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 USAA010839Frame · crackedCLT - FOUND FRAME STIFFENER CRACKED .5 INCH, RESULTING IN MISSING MATERIAL, BS 360, LEFT SIDE OF A/C AT FRAME, WL 215. INSTALLED STRAP AND FILLER PER EA 85025. (M)SDR USAA010842FrameCLT - FOUND FRAME WITH TWO HOLES .1875 INCH, BS 500A, RIGHT SIDE TRANSITION ANGLE, FORWARD CARGO HOLD. DAMAGE REMOVED, INSTALLED FRAME SPLICE PER EA 85041. (M)SDR USAA010843Frame · dentedCLT - FOUND FRAME DENTED 1 INCH DIAMETER, BS 1064, 2 INCHES OUTBOARD OF STRINGER 2R. DAMAGED REMOVED, INSTALLED DOUBLER PER EA 69827. (M)SDR USAA010844FrameCLT - FOUND FRAME WITH HOLE .375 INCH, BS 807, AT TIE CLIP FOR STRINGER 27R. INSTALLED DOUBLER PER SRM 51-70-11. (M)SDR USAA010846Skin · gougedCLT - FOUND FUSELAGE SKIN DENTED WITH GOUGE 2 INCHES IN DIAMETER, BS 500B BETWEEN STRINGERS 25 AND 26R. DAMAGE REMOVED, INSTALLED REPAIR PER SRM 53-00-01, FIG 210. (M)SDR USAA010847SkinCLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY INSTALLED DOUBLER 41 INCHES BY 23 INCHES, BS 380, STRINGER 26 TO 27R. INSTALLED NEW DOUBLER PER EO 5300V258 AND TR 53-30-07. (M)SDR USAA010869Skin · crackedTPA - FOUND DOOR EXTERIOR SKIN CRACKED .25 INCH, AFT ENTRY DOOR, UPPER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 52-10-01 AND SERVICE BULLETIN 737-52-1096. (M)SDR DL72S011178Web · crackedFOUND ON E2 LETTER CK R/H INBD VERT TORQUE BOX WEB CRACKED AT UPPER END STA 1214 R/H. REPAIRED PER MM 53-11-000-8.SDR DL72S011177Clip · crackedFOUND ON E2 LETTER CK SKIN CLIP CRACKED FWD STA 1263 ABOVE STR 12R. REPAIRED PER B727 DAL DRD 53-10-4D FIG 803D.SDR AALA20011539Seat TrackTUL - FOUND STATION 256 LEFT LOOSE HARDWARE UNDER SEAT TRACK FLANGE, FLANGE BENT/CRACKED, NR 1 SEAT TRACK. REPAIRED NR 1 SEAT TRACK AT STATION 256 LEFT WITH SPLICE REPAIR PER SRM 53-05. (M)SDR USAA010880Angle · crackedCLT - FOUND WEB ANGLE CRACKED 1.25 INCH, BS 303.9, STRINGER 10L. REMOVED AND REPLACED ANGLE PER SRM 51-10-1. (M)SDR RRXA11412Fitting · corrodedDURING A MAINTENANCE VISIT FOUND C-PIT BACK UP FITTING FOR #1 LWRT LATCH HAS HEAVY CORROSION ON FWD SIDE STA 1168 BETWEEN L33R I/B AND L32R O/B. *** CORRECTIVE ACTION *** REMOVED BACKUP FITTING , REF SRM 51-1-20D. RECEIVED NEW FITTING AND CLIPS. TRIMMED NEWSDR USAA010799BeamPIT - FOUND APU INLET RIGHT BEAM WITH HOLE 2.5 INCHES BY 4 INCHES APU AIR INLET BEAM, FUSELAGE RIGHT STATION 22516-26026. MANUFACTURED REPAIR SPLICE AND CORNER BRACKET RIGHT SIDE APU INLET SCOOP PER EA. (M)SDR AWXA0002009Beam · crackedD: Aft lower cargo door lower beam Tee cracked 1" at aft end BS 838C: Repaired aft lower cargo door Tower beam Tee at aft BS 838 IAW E.O. 52-33-01SDR AALA20011532Skin · gougedTUL - FOUND DEEP GOUGE IN FUSELAGE SKIN AT STATION 1305 ABOVE LONGERON 19R. INSTALLED SCUFF PLATE PER AARD 53-30-00-8. (M)SDR AALA20011535LongeronTUL - FOUND LONGERON 3L CRACKED AT OUTBOARD LEG AT FASTENER AFT SIDE OF STATION 160. INSTALLED SECTION OF LONGERON AND SPLICE PER SRM 53-02. (M)SDR AALA20011474Seat Track · corrodedTUL - FOUND CORROSION ON SEAT TRACK NR 4, STATION 435. CUT OUT CORRODED AREA AND INSTALLED PLUG PER HARD 53-20-00-10. (M)SDR AALA20011538Seat Track · corrodedTUL - FOUND NR 2 SEAT TRACK CORRODED STATION 1190-1201. REMOVED DAMAGED AREA OF NR 2 SEAT TRACK AT BS 1190-1201. INSTALLED SEAT TRACK PLUG, TREATED AND PRIMED PER SRM 53-05 FIG 4A. (M)SDR AALA20011537Seat Track · corrodedTUL - FOUND CORROSION ON SEAT TRACKS NR 5 AT BS 200-216. INSTALLED STRAP PER AARD 53-20-00-13 AFTER REMOVAL OF CORROSION THEN TREATED, PRIMED AND PAINTED. (M)SDR AALA20011536Seat Track · corrodedTUL - FOUND NR 1 SEAT TRACK CORRODED STATION 1200-1210. REMOVED DAMAGED AREA ON NR 1 SEAT TRACK AT STATION 1200-1210. INSTALLED SEAT TRACK PLUG, TREATED AND PRIMED PER SRM 51-10-3 AND 53-05 PAGE 4A. (M)SDR AALA20011475Longeron · crackedTUL - FOUND CRACK AROUND FASTENER AT FS 160 LONGERON 4L. REMOVED LONGERON FROM FS 149-174. INSTALLED NEW LONGERON AND SPLICED PER SRM 53-02 FIG 18 AND SRM 53-14-1. (M)SDR TSAA0153085Skin · crackedFOUND FUSELAGE SKIN CRACKED AT FORWARD GALLEY DOOR UPPER DOOR HINGE CUTOUT. TRIMMED OUT DAMAGE AREA TO MAINTAIN A MINIMUM RADIUS OF .70 INCH, HFEC INSPECTION AROUND CUTOUT AREA NO DEFECTS NOTED. FABRICATED AND INSTALLED .50 INCH 2024-T3 FILLER AND .063 INCH SDR SIMA200119702Frame · damagedABI - DURING MBV INSPECTION, MAINTENANCE FOUND FRAME 630.12 WAS DAMAGED ON THE RIGHT SIDE ABOVE WL 73.5. DAMAGE WAS REPAIRED IAW SAAB SRM AND AIRCRAFT WS RETURNED TO SERVICE. (M)SDR SIMA200119704Frame · damagedABI - DURING MBV INSPECTION MAINTENANCE, FOUND FRAME 658.5 TO HAVE WEB DAMAGE ON THE RIGHT SIDE ABOVE WL 73.5 DAMAGE WAS REPAIRED IAW SAAB 340 SRM AND AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200119705Frame · damagedABI - DURING MBV INSPECTION MAINTENANCE, FOUND FRAME 668 TO BE DAMAGED ON THE RIGHT SIDE ABOVE WL 73.5 DAMAGED WAS REPAIRED IAW SAAB SRM AND AIRCRACT WAS RETURNED TO SERVICE. (M)SDR SIMA200119706Frame · damagedABI - DURING MBV INSPECTION, FOUND FRAME 677 TO BE DAMAGED ON THE RIGHT ABOVE WL 73.5 DAMAGE WAS REPAIRED IAW SRM AND AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR AWXA0002129Angle · corrodedD: During "D" check inspection found frame angle aft side 1088 bulkhead, top side of torque box at duct inlet corrodedC: Removed and replaced frame angle aft side 1088 Bulkhead top side or torque box at duct inlet IAW B737 SRM 51-30-2SDR USAA010790Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 867, BETWEEN STRINGERS 8 AND 9L. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-10-14. (M)SDR USAA010791Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 867, BETWEEN STRINGERS 8 AND 9R. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-10-14. (M)SDR USAA010784Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 400, BETWEEN STRINGER 8 AND 9L. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M)SDR USAA010787Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 727D, BETWEEN STRINGERS 8 AND 9R. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-10-14. (M)SDR USAA010788Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 787 BETWEEN STRINGERS 8 AND 9R. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-10-14. (M)SDR AALA20011470Seat Track · corrodedTUL - FOUND CORROSION ON SEAT TRACK NR 2, STATION 1200. REMOVED CORROSION, INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A. (M)SDR AALA20011409Shear Tie · corrodedTUL - FOUND CORROSION ON SHEAR TIE BS 720A AT STRINGER 28. REMOVED CORROSION AND REMOVED DAMAGED AREA, AND REPAIRED PER SRM 53-10-04. (M)SDR COMA0160477Angle · corrodedAFT "J" ANGLE AT F.S. 280 IS CORRODED BETWEEN LBL9 AND RBL 9.REMOVED DAMAGED, FABRICATED AND INSTALLED SPLICE "J" ANGLE I/A/W WVAC EO 601R-53-2552A.SDR COMA0160476Channel · corroded"U" CHANNEL P/N 601R31527-141 AT F.S. 349.00 IS CORRODED.REMOVED AND REPLACED "U" CHANNEL P/N 601R31527-141 AT F.S. 349.00 I/A/W WVAC EO 601R-53-2558.SDR COMA0160447Angle · crackedVERTICAL "J" ANGLES LOCATED INSIDE CBPI, CBP2 AT BL9 L/H AND R/H ARE CRACKED.REMOVED DAMAGED "J" ANGLES, FABED NEW ANGLES AND INSTALLED I/A/W WVAC E.O. 601R-53-2544.SDR COMA0160473Beam · corrodedTHE FLOOR BEAM WEB AT F.S. 280.00 IS CORRODED ON UPPER EDGE BETWEEN RBL9 AND LBL9.TRIMMED OUT DAMAGED AREA, FABED FILLER, FABED REPAIR DOUBLER, AND INSTLALED I/A/W WVAC E.O. 601R-53-2553.SDR COMA0160445Angle · corrodedTHE THRESHOLD SUPPORT ANGLE AT THE PASSENGER DOOR IS SEVERELY CORRODED.REMOVED CORRODED THRESHOLD ANGLE P/N 601R31527-221, FABED NEW THRESHOLD ANGLE AND INSTALL I/A/W W.V.A.C. T.O. 601R-53-2557.SDR COMA0160472Threshold · corrodedTHE THRESHOLD/SILL PANEL AFT OF THE SERVICE DOOR IS CORRODED.TRIMMED THRESHOLD AREA, FABED SPLICE ANGLE AND INSTALLED I/A/W WVAC EO 601R-53-2554A.SDR COMA0160471Doubler · corrodedDOUBLER P/N 601R38669-49 FWD OF SERVICE DOOR IS CORRODED.REMOVED AND REPLACED DOUBLER P/N 601R38669-49 FWD OF SERVICE DOOR I/A/W WVAC E.O. 601R-53-2550.SDR COMA0160470Angle · corrodedTHE FWD "J" ANGLE AT F.S. 280.00 BETWEEN LBL9 AND RBL 9 IS CORRODED.REMOVED AND REPLACED FWD "J" ANGLE AT FS 280.00 BETWEEN LBL9 AND RBL9 I/A/W WVAC E.O. 601R-53-1551.SDR COMA0160446Beam · corrodedTHE FLOOR BEAM WEB AT F.S. 280.00 IS CORRODED ON UPPER EDGE BETWEEN RBL9 AND LBL9.TRIMMED OUT DAMAGED AREA, FABED FILLER, FABED REPAIR DOUBLER, AND INSTLALED I/A/W WVAC E.O. 601R-53-2553.SDR COMA0160444Threshold · corrodedTHE THRESHOLD/SILL PANEL AFT OF THE SERVICE DOOR IS CORRODED.TRIMMED THRESHOLD AREA, FABED SPLICE ANGLE AND INSTALLED I/A/W WVAC EO 601R-53-2554A.SDR COMA0160443Doubler · corrodedDOUBLER P/N 601R38669-49 FWD OF SERVICE DOOR IS CORRODED.REMOVED AND REPLACED DOUBLER P/N 601R38669-49 FWD OF SERVICE DOOR I/A/W WVAC E.O. 601R-53-2550.SDR COMA0160442Angle · corrodedTHE FWD "J" ANGLE AT F.S. 280.00 BETWEEN LBL9 AND RBL 9 IS CORRODED.REMOVED AND REPLACED FWD "J" ANGLE AT FS 280.00 BETWEEN LBL9 AND RBL9 I/A/W WVAC E.O. 601R-53-1551.SDR USAA010865Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED, AFT END OF AIRSTAIR HANDLE CUTOUT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-30-03. (M)SDR RRXA11400Fitting · crackedDURING A MAINTENANCE VISIT FOUND MAIN CARGO DOOR LATCH FITTING BACK-UP FITTING CRACKED BELOW CUSP ANGLE STA 140 AND CUSP JOINT TO LBL 48. *** CORRECTIVE ACTION *** REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3772916 AND DC8 SRM 51-1-20D AND 53-1-0SDR AALA20011403Skin · corrodedTUL - FOUND SKIN BULGING IN AREA PREVIOUSLY WORKED, SKATE ANGLE (APPEARS TO BE RE-CORRODING) JUST ABOVE RIGHT NOSE GEAR STRUT DOOR .294.5 TO 335. SKIN BULGING AROUND REPAIR AREA FASTENERS, SIX INCHES ABOVE SKATE ANGLE STATION 295-333. REPAIRED AREA PER ESO 1SDR GAIA01257STFrameDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 380 FRAME HAS SEVERAL HOLES IN THE INBOARD RADIUS BETWEEN STRINGER 4-7L. ACCOMPLISHED BS 380 FRAME REPAIR STRINGER 4-7. IAW B727 SRM 53-10-4 FIG 1. FASI NON ROUTINE 08343. (M)
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