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 AALA20011161Skin · corrodedTUL - FOUND CORROSION AT STRINGER END FITTING STATION 1183 STRINGER 27R. INSTALLED REPAIR DOUBLER PER ESO 11697 DATED 5/24/01. (M)May 24, 2001 · N866AA · Boeing 727223SDR SIMA200114403Seat Track · corrodedSAW - DURING MBV-1 INSPECTION MAINTENANCE REPORTED RIGHT AFT INBOARD AND LEFT AFT INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. (M)May 24, 2001 · N270AT · Aerosp ATR72212SDR AALA20011162Web · crackedTUL - FOUND NR 2 CARGO DOOR FUSELAGE CUT OUT, FORWARD DOOR JAMB WEB CRACKED AT BOTTOM DOOR STOP FITTING. INSTALLED DOUBLER PER S/B 727-53A0199. (M)May 23, 2001 · N866AA · Boeing 727223SDR USAA010585Skin · corrodedPIT - FOUND SKIN CORRODED 1 INCH BY 2 INCHES, STATION 969 BETWEEN RIGHT STRINGER 27 AND 28. CORROSION LEVEL 1, TASK NR C53-208-01. INSTALLED DOUBLER PER EA NR 70922. (M)May 22, 2001 · N522AU · Boeing 7373B7SDR SIMA200114312Skin · corrodedABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE AFT GALLEY DIGITAL TO BE CORRODED. MAINTENANCE REPAIRED AFT GALLEY DIGITAL IAW EMB GST 1630/01. (M)May 21, 2001 · N701MH · Emb EMB135LRSDR SIMA200114311Skin · corrodedABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE FORWARD GALLEY DIGITAL CORRODED. MAINTENANCE REPAIRED THE GALLEY DIGITAL IAW EMB REPAIR STATEMENT GST-1630/01. (M)May 21, 2001 · N701MH · Emb EMB135LRSDR SIMA200114310Skin · corrodedABI - DURING MBV MAINTENANCE, FOUND CORROSION IN THE OMEGA BEAM. MAINTENANCE REPAIRED OMEGA BEAM IAW EMB SRM 53-21-10. (M)May 21, 2001 · N701MH · Emb EMB135LRSDR QXEA0100952Skin · dentedYYC - OUTWARD DENT FOUND BETWEEN FRAME 9305 AND 9305A AT STRINGER 3. REPAIRED IAW FOKKER SRM 53-02-01, FIGURE 1, PAGE 3.May 21, 2001 · N481US · Fokker F28MK4000SDR USAA010588Frame · crackedPIT - FOUND FRAME CRACKED 1.25 INCH, LEFT SIDE TOP OF OBLIQUE FRAME 67.2. TEMPORARY REPAIR WITH STOP DRILL PER EA 71082 AND SRM 51-22-01. (M)May 19, 2001 · N887US · Fokker F28MK0100SDR SIMA20011403Skin · corrodedABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE FORWARD DIGITAL CORRODED. CORROSION WAS REMOVED AND A DOUBLER WAS INSTALLED IAW EMB GST-1595/01. (M)May 18, 2001 · N638AE · Emb EMB145LRSDR SIMA20011404Skin · corrodedDURING MBV INSPECTION, MAINTENANCE FOUND THE OMEGA BEAM AT FRAME 20 CORRODED. MAINTENANCE REMOVED CORROSION AND INSTALLED DOUBLER REPAIR IAW EMB GST 1630/01. (M)May 18, 2001 · N701MH · Emb EMB135LRSDR USAA010556Shear Tie · corrodedCLT - FOUND FRAME SHEAR TIE CORRODED 5 INCHES BY 1 INCH, BS 986 STRINGER 24R/25R. FABRICATED AND REPLACED SHEAR TIE PER BAC DRAWING 65-46564, SRM 51-10-0 AND 51-30-0. (M)May 18, 2001 · N247US · Boeing 737201SDR USAA010560Web · crackedCLT - FOUND PRESSURE BULKHEAD WEB WITH CRACKS .125 INCH TO 1 INCH, BS 178, LBL 12 TO RBL 17, WL 188 TO WL 214. DAMAGED REMOVED, INSTALLED REPAIR DOUBLER PER EO 5300V153 AND EA 69493. (M)May 18, 2001 · N247US · Boeing 737201SDR USAA010563Beam · crackedCLT - FOUND BEAM CRACKED 3 INCHES, BS 663, BL 0. INSTALLED REPAIR ANGLES PER EA 69611. (M)May 18, 2001 · N247US · Boeing 737201SDR USAA010564Skin · crackedCLT - FOUND SKIN CRACKED .25 INCH, BS 345, AFT LOWER CORNER OF AIRSTAIR CUTOUT. REMOVED AND REPLACED REPAIR TRIPLER PER EA 69582. (M)May 18, 2001 · N247US · Boeing 737201SDR USAA010565Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED .25 INCH AFT ENTRY DOOR, UPPER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 543-30-3, FIG 21A. (M)May 18, 2001 · N247US · Boeing 737201SDR USAA010566Skin · corrodedCLT - FOUND FUSELAGE SKIN CORRODED, BS 468, BL 0. REMOVED DAMAGE, INSTALLED REPAIR DOUBLER PER SRM 51-20-4 AND 53-30-3. (M)May 18, 2001 · N247US · Boeing 737201SDR USAA010552Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 639, STRINGER 17R. INSTALLED REPAIR DOUBLER PER SRM 51-40-2, FIG 1. (M)May 18, 2001 · N247US · Boeing 737201SDR USAA010553Frame · crackedCLT - FOUND FRAME CRACKED .375 INCH, LATERALLY THROUGH EDGE OF FRAME BS 440, LBL 21. INSTALLED FORMED FRAME REPAIR DOUBLER PER SRM 51-40-3, FIG 1. (M)May 18, 2001 · N247US · Boeing 737201SDR USAA010555Doubler · crackedCLT - FOUND DOUBLER CRACKED 2 INCHES, BS 676, BETWEEN LBL 24 AND RBL 24, WL 206. INSTALLED RE-INFORCEMENT CHANNELS PER EO 5791G632. (M)May 18, 2001 · N247US · Boeing 737201SDR AALA20011115WebTUL - FOUND ACCESS HOLE REQUIRED TO FOM AT STATION 200-210 BETWEEN SEAT TRACK 5/6 RT. INSTALLED DOUBLER OVER ACCESS HOLE AT STATION 200-210 PER SRM 53-01 FIG 4. (M)May 18, 2001 · N3515 · Doug DC982SDR AALA20011114Seat Track · corrodedTUL - FOUND SEAT TRACK NR 5 CORRODED STATION 200-245. INSTALLED SEAT TRACK FROM STATION 200-245 NR 5. (M)May 18, 2001 · N3515 · Doug DC982SDR USAA010735Skin · crackedPIT - FOUND SKIN CRACKED .25 INCH, BS 947 AT STRINGER 11R. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-60-01. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010736Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, BS 663 AT S2L. CUT OUT DAMAGE, INSTALLED DOUBLER PER SRM 53-00-07 FIG 208, SRM 51-70-13, SRM 53-60-08, SRM 53-60-08. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010737Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, BS 747 AT S8R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010738Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, BS 440 AT S8L. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010739Clip · crackedPIT - FOUND CLIP CRACKED .25 INCH, BS 360 AT S13L. FABRICATED, HEAT TREATED AND INSTALLED PER SRM 53-00-07 FIG 205. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010740Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, BS 440 AT STRINGER 8R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010708Web · crackedPIT - FOUND WEB CRACKED .75 INCH, STATION 178 BULKHEAD WL 184. REPAIRED FILLERS, DOUBLERS AND SHIMS PER SRM 53-10-08 FIG 211. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010711Web · crackedPIT - FOUND WEB CRACKED 5 INCHES, STATION 178 BULKHEAD RIGHT FLOOR WEB AT WL 207. REMOVED AND REPLACED FLOORWEB. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010712Angle · crackedPIT - FOUND ANGLE CRACKED .125 INCH, STATION 178 BULKHEAD RIGHT CHORD ANGLE AT WL 207. REPAIRED DOUBLER, CHORD, CLIPS, SPLICE ANGLE PER SRM 53-10-08. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010713Angle · crackedPIT - FOUND ANGLE CRACKED .125 INCH, STATION 178 BULKHEAD LEFT CHORD ANGLE AT WL 207. REPAIRED FILLER, DOUBLER AND SHIMS PER SRM 53-10-08 FIG 211. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010715Web · crackedPIT - FOUND WEB CRACKED .25 INCHES IN LENGTH, STATION 178 BULKHEAD LBL 5.7 WL 210 UPPER ANTENNA MOUNT. REPAIRED FILLER, DOUBLER AND SHIMS PER SRM 53-10-08 FIG 211. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010716Clip · crackedPIT - FOUND CLIP CRACKED .25 INCH, BS 639 AT S11L. MANUFACTURED, HEAT TREATED, INSTALLED CLIP PER BOEING PRINT 66-2411241-1. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010723Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, BS 480 AT STRINGER 8R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14 AND EA 70650. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010724Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, BS 500C AT STRINGER 8R. ROUTED OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14 AND EA 70647. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010725Angle · crackedPIT - FOUND ANGLE CRACKED 1.5 INCH, BS 616 BELOW S17L. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-62-01. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010727Angle · crackedPIT - FOUND ANGLE CRACKED .5 INCH, BS 454 AT OUTBOARD FLOOR PANEL SUPPORT ANGLE. MANUFACTURED NEW CLIP AND INSTALLED, HEAT TREAT. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010726Angle · crackedPIT - FOUND ANGLE CRACKED 1.5 INCHES, BS 616 BELOW STRINGER S17R. REMOVED DAMAGED, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-62-01. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010707Web · crackedPIT - FOUND WEB CRACKED .5 INCH, FORWARD PRESSURE BULKHEAD STATION 178. REPLACED WEB. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010701Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, BS 380 AT S8R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER SRM 53-00-07 FIG 201. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010702FramePIT - FOUND INDICATION BY HFEC IS DOUBLE FLUSH RIVET, BS 380 AT S8L. CUT OUT DAMAGE, INSTALLED FILLERS AND DOUBLER PER SRM 53-00-07 PAGE 203-206. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010705Web · crackedPIT - FOUND WEB CRACKED .5 INCHES LONG, STATION 178 BULKHEAD ANTENNA MOUNT RIGHT. FILLER, DOUBLER, SHIMS PER SRM 53-10-08 FIG 211. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010706Web · crackedPIT - FOUND WEB CRACKED .25 INCH, BS 178 BULKHEAD LOWER LT ANTENNA MOUNT. FILLER, DOUBLERS, SHIMS PER SRM 53-10-08 FIG 211. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010703StringerPIT - FOUND STRINGER CUT TO FASCILITATE CLIP REMOVAL, BS 967 AT S25L. SPLICED STRINGER PER SRM 53-00-3. (M)May 17, 2001 · N586US · Boeing 737301SDR USAA010687Seat Track · corrodedPIT - FOUND SEAT TRACK CORRODED 1 INCH BY 4 INCHES, LT INBOARD AFT OF BS 344. CORROSION LEVEL 1, TASK NR C53-107-01. CUT OUT DAMAGE, INSTALLED NEW AND SPLICE PER SRM 53-00-52, FIG 203. (M)May 17, 2001 · N586US · Boeing 737301SDR IXXA0100032Web · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON THE VERTICAL WEB IN THE RIGHT WHEEL WELL AT FUSELAGE STATION 860, RIB LINE 14. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED WEB, FABRICATION AND INSTALLATION OA NEW WEB IN ACCORDANCE WITH DOUGLAS DRAWING 565May 17, 2001 · N820BX · Doug DC871FSDR AALA20011163Shear Tie · corrodedTUL - FOUND SHEAR TIE CORRODED FORWARD OF DRAIN MAST STATION 1148 STRINGER 29L. INSTALLED NEW SHEAR TIE PER SRM 51-10-1. (M)May 17, 2001 · N866AA · Boeing 727223SDR AALA20011157Web · corrodedTUL - FOUND CORROSION 6 INCHES BY 1 INCH ON WEB AND PLATE RBL 16. INSTALLED FILLER AND DOUBLER AT STATION 1168-1174 RBL 16 PER 51-40-2. (M)May 17, 2001 · N866AA · Boeing 727223SDR SIMA20011402Skin · corrodedABI - MAINTENANCE FOUND CORROSION IN FLOOR CENTER BEAM AT FRAME 20 AND 22. CORROSION WAS REMOVED AND A DOUBLER WAS INSTALLED IAW EMB GST-159/01. AIRCRAFT WAS RETURNED TO SERVICE. (M)May 17, 2001 · N638AE · Emb EMB145LR
Back to JASC 5300