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 DL72S020213Frame · crackedFOUND ON F-2 LETTER CK 3/4 IN CRACK MLG UPLOCK FRAME SUPPORTSTRUCTURE AT STA 913 RIGHT W/W. REPAIRED PER MM 53-11-000-8.SDR ABXA010765Panel · crackedFITTING OUTBOARD OF CANTED KEEL PANEL AT STATION 603, RIGHT SIDE CRACKED. REPLACED FITTING IAW DC-9 MM.SDR DL72W020206Angle · crackedFOUND ON E-2 LETTER CK 1.25 INCH CRACK THRU ONE FASTENER HOLE TO FASTENER HOLE, AFT FLANGE OF VERTICAL ANGLE STA 870 TO KEEL BEEM. REPAIRED PER SRM 53-10-9D FIG 806D TIME LIMITED REPAIRSDR 2002UALA00254IntercostalAFT CABIN BETWEEN STATION 1640 TO STA 1660, BL0, INTERCOSTAL NEEDS REMOVAL FOR ACCESS. MAJOR REPAIR ACCOMPLISHED. INTERCOSTAL REMOVED AND REINSTALLED WITH NEW ANGLES AND SPACERS.SDR C2XA02IA034Crease Beam · corrodedIAH- DURING "C" CHECK INSPECTION IT WAS NOTED THAT THE RIGHT CREASE BEAM BETWEEN FRAME 22 and 23 WAS CORRODED AROUND THE NUT PLATES, IAH- MAINTENANCE REMOVED and REPLACED THE CREASE BEAM, AND, THE AIRCRAFT WAS APROVED FOR RETURN TO SERVICE, WHEN RELEASED FRSDR C2XA02IA033Crease Beam · corrodedIAH- DURING "C" CHECK INSPECTION IT WAS NOTED THAT THE RIGHT CREASE BEAM BETWEEN FRAME 18 and 20 WAS CORRODED AROUND THE NUT PLATES. IAH- MAINTENANCE REMOVED AND REPLACED THE CREASE BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, WHEN RELEASED FSDR COMA0260086Skin PanelFLIGHT 9461 BIRDSTRIKE ON NOSE OF AIRCRAFT DURING T/O.C/W BIRDSTRIKE INSP - NO DAMAGE FOUND.SDR C2XA02CL031Firewall · crackedDURING ROUTINE MAINTENANCE THE APU FIREWALL WAS FOUND CRACKED AT UPPER RIGHT CORNER OF FIREWALL.THE FIREWALL WAS REPAIRED I/A/W EMBRAER GST-0401/02.THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR 2002UALA00185Intercostal · gougedCABIN FLOOR INTERCOSTAL AT STATION 395 TO 418 RBL 56" STRINGER 17R HAD DEEP GOUGES. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW INTERCOSTAL AND UPPER SURFACE JOGGLE FILLER.SDR C1HA200282006Seat Track · corrodedSEAT TRACK AT RBL 44 STA 344 TO STA 460 HAS CORROSION. (C CHECK FINDING) REPLACED SEAT TRACK SECTION PER SRM.SDR ABXA010713Frame · crackedFUSELAGE FRAME STATION 1152 WAS CRACKED AT LONGERON 15 RIGHT. REPAIRED CRACKED SECTION OF FRAME AT STATION 1152 LONGERON 15 RIGHT IAW DC-9 SRM 53-03.SDR ABXA010700Skin · corrodedCORROSION ON SKIN UNDER LONGERON 30 AT FUSELAGE 870. REMOVED CORROSION IAW DC-9 SRM 53-01. CUT-OUT PORTION OF SKIN PLATING THAT WAS CORRODED BEYOND LIMITS AND REPAIRED IAW DC-9 SRM 53-04.SDR ABXA010699Longeron · crackedLONGERON 30 AT F.S. 870 WAS CORRODED AND CRACKED UNDERNEATH FLANGES. REPLACED LONGERON 30 STATION 862 - 879 IAW DC-9 SRM 53-02. INSTALLED FORWARD AND AFT SPLICES AT STATION 862 - 879 IAW DC-9 SRM 51-30-5.SDR P5CA0200632Seat Track · crackedFORWARD CARGO COMPARTMENT BS 560 - RBL - 45, WL - 118 SEAT TRACK CRACKED. REPAIRED BY SPLICED IN SECTION OF SEAT TRACK IAW 400F SRM 53-00-52, PG 251SDR P5CA0200633Seat Track · crackedFORWARD CARGO COMPARTMENT BS 560 - LBL - 225, WL 118 SEAT TRACK CRACKED. REPAIRED BY SPLICED IN SECTION OF SEAT TRACK IAW 400 SRM 53-00-52, PG. 251SDR ABXA010682Skin · crackedDURING LINE MAINTENANCE VISIT, FUSELAGE SKIN WAS CRACKED AT THE FORWARD ENTRY DOOR, UPPER AFT CORNER, STATION 218, LONGERON 7 LEFT. REPAIRED FUSELAGE SKIN IAW DC-9 SRM.SDR ABXA010698Splice · crackedLONGERON SPLICE CRACKED F.S. 945 TO F.S. 965, LONGERON 22 LEFT. REPLACED SPLICE IAW DC-9 SRM.SDR ABXA010697Longeron · crackedLONGERON 29 LEFT WAS CRACKED BETWEEN STATION 313 TO STATION 332. REPLACED LONGERON 29 LEFT BETWEEN STATION 313 TO STATION 332 IAW DC-9 SRM.SDR ABXA010673Panel · corrodedLEFT SLANT PANEL CORRODED AROUND NUTPLATES. REPLACED SLANT PANEL IAW DC-9 SRM 51-30-1.SDR DHL2002805023Angle · crackedN/R1841NLG W/W DOOR FRAME ANGLE @ STA -99 RT. , CRACKED 1"SDR COMA0260009Doubler · crackedF.S. 718.00 STRINGER 11 R/H AND L/H AFT DOUBLERS ARE CRACKED.REMOVED AND REPLACED R/H AND L/H AFT DOUBLERS F.S. 718.00 STRINGER 11. I/A/W CANADAIR R.E.O. 601R-53-61-193 REV A.SDR DHL2002805011Skin · crackedN/R 0051NOSE LANDING GEAR WHEEL WELL R/H AFT CORNER CRACKED 1/4" STA.8.00 L33R (MAJOR REPAIR)SDR 2001UALA02418Intercostal · corrodedCABIN FLOOR STRUCTURE INTERCOSTAL AT STATION 324 TO 345 RBL 64" CORRODED ON UPPER SURFACE. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW U-SHAPED CHANNEL.SDR DL72S011896Frame · damagedREPAIRED STA 580 SHEAR TIE JUST OUTBD OF STR 28L PER SRM 53-10-4 FIG 15. SSI DATA RETRIEVAL FORM COMPLETED AND SENTSDR DL72S011895Frame · crackedMADE 2 EA REPAIRS TO STA 520 SHEAR TIES ON INBD AND OUTBD SIDES OF STR 28L PER SRM 53-10-4 FIG 15. SSI DATA RETRIEVAL FORM COMPLETED AND SENT.SDR 2001UALA02289Flange · dentedAFT PIT FRAME STATION 1460 UPPER FLANGE DENTED BETWEEN STRINGER 25L AND 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR SPLICE CHANNEL.SDR COMA0160892Skin · dentedFUSELAGE SKIN AT FS310.0 NEAR PAX DOOR HAS TEMPORARY REPAIR THAT REQUIRES PERMANENT REPAIR.PERFORMED A PERMANENT MAJOR REPAIR TO FUSELAGE SKIN AT FS 310.0 I/A/W CRJ REO 601R-53-21-180 AND WVAC EO 601R-53-2832.SDR ABXA010606Track · corrodedFIRST OFFICER'S FORWARD LEFT SEAT TRACK CORRODED AT FORWARD AND AFT MOUNT AREAS. REPLACED SEAT TRACK IAW DC-9 SRM 51-30-1.SDR ABXA010605Angle · crackedSMALL ANGLE CRACKED BENEATH KEEL, LOCATED RIGHT OF ANTI-COLLISION LIGHT WIRE FEED THROUGH. INSTALLED NEW ANGLE IAW DC-9 SRM 51-30-1 AND 51-30-5.SDR 2001UALA02259Crease Beam · corrodedMID CABIN CREASE BEAM BODY STATION 1000 TO BODY STATION 1020 AT STRINGER 17R HAS CORROSION ON UPPER SURFACE OF WEB. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. WEB REPLACED.SDR 2001UALA02258Crease Beam · corrodedMID CABIN CREASE BEAM BODY STATION 1020 TO BODY STATION 1040 AT STRINGER 17R HAS CORROSION ON UPPER SURFACE WEB. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.WEB REPLACED.SDR 2001UALA02257Intercostal · corrodedCABIN FLOOR INTERCOSTAL BELOW DOORWAY DRAIN GUTTER CORRODED ON UPPER SURFACE BETWEEN STA 324 AND 345, RBL 61 AT STRINGER 17R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED Z-ANGLE SHAPED INTERCOSTAL WITH NEW PART.SDR ABXA010587Skin · corrodedSKIN BULGED FROM CORROSION AT FORWARD LOWER CARGO DOOR CUTOUT BETWEEN STATION 386 AND 391. REPAIRED SKIN IAW DC-9 SRM.SDR ABXA010586Doubler · crackedRIGHT WINDOW DOUBLER CRACKED IN THE UPPER FORWARD CORNER OF WINDOW AT STATION 658. REPAIRED CRACK IAW DC-9 SSRM K07226.SDR HNAA010074Bracket · crackedAIRSTAIR DOOR THRESHOLD CENTER LOWER SUPPORT ANGLE BRACKET AT STATION X240.5 IS CRACKED. REPLACED BRACKET.SDR ABXA010578Frame · crackedFRAME AT F.S. 930 WAS CRACKED AT LONGERON 3 RIGHT. REPAIRED FRAME IAW DC-9 SSRM K05159.SDR HNAA0100072Threshold · corrodedAIRSTAIR DOOR THRESHOLD PLATE CORRODED ON TOP SURFACE UNDER PLASTIC STRIP. REPLACED THRESHOLD PLATE.SDR ABXA010574Longeron · crackedLONGERON 3 LEFT WAS CRACKED AT F.S. 160. REPLACED CRACKED LONGERON IAW DC-9 SRM 53-02.SDR DL72S011688Skin · crackedFOUND ON C2 LETTER CK 5/16 IN CRACK FUSELAGE SKIN R-1 DOOR LOWER AFT CUTOUT. REPAIRED PER ERA 381969-14 AND EO 4-58974-3AD.SDR P2EA2001M0008SkinDuring Inspection found Crack in fuselage skin at BS 847 and STR. 25R approx. 1.00" in length.See Vanguard Aircraft log page #92242SDR ABXA010545Clip · crackedSHEAR TIE WAS CRACKED BETWEEN LONGERON "0" AND "1" LEFT AT F.S. 1087, ON AFT SIDE. REPLACED CRACKED SHEAR TIE IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA010547Clip · crackedLEFT FUSELAGE FRAME SHEAR TIE WAS CRACKED AT STATION 945 BETWEEN LONGERON 15 LEFT AND 16 LEFT. REPAIRED SHEAR TIE IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA010542Support · cracked90 DEGREE FITTING WAS CRACKED ON THE END OF LONGERON 28 RIGHT, BOTTOM OF FLOOR PANEL SUPPORT BOTTOM SIDE F.S. 756. REPLACED SUPPORT IAW DC-9 SRM 51-30-1 AND 51-30-5.SDR C2XA01TY152Bushing · wornTYS During a scheduled inspection, the passenger door airframe fitting for the hold open hook has a displaced & loose lower pin bushing. Maintenance removed and replaced the bushing I.A.W.-EMB-GST-1682/01. Repair were satisfactory, Aircraft will be released tSDR ABXA010546Frame · crackedF.S. 737 WAS CRACKED ON THE FORWARD UPPER FLANGE BETWEEN THE OUTBOARD FASTENERS. FRAME WAS REPLACED ON JOB CARD E.A. 53400326-001-3.SDR ABXA010543Fitting · crackedRIGHT UPPER CARGO FLOOR BEAM VERTICAL ATTACH FITTING WAS CRACKED. REPLACED THE ATTACH FITTING IAW DC-9 SRM 51-30-5.SDR COMA0160792SkinFLIGHT #5572. CREW REPORTED A BIRD STRIKE, LEFT WING TIP.C/W BIRDSTRIKE INSPECTION AND NO DAMAGE WAS FOUND.SDR COMA0160801Frame · crackedL/H FRAME AT F.S. 718.00 BETWEEN STRINGERS 11 AND 12 IS CRACKED.PERFORMED A REPAIR ON THE 718.00 FRAME BETWEEN STRINGERS 11 AND 12 I/A/W CANADAIR REO 601R-53-61-193 REV A.SDR DHL2001801537Fitting · crackedAFT BULK HEAD JOINT FITTING CRACKED 1 1/2 IN STA 1966.000 L17R.REMOVED CRACKED FITTING PER SRM 51-1-20D PG 21.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20 PG 9.SDR COMA0160802Doubler · crackedR/H AFT DOUBLER AT F.S.718.00 BETWEEN STRIGER 11 AND 12 IS CRACKED.REMOVED CRACKED R/H AFT DOUBLER AT F.S. 718.00 AND INSTALLED NEW DOUBLER I/A/W CANADAIR REO 601R-53-61-193 REV A.
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