JASC 5300
Service difficulty reports · 8,206
Reports filed under 5300 · Fuselage Structure (General), newest first.
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 jasc_code = '5300' 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 jasc_code = '5300' 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 377PA0003Skin · damagedFuselage skin damaged by belt loader sta 767 to sta 772 between str27Lt. and str27Rt.SDR SIMA200217701Bulkhead · corrodedDURING MBV1 INSPECTION FOUND BONDING POINTS ON FORWARD BULKHEAD TO BE CORRODED. REPAIRED IAW ATR SRM. AIRCRAFT WAS RETURNED TO SERVICE.SDR C2XA02SH015Strap · corrodedSHV - DURING C-CK INSPECTION, THE CENTER STRAP AT BETWEEN FRAMES 14 AND 17 WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED SECTION OF THE STRAP, FABRICATED AND INSTALLED A REPAIR DOUBLER IN ACCORDANCE WITH EMB-145 SRM 53-21-02, AND THE AIRCRAFT WAS SDR ASOA02344Support · crackedDURING HANGER MAINTENANCE, THE LEFT ENGINE SUPPORT BEAM WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE CRACKED ENGINE SUPPORT BEAM IAW REO. THIS REO GIVES REPAIR SPECIFICATIONS FOR THE ENGINE SUPPORT BEAM CRACK, AS WELL AS OUTLINES A THRESHOLD OF CYCLES FSDR ASOA02333Beam · crackedDURING HANGER MAINTENANCE, CRACKS WERE FOUND ON THE ENGINE SUPPORT BEAM AT BL 36.20 ON BOTH SIDES. MAINTENANCE REPAIRED THE CRACKED ENGINE SUPPORT BEAM IAW REO. THIS REO GIVES REPAIR SPECIFICATIONS FOR THE ENGINE SUPPORT BEAM CRACK ON AIRCRAFT AS WELL AS OUTSDR SIMA200216515Frame · corrodedDURING CPCP 2 INSP FOUND FRAME 37R CORRODED AT FLOOR LEVEL.SDR SIMA200216514Sill · corrodedDURING CPCP 2 INSPECTION FOUND SERVICE DOOR SILL PLATE CORRODED.SDR SIMA200216513Pan · crackedDURING MBV INSPECTION FOUND LOWER CORNER OF SERVICE DOOR PAN CRACKED.SDR SIMA200216512Seat Spring · corrodedDURING CPCP2 INSPECTION FOUND AFT CARGO WALL AND LEFT MIDDLE INBOARD SEAT TRACKS TO BE CORRODED.SDR SIMA200216311Stringer · chafedDURING AN IMBV INSPECTION FOUND STRINGER 19L CHAFED BETWEEN FRAMES 52 AND 53. BLENDED CHAFE. PERFORMED NDT INSPECTION NO DEFECTS. FABRICATED A DOUBLER ANGLER, AND TWO SHIMS. REPAIR DONE IAW STANDARD SRM PRACTICES.SDR SIMA200216310Stringer · chafedDURING AN IMBV INSPECTION FOUND STRINGER 19R CHAFED BETWEEN FRAMES 52 AND 53. BLENDED AREA, PERFORMED NDT INSPECTION NO DEFECTS. FABRICATED A DOUBLER ANGLE, AND TWO SHIMS. REPAIR DONE IAW STANDARD SRM PRACTICES.SDR ASOA02343Sill · corrodedDURING (C) CHECK INSPECTION, THE LEFT FLOOR SILL PLATE WAS CORRODED OUT OF LIMITS BETWEEN FRAMES 15A AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED SILL PLATE IAW SRM.SDR ASOA02342Sill · corrodedDURING (C) CHECK INSPECTION, THE RIGHT HAND SILL PLATE WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN FRAMES 13 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED SILL PLATE IAW SRM.SDR ASOA02341Butt Strap · corrodedDURING (C) CHECK INSPECTION, THE LEFT HAND BUTT STRAP WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN STA 6653.1 AND FRAME 25. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRM.SDR ASOA02340Butt Strap · corrodedDURING (C) CHECK INSPECTION, THE CENTER BUTT STRAP WAS CORRODED BEYOND LIMITS BETWEEN FRAMES 13 AND 16. MAINTENANCE REMOVED AND REPLACED THE CORRODED CENTER BUTT STRAP IAW SRM.SDR ASOA02339Crossbeam · corrodedDURING (C) CHECK INSPECTION, THE LEFT INBOARD CROSS BEAM WAS FOUND TO BE CORRODED BEYOND LIMITS AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSS BEAM IAW SRM.SDR ASOA02338Stringer · corrodedDURING (C) CHECK INSPECTION, STRINGERS 20 RIGHT AND 21 RIGHT WERE FOUND TO BE CORRODED OUT OF LIMITS AT FRAME 17. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTIONS OF STRINGER AND INSTALLED SPLICES IAW SRM.SDR ASOA02337Stringer · corrodedDURING (C) CHECK INSPECTION, STRINGER 19 LEFT WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN FRAMES 15 AND 15A. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTION OF STRINGER AND INSTALLED A SPLICE IAW SRM.SDR ABXA020137Seat TrackSEAT TRACK P/N 96FS667743-101 LOWER HORIZONTAL OUTBOARD FLANGE AT STATION 753-45, LEFT BUTT LINE 86.38, DRILLED BY MISTAKE. REPAIRED AREA IAW REA B653-43514-DE.SDR SIMA200216408Longeron · dentedLEFT UPPER COWLING LOWER INBOARD LONGERON DENTED. RECONTOURED LONGERON, PERFORMED EDDY CURRENT, NO DEFECTS. ACCEPTED AS IS IAW. TREATED FOR CORROSION.SDR SIMA200216407Gusset · gougedCENTER GUSSET GOUGED FROM FRAMES 20 T0 22. C/A REMOVED GOUGED BY BLENDING, WITHIN SRM LIMITS. RESTORED SURFACE PROTECTION.SDR SIMA200216405Extinguisher · chafedAFT FLOOR EXTENTION IS CHAFED FROM FRAMES 22-23. C/A PERFORMED EDDY CURRENT INSPECTION. NO DEFECTS. BLENDED CHAFE IAW SRM LIMITS.SDR SIMA200216401Frame · crackedDURING MBV-1 INSPECTION, FRAME 25 LEFT AND RIGHT SIDES FOUND CRACKS IN LOWER OUTBOARD RADIUS OF HYDRAULIC LINE PASS THROUGH CUTOUTS.SDR SIMA200216201Beam · elongatedDURING AN IMBV INSPECTION FOUND CENTER BEAM UPRIGHT AT FRAME 20 HAD AN ELONGATGED HOLE. REMOVED DAMAGED UPRIGHT. FRABRICATED A SERVICEABLE UPRIGHT IAW STANDARD SRM PRACTICES.SDR SIMA200216409Bracket · gougedAPU FIREWALL GOUGED BY APU BLEED AIR VALUE BRACKET. PERFORMED EDDY CURRENT, NO DEFECTS. REPAIR DONE ON GOUGE IAW SRM.SDR SIMA200216006Frame · dentedDENT ON FRAME 9 BELOW STRINGER 15R .005 X .7 X 1.0. SUP, DENT ACCEPTED AS IS IAW MFG GST.SDR SIMA200216005Frame · dentedDENT FORWARD OF FRAME 18 BELOW STRINGER 20L. .013 X 2.0 X 1.7 (SUP) DENT ACCEPTED AS IS IAW MFG GST.SDR SIMA200216001Frame · dentedDENT AFT FRAME 19 BELOW STRINGER 13L. .006 X 2.5 X 1.1. (SUP) DENT ACCEPTED AS IS IAW MFG GST.SDR 159PL0021Skin · corrodedCorrosion on fuselage skin at Sta986.5 at Str22Lt & Str23Lt. Corrosion on frame shear tie clipSDR 159PL0020Skin · corrodedCorrosion in fuselage skin at BS908 Butt jointSDR 159PL0018Skin · crackedFuselage skin cracked at fwd entry door lower hinge cutout at Sta303SDR 159PL0017Beam · crackedCargo floor beam cracked at BS460 at Str27Rt.SDR 159PL0011Galley Track · corrodedCorrosion on right O/B galley track at fwd endSDR 159PL0004Tie Clip · crackedStringer tie clips cracked upper lobe of cabin various locations (41) totalSDR SIMA200216503Stabilizer · dentedLEFT HORIZONTAL STABILIZER TOP HAS FOUR DENTS.SDR ABXA020090Angle · corrodedCORRODED ANGLE BETWEEN STATIONS 632 - 654 AND BETWEEN STRINGERS 34 - 35. REPLACED ANGLE IAW B767 AMM.SDR ASOA02311Beam · crackedDURING A HANGER INSPECTION, WHILE COMPLYING WITH EO, INSPECTION OF ENGINE SUPPORT BEAM CRACKS, A CRACK WAS DISCOVERED ON THE BEAM AT THE LEFT ACCESS PANEL FORWARD CORNER. MAINTENANCE REPAIRED THE CRACK IN THE ENGINE SUPPORT BEAM.SDR ASOA02310Frame · crackedDURNG HANGER MAINTENANCE, A CRACK WAS DISCOVERED IN FRAME STATION 718 BETWEEN STRINGERS 10 AND 12 ON THE LEFT AND RIGHT SIDES. MAINTENANCE REPAIRED THE CRACKED FRAME IAW EO/REO/SRM.SDR ASOA02309Frame · crackedDURING HANGER MAINTENANCE, A CRACK WAS DISCOVERED IN FRAME STATION 718 BETWEEN STRINGERS 10 AND 12 ON THE LEFT AND RIGHT SIDES. MAINTENANCE REPAIRED THE CRACKED FRAME IAW EO/REO.SDR ASAA0240071Frame · corrodedPAE - DURING SI CHECK, FOUND FRAME AT BS 794, RBL 20 WL 153 IS CORRODED. REMOVED AND REPLACED FRAME IAW SRM 53-00-07. (M)SDR SIMA200215118Frame · misdrilledDURING AN MBV INSPECTION, FOUND DAMAGE TO STRINGER 16L FORWARD OF FRAME 20, AT JOINT DRILL MARKS AND OVERSIZE HOLE. REMOVED DRILL MARKS BY BLENDING. REAMED HOLES, INSTALLED NEW FASTENERS IAW STANDARD SRM PRACTICES.SDR SIMA200215108Frame · dentedDURING AN MBV INSPECTION, FOUND FRAME 677 DENTED. REMOVED DAMAGE BY CUTOUT. PERFORMED NDT, NO DEFECTS. FAB REPAIR DOUBLER, REPAIR DONE IAW SDS AND STANDARD SRM PRACTICES.SDR UIEA200200024Skin Panel · puncturedFuselage Skin damaged from BS 460 to 480 from between Stringer 38R and 39R by cargo container during loading operation. Stringers 38R and 39R at this location deformed by container. Damaged skin area trimmed out. Damaged area of stringer 38R trimmed out. StrinSDR ASOA02304Butt Strap · corrodedDURING (C) CHECK INSPECTION, THE LEFT BUTT STRAP, BETWEEN FRAMES 14 AND 21, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRM.SDR ASOA02302Crossbeam · corrodedDURING (C) CHECK INSPECTION, CORROSION WAS FOUND ON TOP OF THE LEFT HAND CROSSBEAM AT FRAME 28. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAM IAW SRM.SDR ASOA02301Crossbeam · corrodedDURING (C) CHECK INSPECTION, CORROSION WAS DISCOVERED ON THE LEFT HAND INBOARD AND OUTBOARD CROSS BEAMS AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE TWO CORRODED LEFT HAND CROSS BEAMS IAW SRM.SDR ASOA02295Frame · crackedDURING HANGER MAINTENANCE, A CRACK WAS FOUND TO FUSELAGE FRAME FS718.00 BETWEEN STRINGERS 10 AND 12. MAINTENANCE REPAIRED THE CRACKED FRAME IAW EA/REO.SDR SIMA200215107Doubler · dentedDURING MBV INSPECTION NO SUBSTANTIATING DOCUMENTATION COULD BE FOUND FOR DOUBLER REPAIR ON LEFT AFT FUSELAGE AFT OF STATIC PORT. REMOVED PREVIOUS INSTALLED REPAIR DOUBLER. PERFORMED NDT INSPECTION, NO DEFECTS NOTED. FAB REPAIR DOUBLER, INSTALLED IAW SRM ANDSDR C2XA02SH008Plate · corrodedSHV - DURING C-CHECK INSPECTION, THE SERVICE DOOR FORWARD SILL PLATE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PLATE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA02SH007Plate · corrodedSHV - DURING C-CHECK INSPECTION, THE SERVICE DOOR AFT SILL PLATE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL PLATE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
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