUND HILOK CRACKED, XRS 72.000 S.9PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 17, EO SEMAN NR 20051211 DATED 09-21-05. REMOVED FASTENERS IAW SRM . REMOVED DAMAGED SECTION IAW SRM 57-2-1 FIG 17. PERFORMSDR IXXA05SMN194SCap · crackedDURING ROUTINE C CHECK INSPECTION, MID ACCY CMPT. CAP CRACKED 1, STA 680.000 BETWEEN L 27 AND L 28LPERFORMED MAJOR REPAIR IAW SRM 53-2-5 FIG 14, EO SEMAN NR 20051313 DATED 09-30-05. REMOVED FASTENERS IAW SRM 51-1-20D PG 1. STOP DRILLED ON CRACK END IAW SRMSDR IXXA05SMN195SSkin · crackedDURING ROUTINE C CHECK INSPECTION, LT WING IB AILERON UPPER PLATING CRACKED 1, XA 502.000 PERFORMED MAJOR REPAIR IAW SRM 57-7-0 FIG 1, SRM 57-8-1 FIG 1, EO SEMAN NR 20051336. REMOVED DAMAGED PLATING IAW SRM 51-1-21. FABRICATED NEW PLATING (AL7075T6 0.040) SDR ASAA0540495Floor Support · crackedPAE - FLOOR SUPPORT CRACKED AT FRAME FASTENERS. REPAIRED CRACKED FLOOR SUPPORT IAW SRM. (K)SDR IXXA05SMN182SDoor · crackedDURING ROUTINE C CHECK INSP, FWD ENTRANCE DOOR.- JAMB FWD LWR CORNER CRACKED, STA 130.000 L-21L.PERFORMED MAJOR REPAIR IAW AD 2000-20-08, S/B 53-075, SRM 53-2-0 FIG 15 SHEET 2, SRM 53-2-0, TR NR 53-196, MFG DWG NR SRD8530021, EO NR 20051204 DATED 09-21-05, DSDR IXXA05SMN183SSkin · crackedDURING ROUTINE C CHECK INSPECTION, NOSE SECTION. RT PRIMARY HEAT EXCHANGER AFT LWR CORNER HAS STRUCTURAL MODIFICATION CRACKED .7500 ON DOUBLER STA 12.000 L-27R. PERFORMED MAJOR REPAIR IAW MM 53-30-09, EO SEMAN NR 20051205 DATED 09-21-05. REMOVED FASTENERS IAWSDR IXXA05SMN184SDoor · crackedDURING ROUTINE C CHECK INSP, EXTERNAL FUS. FREON SYS EXHAUST DOOR AFT UPPER CORNER CRACKED .5, STA 54.000 L-2/8L L29L. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 13 (SHEET 1, 5), TR NR 53-169, EO SEMAN NR 20051190 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLSDR AWXA200501179Cargo Track · corrodedDURING C18 CHECK, DISCOVERED CORROSION ON THE AFT CARGO COMPARTMENT RT TIE DOWN TRACK AT BS 945, BL 13.8R AND WL 158. MAINTENANCE TRIMMED OUT CORROSION ON TIE DOWN TRACK IAW (EO) NR 03-5300-05277-SS2. FABRICATED REPAIR ANGLES AND FILLERS IAW EO 03-5300-05277SDR DHL2005806541Bracket · corrodedITEM REF NR 041572: RT ELEVATOR SYSTEM 1EA BRACKET CORRODED STA -141.000. REMOVED AND REPLACED RT ELEVATOR SYSTEM BRACKET STA -141.000. TIGHTENED BOLT IAW MM 20-16-0 PG. 201. ADJUSTED ELEVATOR CONTROL CABLES IAW MM 27-30-0 PG. 512-513. REFER TO NR 041920 FOR OSDR DHL2005806540Bracket · corrodedITEM REF NR 041577: RT ELEVATOR SYSTEM, 1EA BRACKET CORRODED, STA -90.000. REMOVED AND REPLACED RT ELEVATOR SYS BRACKET AT STA -90.000. TIGHTENED BOLT IAW MM 20-16-0 PG. 201. ADJUSTED CONTROL CABLES IAW MM 27-30-0 PG. 512-513. OPS CHECKED SEE NR 041920SDR AU510002088Outflow Valve · faultyPRESSURIZATION SYSTEM PROBLEMS. INVESTIGATION FOUND INBOARD AND OUTBOARD POSITIVE PRESSURE RELIEF VALVES TO BE UNSERVICEABLE. BOTH VALVES REPLACED. OUTBOARD VALVE CURRENTLY CONSIDERED TO BE THE PRIMARY CAUSE OF THE CABIN DEPRESSURIZATION EVENT.SDR 2006FA0000505Bearing · wornBEARING IS FROM SNR PRODUCTION. ROLLER BEARING WAS SENT FOR AN INSPECTION. WE COULD ONLY PERFORM A LEVEL 1 INSPECTION, WITHOUT DISASSEMBLING THE INNER RING, CAGE AND ROLLERS. DURING THE INSPECTION OF THE BEARING, NOTICED SOME HEAVY WEAR TRACES AND MARKS ON SDR AU510001838Hose · leaking(AUS) RT ENGINE DRIVEN HYDRAULIC PUMP TO PYLON QUICK DISCONNECT PRESSURE HOSE LEAKING.SDR AU510001722Cable · misroutedLT LOWER ELEVATOR CONTROL CABLE INCORRECTLY ROUTED AT FUSELAGE FRAME LOCATED AT BS 1138. CABLE IS ROUTED OVER FRAME INSTEAD OF THROUGH LIGHTENEING HOLE. CABLE HAS CAUSED DAMAGE TO FRAME.SDR SWAA052707Fan Blade · shingledVIBRATION FELT THROUGHOUT FLIGHT - NOTICEABLY LOUD UPON LANDING DURING REVERSE THRUST OPERATIONS. FOUND SEVERAL FAN BLADES ON NR 2 ENGINE DAMAGED & SHINGLED. REMOVED AND REPLACED NR 2 ENGINE FAN BLADE SET PER MM.SDR DHL2005806534Fitting · crackedITEM REF NR 040974: FWD CARGO COMPARTMENT, FLOORBEAM FITTING CRACKED 0.250 IN, STA 280.000 BL 0 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED PRC SEALASDR 2005UALA00931Bulkhead · gougedAFT PRESSURE BULKHEAD HAS SEVERAL GOUGES AND SCRATCHES AT UPPER ELECTRICAL CONDUIT THROUGH LT SIDE LBL 5 TO LBL 3 WL 84.SDR 2005UALA00932Floorbeam · corrodedCABIN FLOOR BS 312 LBL 1 AND LBL 6 SMALL AREA OF CORROSION ON UPPER SURFACE OF FLOORBEAM.SDR 2005UALA00925Power Supply · inoperativeTHE FOLLOWING EMERGENCY LIGHTS ARE INOP: EEL LIGHTS AFT OF ROW 14, SLIDE LIGHT DOOR 2L. EXIT SIGN DOOR 2R, AFT ENTRY EXIT SIGN, AISLE LIGHT ROW 17. REPLACED POWER SUPPLY AND BATTERY.SDR DHL2005806517Doubler · crackedPRIMARY HEAT EXCHANGER AFT LWR CORNER ACS STRUCTURAL MODIFICATION DOUBLER CRACKED 0.75 IN STA -12.000 L-27L (MAJOR REPAIR). REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGE SECTION IAW DWG NR U80-R19. PERFORMED DETAIL VISUAL INSP OF REWORKED AREA. NO CRACK ORSDR DHL2005806514Doubler · crackedITEM REF. NR. 040957: PRIMARY HEAT EXCHANGER AFT LWR CORNER ACS STRUCTURAL MODIFICATION DOUBLER CRACKED 0.750 IN STA -12.000 L-27R. DWG U80-R18 REV. IR DATED 08-08-05. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW DWG U80-R18. PSDR ASAA0540433Frame · dentedFWD CARGO BAY, BSTA 440, RBL 22, WL 156, FRAME IS DENTED AT FASTENER. TRIMMED OUT DAMAGE AND INSTALLED REPAIR IAW EA. (K)SDR ASAA0540434Bulkhead · corrodedCORROSION ON AFT PRESSURE BULKHEAD C-CHANNEL. REMOVED DAMAGED SECTION OF AFT PRESSURE BULKHEAD AND VERTICAL STIFFENER, FABRICATED REPAIR PARTS AND INSTALLED IAW EA. (K)SDR 2005UALA00913Door Frame · corrodedR1 DOOR FRAME STA 296 RBL 54 CORRODED, S17R, WL 208.SDR 2005UALA00914Shear Tie · dentedEXTERNAL FUSELAGE STA 807 BETWEEN 28L AND 28R HAS A DENT AND SHEAR TIE BENT AT RADIUS.SDR 2005UALA00892Stringer · crackedSTR 10L UPR FLANGE IS CRACKED AT STA 294.SDR 2005UALA00893Door Frame · corrodedFWD GALLEY DOOR STUB FRAME AT STA 296 AND RBL 54 CORRODED AT STRINGER S-17R AND WL 208.SDR 2005UALA00844Skin · puncturedPUNCTURE OF SKIN BELOW AND AFT OF DOOR 2R.SDR 2005UALA00848Skin · damagedEXTERNAL FUSELAGE STA 434 STR 2R BLENDED SKIN AROUND A FASTENER IS DAMAGED.SDR 2005UALA00845Floor Support · corrodedCABIN FLOOR SUPPORT AT AFT ENTRY DOOR HAS CORROSION STA 957-986 LBL 62.5 WL 208 AND LBL 63.0 WL 208.SDR 2005UALA00846Angle · corrodedAFT GALLEY DOOR THRESHOLD ZEE ANGLE CORRODED STA 978 TO 984 RBL 62.5 STR 17 WL 208.SDR 2005UALA00847Structure · dentedAFT CARGO DOOR HAS SEVERAL OVERLAPPING DENTS AND SKIN IS DAMAGED ON FWD SIDE. INSTALLED A REPAIR DOUBLER 53 BY 48 INCHES REF SRM 52-00-01 AND SRM 51-00-01 FIG 202.
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