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 UPS05845656Stiffener · corrodedC2 A-PIT STA 283 AT LWR FWD DOOR CUTOUT, EXTRUDED STIFFNER IS CORRODED OUT OF LIMITS. REMOVED A-PIT LWR FWD DOOR CUTOUT STIFFNER IAW SRM 51-1-24 FABRICATED AND HEAT TREATED STIFFNER IAW DWG 5733892 AND INSTALLED STIFFNER AT STA 283 LWR FWD DOOR CUTOUT IAW DWGSDR 2005UALA01128Door Frame · crackedFORWARD GALLEY DOOR, FORWARD SIDE LOWER END FRAME IS CRACKED AT FASTENER HOLE. REMOVED DAMAGE. FABRICATED FRAME & FRAME SPLICE PARTS PER UAL SM-90-52-40-14-JD. INSTALLED REPAIR PER SM-90-52-40-14-JD.SDR 2005UALA01129Door Frame · crackedFORWARD ENTRY DOOR AFT SIDE LOWER END FRAME IS CRACKED AT FASTENER HOLE. REMOVED DAMAGE. INSTALLED REPAIR KIT, INNER SKIN & AFT LOWER STOP PER SM-90-52-40-14-JD.SDR 2005UALA01130Crease Beam · corrodedAFT GALLEY DOOR CUTOUT AREA LOWER THRESHOLD CREASE BEAM CORRODED STA 913 TO 1016. REMOVED & REPLACED CREASE BEAM IN ACCORDANCE WITH SRM 51-40-02.SDR 2005UALA01131Skin · damagedLT ELEVATOR UPPER SURFACE HAS A ONE SQUARE INCH AREA OF CORE DAMAGE AT 88 INCHES OUTBOARD OF INBD EDGE. REMOVED DAMAGE. ACP. LAYUP AND COOK PER SRM 51-70-05 & SRM 55-20-01.SDR UPS05845655Longeron · crackedINSPECTION TYPE:C2 FS 1790 TO FS 1880 L36 IS CRACKED AND HAS ELONGATED HOLES. REMOVED LONGERON 26 AT FS 1790 TO 1880 IAW SRM 51-1-20D FABRICATED AND INSTALLED LONGERON 36 AND SPLICE REPAIR IAW S1415997 AND SRM 51-1-20D, AND 51-1-20.SDR UPS05845658Shear Tie · crackedINSPECTION TYPE: C2 SHEAR TIE AT STA 710 L35L IS CRACKED. REMOVED SHEAR TIE AT STA 710 L35L IAW SRM 51-1-20D, FABRICATED AND INSTALLED SHEAR TIE AT STA 710 L35L IAW DWG 5750365, AND SRM 51-1-21D.SDR 2005UALA01120Floorbeam · corrodedCABIN FLOORBEAM CORRODED ON UPPER CAP STA 986.5, RBL 25-45 AT WL 208. MAJOR REPAIR ACP'D PER MM 53-10-95, APPROX 50" SECTION OF UPPER "T" CAP SPLICE TYPE REPAIR SCHEME.SDR 2005UALA01121Frame · crackedFORWARD CARGO PIT STA 482A BETWEEN STR 28 LEFT AND STR 28 RIGHT FRAME HAS SEVERAL CRACKS. REMOVED DAMAGED AREAS PER MM53-11-87. NDT FOR CRACKS. NONE FOUND. FABRICATED & INSTALLED FILLER & DOUBLER PER MM 53-11-87 FIG. 801.SDR 2005UALA01122Floorbeam · corrodedCABIN FLOORBEAM AT STA 294 RBL 38 TO RBL 39 AT WL 208 CORRODED AT BOLT HOLES. REMOVED CORROSION & FOUND BLEND OUT OF LIMITS. FABRICATED & INSTALLED REPAIR STRAP PER SRM 53-00-51 REPAIR NR 3.SDR 2005UALA01123Frame · crackedCABIN FRAME CRACKED AT STA 400 BETWEEN STRINGER 8L AND 9L AT STOW BIN RAIL ATTACH. REMOVED DAMAGE PER MM 53-10-84. NDT TO VERIFY NO CRACKS. FABRICATED & INSTALLED NESTED ANGLE REPAIRS & FILLER PER MM 53-10-84.SDR 2005UALA01104Frame · crackedAFT CABIN STA 787 FRAME CRACKED BETWEEN STR 8L AND 9L. REMOVED CRACK AND INSTALLED ANGEL REPAIR AND FILLER PER MM 53-10-84.SDR 2005UALA01105Frame · crackedSTA 400 STR 8R AND 9R FUSELAGE FRAME CRACKED. REMOVED CRACK, INSTALLED REPAIR ANGLE AND FILLER PER MM 53-10-84.SDR 2005UALA01106Frame · crackedAFT CABIN STA 827 FRAME IS CRACKED BETWEEN STR 8L & 9L. REMOVED CRACK, INSTALLED REPAIR ANGELS PER MM 53-10-84 REPAIR III.SDR 2005UALA01107Frame · crackedAFT CABIN STA 907 FRAME IS CRACKED BETWEEN STR 8L AND 9L. REMOVED CRACK, INSTALLED REPAIR ANGLES PER MM 53-10-84 REPAIR III.SDR 2005UALA01108Stringer Clip · crackedAFT CABIN STA 887 STR 4R IS CRACKED AT STRINGER CLIP. REMOVED CRACK, INSTALLED REPAIR ANGLES AND CLIP PER SRM 53-00-03.SDR 2005UALA01109Frame · crackedAFT CABIN STA 867 FRAME IS CRACKED BETWEEN STR 8R AND 9R. REMOVED CRACK, FABRICATED REPAIR ANGELS AND INSTALLED PER MM 53-10-84.SDR 2005UALA01110Frame · crackedCABIN STA 440 BTWN STR 8R AND 9R FUSELAGE FRAME CRACKED. REMOVED CRACKED,INSTALLED REPAIR ANGELS PER MM 53-10-84.SDR 2005UALA01112Elevator · malfunctionedABORTED TAKE OFF AT 140 KNOTS DUE TO NO ELEVATOR MOVEMENT. UNSECURED ELEVATOR BALANCE WEIGHT BECAME LODGED BETWEEN LOWER SURFACE OF BALANCE BAY & ANGLE USED TO SUPPORT ACCESS PANEL AT STABILIZER BS 94.07. SUBJECT BALANCE WEIGHT BECAME DISLODGED FROM BALANCE STSDR 2005UALA01101Frame · crackedAFT CABIN STA 927 FRAME IS CRACKED BETWEEN STR 8L AND 9L. REMOVED CRACKED AREA, ACCOMPLISHED A DOUBLER AND FILLER REPAIR PER SRM 53-00-07 FIG.201 REPAIR 2.SDR 2005UALA01102Frame · crackedAFT CABIN STA 747 FRAME CRACKED BETWEEN STR 8L AND 9L. REMOVED CRACK, INSTALLED REPAIR ANGLES AND FILLER PER MM 53-10-84 REPAIR III.SDR 2005UALA01103Frame · crackedAFT CABIN STA 727B FRAME IS CRACKED BETWEEN STR 8L AND 9L. REMOVED CRACK, INSTALLED ANGLE AND FILLER REPAIR PER MM 53-10-84.SDR 2005UALA01097Stringer Clip · crackedFOUND STA 907 STR 8L CLIP IS CRACKED AT IB FASTENER. REMOVED AND REPLACED STR. CLIP PER SRM 51-40-02.SDR 2005UALA01098Frame · crackedFOUND STA 440 BET STR 8L AND 9L FRAME CRACKED WHERE STOW BIN RAIL ATTACHES TO THE FRAME. REMOVED CRACKED AND ACCOMPLISHED A DOUBLER AND FILLER REPAIR PER MM 53-10-84,SDR 2005UALA01099Frame · crackedAFT CABIN STA 827 FRAME IS CRACKED BETWEEN STR 8R AND 9R. REMOVED CRACK, ACCOMPLISHED A DOUBLER AND FILLER REPAIR PER MM 53-10-84.SDR 2005UALA01100Frame · crackedCABIN FRAME CRACKED AT FASTENER HOLE STA 867 BETWEEN STR 7 AND 8 LEFT. REMOVED CRACK ACCOMPLISHED A DOUBLER AND FILLER REPAIR PER MM 53-10-84.SDR UPS05845661Skin · crackedINSPECTION TYPE: C2 FUSELAGE SKIN HAS A .5 INCH CRACK AT MCD LWR AFT CORNER, UNDER REMOVED SCUFF PLATE, AT PREVIOUS CUT OUT. TRIMMED OUT CRACK AT MCD LWR AFT CORNER IAW DWG SR 08530027, FABRICATED AND INSTALLED -11 FILLERS, -4 DOUBLER AND -7 DOUBLER IAW DWG SDR UPS05845649Fitting · corrodedC2 A- PIT BAG BIN, INTERGRANULAR CORROSION ON BATH TUB FITTING AT STA 280 L32L. REMOVED AND REPLACED BATH TUB FITTING AT STA 280, L32L IAW SRM 53-02-00 FIG 002D AND SRM 51-1-21.SDR UPS05845654Fitting · corrodedC2 C-PIT STA 1200 L26L BANANA FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED BANANA FITTING AT STA 1200 L26L IAW SRM 53-2-0, AND 51=1-20D,AND SRM 51-3-2.SDR 2005UALA01081Light · inoperativeEMERGENCY EXIT PATH LIGHTING IN REAR THIRD OF AIRCRAFT NOT WORKING. REPLACED POWER STRIP.SDR 2005UALA01071Stringer · crackedAFT CABIN STA 907 STR 4L IS CRACKED AT 2 EA FASTENER HOLES. REPLACED STRINGER SPLICE. REF SRM 51-40-02.SDR MZZA0500010Skin · corrodedINSPECTION FOUND CORROSION TO THE EXTERIOR OF THE FUSELAGE SKIN ADJACENT TO THE DRAIN HOLE AT STA 727J, BL 0. THE SKIN WAS REPAIRED IAW ECRA 5330-03490.SDR UPS05845662Cusp Web · crackedINSPECTION TYPE: C2 C CUSP CRACKED 3 INCH LONG STA 1080 L21L. REMOVED DAMAGED AREA IAW SRM 53-02-05-0 AT FS 1080 L21L FABRICATED AND INSTALLED CUSP SPLICE,-7 DOUBLER, -3 AND -5 ANGLES AND -9 CUSP IAW 51-1-21, AND SRM 53-2-5 FIG 1.SDR 2005UALA01076Transformer · overheatedNR 1 TRANSFORMER, RECTIFIER WAS FOUND TO HAVE OVERHEAT DAMAGE. FOUND GRND PWR CB-S BURNT. COVER OVER ALL THREE TRANSFORMER-RECTIFIER UNITS WAS BURNED, DUE TO SUSPECTED OVERHEAT IN ONE OR MORE TRS. ALL THREE TRS REPLACED, AS WAS THE BATTERY, BATTERY CHARGER,SDR UPS05845657Pressure Panel · corrodedC2 CORROSION UNDER DOUBLER ON LT W/W CEILING STA 960 LBL 57-62, CORROSION AT SAME LOCATION IN MAIN CABIN UNDER FLOORBEAM. REMOVED MLG LT WHEEL WELL HORIZ. PRESSURE PANEL WEB AT FS 960 LBL 57-62 IAW SAA SK 866-832452, AND UPS EO FABRICATED AND INSTALLED PRESSUSDR 2005UALA01048Frame · crackedFWD SIDE OF DOOR LOWER END FRAME CRACKED AT FASTENER HOLE FWD GALLEY DOOR. ACCOMPLISHED A REPAIR PER MM 51-40-02, FABRICATED AND INSTALLED FRAME SPLICES REF BOEING DRW 69-69430,SDR IXXA05SMN218SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, FWD ACCY COMPT FITTING CORRODED, STA 60.000, 70.000 L-34R. REMOVED CORROSION FROM FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-21, SRM 51-1-20D. CLEANED,SDR IXXA05SMN219SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, FWD ACCY COMPT, FITTING CORRODED, STA 60.000, 70.000 L-34R. PERFORMED MAJOR REPAIR IAW MSG NR 1-126059161-2 DATED 09-26-05, SRM 52-1-0 PG 1. REMOVED DAMAGED SKIN IAW SRM 51-1-21. FABRICATED NEW SKIN (AL7075T6 0.050) IAW MSSDR IXXA05SMN220SSkin · scratchedDURING ROUTINE C CHECK INSPECTION, EXTERNAL FUS. (C) BELLY PIT DOOR SKIN SCRATCHES OUT OF LIMITS. PERFORMED MAJOR REPAIR, REMOVED FASTENERS IAW SRM 51-1-20D. REMOVED DAMAGED SECTION IAW DWG NR ED-4075. NDT INSPECTED IAW NDT SPM PART 06-10-01-001. NEITHERSDR IXXA05SMN201SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT FWD FITTING CRACKED 2, STA 781.000 L-19L. REMOVED CRACKED FITTING IAW SRM 51-1-20D. FABRICATED NEW FITTING (AL7075T651) IAW MFG DWG NR 3779978, EA NR 20051313. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-SDR IXXA05SMN202SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT. AFT FITTING CRACKED 3, STA 834.5 L-14RREMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9, SRM 51-3-1 (TORQUE).SDR IXXA05SMN203SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT. AFT FITTING CRACKED 1, STA 857.000 L-19LREMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1. (TORQUE)SDR IXXA05SMN204SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT FITTING CRACKED 1.5, STA 902.000 L-19L. REMOVED CRACKED FITTING IAW SRM 51-1-20D. FABRICATED NEW FITTING (AL7075T651) IAW MFG DWG NR 3779498, EA NR 20051314. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00SDR IXXA05SMN207SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT LWR CARGO BILGE INTERIOR, FITTING CRACKED 2, STA 1215.000 L-29R. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1. CLEANED, TREATED, PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0, SRM 51-1-20D, SRM 51-3-SDR IXXA05SMN209SSkin · crackedDURING ROUTINE C CHECK INSPECTION, RT OUTER WING IB L/E LOWER SKIN, .2500 IN CRACK, STA XFS 597.500. PERFORMED MAJOR REPAIR DATED 10-07-05, DWG NR ED-4069 DATED 10-06-05, EO NR 20051275 DATED 10-07-05. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. PERFORMESDR IXXA05SMN211SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT RT TUNNEL SPLICE FITTING CRACKED 2, STA 445.000 L-27R REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20DSDR IXXA05SMN212SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FWD LOWER FUSELAGE. SPLICE FITTING CRACKED 2 , STA 445.000, STA 455.000 L-31R. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D AND SDR IXXA05SMN213SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FWD LOWER FUSELAGE SPLICE FITTING CRACKED 8, STA 445, STA 455.000 L-31L. REMOVED CRACKED FITTING IAW SRM 51-1-20D, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 5SDR IXXA05SMN214SSkin · crackedDURING ROUTINE C CHECK INSPECTION, RT IB AIL L/E UPPER PLATING CRACK .2500 AT STA XA 470.000. PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 1, EO SEMAN NR 20051280 DATED 09-26-05. REMOVED DAMAGED PLATING IAW SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040) SDR IXXA05SMN215SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE SPLICE FITTING CRACKED 2, STA 1770.000 RT, L-17R. REMOVED CRACKED FITTING IAW SRM 51-3-0, SRM 51-21-1. FABRICATED NEW FITTING (AL7075T651) IAW ATI REPAIR SPECIFICATION NR 2003-05, EA SEMAN NR 20051318. HEAT TR
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