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 SWAA2015040638114Bulkhead · crackedLEFT MLG VERTICAL BULKHEAD PRESS DECK CRACKED AT BS 663, BETWEEN LBL 34 - 41. REPAIRED BULKHEAD IAW SRM.Mar 23, 2015 · N208WN · Boeing 7377H4SDR AALA20150323006Stiffener · crackedVERTICAL STIFFENER ON FWD CTR SIDE OF STATION 1338 BULKHEAD, ABOVE VAULT DOOR JAMB, IS CRACKED AT UPPER END. R & R STIFFENER IAW AARD 51-10-00-5 & DWG 9915562.Mar 23, 2015 · N9625W · Doug DC983SDR SWAA2015043039185Stiffener · crackedFORWARD PIT AFT PRESS BULKHEAD SEVERAL STIFFENERS CRACKED AT BS 663, RBL 22. R & R STIFFENER IAW SRM & DWG.Mar 22, 2015 · N930AT · Boeing 717200SDR SWAA2015040638107Bulkhead · crackedLEFT WW FWD BULKHEAD OTBD OF PACK EXHAUST CRACKED. REPAIRED BULKHEAD IAW EA.Mar 22, 2015 · N208WN · Boeing 7377H4SDR EVCA20150324075Stiffener · crackedCRACKS ON THE LT & RT 145 BULKHEADS AS FOLLOWS, LT 145 STIFFENER HAS A CRACK COMING FROM THE MIDDLE RIVET & RT SIDE JUST PAST THE STIFFENER THERE IS A CRACK APPROX 2 INCHES LONG IN THE UPPER RADIUS. THE CRACKS & DAMAGE ARE BEHIND THE CLIPS THAT HOOK THE TOP OMar 22, 2015 · N282AE · Bell 206L3SDR SWIA201541020Bulkhead · crackedINDICATION AT FWD SIDE OF BULKHEAD FS 202.75 POST AT LBL 30.00. REPAIRED IAW REO.Mar 21, 2015 · N217AG · Cndair CL6002C10SDR ASOA2015041712624Bulkhead Web · corrodedLT SIDE 280 WEB IS CORRODED. COMPLIED WITH EC/TC REO 670-53-11-594 AND GREO 670-53-11-594 REV-DATED: 04/27/2011.Mar 21, 2015 · N718EV · Cndair CL6002C10SDR ASOA2015041712623Bulkhead Web · corrodedRT SIDE 280 WEB IS CORRODED. COMPLIED WITH EC/TC REO 670-53-11-594-01 GREO 670-53-11-594 REV DATED: 04/27/2011.Mar 21, 2015 · N718EV · Cndair CL6002C10SDR CALA2015032300195Pressure Panel · crackedINSPECTION HFEC CTR WING SPAR VERTICAL PRESS WEB BETWEEN LBL 24.92 - 45.64. FOUND WEB BETWEEN LBL 31.83 & 40.00 HAS A 1/2" CRACK MARKED AT STATION 663. REPAIRED IAW SRM 57-10-10 REP 3 ALT 1. INSPECTION THRESHOLD AT 56000 FLIGHT CYCLES AFTER REPAIR, FOLLOWEDMar 21, 2015 · N37409 · Boeing 737924SDR HALA2015032000049Bulkhead Web · damagedBS 110 BULKHEAD WEB JUST AFT OF NLG CENTER LOCKING DAMAGED. REPAIRED IAW SRM 53-02-01, REPAIR FIG 202, SHEET 3.Mar 20, 2015 · N491HA · Boeing 717200SDR SWAA2015032337693Pressure Panel · crackedRIGHT MAIN WW 3" BELOW UPPER WEB CRACKED AT BS 663, RBL 43. REPAIRED WEB IAW EA.Mar 20, 2015 · N212WN · Boeing 7377H4SDR SWAA2015032337692Pressure Panel · crackedRIGHT MAIN WW 2" BELOW UPPER WEB CRACKED AT BS 663, RBL 43. REPAIRED WEB IAW EA.Mar 20, 2015 · N212WN · Boeing 7377H4SDR SWAA2015032337691Pressure Panel · crackedLEFT MAIN WW UPPER WEB CRACKED AT BS 663, LBL 43. REPAIRED WEB IAW EA.Mar 20, 2015 · N212WN · Boeing 7377H4SDR SWIA201540959Angle · chafedAFT PRESSURE BULKHEAD AFT SIDE DOUBLING ANGLE, VERTICAL STIFFENER, AT BL 0.0 HAS CHAFE AT LOWER FWD END. CAUSED BY CONTACT WITH FLOTATION VALVE MIGRATED HINGE PIN, CAMP 11987372, JOB 91506171, OP 121, C-CHECK RO 4/1/15. COMPLIED WITH REPAIR OF AFT PRESSURE BMar 19, 2015 · N802SK · Cndair CL6002D24SDR A6WA201542535Bulkhead · chafedAFT SIDE OF 280 BULKHEAD HAS CHAFE NEAR RBL 10.Mar 19, 2015 · N460AW · Cndair CL6002B19SDR LR7A2015031800545Bulkhead · crackedDURING SCHEDULED C-11 CHECK WHILE PERFORMING SB 382-57-85 R2 APPENDIX A NDI AND SP-141 NDI, FOUND 3 CRACKS EVIDENT ON THE RT FS577-FS617 SIDEWALL AT FS576, FS577, & FS588, RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-60 AND 51-70. NR 2267.Mar 18, 2015 · N405LC · Lkheed 382GSDR LR7A2015031800544Bulkhead · crackedDURING SCHEDULED C-11 CHECK WHILE PERFORMING SB 382-57-85 R2 APPENDIX A NDI AND SP-141 NDI, FOUND 2 CRACKS EVIDENT ON THE RT FS528-FS577 SIDEWALL AT FS528, RBL61. REPAIR BY SIDEWALL REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-60 AND 51-70. NR 2266.Mar 18, 2015 · N405LC · Lkheed 382GSDR LR7A2015031800537Bulkhead · crackedDURING SCHEDULED C-11 CHECK, FOUND THE RT MAIN WHEEL WELL BULKHEAD WEB HAD CRACKED AT FS 599, WL 190, RBL 62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, CHAPTER 51-60 AND 51-70, NR 2240, PSE 53-40-17, AD 2012-06-09.Mar 18, 2015 · N405LC · Lkheed 382GSDR LR7A2015031800529Stiffener · crackedDURING SCHEDULED C-11 CHECK, FOUND THE FS 93 NOSE RADOME BULKHEAD STIFFENER HAD CRACKED AT RBL 27, WL 150. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583 CHAPTER 51-60 AND 51-70, NR 2203, PSE 53-30-15, AD 2012-06-09.Mar 18, 2015 · N405LC · Lkheed 382GSDR LR7A2015031800523Bulkhead Web · crackedDURING SCHEDULED C-11 CHECK, FOUND THE LT AFT FUSELAGE INTERIOR FS880 BULKHEAD WEB HAD CRACKED AT WL 200, LBL66. REPAIR BY WEB REPLACEMENT ACCOMPLISHED IAW SMP 583, CHAPTER 51-60, 51-70 AND 51-140-17. NR 2102.Mar 18, 2015 · N405LC · Lkheed 382GSDR SWAA2015033037991Bulkhead · crackedVERTICAL BULKHEAD WEB CRACKED AT BS 663, BETWEEN RBL 40 - 45. R & R WEB IAW SRM.Mar 16, 2015 · N933WN · Boeing 7377H4SDR CALA2015031700167Pressure Deck · crackedVERTICAL PRESS DECK CRACKED STATION 663, LBL 40.00 - 45.64 BETWEEN WL 192.0 & WL 200.6. INSTALLED REPAIR DOUBLER IAW SRM 57-10-10 REPAIR 3, ALTERNATIVE 2. INSPECTION THRESHOLD OF 56000 FLIGHT CYCLES AFTER REPAIR INSTALLATION & 36000 FLIGHT CYCLES INTERVAL IAMar 16, 2015 · N24211 · Boeing 737824SDR ASOA2015033112520Isolator · brokenMULTIPLE BROKEN ISOLATORS ON FS 621.00 BULKHEAD. R & R 7 EA ISOLATORS ON FS 621.00 BULKHEAD IAW SRM 51-42-06.Mar 15, 2015 · N881AS · Cndair CL6002B19SDR SWAA2015043039178Stiffener · crackedAFT FACE OF PRESS BULKHEAD STIFFENER CRACKED AT BS 727, RBL 6.3. REPLACED STIFFENER IAW SRM & DWG.Mar 14, 2015 · N354SW · Boeing 7373H4SDR SWIA201540978Bulkhead · crackedSUSPECTED CRACK AT FORWARD HYD BAY, FS 202.00 BULKHEAD WHERE BRAKE CONTROL CABLE GOES THROUGH. C-CHECK, RO 4/2/15, REPAIRED SUSPECTED CRACK AT FORWARD HYD BAY FS 202.00 BULKHEAD WHERE BRAKE CONTROL CABLE GOES THROUGH REF REO LEAK CHECK GOOD COMPLIED WITH ST 5Mar 14, 2015 · N448SW · Cndair CL6002B19SDR FDEA201503140930Firewall · gougedAPU COMPARTMENT BS 1885.20 LOWER MID-SECTION AT FIREWALL, RT SIDE EXISTING DOUBLER HAS DEEP GOUGE. REMOVED EXISTING DOUBLER AT FIREWALL IAW SRM 51-40-02. FABRICATED NEW DOUBLER FROM PN TI-6AL-4V .025, PO 956AT-00176. DIMENSIONS ARE 6.5" X 3.85". IAW SRM 53Mar 14, 2015 · N947FD · Boeing 757236SDR SWAA2015031737526Pressure Panel · crackedLEFT MAIN WW SPAR VERTICAL WEB CRACKED AT BS 663, BETWEEN LBL 24.92 TO LBL 34. REPAIRED WEB IAW EA.Mar 14, 2015 · N210WN · Boeing 7377H4SDR SWAA2015031737525Pressure Panel · crackedRIGHT MAIN WW SPAR VERTICAL WEB CRACKED AT BS 663, BETWEEN RBL 31.83 TO RBL 40. REPAIRED WEB IAW EA.Mar 14, 2015 · N210WN · Boeing 7377H4SDR ASOA2015040812555Bulkhead Web · corrodedFS 280.00 BULKHEAD LOWER WEB RT SIDE CORRODED. WEB CORRODED BEYOND LIMITS AT FS280 RBL 12, WL72.50 IAW SRM 51-21-06-001-001-A01. COMPLIED WITH ECTC REO 670-53-11-594 01 AND GREO 670-53-11-594, REV , DATED: 04-27-2011. R & R 2EA STIFFENER ANGLES AT RBL 17.46Mar 13, 2015 · N228PQ · Cndair CL6002D24SDR ASOA2015040812554Bulkhead Web · corrodedFS 280.00 BULKHEAD LOWER WEB LT SIDE CORRODED. WEB CORRODED BEYOND LIMITS AT FS280 LBL, WL72.50 IAW SRM 51-21-06-001-001-A01. COMPLIED WITH ECTC REO 670-53-11-594 AND GREO 670-53-11594, REV DATED: 04/27/2011. R & R STIFFERNER ANGLE AT LBL33 IAW SRM 51-42-06Mar 13, 2015 · N228PQ · Cndair CL6002D24SDR ASOA2015040212531Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT BL 0.0 BETWEEN WL 128 TO WL 134 APPROX 5" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. COMPLIED WITH REO 601R-53-61-5456, REV, DATED 2015/03/17 IN IT'S ENTIRETY. COMPLIED WITH EC/TC REO 601R-53-61Mar 13, 2015 · N881AS · Cndair CL6002B19SDR AALA20150321006Pressure Deck · corrodedRIGHT MAIN WW PRESS DECK CORRODED AT APPROX FS 1170 & RBL 60 ABOVE EMER SLIDE CONTAINER. REPAIRED IAW EA 53-039083 DATED 03 20 2015.Mar 13, 2015 · N692AA · Boeing 757223SDR AALA20150321005Pressure Deck · corrodedRIGHT MAIN WW PRESS DECK CORRODED AT APPROX FS 1165 & RBL 49 ABOVE EMER SLIDE CONTAINER. REPAIRED IAW EA B757-53-039083 DATED 03 20 2015.Mar 13, 2015 · N692AA · Boeing 757223SDR AALA20150321004Pressure Deck · corrodedRIGHT MAIN WW PRESS DECK CORRODED AT APPROX FS 1151 & RBL 51 ABOVE EMER SLIDE CONTAINER. REPAIRED IAW EA 53-039083 DATED 03 20 2015.Mar 13, 2015 · N692AA · Boeing 757223SDR AALA20150321003Pressure Deck · corrodedLEFT MAIN WW PRESS DECK HAS CORROSION AT APPROX FS 1170 & LBL 68 ABOVE EMER SLIDE CONTAINER. REPAIRED IAW EA 53-038994 DATED 03 20 2015.Mar 13, 2015 · N692AA · Boeing 757223SDR SWAA2015031837581Attach Angle · crackedPRESSURE BULKHEAD ATTACH ANGLE CRACKED AT BS 1016, RBL 16. R & R ANGLE IAW SRM & DWG.Mar 13, 2015 · N694SW · Boeing 7373T5SDR WVER0313201500002Bulkhead · distortedSHOP FLOOR FINDS THE RT NLG WHEEL WELL BULKHEAD DISTORTED. PERFORMED A MAJOR REPAIR TO NLG WHEEL WELL RT BULKHEAD, PN CC670-32127 AT THE GROUNDING POINT IAW REO 690-53-11-746, REV REF CO 15025315, JOB 41502531, OP 54.Mar 12, 2015 · N925FJ · Cndair CL6002D24SDR SWAA2015031837576Bulkhead · crackedFUSELAGE BULKHEAD CHORD FASTENER HOLE C CRACKED AT BS 540, BETWEEN STRINGER 22L TO 23L, 3RD HOLE DOWN AFT. REPAIRED CHORD IAW ACO.Mar 11, 2015 · N273WN · Boeing 7377H4SDR SWAA2015031737515Bulkhead · crackedFUSELAGE BULKHEAD CHORD CRACKED AT BS 540, BETWEEN STRINGER 22L - 23L, 2ND HOLE DOWN AFT. REPAIRED CHORD IAW ACO.Mar 11, 2015 · N273WN · Boeing 7377H4SDR CA150514004Plate · cracked(CAN) DURING A SPECIAL INSPECTION OF THE AFFECTED AREA, SEVERAL CRACKS WAS DISCOVERED ON THE FWD LT LANDING GEAR REINFORCEMENT PLATE, PN-0613105-2. THE CRACKS RADIATED TANGENTIALLY FROM THE LOWER OTBD 5/16 HOLE AT THE 5:00 & 7:00 POSITION FOR ABOUT 1/2", TERMMar 10, 2015 · Cessna 305CSDR CA150311008Skin · damaged(CAN) DURING EVENT 3 INSPECTIONS, AT THE AFT-SIDE LT FIREWALL, THE LT NACELLE BOTTOM INBD SKIN, IPC SEC VII POWER PLNT GRP ITEM 85-28, FOUND 2 RIVETS PULLED THROUGH. THESE RIVETS PASS THROUGH THE INBD L/E EDGE OF THE LT WING BOTTOM CENTER SKIN, PA31-350, IPC Mar 10, 2015 · Piper PA31350SDR SWAA2015060340336Repair · corrodedEXISTING REPAIR AT BULKHEAD WEB CORRODED, STATION 1017, LBL 10 - 15, WL 193. REPAIRED WEB IAW EA.Mar 10, 2015 · N697SW · Boeing 7373T0SDR DALA2015031102128Bulkhead · crackedBS 1809 BULKHEAD LT FED OUTER CHORD HAS A ONE INCH CRACK AFT OF AND JUST BELOW STRINGER 7. REPAIRED IAW SRM 53-80-08.Mar 10, 2015 · N128DL · Boeing 767332SDR SWAA2015031237387Bulkhead · crackedLEFT MLG WW FWD BULKHEAD VAPOR BARRIER CRACKED AT BS 663, BETWEEN LBL 28 TO LBL 38. REPAIRED BARRIER IAW EA.Mar 10, 2015 · N907WN · Boeing 7377H4SDR AALA20150310009Stiffener · corrodedSTIFFENER ON FS 1180 BULKHEAD 1180 IN RT MLG WW IS CORRODED 12 INCHES IN FROM OTBD END. REPAIRED STIFFENER BY BLENDING IAW 53-038921 REV A.Mar 10, 2015 · N642AA · Boeing 757223SDR ASOA2015032712490Bulkhead Web · corrodedCORROSION FOUND ON THE LT WEB AT FS280.00. REMOVED CORROSION FROM WEB AT LBL 11, FS 280 IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-11-10-201-003-A01, FIG 53-11-10-994-804. RECEIVED AND COMPLIED WITH EA 32-201-085 AS PERMANEMar 9, 2015 · N137EV · Cndair CL6002D24SDR GLBA2015030900501Bulkhead · buckledDURING A SCHEDULED INSPECTION, FOUND THE CANTED BULKHEAD AT FS 588.10 BUCKLED FROM STRINGER 12R TO 12L. REPAIRED THE BULKHEAD IAW EO 15-120-53-001. MAJOR REPAIR.Mar 9, 2015 · N201GL · Beech 1900DSDR SWAA2015050439245Pressure Deck · crackedMAIN WW PRESS DECK CRACKED AT BS 664+1.750, LBL 45.50. REPAIRED WEB IAW EA.Mar 8, 2015 · N354SW · Boeing 7373H4SDR SWAA2015042939131Bulkhead · crackedFLOOR BULKHEAD WEB CRACKED AT BS 1016, RBL 35. R & R WEB IAW SRM.Mar 6, 2015 · N7816B · Boeing 7377L9SDR SWAA2015041538513Bulkhead · crackedBULKHEAD CHORD CRACKED AT BS 178, RBL 17. REPAIRED CHORD IAW SRM & EA.Mar 6, 2015 · N612SW · Boeing 7373H4
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