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.

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)Jul 16, 2001 · N371US · Boeing 7373B7SDR 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)Jul 16, 2001 · N371US · Boeing 7373B7SDR USAA010843Frame · dentedCLT - FOUND FRAME DENTED 1 INCH DIAMETER, BS 1064, 2 INCHES OUTBOARD OF STRINGER 2R. DAMAGED REMOVED, INSTALLED DOUBLER PER EA 69827. (M)Jul 16, 2001 · N371US · Boeing 7373B7SDR USAA010844FrameCLT - FOUND FRAME WITH HOLE .375 INCH, BS 807, AT TIE CLIP FOR STRINGER 27R. INSTALLED DOUBLER PER SRM 51-70-11. (M)Jul 16, 2001 · N371US · Boeing 7373B7SDR 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)Jul 16, 2001 · N371US · Boeing 7373B7SDR 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)Jul 16, 2001 · N371US · Boeing 7373B7SDR 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)Jul 16, 2001 · N384US · Boeing 7373B7SDR 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.Jul 16, 2001 · N544DA · Boeing 727232SDR 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.Jul 16, 2001 · N544DA · Boeing 727232SDR 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)Jul 15, 2001 · N438AA · Doug DC983SDR USAA010880Angle · crackedCLT - FOUND WEB ANGLE CRACKED 1.25 INCH, BS 303.9, STRINGER 10L. REMOVED AND REPLACED ANGLE PER SRM 51-10-1. (M)Jul 15, 2001 · N255AU · Boeing 737201SDR 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 NEWJul 14, 2001 · N873SJ · Doug DC873FSDR 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)Jul 14, 2001 · N860US · Fokker F28MK0100SDR 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. 52-33-01Jul 14, 2001 · N182AW · Boeing 737277SDR AALA20011532Skin · gougedTUL - FOUND DEEP GOUGE IN FUSELAGE SKIN AT STATION 1305 ABOVE LONGERON 19R. INSTALLED SCUFF PLATE PER AARD 53-30-00-8. (M)Jul 13, 2001 · N438AA · Doug DC983SDR 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)Jul 13, 2001 · N438AA · Doug DC983SDR 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)Jul 13, 2001 · N7522A · Doug DC982SDR 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)Jul 12, 2001 · N488AA · Doug DC982SDR 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)Jul 12, 2001 · N438AA · Doug DC983SDR 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)Jul 12, 2001 · N438AA · Doug DC983SDR 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)Jul 12, 2001 · N522AA · Doug DC982SDR 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 Jul 12, 2001 · N806AL · Boeing 7372S2CSDR 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)Jul 12, 2001 · N340RC · Saab 340BSDR 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)Jul 12, 2001 · N340B · Beech 95C55SDR 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)Jul 12, 2001 · N340RC · Saab 340BSDR 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)Jul 12, 2001 · N340RC · Saab 340BSDR 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 51-30-2Jul 10, 2001 · N187AW · Boeing 737277SDR USAA010790Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 867, BETWEEN STRINGERS 8 AND 9L. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-10-14. (M)Jul 10, 2001 · N440US · Boeing 7374B7SDR USAA010791Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 867, BETWEEN STRINGERS 8 AND 9R. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-10-14. (M)Jul 10, 2001 · N440US · Boeing 7374B7SDR USAA010784Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 400, BETWEEN STRINGER 8 AND 9L. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M)Jul 10, 2001 · N440US · Boeing 7374B7SDR USAA010787Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 727D, BETWEEN STRINGERS 8 AND 9R. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-10-14. (M)Jul 10, 2001 · N440US · Boeing 7374B7SDR USAA010788Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 787 BETWEEN STRINGERS 8 AND 9R. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-10-14. (M)Jul 10, 2001 · N440US · Boeing 7374B7SDR 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)Jul 9, 2001 · N7522A · Doug DC982SDR 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)Jul 9, 2001 · N726AA · Boeing 727227SDR 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.Jul 8, 2001 · N916CA · Cndair CL6002B19SDR 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.Jul 8, 2001 · N916CA · Cndair CL6002B19SDR 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.Jul 8, 2001 · N916CA · Cndair CL6002B19SDR 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.Jul 8, 2001 · N916CA · Cndair CL6002B19SDR 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.Jul 8, 2001 · N916CA · Cndair CL6002B19SDR 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.Jul 8, 2001 · N916CA · Cndair CL6002B19SDR 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.Jul 8, 2001 · N916CA · Cndair CL6002B19SDR 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.Jul 8, 2001 · N916CA · Cndair CL6002B19SDR 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.Jul 8, 2001 · N916CA · Cndair CL6002B19SDR 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.Jul 8, 2001 · N916CA · Cndair CL6002B19SDR 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.Jul 8, 2001 · N916CA · Cndair CL6002B19SDR 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.Jul 8, 2001 · N916CA · Cndair CL6002B19SDR USAA010865Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED, AFT END OF AIRSTAIR HANDLE CUTOUT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-30-03. (M)Jul 7, 2001 · N269AU · Boeing 7372B7SDR 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 53-1-0Jul 6, 2001 · N873SJ · Doug DC873FSDR 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 1Jul 6, 2001 · N726AA · Boeing 727227SDR 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)Jul 6, 2001 · N6827 · Boeing 727223
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