JASC 5300

Service difficulty reports · 8,206

Reports filed under 5300 · Fuselage Structure (General), newest first.

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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"

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SDR AALA20011305Stringer · corrodedTUL - FOUND STRINGER 26L HAS HEAVY CORROSION AT STATION 683 TO 686, OUTBOARD SIDE OF STRINGER. INSTALLED STRINGER REPAIR PER SRM 53-10-03. (M)Jun 23, 2001 · N869AA · Boeing 727223SDR AALA20011392SkinTUL - FOUND LIGHTNING STRIKE PRODUCED ONE BURN HOLE .125 INCH IN DIAMETER AT STATION 454 LONGERON 7 LEFT. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-04-00 FIG 18 SHEET 24-38. (M)Jun 22, 2001 · N433AA · Doug DC983SDR AALA20011303Stringer · corrodedTUL - FOUND CORROSION 1 INCH BY 2 INCHES ON INSIDE OF STRINGER 27R. REMOVED CORROSION AND REPAIRED STRINGER PER SRM 53-10-3. (M)Jun 22, 2001 · N869AA · Boeing 727223SDR USAA010758SkinCLT - FOUND SKIN WITH PREVIOUSLY INSTALLED REPAIR 8 INCH BY 8 INCH, BS 700, STRINGER 23R. REPAIR DOUBLER PER SRM 53-00-01, FIG 203. (M)Jun 21, 2001 · N623AU · Boeing 7572B7SDR USAA010762Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED .75 INCH, BS 294.5, MED LOWER HINGE CUTOUT. INSTALLED REPAIR DOUBLER PER SRM 53-10-01, FIG 205. (M)Jun 21, 2001 · N418US · Boeing 737401SDR AALA20011385Longeron · crackedTUL - FOUND LONGERON 4 LEFT CRACKED IN RADIUS AT STATION 160. CUT OFF DAMAGED LONGERON AND INSTALLED NEW SECTION PER SRM 53-02 PAG 48-53 FIG 18. (M)Jun 21, 2001 · N433AA · Doug DC983SDR AALA20011298Stringer · corrodedTUL - FOUND STRINGER 27R CORRODED AT STATION 1130 INBOARD SIDE. REMOVED DAMAGED STRINGER AND INSTALLED NEW STRINGER SECTION AND SPLICE PER SRM 53-10-3. (M)Jun 21, 2001 · N725AA · Boeing 727227SDR AALA20011391Seat Track · corrodedTUL - FOUND CORROSION IN TRACK NR 6 AT STATION 1088. REMOVED DAMAGED AREA SEAT TRACK, TREATED AND PRIMED. INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A, PRIMED AND TREATED AND PAINTED PLUG. (M)Jun 20, 2001 · N433AA · Doug DC983SDR AALA20011390Seat Track · corrodedTUL - FOUND CORROSION ON SEAT TRACK NR 3 AT STATION 1300. CORROSION REMOVED AND SEAT TRACK PLUG INSTALLED PER SRM 53-05, FIG 4A. (M)Jun 20, 2001 · N433AA · Doug DC983SDR AALA20011289Seat Track · corrodedTUL - FOUND CORROSION ON TRACK NR 2 AT STATION 1196-1206 AND 1300. CORROSION REMOVED, SEAT TRACK PLUGS INSTALLED TWO LOCATIONS STATION 1196-1206 AND STATION 1300 PER SRM 53-05 FIG 4A. (M)Jun 20, 2001 · N433AA · Doug DC983SDR AALA20011381Seat Track · corrodedTUL - FOUND CORROSION ON SEAT TRACK NR 5 AT STATION 232-237. SEAT TRACK PLUG REPAIR COMPLETED AS PER SRM 53-05 FIG 4A. (M)Jun 20, 2001 · N433AA · Doug DC983SDR AALA20011341Longeron · crackedTUL - FOUND L4L HAS A CRACK AROUND FASTENERS AT STATION 160. INSTALLED NEW LONGERON AND LONGERON SPLICE PER SRM 53-02 FIG 18. (M)Jun 20, 2001 · N7521A · Doug DC982SDR SIMA200117109Seat Track · corrodedSAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED SEAT TRACKS, LEFT OUTBOARD MID, LEFT INBOARD MID, RIGHT OUTBOARD AND RIGHT INBOARD MID CORRODED. MAINTENANCE REMOVED AND REPLACED SEAT TRACKS IAW EO E2-53MR-115. AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 20, 2001 · N426AT · Aerosp ATR72212SDR AALA20011292Skin · crackedTUL - FOUND SKIN CRACKED AT RIVIT HOLE STATION 328 JUST BELOW STRINGER 206. ALSO, FOUND SKIN CRACKED AT TWO RIVITS STATION 328 JUST BELOW STRINGER 21L. CUT OUT DAMAGED SECTION OF SKIN AND INSTALLED DOUBLER PER SRM 53-30-3. (M)Jun 20, 2001 · N725AA · Boeing 727227SDR AALA20011343Seat Track · corrodedTUL - FOUND CORROSION ON SEAT TRACK NR 3. REMOVED CORRODED SEAT TRACK NR 3 AND INSTALLED NEW TRACK FROM FS 1164 THRU 1308 SRM 53-05. (M)Jun 19, 2001 · N7521A · Doug DC982SDR AALA20011355Skin · damagedTUL - FOUND FUSELAGE SKIN DAMAGED WITH TEMPORARY REPAIR AT STATION 218 BETWEEN LONGERON 21L AND 23L. INSTALLED DOUBLER PER SRM 53-04 FIG 12B SHEET 3. (M)Jun 19, 2001 · N7521A · Doug DC982SDR USAA010765Stringer · corrodedCLT - FOUDN STRINGER CORRODED 10 SQUARE INCHES, BS 967, STRINGER 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM 53-10-3, FIG 1. (M)Jun 19, 2001 · N254AU · Boeing 737201SDR COMA0160395Splice Plate · mismanufacturedTWO SPLICE PLATES P/N 601R31030-71 WERE FABED INCORRECTLY BY MANUFACTURER.FABED TWO DOUBLER PLATES, REWORKED SPLICE PLATES AND INSTALLED DOUBLER PLATES I/A/W WVAC EO 601R-53-2511.Jun 19, 2001 · N967CA · Cndair CL6002B19SDR AALA20011293Stringer · corrodedTUL - FOUND STRINGER SPLICE AT STATION 675 STRINGER 28R HAS CRACK AND IS BULGED, EMITTING CORROSION. REMOVED CORRODED SPLICE AND 5 INCHES OF STRINGER. FABRICATED AND INSTALLED NEW SPLICE IAW SRM 53-10-3. TREATED AND PRIMED ALL PARTS IAW MM 51-20-0. (M)Jun 19, 2001 · N725AA · Boeing 727227SDR AALA20011340Skin · dentedTUL - FOUND DENT RIGHT FUSELAGE 5 FEET AFT OF SERVICE DOOR. INSTALLED DOUBLER PER SRM 53-04 FIG 12B. (M)Jun 18, 2001 · N7521A · Doug DC982SDR RRXA11307Splice · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA.1020 AND L30L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 53-2-0,Jun 18, 2001 · N606AL · Doug DC873FSDR USAA010749Skin · crackedTPA - FOUND SKIN CRACKED 1 INCH, AFT OF STATION 907 STRINGER 18L. INSTALLED DOUBLER PER EA 71383 AND SRM 53-00-01 FIG 223. (M)Jun 18, 2001 · N254AU · Boeing 737201SDR TSAA0153077Spar · corrodedFOUND CORROSION DURING HEAVY CHECK AT RIGHT WING FRONT SPAR LOWER CHORD FORWARD FLANGE LOWER SURFACE AT FSS 476.0 THROUGH FSS 481.7. (M)Jun 18, 2001 · N805AL · Boeing 7372M6CSDR USAA010766Skin · crackedTPA - FOUND SKIN CRACKED 1 INCH, BS 907, STRINGER 18L. DAMAGED REMOVED, REPAIR DOUBLER INSTALLED PER SRM 53-00-01, AND EA 7183. (M)Jun 17, 2001 · N254AU · Boeing 737201SDR RRXA11302Shear Tie · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SHEAR TIE AT STA.55 AND L34L-L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AJun 16, 2001 · N606AL · Doug DC873FSDR RRXA11301Shear Tie · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO DOOR PAN SHEAR TIE AT STA.35 AND L34L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-Jun 16, 2001 · N606AL · Doug DC873FSDR USAA010743Skin · crackedPIT - FOUND SKIN CRACKED 5 INCHES BY 7 INCHES, FRAME STATION 580, S5L. REPAIR PCW, 5 INCHES BY 7 INCH DOUBLER INSTALLED PER SRM 53-00-01 FIG 202. (M)Jun 15, 2001 · N524AU · Boeing 7373B7SDR USAA010744Skin · crackedPIT - FOUND SKIN CRACKED 6 INCHES BY 7 INCHES, FRAME STATION 556, STRINGER 5L. REPAIRED PCW, 6 INCHES BY 7 INCH DOUBLER INSTALLED PER SRM 53-00-01 FIG 202. (M)Jun 15, 2001 · N524AU · Boeing 7373B7SDR USAA010745Skin · crackedPIT - FOUND SKIN CRACKED 8 INCHES BY 6 INCH AREA, BETWEEN FRAME STATION 500C AND 500D, S5L, 6 INCHES AFT 500C. REPAIR PCW, 8 INCHES BY 6 INCH DOUBLER INSTALLED PER SRM 53-00-01 FIG 201. (M)Jun 15, 2001 · N524AU · Boeing 7373B7SDR USAA010746Skin · crackedPIT - FOUND SKIN CRACKED 4.75 INCHES BY 4.75 INCH AREA, BETWEEN FRAME 500B AND 500C, S5L, 4 INCHES AFT OF 500C. REPAIRED PCW, 4.75 INCHES CIRCULAR DOUBLER INSTALLED PER SRM 53-00-01 FIG 208. (M)Jun 15, 2001 · N524AU · Boeing 7373B7SDR SIMA200117801Sill · corrodedSAW - DURING CPCP2 INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR SILL CORRODED. SILL AS REMOVED AND REPLACED IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 14, 2001 · N426AT · Aerosp ATR72212SDR RRXA11289Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO C-PIT CROSS SLIDE DOOR FWD UPPER CUTOUT SUPPORT FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW Jun 14, 2001 · N606AL · Doug DC873FSDR USAA010806Skin Panel · crackedPIT - FOUND BULKHEAD SKIN PANEL CRACKED 1.5 INCH, STATION 178 BULKHEAD WL 201 AND 204 LBL 5.7. CUT OUT, INSTALLED DOUBLER PER SRM 53-10-08 FIG 211. (M)Jun 13, 2001 · N335US · Boeing 737301SDR USAA010675Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .5 INCH, BS 278, S14R. STOP DRILLED CRACK, INSTALLED DOUBELR PER SRM 51-70-11. (M)Jun 13, 2001 · N584US · Boeing 737301SDR USAA010672Attach Angle · crackedCLT - FOUND ATTACH ANGLE CRACKED 1 INCH, BS 290, INTERCOSTAL BETWEEN S12R AND S13R. REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE PER SRM 51-10-02. (M)Jun 13, 2001 · N584US · Boeing 737301SDR USAA010673Attach Angle · crackedCLT - FOUND ATTACH ANGLE CRACKED 1 INCH, BS 290, INTERCOSTAL BETWEEN S11R AND S12R. REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE PER SRM 51-10-02. (M)Jun 13, 2001 · N584US · Boeing 737301SDR USAA010671Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, BS 330, 4 INCHES ABOVE STRINGER 17R. DAMAGED REMOVED, INSTALLED DOUBLER AND TRIPLER. (M)Jun 13, 2001 · N584US · Boeing 737301SDR USAA010663Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 380, STRINGER 8R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)Jun 13, 2001 · N584US · Boeing 737301SDR USAA010666Door Frame · crackedCLT - FOUND FRAME CRACKED INTERNAL .5 INCH, BS 295, FORWARD SERVICE DOOR CUTOUT, LOWER FORWARD CORNER. INSTALLED REPAIR ANGLES PER SRM 51-70-11. (M)Jun 13, 2001 · N584US · Boeing 737301SDR USAA010668Stringer · corrodedCLT - FOUND STRINGER CORRODED APPROXIMATELY .5 INCH, BS 1100, STRINGER 5R. REMOVED DAMAGE, SPLICED IN NEW STRINGER SECTION PER SRM 53-00-03, 51-30-01, 51-40-02. (M)Jun 13, 2001 · N584US · Boeing 737301SDR COMA0160469Splice Plate · defectiveTWO SPLICE PLATES WERE FABRICATED INCORRECTLY.FABED DOUBLER PLATES, REWORK SPLICE PLATES AND INSTALLED DOUBLERS I/A/W WVAC EO 601R-53-2500.Jun 13, 2001 · N936CA · Cndair CL6002B19SDR USAA010648SkinCLT - FOUND SKIN WITH PREVIOUSLY INSTALLED DOUBLER, 11 INCH BY 12.25 INCH, BS 895-907, STRINGER 16 AND 17L. DOUBLER HAS BEEN INSTALLED PER SRM 53-00-01. (M)Jun 12, 2001 · N584US · Boeing 737301SDR USAA010805Skin Panel · crackedPIT - FOUND BULKHEAD SKIN PANEL CRACKED 2 INCHES STOP DRILLED, STATION 178 RBL 5.7 WL 201. CUT OUT, INSTALLED DOUBLER PER SRM 53-10-08 FIG 211. (M)Jun 12, 2001 · N335US · Boeing 737301SDR USAA010807SkinPIT - FOUND SKIN OIL CANNING 12 INCH BY 12 INCH, 178 BULKHEAD BETWEEN WL 195-207 BL 17L AND BL 17R. ACCOMPLISHED EXTERNAL DOUBLER, REMOVED DAMAGE PER SRM 53-10-08 FIG 211. (M)Jun 12, 2001 · N335US · Boeing 737301SDR SIMA20011711Seat Track · corrodedSAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE LEFT OUTBOARD, LEFT F/A, AND RIGHT F/A SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPALCED THE SEAT TRACK IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 12, 2001 · N499AT · Aerosp ATR72212ASDR USAA010662Web · crackedCLT - FOUND WEB CRACKED .25 INCH AND .125 INCH, BS 178, WL 198 AT LBL 6, WL 234 AT LBL 13.3. DAMAGED REMOVED, INSTALLED DOUBLER AND FILLERS PER EO 5300V153. (M)Jun 12, 2001 · N584US · Boeing 737301SDR USAA010649Web · corrodedCLT - FOUND CREASE BEAM WEB CORRODED, .5 INCH BY 10 INCHES, BS 747 TO 767, STRINGER 17L. FABRICATED AND INSTALLED NEW WEB PER BOEING DRAWING NR 65-46818, SRM 51-40-02, 51-10-02. (M)Jun 12, 2001 · N584US · Boeing 737301SDR USAA010642Skin · crackedTPA - FOUND SKIN CRACKED BETWEEN STATION 727A AND 727B BELOW 13L. INSTALLED DUOBELR PER SRM USING BLIND FASTENERS PER SRM 53-30-3 FIG 1 AND MPP 308-25. (M)Jun 11, 2001 · N232US · Boeing 737201SDR USAA010683Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, STATION 1437 AT L16R. STOP DRILLED CRACK, INSTALLED DOUBLER PER TYPICAL REPAIR 53-01. (M)Jun 11, 2001 · N812US · Doug DC981SDR GAIA01187STSeat TrackDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT SEAT TRACK BS 720C LBL 45.50 HAS ELONGATED LOCK HOLES. ACCOMPLISHED SEAT TRACK REPAIR BS 690-740 LBL 45.50 IAW B727 SRM 53-10-5 FIG 1. (M)Jun 11, 2001 · N252US · Boeing 727251
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