JASC 5312

Service difficulty reports · 20,047

Reports filed under 5312 · Fuselage Main, Bulkhead, 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 = '5312'
  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 DL733010229Bulkhead · crackedDURING INSPECTIONS PER S/B 737-53A1173 CRACKS WERE FOUND IN THE CENTER WEB OF THE FS 178 BULKHEAD AT WL 234 AND LBL 6. THE CRACKS WERE REPAIRED PER S/B AND SRM 53-10-8, FIGURE 209THE DAMAGE WAS FOUND AT CV.Feb 9, 2001 · N307WA · Boeing 737347SDR AWXA0001328Bulkhead · crackedCENTER WEB CRACKED FS 178 WL 202 LBL 5.0. REMOVED DAMAGED AREA OF WEB IAW SRM 53-10-08 FIG 209; FABED AND INSTALLED 3 FILLERS AND 1 DOUBLER IAW SRM 53-10-08 FIG 209.Feb 9, 2001 · N331AW · Boeing 7373Y0SDR AWXA0001327Bulkhead · crackedCENTER WEB CRACKED RBL 5.0 WL 202 FS 178. REMOVED DAMAGED AREA OF WEB IAW SRM 53-10-08 FIG 209; FABED 3 FILLERS AND 1 DOUBLER; INSTALLED DOUBLER AND FILLERS IAW SRM 53-10-08 FIG 209.Feb 9, 2001 · N331AW · Boeing 7373Y0SDR AWXA0001308Bulkhead · crackedULTRASONIC INSPECTION REVEALED CRACK INDICATION AT FS 178 BULKHEAD WEB BENEATH STRAP AT RBL 7 TO RBL 15 WL 218. REMOVED STIFFENERS, BRACKETS AND ANGLES; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER, FILLERS AND SHIMS IAW SRM 53-10-11; INSTALLED STIFFENERS BRFeb 9, 2001 · N180AW · Boeing 737277SDR AWXA0001307Bulkhead · crackedHFEC INDICATES A .200 INCH LONG CRACK EMINATING FROM FASTENER HOLE AT BLKHD FS 178 RBL 12.75 WL 234. REMOVED STIFFENERS, BRACKETS AND ANGLES; FABED, DRILLED, TREATED AND INSTALLED DOUBLER, FILLERS AND SHIMS IAW SRM 53-10-11; REINSTALLED STIFFENERS, BRACKETS AFeb 9, 2001 · N180AW · Boeing 737277SDR DHL2001712521Pressure Panel · crackedC-CHECK, MAIN CARGO MLG WHEEL WELL TOP SURFACE SHOWS 4 CRACKS OF .5 INCH BETWEEN RBL 17 AND RBL 25, STA 910 AND STA 920. REMOVED FLOOR PANELS, BRACKETS, CLIPS, STRAPS DWG 65-89360-3. PERFORMED STOP DRILL IAW DWG 65-89360-3. FABRICATED DOUBLER (ALCLAD 2024, Feb 8, 2001 · N712DH · Boeing 72729SDR AWXA0001303Bulkhead · crackedULTRASONIC INSPECTION REVEALED CRACK INDICATION AT FS 178 BLKHEAD BENEATH STRAP FROM LBL 5 TO LBL 8 WL 217 IN WEB. REMOVED STIFFENERS, BRACKETS AND ANGLES AT FS 178 WL 207 TO WL 241 FROM RBL 18 TO LBL 18; LOCATED, DRILLED, TREATED AND INSTALLED REPAIR DOUBLERFeb 8, 2001 · N180AW · Boeing 737277SDR AWXA0001301Bulkhead · crackedULTRASONIC INSPECTION REVEALED CRACK INDICATION AT FS 178 BLKHEAD WEB BENEATH STRAP AT LBL 6 WL 230 TO 233. REMOVED STIFFENERS, BRACKETS AND ANGLES; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER, FILLERS AND SHIMS IAW B737-200 SRM 53-10-11; INSTALLED STIFFENEFeb 8, 2001 · N180AW · Boeing 737277SDR AWXA0001288Bulkhead · crackedHFEC AND VISUAL (10X) CONFIRMS CRACK OF UNDETERMINED LENGTH UNDER STRAP AT BS 178 RBL 4 7/8 WL 199.5 TO 201.5. REMOVED STIFFENERS, RADOME ATTACH BRACKETS AND BACKUP STRIPS BS 178 WL 188 TO 218 RBL 10 TO LBL 4; LOCATED, DRILLED AND INSTALLED DOUBLER AND FILLERFeb 8, 2001 · N509DC · Boeing 73733ASDR AWXA0001287Bulkhead · crackedULTRASONIC INSPECTION REVEALED CRACK INDICATION BS 178 BULKHEAD WEB AT RBL 1.3 TO UNDETERMINED POINT BENEATH STRAP AT WL 205.7; CONFIRMED HFEC. REMOVED LOWER L-ANGLE BS 178 WL 184 RBL 18 TO LBL 18; CUTOUT DAMAGED AREA WHERE HFEC CONFIRMED CRACK; LOCATED, DRILFeb 8, 2001 · N509DC · Boeing 73733ASDR ASAA0110065Bulkhead · corrodedPHX - DURING SCHEDULED D-CHECK, FOUND AFT PRESSURE BULKHEAD AT BS 1016-1030, STRINGER 27L-27R CORRODED. REPAIRED PER EA. (M)Feb 7, 2001 · N742AS · Boeing 737290CSDR SWAA010379Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT LBL 17.1, WL 229. REPAIRED VERTICAL BEAM WEB PER BFG ER.Feb 7, 2001 · N375SW · Boeing 7373H4SDR AWXA0001272Bulkhead · cracked3 CRACKS ON PRESSURE BULKHEAD 178 WEB, LT SIDE JUST INBOARD OF LBL 57 BELOW.Feb 7, 2001 · N157AW · Boeing 7373G7SDR AWXA0001271Bulkhead · crackedTWO CRACKS ON PRESSURE BULKHEAD STA 178 RT SIDE I/B OF RBL 5.7 BELOW WL 207. SERVICE BULLETIN 737-53A1173 FUSELAGE - BODY STATION 178 BULKHEAD - INSPECTION, REPAIR AND PREVENTATIVE MODIFICATION INCORPORATED.Feb 7, 2001 · N157AW · Boeing 7373G7SDR AWXA0001263Bulkhead · crackedSTA 178 FWD BULKHEAD RT UPPER WEB RBL 17 WL 225 IS CRACKED. REPLACED WEB IAW SRM 51-10-02 PG 12.Feb 7, 2001 · N157AW · Boeing 7373G7SDR USAA010125Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .125 INCH, BS 1016, STRINGER 6L. INSTALLED DOUBLER AND TRIPLER PER SRM 53-10-4 FIG 15. (M)Feb 6, 2001 · N251AU · Boeing 737201SDR SWAA010386Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND 2 BS 178 BULKHEAD WEB CRACKS AT WL 187.5, LBL 1 & RBL 1. REPAIRED BULKHEAD WEB PER SRM.Feb 6, 2001 · N660SW · Boeing 737301SDR DL733010203Bulkhead · crackedWEB CRACKS WERE FOUND IN THE FS 178 BULKHEAD AT WL 207, RBL AND LBL 25. THE WEBS WERE REPLACED PER S/B 737-53A1173 AT CV.Feb 6, 2001 · N307WA · Boeing 737347SDR ASAA0110040Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB AT BS 178, LEFT BUTTOCK LINE 6-18 CRACKED. REPAIRED PER SRM. (M)Feb 5, 2001 · N742AS · Boeing 737290CSDR 20010322CW003Bulkhead · crackedHORIZONTAL STABILIZER WAS REMOVED FOR THE REPLACEMENT OF AFT REINFORCEMENTS. THE BULKHEAD ASSEMBLY PN1212133-1 WAS NOTICED TO BE CRACKED AT LEFT AFT RELIEF CUTOUT, JUST FORWARD OF THE HORIZONTAL STABILIZER AFT ATTACHMENT. CRACK WAS ABOUT .3750 INCH LONG. PNFeb 5, 2001 · N967CC · Cessna T210NSDR USAA010113Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .250 INCH, STATION 178 BULKHEAD, WL 224, RBL 2. INSTALLED TRIPLER PER EA 68961 AND EO 5300V153. (M)Feb 5, 2001 · N251AU · Boeing 737201SDR RRXA10870Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATH TUBE FITTING AT STA. 1690 AND L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-Feb 4, 2001 · N8091U · Doug DC871FSDR USAA010262Bulkhead · crackedCLT - FOUND PRESSURE BULKHEAD CRACKED 6.5 INCHES, BS 1016 PLUS 1 AT STRINGER 6L. INSTALLED FILLER, DOUBLER AND SHIMS. (M)Feb 4, 2001 · N249US · Boeing 737201SDR RRXA10837Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON FITTING L34L AT STA 1260 AND C-PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVE DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 5Feb 2, 2001 · N801GP · Doug DC871FSDR ASAA0110035Bulkhead · crackedPHX - DURING SCHEDULED D-CHECK, FOUND WEB AT STATION 178, RIGHT BUTTOCK LINE 11 CRACKED. REPAIRED PER SRM. (M)Feb 2, 2001 · N742AS · Boeing 737290CSDR SWAA010337Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 4.75, WL 202. REPAIRED BULKHEAD WEB PER SRM.Feb 2, 2001 · N660SW · Boeing 737301SDR DL73K010198Bulkhead · crackedDURING ACCOMPLISHMENT OF THE FS 178 BULKHEAD INSPECTIONS PER AD 2000-05-29, CRACKS WERE FOUND IN THE ADJACENT FLOOR WEB AT WL 207 & LBL 25. THE CRACKS ARE TYPICAL OF BAC S/B 737-53A1173. THE CRACKED WEB WAS REMOVED AND A NEW WEB INSTALLED PER THE BAC S/BFeb 2, 2001 · N238WA · Boeing 737247SDR DHL2001712511Bulkhead · crackedC-CHECK- AFT BAGGAGE RT AFT BULKHEAD PANEL CRACKED 2.0 INCHES AT STA 1166.0. CLEANED AND REPAIRED AFT BAGGAGE RT AFT BULKHEAD PANEL AT STA 1166.0 WITH FIBER GLASS CLOTH AND RESIN POLYSTER IAW SRM 51-20-03, FIG 2. (NON-ROUTINE CARD 0995).Feb 2, 2001 · N712DH · Boeing 72729SDR RRXA10801Stringer · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO STRINGER #75 AND FWD SIDE STRINGER SPLICE AT STA. XCW 23 X=0 AND INSIDE R/H CENTER TANK THRU MID SPAR ACCESS 560E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATFeb 1, 2001 · N801GP · Doug DC871FSDR RRXA10800Stringer · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LWR STRINGER#76 AT STA. XCW47&23 AND INSIDE R/H CENTER TANK THRU MID SPAR ACCESS 560E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.Feb 1, 2001 · N801GP · Doug DC871FSDR RRXA10786Stringer · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO STRINGER #76 AT STA. XCW23 AND XCW46 AND INSIDE L/H CENTER WING TANK THRU MID SPAR ACCESS HOLE 560E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DCFeb 1, 2001 · N801GP · Doug DC871FSDR UPS01835121Bulkhead · corrodedINSPECTION TYPE:C1/3, LEFT NWW TUNNEL, BOTTOM OF PRESSURE WEB AT FS -67 FROM CUSP TO INBD STIFFENER CORRODED. WEB REPAIRED IAW REO-G07874.Feb 1, 2001 · N810UP · Doug DC873FSDR UPS01435086Bulkhead · crackedINSPECTION TYPE:C, 2 INCH CRACK FOUND BS 260 CANTED BULKHEAD AT UPPER EDGE LT SIDE. REPAIR ACCOMPLISHED IN ACCORDANCE WITH QUERY NOTE 17 / 01.Feb 1, 2001 · N677UP · Boeing 747123FSDR SWAA010327Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND 3 BS 178 BULKHEAD WEB CRACKS AT WL 234, LBL 12, LBL 10 & RBL 10. REPAIRED BULKHEAD WEB PER SRM.Feb 1, 2001 · N660SW · Boeing 737301SDR SWAA010324Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND 2 BS 178 BULKHEAD VERTICAL BEAM WEB CRACKS AT RBL 17, WL 230. REPAIRED VERTICAL BEAM WEB PER ER.Feb 1, 2001 · Boeing 7372H4SDR DL733010182Bulkhead · crackedTHE CENTER WEB OF THE FS 178 BULKHEAD WAS FOUND CRACKED AT WL 195 AT BOTH LBL 5 AND RBL 5. THE CRACKS WERE REPAIRED PER S/B 737-53A1173, REV 3.Feb 1, 2001 · N241DL · Boeing 737300SDR RRXA10811Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TOR/H KEEL BEAM PANEL AT PLATE ATTACH POINT 30" FROM FWD. EDGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSJan 31, 2001 · N801GP · Doug DC871FSDR RRXA10758Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO AFT LWR. CARGO BILGE INTERNAL DOUBLER AT STA. 1155-1170 AND L35L TO L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PJan 31, 2001 · N8091U · Doug DC871FSDR SWAA010318Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 17.1, UPPER SECTION. REPAIRED VERTICAL BEAM WEB PER RA.Jan 31, 2001 · N374SW · Boeing 7373H4SDR SWAA010312Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT LBL 5.7, WL 205. REPAIRED VERTICAL BEAM WEB PER ER.Jan 31, 2001 · Boeing 7372H4SDR USAA010105Strap · crackedCLT - FOUND STRAP .75 INCH, BS 178 BULKHEAD LBL 5-7, WL 205. INSTALLED DOUBLER PER EA 68728. (M)Jan 30, 2001 · N520AU · Boeing 7373B7SDR SWAA010305Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 17, WL 277. REPAIRED VERTICAL BEAM WEB PER RA.Jan 30, 2001 · N374SW · Boeing 7373H4SDR USAA010085Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .5 INCH, WL 234, RBL 10. INSTALLED DOUBLER PER SRM 53-10-08. (M)Jan 29, 2001 · N251AU · Boeing 737201SDR USAA010084Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .250 INCH, STATION 178, BULKHEAD WL 218, RBL 13. INSTALLED DOUBLER PER EO 5300V153. (M)Jan 29, 2001 · N251AU · Boeing 737201SDR USAA010083Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .250 INCH, STATION 178, BULKHEAD, WL 218, LBL 12.5. INSTALLED DOUBLER PER EO 5300V153. (M)Jan 29, 2001 · N251AU · Boeing 737201SDR USAA010082Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .250, STATION 178, BULKHEAD WL 218, RBL 10.0. INSTALLED DOUBLER PER EO 5300V153. (M)Jan 29, 2001 · N251AU · Boeing 737201SDR USAA010081Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .250 INCH, STATION 178 BULKHEAD WL 210.5, RBL 6.75. INSTALLED DOUBLER PEREO 5300V153. (M)Jan 29, 2001 · N251AU · Boeing 737201SDR USAA010080Bulkhead · crackedCLT - FOUND BULKHEAD .250 INCH CRACK, STATION 178, BULKHEAD, WL 214, LBL 6.5. INSTALLED DOUBLER PER EO 5300V153. (M)Jan 29, 2001 · N251AU · Boeing 737201SDR USAA010079Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .250 INCH, STATION 178, BULKHEAD, WL 214, RBL 5. INSTALLED DOUBLER PER EO 5300V153. (M)Jan 29, 2001 · N251AU · Boeing 737201SDR USAA010078Bulkhead · crackedCLT - FOUND BULKHEAD .250 INCH CRACKED, STATION 178, WL 214, LBL 5. INSTALLED DOUBLER PER EO 5300V153. (M)Jan 29, 2001 · N251AU · Boeing 737201
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