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 GUUA94253081809CPressure Blkhd · chafedDURING SCHEDULED ROUTINE INSP, DISCOVERED RT PRESSURE BULKHEAD CHAFED AT APPROX FS 256. BLENDED AND POLISHED CHAFED AREA AND PERFORMED NDT-DYE PENETRANT INSP TO CHAFE AREA NO DEFECTS NOTED.Aug 18, 2009 · N47542 · Beech 1900DSDR ASOA200900902Bulkhead · damagedREAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS A INDICATION NOTED APPROX .2 INCH IN LENGTH 90 PERCENT FSH FAILED NDT INSP. REPAIRED PER EC/TC REO 601R-53-61-1230, C/W THE REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230 REV D.Aug 18, 2009 · N875AS · Cndair CL6002B19SDR SWAA095318Stiffener · crackedDURING SCHEDULED 10Y CHECK, FOUND DIAGONAL STIFFENER ANGLE CRACKED AT FWD RT MAIN WHEEL WELL BULKHEAD AT BS 663. REMOVED AND REPLACED ANGLE PER SRM.Aug 18, 2009 · N737JW · Boeing 7377H4SDR EE4Y090216Bulkhead · crackedLOWER FUSELAGE RT MAIN WHEEL WELL AFT BULKHEAD WEB WITH CRACK IN BS 727 RBL 6 WL 160.Aug 18, 2009 · N733TW · Boeing 7372H4SDR 2009FA0000763Bulkhead · crackedFOUND AFT VERTICAL FIN SPAR TO BULKHEAD BRACKET CRACKED. STA 258.75. THIS PROBLEM HAS BEEN ADDRESSED BY AD 74-16-08 AND MFG SL 679 ON OTHER SERIES ACFT BUT NOT ON THIS ONE. (K)Aug 17, 2009 · N9364P · Piper PA24260SDR 2009FA0000762Bulkhead · crackedFOUND AFT VERTICAL FIN SPAR TO BULKHEAD BRACKET CRACKED AT STA 258.75. THIS PROBLEM HAS BEEN ADDRESSED BY AD 74-16-08 AND MFG SL 679 ON OTHER SERIES ACFT BUT NOT ON THIS ONE. (K)Aug 17, 2009 · N5130P · Piper PA24SDR IPXA09557156Support Angle · crackedINSPECTION TYPE:C2 AFT CARGO BAY STATION 1640, AFT BULKHEAD SUPPORT ANGLE IS CRACKED, (LT SIDE FLOOR TO LOWER SIDEWALL TRANSITION ANGLE). REMOVED & REPLACED PER SRM.Aug 17, 2009 · N464UP · Boeing 75724APFSDR ASOA200900923Bulkhead · crackedWHILE PERFORMING HFEC INSPECTION OF FS 559.00 BULKHEAD WEB AND CAP ANGLE, A 50% FSH INDICATION APPROX 0.5" IN LENGTH WAS NOTED ON THE WEB AT RBL 19.00 AND WL 59.10. FAILS NDT AT THIS TIME. C/W EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV C. REF CO 75Aug 17, 2009 · N875AS · Cndair CL6002B19SDR USAA2009081892168Bulkhead · crackedCLT - Q3 - MAJOR REPAIR - FOUR (4) CRACKS ON BS 178 BULKHEAD VERTICAL BEAM WEB BETWEEN WL 228 TO WL 234, LBL 17. REPAIRED BS 178 BULKHEAD VERTICAL BEAM WEB BETWEEN WL 228 TO WL 234, LBL 17 IAW B737 SRM 53-10-08.Aug 15, 2009 · N451UW · Boeing 7374B7SDR USAA2009090892402Pressure Panel · crackedSAL - BC-7 - MAJOR REPAIR - CRACK IN FORWARD FLOOR STRUCTURE PANEL AT FR36, Y1292. REPAIRED PRESSURE PANEL AT FR36, Y1292 IAW US AIRWAYS JOB CARD M2C53307.Aug 14, 2009 · N622AW · Airbus A320231SDR USAA2009090892401Pressure Panel · crackedSAL - BC-7 - MAJOR REPAIR - CRACK IN FORWARD FLOOR STRUCTURE PANEL AT FR36, -Y1292. REPAIRED PRESSURE PANEL AT FR36, -Y1292 IAW US AIRWAYS JOB CARD M2C53307.Aug 14, 2009 · N622AW · Airbus A320231SDR SWIA190022325Fitting · crackedREAR PRESSURE BULKHEAD CLIPS CRACKED. (C CHECK) REPLACED PER SRM.Aug 14, 2009 · N913EV · Cndair CL6002B19SDR A6WA200940562Bulkhead · crackedAFT PRESSURE BULKHEAD AT FS 621.00, LBL 27.50, WL 130.00 ABOVE CARGO DOOR TRACK FOUND CRACKED (.500 LENGTH). AFT PRESSURE BULKHEAD REPAIRED AT FS 621.00, LBL 27.50, WL 130 ABOVE CARGO DOOR TRACK CARRIED OUT IAW REO 601R-53-61-1541 REV "B".Aug 13, 2009 · N464AW · Cndair CL6002B19SDR A6WA200940506Bulkhead · crackedAFT PRESSURE BULKHEAD WEB IS CRACKED ABOVE THE CARGO DOOR TRACK AT FS 621.00, LBL 27.50, WL 130.00 CRACK LENGTH IS .250 INCH. REPAIR ON AFT PRESSURE BULKHEAD WEB ABOVE CARGO DOOR TRACK IAW REO 601R-53-16-1541, REV B. (K)Aug 13, 2009 · N424AW · Cndair CL6002B19SDR A6WA200940475Bulkhead · crackedEDDY CURRENT INSPECTION SHOWS STRONG DISCONINUITY INDICATION OF FWD FACE OF AFT PRESSURE BULKHEAD AT APPROX LBL 11.0 AND WL 116.0. INDICATION IS APPROX 0.5" IN LENGTH AND RUNS ROUGHLY VERTICALLY. EO 601R-53-61-3301, REV A AND GREO 601R-53-61-1285 TO REAR PREAug 13, 2009 · N431AW · Cndair CL6002B19SDR SWAA095264Attach Fitting · corrodedDURING SCHEDULED 20Y CHECK, FOUND BULKHEAD ATTACH CHORD CORRODED AT BS 219, BETWEEN BL 0 TO LBL 5. REPAIRED CHORD PER AAR EA.Aug 13, 2009 · N506SW · Boeing 7375H4SDR ASOA200900881Angle · crackedRIGHT 625 AFT BULKHEAD ANGLE CRACKED AT STRINGER 14. REMOVED AND REPLACED THE RIGHT BULKHEAD ANGLE AT FS 625, STR 14 IAW SRM 51-42-21.Aug 13, 2009 · N872AS · Cndair CL6002B19SDR ASOA200900880Angle · crackedLEFT 625 AFT BULKHEAD ANGLE CRACKED AT STRINGER 14. REMOVED AND REPLACED THE LEFT BULKHEAD ANGLE, FS 625 IAW SRM 51-42-21.Aug 13, 2009 · N872AS · Cndair CL6002B19SDR AALA20090814TUL06Bulkhead · corrodedCORROSION ON LOWER FORWARD SIDE OF AFT PRESSURE BULKHEAD LONGERON 28L TO LONGERON 28R OUT OF LIMITS. REPAIRED UNDER AARD 53-03-00 AND EA MD80-53-007109.Aug 12, 2009 · N9628W · Doug DC983SDR SWAA095209Bulkhead · crackedDURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE DOME BULKHEAD Y-CHORD CORRODED AT BS 1016, 6 O'CLOCK POSITION. REMOVED AND REPLACED BULKHEAD SECTION PER SRM.Aug 12, 2009 · N687SW · Boeing 7373Q8SDR SWAA095208Bulkhead · crackedDURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD FWD SIDE CRACKED AT BS 1016, LBL 3. REPAIRED BULKHEAD PER BAC DWG.Aug 12, 2009 · N687SW · Boeing 7373Q8SDR SWAA095206Bulkhead · corrodedDURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD FWD SIDE CORRODED AT BS 1016, LBL 6. REPAIRED BULKHEAD PER BAC DWG.Aug 12, 2009 · N687SW · Boeing 7373Q8SDR ASOA200900872Bulkhead · crackedAFT PRESSURE BULKHEAD SKIN IS CRACKED AT LINTEL ATTACH POINT ABOVE LINTEL. REPAIR PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETE AND THE REPAIR COMPLIES WITH THE REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230 REV. D.Aug 11, 2009 · N872AS · Cndair CL6002B19SDR SWAA095179Support Channel · corrodedDURING SCHEDULED 24Y CHECK, FOUND RT BULKHEAD SUPPORT CHANNEL CORRODED AT BS 1017, BL 0. REMOVED AND REPLACED CHANNEL PER SRM.Aug 11, 2009 · N316SW · Boeing 7373H4SDR COMA2009081150182Bulkhead · crackedFWD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE CUTOUT. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-11-593 AND EA 10-5311-02720.Aug 11, 2009 · N969CA · Cndair CL6002B19SDR A6WA200940483Bulkhead · crackedAFT PRESSURE BULKHEAD WEB IS CRACKED ABOVE THE CARGO DOOR TRACK AT FS 621.00, LBL 27.50, WL 130.00, CRACK LENGTH IS .250 INCH REO 601R-53-61-1541 PERFORMED. (K)Aug 9, 2009 · N466AW · Cndair CL6002B19SDR CA090812007Bulkhead · cracked(CAN) DURING 12 MONTH SCHEDULED INSPECTION OF BOXBEAM AND AREA ACCESS PANEL WAS REMOVED FOR INTERIOR INSPECTION. ONE (1) INCH CRACK EMINATING FROM TOP STARBOARD RIVET OF BULKHEAD TO CORNER WAS DISCOVERED. REPLACEMENT OF BULKHEAD NOW UNDERWAY. (TC# 20090812007)Aug 7, 2009 · Bell 206B3SDR SWIA200922786Fitting · crackedFS 202 BULKHEAD CLIP CRACKED. (C CHECK) REPLACED PER SRM.Aug 7, 2009 · N908SW · Cndair CL6002B19SDR ASOA200900861Bracket · crackedFS 621 FWD PRESSURE BULKHEAD HAS A CRACKED ISOLATOR BRACKET JUST ABOVE WL 106 AT LBL 18.Aug 7, 2009 · N856AS · Cndair CL6002B19SDR SWIA200922267Bulkhead · crackedAFT PRESSURE BULKHEAD LINTEL FITTING CRACKED. (C-CHECK) REPAIRED PER REO.Aug 7, 2009 · N913EV · Cndair CL6002B19SDR A6WA200940494Bulkhead · crackedRT PILOTS BULKHEAD FS 280.00, RBL 9.0 CRACKED (LOWER CROSSBEAM SECTION) RT PILOT BULKHEAD FS 280.00, RBL 9.0, REPAIRED C/O IAW REO 601R-53-11-171, REV D. (K)Aug 6, 2009 · N424AW · Cndair CL6002B19SDR A6WA200940510Bulkhead · crackedAFT PRESSURE BULKHEAD (FS 621) CRACK AT LINTEL FITTING LOCATION, CRACK LENGTH .500 INCH. AFT PRESSURE BULKHEAD AT FS 621 REPAIRED IAW REO 601R-53-61-1230, REV D.Aug 6, 2009 · N466AW · Cndair CL6002B19SDR A6WA200940492Bulkhead · crackedLEFT PILOTS BULKHEAD FS 280, LBL 9 CRACKED (LOWER CROSSBEAM SECTION) LENGTH .900 FT LT PILOTS BULKHEAD FS 280, LBL 9 REPAIRED IAW REO 601R53-11-171. (K)Aug 6, 2009 · N424AW · Cndair CL6002B19SDR A6WA200940514Bulkhead · crackedRIGHT PILOTS BULKHEAD FS 280.00, RBL 9.0 CRACKED (LOWER CROSSBEAM SECTION) RT PILOT BULKHEAD FS 280.00, RBL 9.0 REPAIRED C/O IAW REO 601R-53-11-171, REV D. (K)Aug 6, 2009 · N424AW · Cndair CL6002B19SDR A6WA200940517Bulkhead · crackedFS 202.75 AT LBL 23.71, PRESSURE BULKHEAD CRACKED AT PARKING BRAKE LOCATION 3 CRACKS: 1.00 INCH, 1.00 INCH, .500 INCH. REPAIR IAW REO 601R-53-11-1738 AND 601R-53-11-563. (K)Aug 6, 2009 · N424AW · Cndair CL6002B19SDR A6WA200940496Pressure Blkhd · crackedFS 202.75 AT LBL 23.71 PRESSURE BULKHEAD CRACKED AT PARKING BRAKE LOCATION, 3 CRACKS, 1.00 INCH, 1.00 INCH, .500 INCH. REPAIR IAW REO 601R-53-11-1738 AND 601R-53-11-563. (K)Aug 6, 2009 · N424AW · Cndair CL6002B19SDR ASOA200900866Pressure Panel · damagedWHILE PERFORMING HFEC INSPECTION OF FS 460.00 PRESSURE FLOOR MULTIPLE INDICATIONS OF VARYING LENGTHS WERE NOTED APPROX 1.25 INCH FWD OF INTERCOSTALS IN THE THREE BAYS BETWEEN LBL 18.00 AND RBL 9.00. INDICATIONS RANGE FROM 30 - 60 PERCENT FSH. FAILS NDT INSPECAug 5, 2009 · N856AS · Cndair CL6002B19SDR ASOA200900851Bulkhead · damagedRIGHT FS 559 BULKHEAD WEB HAS 2 INDICATIONS NOTED: 1) O/B OF RBL 9.0 WL 58.70 APPROX .2 INCH IN LENGTH 80 PERCENT FSH, 2) I/B OF RBL 18.0 WL 59.10 APPROX .3 INCH IN LENGTH 80 PERCENT FSH. BOTH AREAS FAILED NDT INSPECTION.Aug 5, 2009 · N856AS · Cndair CL6002B19SDR A6WA200940487Pressure Blkhd · crackedCRACK FOUND ON PRESSURE BULKHEAD AT FS 202.75, LBL 23.71 AT PARKING BRAKE LOCATION. CRACK LENGTH .50 INCH CRACK ON PRESSURE BULKHEAD AT FS 202.75, LBL 23.71 AT PARKING BRAKE LOCATION, REPAIRED IAW REO 601R-53-11-563. (K)Aug 4, 2009 · N466AW · Cndair CL6002B19SDR ASOA200900846Bulkhead · damagedREAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS AN INDICATION NOTED APPROX .1 INCH IN LENGTH 60 PERCENT FSH, FAILED NDT INSPECTION. C/W REO 601R-53-61-1230 STEPS 1-24 REPAIR TO PRESSURE BULKHEAD WEB FS 621 LINTEL REV D.Aug 4, 2009 · N856AS · Cndair CL6002B19SDR C2XA09TY212Firewall · crackedTYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND A CRACK IN THE APU FIREWALL. MAINTENANCE REMOVED AND REPLACED THE FIREWALL IAW EMB 145 SRM 51-40-02 AND IC 2009-145/06143. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Aug 4, 2009 · N14933 · Emb EMB145EPSDR SWIA200922635Bulkhead · crackedFS 621 BULKHEAD CARGO TRACK FITTING CRACKED. (C CHECK) REPAIRED PER REO.Aug 3, 2009 · N912EV · Cndair CL6002B19SDR USAA2009080492008Bulkhead · crackedPIT - FPBH - MAJOR REPAIR - 2 CRACKS ON BS 178 BULKHEAD WEB AT WL 233 & WL 228, RBL 17. REPLACED BS 178 BULKHEAD WEB AT WL 233 & WL 228, RBL 17 IAW B737 SRM 53-10-08.Aug 3, 2009 · N421US · Boeing 737401SDR A6WA200940466Bulkhead · crackedFWD PRESSURE BULKHEAD IS CRACKED AT FS 202.75, LBL27.5, WL 69.00 AND QTY 1 ELONGATED HOLE EXISTS IN WEB AND STIFFNER FS 202.75, LBL 9.00, WL 69.00. FWD PRESSURE BULKHEAD REPAIRED AT FS 202.75, WL 69.00 AND QTY 1 ELONGATED HOLE REPAIRE IN WEB AND STIFFNER FS 2Aug 2, 2009 · N423AW · Cndair CL6002B19SDR SWIA200922777Bulkhead · crackedFS 202 BULKHEAD CRACKED. (C CHECK) REPAIRED PER REO.Aug 1, 2009 · N913EV · Cndair CL6002B19SDR A6WA200940470Angle · crackedPRESSURE BULKHEAD LOWER FRAME CAP ANGLE IS CRACKED IN THE RADIUS. PRESSURE BULKHEAD LOWER FRAME CAP ANGLE REPAIRED IAW REO 601R-53-41-1022 AND REO 601R-53-41-260, REV C. (K)Jul 30, 2009 · N423AW · Cndair CL6002B19SDR USAA2009080492007Bulkhead · crackedPIT - FPBH - MAJOR REPAIR - CRACK ON BS 178 BULKHEAD BEAM WEB AT WL 184, LBL 17. REPLACED BS 178 BULKHEAD BEAM WEB AT WL 184, LBL 17 IAW B737 SRM 53-10-08.Jul 30, 2009 · N421US · Boeing 737401SDR USAA2009080492006Bulkhead · crackedPIT - FPBH - MAJOR REPAIR - 3 CRACKS ON BS 178 BULKHEAD FRAME WEB AT WL 227 TO WL 232, LBL 17. REPLACED BS 178 BULKHEAD FRAME WEB AT WL 227 TO WL 232, LBL 17 IAW B737 SRM 53-10-08.Jul 30, 2009 · N421US · Boeing 737401SDR EE4Y090200Bulkhead · crackedUPPER FUSELAGE AT BS 178, LBL 7.5, WL 231 PRESSURE BULKHEAD WEB WITH CRACK.Jul 30, 2009 · N472BC · Boeing 737219SDR ASAA0946309Support Angle · corrodedFCB AFT BULKHEAD FLOOR TO BULKHEAD SUPPORT ANGLE ASSY IS CORRODED. REMOVED AND REPLACED AFT BULKHEAD FLOOR TO BULKHEAD SUPPORT ANGLE.Jul 29, 2009 · N769AS · Boeing 7374Q8
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