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 2003UALA00746Autopilot Sys · malfunctionedWITH EITHER AUTO PILOTS ENGAGED AND ATTEMPTING TO ACCELERATE THE AIRCRAFT PITCHES UP. UPDATE DURING BITE CHECK OF THE AUTOPILOT BITE, FOUND FCC-B FAULTED, DADC2 FAULTED. DURING FULL TEST OF AUTOPILOT, OBSERVED FAULT WITH AFAU. REPLACED FCC-B, DADC, AND AFAUSDR 2003UALA00760Stringer Clip · crackedSTRINGER CLIP AT STA 727C LBL 52 CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STRINGER CLIP.SDR 2003UALA00761Skin · gougedFUSELAGE SKIN GOUGED AT STA 737 STR 1L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER REPAIR.SDR 2003UALA00762Skin · dentedFUSELAGE SKIN DENTED STA 927 BELOW STR 20L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER REPAIR.SDR 2003UALA00763Door Frame · gougedFORWARD CARGO DOOR FRAME GOUGED STA 490. MAJOR REPAIR ACCOMPLISHED. BLENDED AREA AND INSTALLED REPAIR PARTS.SDR 2003UALA00745Switch · failedUNABLE TO SELECT NOSE DOWN ELEVATOR TRIM FROM BOTH YOKES. MAINTENANCE TECHNICIANS DUPLICATED THE PROBLEM ON GROUND. THE PROBLEM WAS TRACED TO A FAULTY FLAPS UP SWITCH (S245). THE SWITCH WAS REPLACED. OPERATIONAL CHECKS WERE PERFORMED SATISFACTORILY.SDR UPS03841373Rib · crackedINSPECTION TYPE: C1, VERTICLE STAB LE RT RIB IS CRACKED AT ZFS 68. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATED CRACK,FABRICATED AND INSTALLED REPAIR ANGLE I.A.W. SRM. 55-2-0 FIG.2SDR CALA0300576Skin · damagedTHE FORWARD CARGO DOOR INNER SKIN WAS FOUND WITH THREE EXISTING REPAIRS AND ADDITIONAL DAMAGE TO THE INNER SKIN WHILE AIRCRAFT WAS IN 4C CHECK AT HOU. THE THREE SMALL REPAIR DOUBLERS WERE REMOVED. ONE REPAIR DOUBLER INCORPORATING THE PREVIOUS REPAIRS AND THE DSDR AWXA200301277Seat Track · corrodedDURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON SEAT TRACK FROM BS 827 TO BS 867, LBL 45. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED SEAT TRACK FROM BS 807 TO BS 867, LBL 45; FABRICATED A NEW REPLACEMENT SECTISDR AWXA200301278Seat Track · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON SEAT TRACK FROM BS 460 TO BS 480, RBL 25. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF SEAT TRACK FROM BS 460 TO BS 480, RBL 25; FABRICATED ASDR AWXA200301280Seat Track · corrodedDURING C-17 CHECK CORROSION WAS FOUND ON SEAT TRACK BS 887 TO BS 947, LBL 45. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF SEAT TRACK BS 887 TO BS 947, LBL 45; FABRICATED A NEW REPLACEMENT SECTION OF SSDR AWXA200301281Seat Track · corrodedDURING C-17 CHECK CORROSION WAS FOUND ON SEAT TRACK FROM BS 440 TO BS 500A, RBL 45. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED SEAT TRACK FROM BS 360 TO BS 500A, RBL 45; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTASDR AWXA200301273Angle · corrodedDURING C-17 CHECK INTERGRANULAR CORROSION WAS FOUND ON LOWER SURFACE OF R-2 DOOR CREASE BEAM LOWER SUPPORT ANGLE BS 964, RBL 48. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED SUPPORT ANGLE BS 964, RBL 48; FABRICATESDR AWXA200301274Web · corrodedDURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF RT AFT OUTBOARD SHEAR WEB AT BS 1015, RBL 43.5, WL 207. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED RT AFT OUTBOARD SHEAR WEB AT BS 1015, RBL SDR AWXA200301276Channel · corrodedDURING C-17 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT RT SIDE PLATE CHANNEL BS 767-787, RBL 20. MAINTENANCE REMOVED CORRODED RT SIDE PLATE CHANNEL BS 767-787, RBL 20; FABRICATED A NEW REPLACEMENT CHANNEL IAW DWG 69-43477; INSTALLED REPAIR PART IAW B73SDR AWXA200301284Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A .1250 INCH CRACK WAS FOUND ON STRINGER TIE CLIP IN AFT CARGO COMPARTMENT AT BS 727B, STR 23 LT. MAINTENANCE REMOVED AND REPLACED CRACKED STRINGER TIE CLIP AT BS 727B, STR 23 LT IAW DWG 69-46596.SDR AWXA200301285Frame · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A .3750 INCH CRACK WAS FOUND ON BS 178 BULKHEAD SIDE CHORD AT RBL 30, WL 207. MAINTENANCE REMOVED R/H SIDE CHORD BS 178, RBL 30, WL 207; FABRICATED A NEW REPLACEMENT RT SIDE CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 5SDR AWXA200301287Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A .2500 INCH CRACK WAS FOUND ON BS 178 BULKHEAD VERTICAL WEB EMANATING FROM FORWARD INSULATION HOLE AT RBL 17.1, WL 183. MAINTENANCE REMOVED CRACKED BS 178 BULKHEAD VERTICAL WEB AT RBL 17.1, WL 183; FABRICATED A NEW REPLASDR AUS20031015Bushing · missing(AUS) GROUND SPOILER BUSHES (2 OFF) MISSING FROM NUT END OF NR 1 AND NR 12 SPOILERS. THIS IS A NEW AIRCRAFT AND WAS DELIVERED FROM THE FACTORY WITH THE BUSHINGS MISSING. MANUFACTURING ERROR.SDR AWXA200301199Retainer · missingON ROLL BACK PRIOR TO TAXI RT INBOARD MAIN LANDING GEAR WHEEL ASSEMBLY WAS NOTICED COMING OFF AXLE. UPON FURTHER INVESTIGATION THE NR 3 WHEEL RETAINER RING WAS FOUND MISSING AND THE AXLE NUT WAS BACKED OFF. DAMAGE WAS NOTED TO THE WHEEL AND BRAKE ASSEMBLIES, SDR AWXA200301268Container · will not testDURING C-17 CHECK THE FORWARD LAVATORY OXYGEN MASK DOOR CONTAINER TEST STOP BUTTON FAILED TEST. MAINTENANCE REMOVED AND REPLACED FORWARD LAVATORY OXYGEN MASK ASSEMBLIES IAW BMM TASK 35-22-31-004-059, AND TASK 35-22-31-404-051, OPERATIONAL CHECK WAS GOOD.SDR 2003UALA00729Light · inoperativeAFT SECTION OF EMERGENCY EEL LIGHT SYSTEM IS INOP. REPLACED AFT SECTION OF RIBBON & AFT EEL GALLEY LIGHT.SDR AWXA200301288Angle · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A .2500 INCH CRACK WAS FOUND ON RT UPPER WING TRAILING EDGE SUPPORT ANGLE ON NR 2 FLAP TRACK OUTBOARD, WBL 204. MAINTENANCE REMOVED CRACKED SUPPORT ANGLE AT WBL 204; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PASDR 2003UALA00725Skin · damagedSKIN LAP REPAIR AT STA 328 AND STR 24R. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR.SDR AWXA200301256Skin · debondedMCN - MINOR REPAIR - DURING C-17 CHECK FOUND TOP CENTER AREA OF TAIL CONE DISBONDED, 18 INCHES-22 INCHES FROM FORWARD EDGE. MAINTENANCE CUTOUT DISBONDED AREA OF TOP CENTER TAIL CONE, 18 INCH-22 INCHES FROM FORWARD EDGE AND PERFORMED A BOND REPAIR IAW B737-300 SDR 2003UALA00723Floorbeam · corrodedCABIN FLOORBEAM AT STA 294.4 HAS CORROSION FROM RBL 24 TO RBL45. MAJOR REPAIR ACCOMPLISHED, INSTALLED REPLACEMENT WITH ANGLE SPLICE.SDR 2003UALA00730Skin · dentedTHREE DENTS IN FUSELAGE SKIN ABOUT 24 INCHES AFT OF DOOR 2R, JUST FWD OF APU INLET. MAJOR REPAIR ACCOMPLISHED, INSTALLED REPLACEMENT PANEL.SDR CALA0300560Battery Pack · inoperativeTHE INTERIOR EMERGENCY AISLE LIGHTS AT ROWS 14R, 16L, 19L, 21R, AND 23L WERE FOUND INOPERATIVE. REPLACED BATTERY PACKS AT M1135 AND M1136 POWER SUPPLIES IAW MM 33-51-51, PARAGRAPH 3, PAGES 203-206. OPERATIONAL CHECKS WERE GOOD.SDR DHL2003802013Fire Loop · shortedNR 2 ENGINE SHORT CIRCUIT LIGHT ILLUMINATED ON LOOP (A). LOOP (B) OPS CHECKED NORMAL. CLEANED CONNECTOR ON NR 2 ENGINE SYSTEM OPS CHECK GOOD IAW DC8 M/M 26-10-0.SDR CALA0300555Skin · dentedINSPECTION FOUND TWO DENTS IN AFT FUSELAGE SKIN FROM STA 934-943 BETWEEN S23L AND S24L. A REPAIR WAS INSTALLED IAW SRM 53-00-01.SDR CALA0300556Pan · corrodedINSPECTION FOUND CORROSION ON LT AFT LAV FLOOR PAN AT DUMP CHUTE, STA 1006, LBL 10. A NEW LAV PAN WAS INSTALLED IAW SRM 51-20-07 AND 51-10-02.SDR CALA0300557Pan · corrodedINSPECTION FOUND RT AFT LAV PAN CORRODED AT STA 1028, RBL 18. A NEW LAV PAN WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02.SDR CALA0300558Strap · corrodedINSPECTION FOUND STRESS WEB UPPER STRAP CORRODED AT STA 1006-1022, RBL 28. THE CORRODED STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02.SDR CALA0300559Strap · corrodedINSPECTION FOUND STRESS WEB UPPER STRAP CORRODED AT STA 1028, RBL 18. THE CORRODED STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02.SDR F3LA200300148Floorbeam · corrodedDURING A-4 CHECK, INSPECTION REPORTED FLOOR BEAM AT STA. 947.5 CORRODED ON TOP CAP, UPPER AND LOWER SURFACE. FABRICATED AND INSTALLED REPLACEMENT TEE CHORD CAP AND REPAIR SPLICES IAW SRM 53-60-51 AND EA B3-53R-10150.SDR 2003UALA00717Door Frame · damagedFWD LOWER FRAME OF THE FWD RT DOOR CUT-OUT HAS A PIECE MISSING. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR.SDR 2003UALA00720Frame · corrodedSTA 805 FUSE FRAME HAS CORROSION ON THE AFT SIDE, JUST ABOVE AND FWD OF THE CARGO DOOR THRESHOLD. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR.SDR 2003UALA00722Light · inoperativeFLOOR EMERGENCY EXIT LIGHTS INOP FROM ROW 15 TO AFT END OF CABIN. REPLACED POWER STRIP.SDR UPS03841371Rib · crackedINSPECTION TYPE: C1, RT WING LE. RIBS CRACKED AT XFS760 UPPER,XFS 766.25 UPPER, XFS 822.5 LOWER STOP DRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATE CRACKS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM. 57-2-0 FIG. 2SDR F3LA200300147Mount · corrodedDURING C-4 CHECK, INSPECTION REPORTED LAV MOUNT AT STA. 947.5, LBL 25, CORRODED. REPLACED LAV MOUNT IAW SRM 51-40-02.SDR 2003UALA00714Floorbeam · crackedCABIN FLOORBEAM IS CRACKED IN THE RADIUS AT STA 927 RBL 45. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR.SDR 2003UALA00715Floorbeam · gougedCABIN FLOORBEAM IS GOUGED AT STA 360 AND BL 0. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR.SDR 2003UALA00716Wheel · separatedON LANDING DCA, NOSE LANDING GEAR COLLAPSED. UPON ROTATION IN ORD, THE NOSE WHEEL ASSEMBLIES DEPARTED THE AXLE. AIRCRAFT LANDED ON THE AXLE IN DCA. CAUSE OF FAILURE WAS THE REPAIR SHAFT, UAL P/N 3F13178-2. IT WAS DETERMINED THAT THE REPAIR SHAFT THREADS WERE SDR UPS03841376Seat Track · corrodedINSPECTION TYPE: C1, SEAT TRACK CORRODED BEYOND LIMITS AT STA. 1188 AT RBL 60. REMOVED SEAT TRACK SECTION BETWEEN STA. 1070 TO 1210, FABRICATED AND INSTALLED REPLACEMENT SECTION I.A.W. SRM. 53-2-3 FIG. 14SDR UPS03841377Seat Track · corrodedINSPECTION TYPE: C1, SEAT TRACK IS CORRODED BEYOND LIMITS AT STA. 1325 LBL. 50. REMOVED SEAT TRACK SECTION STATION 1270 TO 1470, FABRICATED AND INSTALLED SEAT TRACK SECTION DC8-5320-8309SDR AWXA200301257Connector · damagedMCN - EEL - DURING C-17 CHECK SEVERAL EMERGENCY ESCAPE PATH LIGHT HARNESS CONNECTORS WERE FOUND DAMAGED BETWEEN BS 370 TO BS 920 L/H SIDE. MAINTENANCE REMOVED AND REPLACED DAMAGED EMERGENCY ESCAPE PATH LIGHT HARNESS CONNECTORS AND SPLICES BETWEEN BS 370 TO BS SDR F3LA200300142Seat Track · corrodedDURING C-4 CHECK, INSPECTION REPORTED SEAT TRACK AT STA. 328 TO STA. 360, RBL 24, CORRODED. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK IAW SRM 51-40-02, MFG DRAWING 65C34624 AND SOPM 20-41-02.SDR F3LA200300143Support · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON RT. ZEE SUPPORT IN AFT CARGO COMPARTMENT FROM STA. 767 TO STA. 797.2. REPLACED ZEE SUPPORT IAW SRM 51-40-02, 53-60-53 AND DRAWING 69-43477.SDR F3LA200300144Strip · crackedDURING C-4 CHECK, INSPECTION REPORTED CAP STRIP BETWEEN STA. 344 AND 360, RBL 12 TO 24, CRACKED. FABRICATED AND INSTALLED REPLACEMENT CAP STRIP IAW SOPM 51-40-02 AND DRAWING 65C33971.SDR CALA0300553Pan · corrodedINSPECTION FOUND RT AFT LAV FLOOR PAN CORRODED AT SERVICE WATER FITTING. THE PAN WAS REMOVED AND A NEW PAN WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02.
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