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 2003UALA00811Stringer · crackedSTR 4 LT IS CRACKED BETWEEN RIVETS FROM STA. 917 TO 918. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SECTION AND SPLICE PIECES.SDR 2003UALA00805Light · inoperativeEEL LIGHTS INOP FROM ROW 19 AFT. REPLACED EEL LIGHT STRIPS AT ROWS 19-20.SDR 372PA0038Connector · dirtyAUTO PILOT B WILL NOT ENGAGE AND AUTO PILOT A IS INTERMITTENT. REMOVED DIRT FROM AUTO PILOT A AND AUTO PILOT B CONNECTORS. A AND B SYSTEMS TEST OK IAW MM 22-10-00.SDR AUS20031076Fire Detector · inoperative(AUS) NR 1 ENGINE FIRE DETECTOR SYSTEM INOPERATIVE.SDR 2003UALA00809Attach Fitting · corrodedVERTICAL STAB RIGHT O/B ATTACH LOG AND BOLT CORRODED. MAJOR REPAIR ACCOMPLISHED. REWORKED STAB ATTACHED LOG.SDR 2003UALA00803Shear Tie · crackedCRACK IN STR 11R FRAME ANGLE AT BS 706. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP.SDR 2003UALA00791Shear Tie · crackedCRACK IN STRINGER-FRAME SHEAR TIE AT BS 663.75. MAJOR REPAIR ACCOMPLISHED. REPLACED STR SHEAR CLIP.SDR 2003UALA00801Shear Tie · crackedCRACK IN STR FRAME SHEAR TIE AT BS 663.75. MAJOR REPAIR ACCOMPLISHED. REPLACED STR SHEAR CLIP.SDR 2003UALA00802Shear Tie · crackedSHEAR TIE AT STA 639 BELOW STR 7 LT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE.SDR 2003UALA00796Wire · damagedEEL LIGHTS INOP IN AFT CABIN FROM ROWS 15 - 21. REPLACED FEEDER CABLE FROM ROWS 15-21.SDR 2003UALA00800Stringer Clip · crackedSTA 663 AT STR 10L STRINGER CLIP IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP.SDR 2003UALA00795Light · inoperativeAFT GALLEY EEL STRIP INOP. REPLACED AFT GALLEY EEL STRIP.SDR CALA0300606Panel · corrodedAFT CARGO PIT LEFT TRANS PANEL CORRODED AROUND FASTENERS MARKED (STA 847 - 947). FABRICATED AND INSTALLED NEW TRANS PANEL IAW SRM 53-00-01.SDR CALA0300607Panel · corrodedRT TRANS PANEL CORRODED BETWEEN STA 727 AND 767. FABRICATED AND INSTALLED NEW TRANS PANEL IAW SRM 53-60-53.SDR CALA0300604Panel · corrodedCORROSION ON LEFT TRANSITION PANEL FROM STA 727E TO 767. FABRICATED AND INSTALLED NEW PANEL IAW SRM 53-60-53.SDR CALA0300605Strap · corrodedAFT CARGO DOOR STRAP ON TO OF WEB AT STA 773 - 859 CORRODED. REMOVED OLD STRAP. INSTALLED NEW STRAP IAW SRM 51-40-02.SDR CALA0300608Oven · malfunctionedSMOKE IN FLIGHT DECK. REMOVED AND REPLACED OVEN.SDR U30A200300036Warning Light · false activationDURING CRUISE ON FLT 143 PUJ-BWI, THE LT AFT EMERGENCY WINDOW EXIT SHOWED ARMED ON ECAM (ABOVE FL 250). NO CHANGE IN CABIN ALTITUDE. ON GROUND, MAINTENANCE VERIFIED THAT THE PROX SENSOR AT THE LT AFT EMERGENCY EXIT HATCH ACCESS COVER TO BE OPERATIONAL IAW AMM SDR CALA0300603Web · corrodedAFT CARGO PIT CORROSION AROUND FASTENERS AT DOOR THRESHOLD WEB. REMOVED AND REPLACED WEB IAW SRM 51-40-02.SDR 2003UALA00781Control Cable · obstructedCREW REPORTS THAT ELEVATOR BINDS WHEN PULLING CONTROL COLUMN BACK. STICKS AND BINDS TO THE POINT OF HAVING TO USE EXCESSIVE PRESSURE TO GO BACK TO NEUTRAL. FLIGHT CREW REPORTED THAT COLUMN WAS TOTALLY STUCK AT ONE POINT. DURING AN INSPECTION OF THE ELEVATOR CSDR 2004FA0000006Spar · crackedCRACKED AT OB AFT FLAP TRACK LOWER ATTACH HOLES.SDR IXXA0300062OWarning Light · false indicationCREW REJECTED TAKE-OFF FROM KEWR WHEN BELLY DOOR OPEN LIGHT CAME ON DURING TAKE-OFF ROLL. LIGHT EXTINGUISHED AFTER REJECT. MAINTENANCE INSPECTED ALL DOORS AND SWITCHES IAW ALL APPLICABLE MANUALS AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.SDR SWAA032280Engine · failedENGINE SHUT DOWN, DECLARED EMERGENCY, AIR TURN BACK, NR 1 ENGINE FAILED. REMOVED AND REPLACED NR 1 ENGINE PER MM.SDR 2003UALA00774Lamp · inoperativeEEL LIGHTS INOP AT SEATS 15ABC. REPLACED EEL LAMPS.SDR CALA0300588Seat Track · corrodedINSPECTION FOUND CENTER FLOOR RAIL CORRODED AT TOP AND INSIDE CHANNEL AT FLOOR STRAP AFT OF STA 847. THE FLOOR RAIL WAS REPAIRED IAW ECRA 5320-01603.SDR DHL2003873012Striker · out of adjustAFTER DEPARTURE DOOR NOT LATCHED LIGHT ILLUMINATED AFTER GEAR RETRACTION. PERFORMED APPROPRIATE ABNORMAL PROCEDURE AND LIGHT WENT OUT AFTER CYCLING GEAR ONCE. PERFORMED BITE CHECK ON MAIN GEAR DOOR PROXIMITY BOX CHECKED GOOD, ADJUSTED RIGHT MAIN GEAR DOOR STRSDR CALA0300598Beltframe · corrodedFBB BELTFRAME AT STATION 500D HAS CORROSION OUTBOARD OF STRINGER S27L. INSTALLED REPAIR FBB BELTFRAME AT STATION 500D.SDR DHL2003805011Connector · damagedDURING CRUISE NR 1 FIRE LIGHT ILLUMINATED, WARNING BELL SOUNDED. PERFORMED PHASE ONE ITEMS LIGHT REMAINED ON (BLEW BOTH BOTTLES). DUMPED 19000 LBS. OF FUEL AND LANDED SAFE. R AND R NR 1 AND 2 ENG FIRE BOTTLES IAW MM 26-20-01. OPS CHECKED GOOD. NR 1 FIRE LOOP SDR 2003UALA00766Spar · crackedLT WING SPAR UPPER CHORD CRACKED AT MLG BEAM SUPPORT FITTING. MAJOR REPAIR ACCOMPLISHED. SPLICED NEW CHORD.SDR 2003UALA00767Access Panel · damagedLEFT WING INBOARD FLAP LOWER ACCESS PANEL 8407L DAMAGED AT ATTACH HOLE COUNTERSINK. MAJOR REPAIR ACCOMPLISHED. REPLACED PANEL.SDR AWXA200301255Bulkhead · crackedDURING C-17 CHECK A .5000 INCH CRACK WAS FOUND AT FASTENER HOLE ON BS 178 BULKHEAD VERTICAL WEB AT RBL 17.1, WL 234. MAINTENANCE CUTOUT CRACK ON VERTICAL WEB AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A NEW REPLACEMENT SECTION OF VERSDR CALA0300601Angle · crackedFLOOR SUPPORT ANGLE CRACKED AT STA 380 - 400 BL-0. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-40-02.SDR CALA0300602Strap · corrodedMAIN DECK FLOOR WEB STRAP HAS CORROSION AFT OF STA 1016. INSTALLED NEW STRAP PER SRM 51-40-02 AND 51-10-02.SDR AWXA200301275Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 967 TO BS 986.5, LBL 17.61. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED FLOOR SUPPORT AT BS 967 TO BS 986.5, LBL 17.61; FABRICATEDSDR AWXA200301279Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON FLOORBEAM AT BS 993, LBL 15 TO LBL 20.70. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF FLOORBEAM AT BS 993, LBL 15 TO LBL 20.70; FABRICATESDR CALA0300578Seat Track · corrodedINSPECTION FOUND RT SEAT TRACK CORRODED AT STA 910-927. THE SEAT TRACK WAS REMOVED AND REPLACED USING SPLICES AND FILLER IAW SRM 53-00-52, FIGURE 204.SDR CALA0300599Channel · crackedCRACK ON C2 DOOR HOLD OPEN LATCH SUPPORT CHANNEL. REMOVED AND REPLACED SUPPORT CHANNEL IAW SRM 51-10-02.SDR CALA0300600Intercostal · corrodedCORROSION ON INTERCOSTAL ANGLE BETWEEN STA 344 AND 360 AT LBL 12. REMOVED AND INSTALLED NEW CHORD IAW SRM 51-10-02 AND 51-40-02.SDR AWXA200301283Floorbeam · corrodedLCQ - MAJOR REPAIR - DURING C-15 CHECK FOUND AFT CARGO COMPARTMENT FLOORBEAM EXFOLIATED AND SPLIT AT BS 773, RBL 13. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOORBEAM AT BS 773, RBL 13; FABRICATED A REPAIR PLATE, EXTRUSION, ANGLE, AND CHANNEL FILLER; INSTALLED RSDR CALA0300577Seat Track · corrodedINSPECTION FOUND RT IB CABIN SEAT TRACK CORRODED AT STA 916-935. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 204.SDR 2003UALA00764Battery Pack · inoperativeSECTION OF EEL LIGHTS INOP FROM SEATS 3ABC TO 9ABC. REPLACED BATTERY PACK AND INVERTER.SDR AWXA200301252Warning System · malfunctionedON TAKEOFF ROLL AT GEG EN ROUTE FOR PHX WITH THRUST LEVERS MOVING TOWARD TAKEOFF THRUST, THE TAKEOFF WARNING CONFIGURATION WARNING HORN SOUNDED, REJECTED TAKEOFF LESS THAN 60 KTS. FLAPS AT 1, TRIM SET AT 4.8, SPEED BRAKE WAS DOWN, PRIOR TO LOW SPEED ABORT TAPPSDR AWXA200301267Floorbeam · corrodedDURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER OF AFT CARGO COMPARTMENT FLOORBEAM AROUND NUT PLATES AT BS 727+5, LBL 3. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF FLOORBEAM BS 727+5, LBL 3SDR AWXA200301272Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT BS 993.5, LBL 33.80. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED FLOOR SUPPORT FROM BS 986.5 TO BS 1006, LBL 33.80; FABSDR AWXA200301286Web · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1INCH CRACK WAS FOUND ON SHEAR WEB AT BS 1003, LBL 42, WL 208.1. MAINTENANCE REMOVED CRACKED SHEAR WEB AT BS 1003, LBL 42, WL 208.1; FABRICATED A NEW REPLACEMENT SHEAR WEB IAW DWG 65C32677; INSTALLED REPAIR PART IAW B73SDR CALA0300574Frame · crackedINSPECTION FOUND A .5 INCH CRACK AT FASTENER IN RT FRAME AT STA 616. REPAIRED IAW ECRA 5311-01158.SDR 2003UALA00753Skin · dentedLWR FUSELAGE SKIN DENTED AT STA 927 BELOW STR 20L. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR.SDR AWXA200301258Skin · debondedDURING C-17 CHECK 8 AREAS OF TAIL CONE SURFACE WERE FOUND DEBONDED. MAINTENANCE CUTOUT DAMAGE ON TAIL CONE SURFACE AT BS 1176 CENTERLINE, BS 1166.5, 6 INCHES RT OF CENTER, BS 1169 2.5 INCHES RT OF CENTER, BS 1163.5, 3 INCHES RT OF CENTER, BS 1165.5 11INCHES LTSDR W321581A5Beam · brokenSTABILIZING ROD END ON PORTABLE WATER TANK BROKE OUT OF BEAM. DURING NON-ROUTINE MAINTENANCE IN THE AFT LOWER CARGO COMPARTMENT FOUND TURNBUCKLE ASSY PN 971093025 HAD BROKE FREE OF BEAM PN 97109323015. LOCATION IS APPROX FS887, RBL 10.75, WL 202. OPERATOR ISDR DL733030901Indicator · malfunctionedCAPTS VSI STARTED SPARKING WHEN AT THE GATE IN SLC BRIEF ELECTRICAL FIRE FOLLOWED BY SMOKE IN COCKPIT. C PERFORMED EXTERNAL LEAK CHECK OF AREA ABOVE CAPT'S INSTRMENT CLUSTER NO FLUID LEAKS DETECTED. FOUND AN EMPTY SCREW HOLE IN THE GLARE SHIELD ABOVE THE INST
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