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 COMA0160519Angle · corrodedFORWARD J ANGLE AT FS 280 BETWEEN LBL9 AND RBL9 CORRODED.REMOVED AND REPLACED FORWARD J ANGLE I/A/W WVAC EO 601R-53-2588.SDR COMA0160518Threshold · corrodedLBL42 THRESHOLD JUST AFT OF PAX DOOR CORRODED.REMOVED AND REPLACED THRESHOLD WEB I/A/W WVAC EO 601R-53-2590A.SDR COMA0160517Angle · crackedVERTICAL J ANGLE CLIPS LOCATED INSIDE CBP1/CBP2 AT BL9 LEFT AND RIGHT ARE CRACKED.REMOVED AND REPLACED I/A/W WVAC EO 601R-53-2586.SDR COMA0160516Doubler · corrodedDOUBLER P/N 601R38669-49 FWD OF SERVICE DOOR IS CORRODED.REMOVED AND REPLACED I/A/W WVAC EO 601R-53-2587.SDR COMA0160514Channel · corrodedFORWARD AND AFT PAX DOOR U-CHANNELS CORRODED.REMOVED AND REPLACED U-CHANNELS I/A/W WVAC EO 601R-53-2584.SDR COMA0160513Angle · corrodedTHRESHOLD SUPPORT ANGLES AT PAX DOOR CORRODED.REMOVED AND REPLACED I/A/W WVAC EO 601R-53-2575.SDR COMA0160512Angle · corrodedFORWARD J-ANGLE AT FS 280 BETWEEN LBL9 AND RBL9 CORRODED.REMOVED AND REPLACED I/A/W WVAC EO 601R-53-2576.SDR AALA20011534FrameTUL - FOUND TWO WEAR MARKS IN FRAME STATION 522 BETWEEN LONGERON 23L AND 24L 5 INCH APART. TRIMMED OUT DAMAGED AREAS TWO OUT OF LIMITS, J-ANGLE .010 INCH 17.7 CRS HEAT TREAT TO TH1050 ATTACH WITH HI-LOCKS, INSTALLED DOUBLER PER ESO 80554 DATED 7/19/2001. (M)SDR UIEA01074Skin · crackedDURING HFEC INSPECTION FOUND THE LOWER AFT CARGO COMPARTMENT DOOR CUTOUT, UPPER FORWARD CORNER SKIN CRACKED AT STATION 1814, STRINGER 27R. CRACK TRIMMED AWAY. FILLER AND REPAIR DOUBLER FABRICATED AND INSTALLED PER STANDARD PRACTICES IAW SRM 53-30-03 FIG 60 TSDR ABXA010426Angle · crackedSUPPORT STRUT MOUNT ANGLE CRACKED AT UPPER OUTBOARD SIDE OF THE LEFT WHEEL WELL. REPLACED ANGLE AND INSTALLED IAW DC-9 SRM 51-30-5.SDR USAA010965Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .5 INCH, BS 1661 TO 1681. REMOVED AND REPLACED PER SRM 51-10-00. (M)SDR USAA010964Skin · dentedCLT - FOUND SKIN DENTED APPROX 3 INCHES BY 6 INCHES, BS 740 PLUS 1 INCH, BETWEEN S15R AND S16R. INSTALLED DOUBLER PER EA 85087. (M)SDR QXEA0101183Structure · dentedPDX - DENT IN SIDE OF FUSELAGE APT APPROXIMATELY 40 INCHES AFT OF MAIN CABIN DOOR WL 22.047 AND FS 238.779. REPAIRED IAW HORIZON AIR EA 4-53-1513 AND FOKKER SRM 51-31-01.SDR COMA0160492Angle · misdrilledTHE CLEAT FOR LBL27 AT F.S. 364.0 WAS MISDRILLED WHILE INCORPORATING SB601R-53-037 (TITANIUM FLOOR BEAM MOD).FABRICATED AND INSTALLED A NEW CLEAT I/A/W WVAC EO 601R-53-2583.SDR AALA20011481Skin · dentedTUL - FUOND FUSELAGE SKIN DENTED AT RIVET STATION 266 ABOVE LONGERON 23R. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEET 24. (M)SDR USAA010894Skin Panel · buckledCLT - FOUND SKIN PANEL BUCKLED APPROXIMATELY 3 SQUARE INCHES, KEEL BEAM STATION 663 TO 685. REMOVED AND REPLACED KEEL BEAM LOWER PANEL PER SRM 51-10-02. (M)SDR USAA010895Fitting · corrodedCLT - FOUND FITTING CORRODED 3 INCHES BY 2 INCH AREA, BS 727, STRINGER 27R, AFT CARGO COMPARTMENT. CORROSION LEVEL 2 TASK NR C53-202-01. FABRICATED AND INSTALLED FITTING PER BAC DRAWING NR 65-73746 AND SRM 51-10-02. (M)SDR USAA010898Frame · corrodedCLT - FOUND FRAME CORRODED 14 INCH AREA, BS 727B, LEFT AND RIGHT KEEL BEAMS, LOWER FLANGE. REMOVED DAMAGE, INSTALLED NEW FRAME SECTION PER SRM 51-40-02 AND 51-40-05. (M)SDR USAA010911Frame · dentedCLT - FOUND FRAME DENTED .5 INCH IN DIAMETER, BS 1600, BETWEEN S25R AND S26R. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER EA 69860. (M)SDR SIMA200120010Seat Track · corrodedSBP - FOUND CABIN SEAT TRACK AT STATION BL 00.0 IS CORRODED ON THE LOWER INBOARD FLANGE EXTENDING FROM ENTRY WAY TO CARGO AREA, TRACK WAS PREVIOUSLY GROUND. REMOVED AND REPLACED TRACK ASSEMBLY IAW SAAB SRM 53-70-60. (M)SDR USAA010927Bulkhead · crackedPIT - FOUND BULKHEAD WITH CRACKS, ONE AT 1 INCH, ONE AT 1.125 INCH, TWO AT 1.5 INCH AND TWO AT .125 INCH, BS 178 LBL 5.7 WL 216; BL 0, WL 184 - WL 195; RBL 5. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER SRM 53-10-08, EO 5300V152, EO 5300V153. (M)SDR USAA010887Stringer · corrodedCLT - FOUND STRINGER CORRODED 14 INCHES BY 2.5 INCHES, BS 907 TO 927, S25L, BELOW AFT CARGO FLOOR. REMOVED AND REPLACED STRINGER PER SRM 51-40-02. (M)SDR DKAA01017PanelDURING 12 YEAR CORROSION INSPECTION OF CENTER WING FUEL TANK, REMOVABLE PANEL STIFFENER WAS FOUND CRACKED AT THE END OF THE STIFFENER. DASSAULT ENGINEERING WAS CONTACTED AND PROVIDED CHANGE APPROVAL SHEET R245. STIFFENER WAS TRIMMED AND RE-INSPECTED TO ENSURSDR AALA20011529Seat Track · corrodedTUL - FOUND NR 2 SEAT TRACK HAS CORROSION IN CHANNEL, BS 219. CUT OUT DAMAGED SEAT TRACK FROM BS 200-246 PER SRM 53-05 FIG 4F. (M)SDR AALA20011482Frame · crackedTUL - FOUND RIGHT CANT FRAME 1485, RT LOWER END, IS WORN AND CRACKED FROM CONTACT WITH ACTUATOR CASTING. INSTALLED REPAIR DOUBLER AS PER AARD 53-10-00-33 AND RE-INSTALLED FRAME STIFFENER. (M)SDR AALA20011460Web · crackedTUL - FOUND CRACK IN FORWARD AND AFT SIDE OF 870 WEB AT APU LOAD CONTROL DISCHARGE CUT-OUT. INSTALLED REPAIR DOUBLER PER SRM 53-10-2 FIG 1, SHEET 2. (M)SDR AALA20011462Skin · corrodedTUL - FOUND FUSELAGE SKIN RIVET SHEARED AT STATION 1050 INBOARD OF STRINGER 27R NEAR REPAIR DOUBLER, CORROSION ON SKIN. FOUND RIVET SHEARED FROM CORROSION. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-3. (M)SDR USAA010872Stiffener · corrodedTPA - FOUND STIFFENER CORRODED APPROXIMATELY 3 SQUARE INCHES, BS 1016, BETWEEN S28L AND S28R, AFT PRESSURE BULKHEAD. FORMED SECTION REPAIR INSTALLED PER SRM 51-70-11, SRM 53-80-08, SB 737-53A-1075, AND EA 85096. (M)SDR USAA010864Skin · crackedCLT - FOUND SKIN CRACKED .0625 INCH, BS 303, WL 259.88 MED UPPER HINGE CUTOUT. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 AND EA 85093. (M)SDR USAA010868Skin · crackedCLT - FOUND UPPER WING SKIN CRACKED .25 INCH, LEFT WING WBL 165.5 AT REAR SPAR, BS 178. INSTALLED DOUBLER AND TRIPLER PER EA 85075. (M)SDR C2XA01BT141Beam · corrodedYUL---CO4378, DURING 4C INSPECTION YUL MAINTENANCE FOUND FLOOR BEAM (IN COCKPIT) AT FR9 TO BE CORRODED....MAINTENANCE REMOVED AND REPLACED (NEW) BEAM IAW ATR42 SRM 51-25-01.SDR USAA010882Stringer · corrodedTPA - FOUND STRINGER CORRODED 4 INCH AREA, STRINGER 26 RIGHT AT STATION 1016. CORROSION LEVEL 2. REPAIRED STRINGER PER SRM 53-00-02 FIG 201. (M)SDR USAA010873Skin · corrodedTPA - FOUND PRESSURE BULKHEAD SKIN CORRODED APPROX 4 SQUARE INCH AREA, BS 1016, BETWEEN S28L AND S28R. DAMAGE REMOVED, INSTALLED DOUBLER PER EA 85096 AND SB 737-53A-1075. (M)SDR 01FDEA00575Frame · crackedN 240 THERE IS CRACK ON FRAME AT Y=459, X=18 AT FRAME SPLICE INCLUDE IS A PREVIOUS REPAIR FROM X=18 TO X=18. R&R FRAME PER IAW EA & SRM.SDR AALA20011484Stringer · crackedTUL - FOUND CRACKS IN UPPER LEG STRINGER 5R AT STATION 340. ROUTED OUT CRACKED AREAS, INSTALLED TWO J-ANGLE REPAIRS PER SRM 53-10-3. (M)SDR AALA20011540Skin · dentedTUL - FOUND LEFT FUSELAGE HAS DENT 1.5 INCHE BY 1.5 INCHE BY .0555 INCH ABOVE LAV SERVICE PANEL WITH POSSIBLE CRACK .8 INCH LONGERON. CUT OUT DAMAGED AREA OF SKIN, CUT TITANIUM DOUBLER, INSTALLED INTERNAL FINGER DOUBLER PER SRM 53-04 FIG 38. (M)SDR AALA20011533LongeronTUL - FOUND LONGERON 17 LEFT BENT AT BLIND FASTENER REPAIR AREA STATION 250 SKIN ALSO DENTED SAME AREA. CUT OUT DAMAGED SECTION OF LONGERON SPLICED IN NEW SECTION OF LONGERON WITH 2 SPLICES PER SRM 53-02 FIG 18 SHEET 1. SKIN REPAIRED ON E-58-3 9069497. (M)SDR AALA20011471SkinTUL - FOUND SEVERAL DEEP TOOL MARKINGS AROUND RIVET HEAD RIGHT STATION 249 LONGER 21R, FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)SDR AALA20011479Frame · damagedTUL - FOUND DAMAGE TO CARGO FRAME STATION 712, BETWEEN 26L AND 27L. INSTALLED DOUBLER PER AARD 53-10-00-4. (M)SDR USAA010814Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 807, BETWEEN STRINGER 8 AND 9R. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14. (M)SDR USAA010824Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED TWO PLACES .25 INCH, BS 663, STRINGER 10R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02. (M)SDR USAA010826Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 887 BETWEEN STRINGER 8 AND 9L. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M)SDR USAA010828Frame · crackedCLT - FOUND FRAME CRACKED APPROXIMATELY .25 INCH, BS 847, BETWEEN STRINGER 8 AND 9L. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M)SDR USAA010829Frame · crackedCLT - FOUND FRAME CRACKED APPROX .25 INCH, BS 847, BETWEEN STRINGER 8 AND 9R. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M)SDR USAA010830Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED .25 INCH, BS 727C, STRINER 24L. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER SRM 53-00-01, FIG 225. (M)SDR USAA010831Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, BS 616, RIGHT CREASE BEAM, INNER CHORD ANGLE. DAMAGE REMOVED, INSTALLED REPAIR ANGLE AND FILLER PER TYPICAL REPAIR 53-62-01. (M)SDR USAA010832Door Frame · crackedCLT - FOUND DOOR FRAME CRACKED TWO PLACES 1 INCH EACH, BS 294.5, RBL 55, STRINGER 17R. INSTALLED REPAIR DOUBLER PER SRM 51-70-11. (M)SDR USAA010834Frame · crackedCLT - FOUND FRAME CRACKED 3 INCHES, BS 954, BETWEEN STRINGER 9 AND 10R, INNER RADIUS. DAMAGE REMOVED, INSTALLED NEW PARTS PER SRM 51-40-03, 51-40-02 AND BAC DRAWING NR J65-46561. (M)SDR USAA010837Beam · crackedCLT - FOUND BEAM CRACKED .5 INCH, BS 707 TO 711, BBL 0, LOWER ROW OF FASTENERS. INSTALLED REPAIR DOUBLER PER EA 69679 AND SB 737-57-1210 FIG 5. (M)SDR USAA010838Web · crackedCLT - FOUND WEB CRACKED INTERIOR CABIN 1 INCH, BS 947.8, AFT ENTRY DOOR, UPPER HINGE CUTOUT. INSTALLED RE-INFORCING STRAP PER EA 69847. (M)
Back to JASC 5300