JASC 5312

Service difficulty reports · 20,045

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 SWAA090446Bulkhead · crackedDURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17, WL 230. REPAIRED WEB PER SRM.Jan 21, 2009 · N652SW · Boeing 7373H4SDR DLM88090266Bulkhead · corrodedEXFOLIATION CORROSION ON AFT P-DOME SKIN AT LOWER AREA. RELACED DAMAGED PARTS IAW SRM 53-05 FIG 101.Jan 20, 2009 · N976DL · Doug MD88SDR A6WA200940043Bulkhead · crackedAFT PRESSURE BULKHEAD CRACK AT LINTEL LOCATION REPAIR TO LINTEL LOCATION AT PRESSURE BULKHEAD AFT IAW CRJ 200 REO 601R-53-61-1230 REV D.Jan 20, 2009 · N451AW · Cndair CL6002B19SDR ZZDA2009016Bulkhead · damagedDAMAGE (HOLE) IN FWD CARGO COMPARTMENT BULKHEAD. INSTALLED TYPICAL WEB TRIM OUT REPAIR DOUBLER PER B717 SRM 51-70-10 REP 2.Jan 20, 2009 · N906AT · Boeing 717200SDR FDEA200901200269Panel · dentedE/E BAY UPPER CHORD SKIN STRUCTURE HAS BULGE AT BS 328 BL 0. EVALUATED BULGE ON NLG WW UPPER SKIN BS 328 BL0 AS AN OIL CANNING DENT. DETERMINED TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. DRILLED 1 INCH ROUND HOLE TO REMOVE DAMAGE IAW B727 SRM 51-10-1. Jan 20, 2009 · N281FE · Boeing 727233SDR SWIA200921167Bulkhead · crackedC-CHECK, CRACK AT UPPER CORNER LINTEL FITTING TO BULKHEAD WEB. REPAIRED PER REO.Jan 19, 2009 · N710BR · Cndair CL6002B19SDR ASAA0944233Bulkhead · damagedTOOLING DAMAGE ON BULKHEAD RT WEB. RECEIVED NEW RT WEB DRILLED AND INSTALLED ON TASK CARD.Jan 15, 2009 · N709AS · Boeing 737490SDR ASAA0944229Bulkhead · damagedDAMAGE 178 BULKHEAD LT WEB. RECEIVED NEW WEB DRILLED AND INSTALLED.Jan 15, 2009 · N709AS · Boeing 737490SDR SWAA090374Bulkhead · crackedDURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REPAIRED WEB PER SRM.Jan 15, 2009 · N606SW · Boeing 7373H4SDR SWAA090373Bulkhead · crackedDURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17. REMOVED AND REPLACED WEB PER SRM.Jan 15, 2009 · N330SW · Boeing 7373H4SDR SWAA090372Bulkhead · crackedDURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REMOVED AND REPLACED WEB PER SRM.Jan 15, 2009 · N330SW · Boeing 7373H4SDR SWAA090347Bulkhead · crackedDURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7, WL 182. REPAIRED BEAM PER SWA EA.Jan 15, 2009 · N611SW · Boeing 7373H4SDR ASOA200900129Bulkhead · damagedREAR PRESSURE BULKHEAD WEB THAT SURROUND THE LINTEL ATTACHMENT FITTING HAS A INDICATION NOTED APPROX .1" IN LENGTH 70% FSH FAILED NDT INSP.Jan 14, 2009 · N837AS · Cndair CL6002B19SDR ASOA200900128Bulkhead · damagedFS 559.0 BULKHEAD WEB AND CAP ANGLE HAS INDICATIONS NOTED AT LT/RT CAP ANGLE LBL 18 & RBL 18 APPROX .2" IN LENGTH 70% FSH AND RT WEB WL 58.70, WL 59.10 APPROX .5" IN LENGTH 80% FSH ALL AREAS FAILED NDT INSP, MARKED ON ACFT. REPAIRED FS 559.0 BULKHEAD WEB AND Jan 14, 2009 · N837AS · Cndair CL6002B19SDR AALA2009011200171Frame · crackedAFW - DURING BULKHEAD OUTER CHORD INSPECTION CRACK INDICATION WAS NOTICED AT ONE HOLE LOCATION COMMON TO SKIN FORWARD LOWER TENSION FITTING, SPLICE FITTING, AND FORWARD OUTER CHORD. CRACK INDICATION WAS REMOVED BY ONE SIXTY FOURTH INCH HOLE OVERSIZING AND CONJan 12, 2009 · N369AA · Boeing 767323SDR SWIA200921182Bulkhead · crackedDURING C-HECK, AFT PRESSURE BULKHEAD CRACKED. REPAIRED PER REO.Jan 9, 2009 · N409SW · Cndair CL6002B19SDR ASOA200900052Bulkhead · crackedIN REFERENCE TO TASK CARD AWL 53-61-153 02 W/O 107923. DURING EDDY CURRENT INSPECTION OF AFT PRESSURE BULKHEAD, FOUND THAT BULKHEAD IS CRACKED AT LINTEL ATTACH POINT.Jan 7, 2009 · N834AS · Cndair CL6002B19SDR A6WA200940029Bulkhead · crackedAFT PRESSURE BULKHEAD CRACK AT LINTEL LOCATION, CRACK LENGTH .500 AFT PRESSURE BULKHEAD AT LINTEL LOCATION. REPAIR CARRIED OUT IAW REO 601R-53-61-1230 REV D. (K)Jan 6, 2009 · N457AW · Cndair CL6002B19SDR A6WA20090018Bulkhead · crackedCRACK FOUND ON PRESSURE BULKHEAD, FS 202.75, LBL 23.71 AT PARKING BRAKE LOCATION. PRESSURE BULKHEAD FS 202.75, LBL 23.71 AT PARKING BREAK. REPAIRED IAW REO 601R-53-11-563. (K)Jan 6, 2009 · N457AW · Cndair CL6002B19SDR ASOA200900049Bulkhead · crackedFS 559 BULKHEAD WEB AND CAP ANGLE HAVE INDICATIONS NOTED RBL 18, WL 59.10 APPROX .1250 INCH LONG AND LBL IN CAP ANGLE RADIUS APPROX .30 INCH LONG. C/W REO 601R-53-41-260 REV C REPAIR TO PRESSURE BULKHEAD STRUCTURE. C/W EC/TC REO 601R-53-41-260 IAW REO 610R-5Jan 6, 2009 · N882AS · Cndair CL6002B19SDR SWAA090017Bulkhead · crackedDURING SCHEDULED SPV CHECK, FOUND VERTICAL WEB CRACKED AT BS 178, RBL 5.7, WL 182. REPAIRED WEB PER SWA EA.Jan 5, 2009 · N611SW · Boeing 7373H4SDR SWAA090015Bulkhead · crackedDURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7, WL 186. REPAIRED WEB PER SWA EA.Jan 5, 2009 · N642WN · Boeing 7373H4SDR SAJFCALS098003Bulkhead · corrodedFOUND CORROSION (3.8" X 2.7" X 0.060") AT BS 727 MAIN WHEEL WELL AFT BULKHEAD. REPAIR CORRODED AREA BY EO NR 738-53-00-0099. DO NOT HAVE FURTHER LEVEL 2 REPORT AT THIS CASE. WILL CONTIUE TO MONITOR THIS CASE. (B-18610)Jan 4, 2009 · N18610 · Boeing 737809SDR ASOA200900018Fitting · crackedRELEVANT INDICATIONS OF CRACKS NOTED AROUND THE LINTEL ATTACHMENT FITTING ON THE AFT PRESSUR BULKHEAD. CRACKS MIGRATE APPROXIMATELY 3/16" FROM THE UPPER, LOWER AND THE INBD EDGE OF THE FITTING.Dec 30, 2008 · N830AS · Cndair CL6002B19SDR USAA2009012190110Bulkhead · crackedSAL - C19 - MAJOR REPAIR - CRACK AT BS 178 BULKHEAD ON WEB SURFACE OF VERTICAL BEAM, RBL 5.7, BETWEEN WL 180 & WL 190. REPAIRED BS 178 BULKHEAD ON WEB SURFACE OF VERTICAL BEAM, RBL 5.7, BETWEEN WL 180 & WL 190 IAW US AIRWAYS EA 132193.Dec 29, 2008 · N305AW · Boeing 7373G7SDR ASOA200900013Bulkhead · crackedFS 559.0 BULKHEAD WEB AND CAP ANGLE HAS INDICATIONS NOTED AT L CAP ANGLE LBL 18 APPROX .4" IN LENGTH 70% FSH AND RT WEB WL 54.10, WL 58.70 WK 54.10 APPROX .3" AND .5" IN LENGTH 100% FSH ALL FAILED NDT INSP. COMPLIED WITH REO 601R-53-41-260, REPAIRE TO PRESSURDec 29, 2008 · N847AS · Cndair CL6002B19SDR SWAA087346Bulkhead · crackedDURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB PER SWA EA.Dec 28, 2008 · N642WN · Boeing 7373H4SDR ZZDA2008192Bulkhead · crackedRUDDER SUPPORT BULKHEAD CRACKED AT 3 O`CLOCK POSITION STA 1178. REPAIRED RUDDER SUPPORT BULKHEAD CRACK AT STA 1178 L18 IAW B717 SRM 51-70-11. COMPLETED AAR N/R 5837 W/O 2000274 - OK FOR SERVICE.Dec 26, 2008 · N982AT · Boeing 717200SDR SWAA087338Web · crackedDURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 184, LBL 17.5, WL 233. REPAIRED WEB PER SRM.Dec 22, 2008 · N630WN · Boeing 7373H4SDR SWAA087337Web · crackedDURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, LBL 17.5 WL 228. REPAIRED WEB PER SRM.Dec 22, 2008 · N630WN · Boeing 7373H4SDR SWAA087336Web · crackedDURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179, LBL 17.5, WL 227. REPAIRED WEB PER SRM.Dec 22, 2008 · N630WN · Boeing 7373H4SDR SWAA087300Web · crackedDURING SCHEDULED 12Y CHECK, FOUND VERTICAL WEB CRACKED AT BS 180, LBL 17, WL 230. REPAIRED WEB PER SRM.Dec 22, 2008 · N642WN · Boeing 7373H4SDR COMA2008122250040Bulkhead · crackedFORWARD PRESSURE BULKHEAD CRACKED WHERE PARKING BRAKE CABLE PASSES THROUGH. REPAIRED IAW REO 601R-53-11-563.Dec 22, 2008 · N927CA · Cndair CL6002B19SDR CA081219003Bulkhead · cracked(CAN) DURING A ROUTINE 100 HOUR INSPECTION A CRACK WAS DISCOVERED IN THE STN 209 BULKHEAD AT THE UPPER RIVET HOLE OF THE RIGHT STABILIZER ATTACHMENT DOUBLER. FURTHER INVESTIGATION REVILED THE BULKHEAD CRACKED AT THE SAME LOCATION ON THE LEFT SIDE. AFTER REMODec 18, 2008 · Cessna U206GSDR FDEA200812185210Bulkhead · corrodedAFT PIT FWD BULKHEAD AT STGR 38L END FITTING CORRODED. REPLACED THE FITTING AT THE AFT PIT FWD BULKHEAD LT SIDE IF STRINGER 38L IAW SRM 51-40-21.Dec 18, 2008 · N428FE · Airbus A310203SDR FDEA200812185213Fitting · corrodedAFT PIT FWD BULKHEAD AT S43L, CORROSION ON END FITTING. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-15-14; FIG 7; SHEET 2. REMOVED FITTING IAW SRM 51-40-21. RECEIVED NEW FITTING, LOCATED & DRILLED NEW FITTING IAW DWG A53811093. INSTALLED FITTINDec 18, 2008 · N428FE · Airbus A310203SDR FDEA200812185212Fitting · corrodedAFT PIT FWD BULKHEAD AT S40L, CORROSION ON END FITTING. REMOVED CORROSION; FOUND TO BE OUT OF LIMITS IAW SRM 53-15-14; FIG 7; SHEET 2. REMOVED FITTING IAW SRM 51-40-21. RECEIVED NEW FITTING, LOCATED & DRILLED NEW FITTING IAW DWG A53811093. INSTALLED FITTINDec 18, 2008 · N428FE · Airbus A310203SDR FDEA200812185211Fitting · corrodedAFT PIT FWD BULKHEAD AT S39L CORROSION ON END FITTING. REMOVED CORROSION; FOUND TO BE OUT OF LIMITS IAW SRM 53-15-14; FIG 7; SHEET 2. REMOVED FITTING IAW SRM 51-40-21. RECEIVED NEW FITTING, LOCATED & DRILLED NEW FITTING IAW DWG A53811093. INSTALLED FITTINGDec 18, 2008 · N428FE · Airbus A310203SDR FDEA200812185209Bulkhead · corrodedAFT PIT FWD BULKHEAD AT S37L, END FITTING CORRODED. REMOVED CORROSION; FOUND TO BE OUT OF LIMITS IAW SRM 53-15-14; FIG 7; SHEET 2. REMOVED FITTING IAW SRM 51-40-21. RECEIVED NEW FITTING, LOCATED & DRILLED IAW DWG A53811093. INSTALLED FITTING IAW SRM 51Dec 18, 2008 · N428FE · Airbus A310203SDR FDEA200812185208Fitting · corrodedAFT PIT FWD BULKHEAD AT S36L, END FITTING CORRODED. REMOVED CORROSION; FOUND TO BE OUT OF LIMITS IAW SRM 53-15-14; FIG 7; SHEET 2. REMOVED FITTING IAW SRM 51-40-21. RECEIVED NEW FITTING, LOCATED & DRILLED NEW FITTING IAW DWG A53811093. INSTALLED FITTING IADec 18, 2008 · N428FE · Airbus A310203SDR FDEA200812185206Fitting · corrodedAFT PIT FWD BULKHEAD AT S34L, END FITTING CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-15-14 FIG 7 SHEET 2. REMOVED FITTING IAW SRM 51-40-21. RECEIVED NEW FITTING LOCATED & DRILLED NEW FITTING IAW DWG A53811093. INSTALLED FITTING IAW Dec 18, 2008 · N428FE · Airbus A310203SDR SWIA200820817Bulkhead · corrodedDURING C-CHECK, RIGHT LOWER FS 280 BULKHEAD WEB CORRODED AT RBL11. REPAIRED PER SRM.Dec 17, 2008 · N803SK · Cndair CL6002D24SDR A6WA200840649Bulkhead · crackedMWC 15 FS 621 PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING IS CRACKED. PERFORMED A REPAIR BY CUTTING OUT SECTION OF WEB, FABRICATING AND INSTALLING REPAIR PARTS IAW BOMBARDIER REO 601R-53-61-1230 REV D.Dec 17, 2008 · N416AW · Cndair CL6002B19SDR SWAA087237Bulkhead · crackedDURING SCHEDULED 22Y CHECK, FOUND BULKHEAD HORIZONTAL FLANGE CRACKED AT BS 663, LBL 6. REPAIRED BULKHEAD PER DWG.Dec 17, 2008 · N327SW · Boeing 7373H4SDR SWAA087236Bulkhead · crackedDURING SCHEDULED 22Y CHECK, FOUND BULKHEAD HORIZONTAL FLANGE CRACKED AT BS 663, RBL 6. REPAIRED BULKHEAD PER DWG.Dec 17, 2008 · N327SW · Boeing 7373H4SDR SWAA087225Bulkhead · crackedDURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT WL 180, RBL 5.7, BS 178. REPAIRED WEB PER SRM.Dec 17, 2008 · N368SW · Boeing 7373H4SDR SWAA087224Bulkhead · crackedDURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT WL 180, LBL 5.7, BS 178. REPAIRED WEB PER SRM.Dec 17, 2008 · N368SW · Boeing 7373H4SDR USAA2008121792255Bulkhead · crackedPIT - FPBH - MAJOR REPAIR - FORWARD PRESSURE BULKHEAD CRACKED ON FORWARD FACE BS 178, WL 234, RBL 9. REPAIRED FORWARD PRESSURE BULKHEAD AT BS 178, WL 234, RBL 9 IAW B737 SRM 53-10-08 & ENGINEERING ORDER 5300153.Dec 16, 2008 · N406US · Boeing 737401SDR USAA2008121792262Bulkhead · crackedPIT - FPBH - MAJOR REPAIR - CRACK IN FORWARD PRESSURE BULKHEAD AT BS 178, WL 234, LBL 9. REPAIRED FORWARD PRESSURE BULKHEAD AT BS 178, WL 234, LBL 9 IAW SRM 53-10-08 & EO 5300153.Dec 16, 2008 · N406US · Boeing 737401SDR SWAA087119Bulkhead · crackedDURING SCHEDULED SPV CHECK, FOUND BULKHEAD VERTICAL BEAM WEB CHORD CRACKED AT BS 178, RBL 5.7, BETWEEN WL 198 TO WL 199. REPAIRED CHORD PER SRM.Dec 15, 2008 · N368SW · Boeing 7373H4
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