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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR LR7A2020100502414Cap · crackedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND THE CARGO COMPARTMENT FS 577 UNDERFLOOR BULKHEAD UPPER CAP CRACKED AT RBL 54, WL 146. REPAIR BY REPLACEMENT ACCOMPLISHED, IAW LOCKHEED SMP583 SRM, CH 51-60 & 51-70. NR 2712.SDR LR7A2020100502413Cap · corrodedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND THE CARGO COMPARTMENT FS 417 UNDERFLOOR BULKHEAD UPPER CAP CORRODED AT LBL 20, WL 146. REPAIR BY REPLACEMENT ACCOMPLISHED, IAW LOCKHEED SMP583 SRM, CH 51-60 & 51-70. NR 2711.SDR LR7A2020100502410Bulkhead Web · crackedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE AFT FUSELAGE CARGO COMPARTMENT RT FS 880 WL 200 WEB CRACKED. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-17. NR 2631.SDR LR7A2020100502409Bulkhead Web · crackedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE AFT FUSELAGE CARGO COMPARTMENT LT FS 946 LBL 54 UPPER BULKHEAD WEB CRACKED AT 1/2" DIAMETER HOLE WL 265. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-17. NR 2630.SDR LR7A2020100502391Doubler · crackedDURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR FS 1034 AFT BULKHEAD DOUBLER CRACKED. REPAIR BY REPLACEMENT ACCOMPLISHED, IAW LOCKHEED SMP583 SRM, CH 51-60 & 51-70. NR 2553.SDR LR7A2020100502379Stiffener · corrodedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE NOSE WHEEL WELL FS 165 BULKHEAD LBL 27 STIFFENER CORRODED WL 129. REPAIR BY REPLACEMENT ACCOMPLISHED, IAW LOCKHEED SMP583 SRM, CH 51-60 & 51-70. NR 2535.SDR SWIA202053792Bulkhead Web · corrodedFS 280 RT WEB HAS EVIDENCE OF CORROSION AT FLOOR LEVEL AT APPROXIMATELY BL42RH. C-CHECK RO 11/1/2020. REMOVED WEB, EVAULATED AND FOUND TO BE OUT OF LIMITS. INSTALLED NEW WEB, PER REO. COMPLIED WITH SKYWEST TASK CARD.SDR SWIA202053790Bulkhead Web · corrodedLT FS 280 WEB HAS BULGE WITH EVIDENCE OF INTERNAL EXFOLIATION CORROSION AT INBOARD EDGE/FLOOR LEVEL. C-CHECK RO 11/1/2020. PERFORMED EVAL OF THE LT FS 280 WEB. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED FABRICATED BUTTSTRAP (WEB) LT AT FS 280, PER RESDR A6WA202010057308Bulkhead Web · crackedSDI OF THE AFT PRESSURE BULKHEAD FWD FACE, IAW NDTM AWAC SUPPLEMENT 09-008 REV 41. ACCOMPLISHED UT INSPECTION ON AFT PRESSURE BULKHEAD FWD FACE, IAW NDTM PART 4, 53-61-153 REV 41 NO INDICATIONS NOTED. ACCOMPLISHED HFEC INSPECTION ON AFT PRESSURE BULKHEAD FWDSDR A6WA202010057307Bulkhead Web · crackedNDT-3 INDICATION FOUND COMING FROM UNDER MACHINED FITTING OF THE BAGGAGE BAY DOOR (LINTEL AREA) FOUND 3 EACH CRACKS AT FS 621.00. NR 1 VERTICAL CRACK THAT MEASURES 1.7'' UPPER HORIZONTAL CRACK THAT MEASURES .5'' AND LOWER HORIZONTAL CRACK THAT MEASURES .5'' SDR SWAA2020110420090Pressure Blkhd · crackedCRACK INDICATION FOUND AT EXTERIOR SIDE (WHEEL WELL INTERIOR) OF LEFT MAIN WHEEL WELL SPAR VERTICAL PRESSURE WEB AT STA 663 LBL BETWEEN LBL 24.92 AND LBL 31.83 WITH APPROXIMATE LENGTH - 0.118''. REMOVED EXISTING DOUBLER AT VERTICAL PRESSURE WEB REPAIR STA 663SDR SWAA2021072720026Bulkhead · crackedAFT CARGO COMPARTMENT; FWD BULKHEAD PANEL # 142NW CRACKED NOTED ON A PREVIOUS REPAIR (ZONE 142). / REMOVED AND INSTALLED NEW PANEL #142NW AFT CARGO COMPARTMENT; FWD BULKHEAD AS PER B737-700 REFS AMM: 25-52-18-000-801 AND REF AMM: 25-52-18-400-801SDR SWAA2020101919583Bulkhead Web · crackedLT HAND VAPOR BARRIER AT STA 663 HAS A CRACKED AT APPROXIMATELY LBL 41. CLEANED AREA OF DAMAGE, STOP DRILL CRACK. PERFORMED DRY OUT NO WATER FOUND. REPAIRED DAMAGE CRACK SIZE 8' ON STA 663 LBL 4 AT LT VAPOR BARRIER, AS PER B737-700 SRM 51-70-04-2R-10 REPAISDR AALA202010099001Vapor Barrier · crackedAIRCRAFT IN BASE MAINTENANCE. RIGHT HAND MAIN LANDING GEAR WHEEL WELL VAPOR BARRIER CRACKED AT BS 663.75 AND RBL 30. REPAIRED VAPOR BARRIER, PER AARD 57-10-10-9, SRM 57-10-10-2R-2 AND EA 254628.SDR SWAA2021072719600Bulkhead · crackedAFT CARGO FWD BULKHEAD PANEL 141 LW CRACK; P/N 453A2510-20 / RECEIVED NEW PANEL 141LW AT AFT CARGO COMPARTMENT P/N 453A2510-20; NEW PANEL TO BE INSTALLED ON T/C JPANEL-141-CLOSESDR IPXA2020093060809Retainer · bentINSPECTION TYPE: A300 LT AC ACCESS PANEL 147CZ HAS BENT SEAL RETAINER. REPAIRED PANEL ON A300-2570-77956A.SDR N6WA2020093001Bulkhead · corrodedFS 280.00 BULKHEAD HAS CORROSION ON THE BOTTOM LT CORNER OF THE COCKPIT DOOR ENTRY WAY. REMOVED AND REPLACED FS 280 BULKHEAD.SDR SWIA202053519Bulkhead · damagedEVALUATE RT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIV NUT LOCATIONS, REFERENCE RIL 5378. REPAIR IF NEEDED, IAW ENGINEERING INSTRUCTIONS. C-CHECK RO 10/18/2020. COMPLIED WITH MHIRJ EO IN REPAIR OF TOOOLING DAMAGE TO RT 9G BULKHEAD AFT WALL. REPAIR DOUBLER MSDR SWIA202053518Bulkhead · damagedEVALUATE CENTER 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIV NUT LOCATIONS, REFERENCE RIL 5378. REPAIR IF NEEDED, IAW ENGINEERING INSTRUCTIONS. C-CHECK RO 10/18/2020. COMPLIED WITH MHIRJ EO IN REPAIR OF TOOLING DAMAGE TO CENTER 9G BULKHEAD AFT WALL. REPAIR DOSDR SWIA202053517Bulkhead · damagedEVALUATE LT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIV NUT LOCATIONS, REFERENCE RIL NR 5378. REPAIR IF NEEDED, IAW ENGINEERING INSTRUCTIONS. C-CHECK RO 10/18/2020. COMPLIED WITH MHIRJ EO IN REPAIR OF TOOLING DAMAGE TO LT 9G BULKHEAD AFT WALL. REPAIR DOUBLERSDR SWAA2020100821642Pressure Blkhd · crackedAFT PRESSURE BULKHEAD WEB SKIN HAS A CRACK INDICATION RADIATING TOWARD THE CENTER OF THE APB AT THE MOST CENTERED FASTENER COMMON TO THE RADIAL STIFFENER ALIGNED WITH STRINGER 22L. FOUND DURING HFEC INSPECTION OF NDT PART 6; 53-10-64, PER TASK CARD 5311-I-116SDR HALA2020092903133Doubler · cracked492 C CHECK, DURING ROUTINE MAINTENANCE TASKS, HWI DISCOVERED A CRACK IN THE STA 1178 BULKHEAD DOUBLER (PN 9911839-265) AND SKIN PANEL (PN 5912141-77), JUST INBOARD OF L-3L. MINOR REPAIR. E105-492092-PERM C/W DATE 09/10/20, MECH 019536. PENDING INSTALLATIONSDR SWIA202054972Bulkhead · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD-COMPLY WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION FS 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER TR. (J)(2) MODIFYINSDR ABXA20200803194Bulkhead Web · buckledHAECO NR-42871 AFT SIDE OF AFT PRESSURE BULKHEAD JUST BELOW TEAR STRAP TS6 AT RADIAL STIFFENER RS17 SKIN BUCKLED AT MULTIPLE RIVET LOCATIONS, REF ABX-REA-5380-64028-00.SDR AALA202009279010Vapor Barrier · crackedAIRCRAFT IN BASE MAINTENANCE. RIGHT HAND MAIN LANDING GEAR WHEEL WELL VAPOR BARRIER CRACKED UNDER THE HYDRAULIC B RESERVOIR. REPAIRED VAPOR BARRIER, PER AARD 57-10-10-9 AND SRM 57-10-10-2R-2.SDR A6WA202009287297Bulkhead Web · crackedPERFORMED SDI OF AFT PRESSURE BULKHEAD FWD FACE, IAW NDTM AWAC SUPPLEMENT 09-008 REV 41. PERFORMED EDDY CURRENT INSPECTION, IAW NDTM PART 1 51-20-06 REV 41. PERFORMED UT INSPECTION, IAW NDTM PART 4 53-61-153 REV 41. 5 EACH DISCREPANCIES. DISCREPANCY 1: FS SDR SWIA202054508Bulkhead Web · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD-COMPLY WITH PARAGRAPH (J) OF AD: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION FS 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL. (J)(2) MODIFYING THE RPB AND DOING SDR SWIA202054209Bulkhead Web · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD-COMPLY WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION FS 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER. (J)(2) MODIFYING TSDR K11A2020092400021Bulkhead · corrodedRT AFT A/C BAY HAS EVIDENCE OF CORROSION ON AFT BULKHEAD.SDR SWAA2021081217575Bulkhead Web · canningREFERENCE WORK CARD J11415446 DURING REINSPECTION OF THE CRACK AT LBL 45 LEFT WHEEL WELL FOUND CRACK TO GROW TO A TOTAL LENGTH OF APPROX 8.25 INCHES. / STOPPED DRILLED THE CRACK PER SRM 51-10-02 AND EA 1-A57-13410. APPLIED SPEED TAPESDR EVCA2020093002Bulkhead · crackedDURING ROUTINE INSPECTION, LT STA 155 BULKHEAD FRAME CRACKED APPROXIMATELY WL 57.SDR REXA2020092800658Bulkhead Web · corrodedFS 280 WEB IS CORRODED BETWEEN RBL 9 AND LBL 9. CA: REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B DATED 2006/05/10.SDR FDEA202009182247Bulkhead Web · dentedAFT CARGO, STATION 1841 BULKHEAD WEB X=2" TO 18" FOUND DENTS. AFT CARGO STATION 1841 BULKHEAD WEB X=2 TO 18 REMOVED, AS PER SRM 51-33-01-0G AT STATION 1841 X=0 TO X=60. WEB FABRICATED, AS PER DOUGLAS DRAWING AGA 7170 REVISION R. WEB INSTALLED AT STATIONSDR SCNA20201008108Vertical Support · crackedVERTICAL STIFFENER CRACKED AT BS 663 LBL 25 WL 150. REMOVED AND REPLACED VERTICAL STIFFENER AT BS 663 LBL 25 WL 150 WITH PO 802748, IAW SRM 51-40-02-0G-0 AND BOEING DWG 111A1000 REV B 57828U.SDR SWAA2020092116853Bulkhead Web · crackedCENTER WING SECTION REAR SPAR VAPOR BARRIER HAS VERTICAL CRACK APPROX 10 INCHES IN LENGTH LOCATED BETWEEN LBL 45.64 AND LBL 31.83. APPLIED INTERIM REPAIR, IAW SRM 57-10-10-1A-2 PAR 2C (4)(A) AND APB SRM SUPPLEMENT 57-10-10 ALLOWABLE DAMAGE 2.SDR SWAA2020100616305Angle · crackedBS 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT RBL 8 WL 164. REPAIRED PER SRM 57-10-10-2R-5.SDR SWIA202053324Bulkhead Web · chafedAFT SIDE OF THE FS 280.00 BULKHEAD RT CENTER NEAR DOOR POST AREA WEB PATCH CHAFED, MARKED. C-CHECK RO 10/13/2020. REMOVED AND REPLACED AFT SIDE OF THE FS 280.00 BULKHEAD RT CENTER NEAR DOOR POST AREA WEB DOUBLER, REF REO.SDR SWIA202053540Bulkhead · damagedEVALUATE OR REPAIR LT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIVNUT LOCATIONS. C-CHECK RO 10/20/2020. REPAIRED LT 9G BULKHEAD, PER MHIRJ EO. COMPLIED WITH SKYWEST TASK CARD.SDR SWIA202053539Bulkhead Web · damagedEVALUATE OR REPAIR CENTER 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIV NUT LOCATIONS. C-CHECK RO 10/20/2020. REPAIRED CENTER 9G BULKHEAD, PER MHIRJ EO. COMPLIED WITH SKYWEST TASK CARD.SDR SWIA202053538Bulkhead Web · damagedEVALUATE OR REPAIR RT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIV NUT LOCATIONS. C-CHECK RO 10/20/2020. REPAIRED RT 9G BULKHEAD, PER MHIRJ REO. COMPLIED WITH SKYWEST TASK CARD.SDR SWIA202053320Bulkhead Web · damagedPERFORM REPAIR OF FS 280 BULKHEAD WEB LBL 20.75-RBL 20.75, REF REO. C-CHECK RO 10/13/2020. PERFORMED REPAIR OF FS 280 BULKHEAD WEB LBL 20.75-RBL 20.75, REF REO. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD.SDR IPXA2020100861090Profile · crackedINSPECTION TYPE: A300 MCD AFT BULKHEAD FLOOR SUPPORT CRACKED FRAME 80 RT OUTBOARD. REMOVED AND REPLACED, IAW SRM 51-40-21.SDR SWAA2020091515844Bulkhead · crackedRIGHT HAND MAIN LANDING GEAR FORWARD BULKHEAD AT BS 540 VAPOR BARRIER CRACKED IN TWO LOCATIONS. PERFORMED INTERIM REPAIR, PER REPAIR 57 EA-07683 FOR FURTHER CORRECTIVE ACTION REF 943 & NR V005123. REPETITVE ACTION REQUIRED: REMOVE ALUM FOIL TAPE AND PERFORM SDR SWAA2021072715702Bulkhead · crackedAFT CARGO BAY FWD BULKHEAD PANEL 142NWA IS CRACKED / RECEIVED NEW AFT CARGO BAY FWD BULKHEAD PANEL 142NWA; TO BE INSTALLED ON CUSTOMER CARD JPANEL-141-CLOSE.SDR SWIA202053099Post · crackedFS 409.00+128 RBL 27 INTERIOR BULKHEAD POST POSSIBLE CRACK INNER BOTTOM AFT CORNER AREA, MARKED. C-CHECK RO 10/4/2020. REMOVED AND REPLACED THE FS 409+128 RBL 27 BULKHEAD POST, REF REO SRM AND DWG. COMPLIED WITH SKYWEST TASK CARD. ALL CHECKS GOOD.SDR SWIA202053098Post · crackedFS 409.00+128 LBL 18 INTERIOR BULKHEAD POST POSSIBLE CRACK OUTER BOTTOM AFT CORNER AREA, MARKED. C-CHECK RO 10/4/2020. PERFORMED NDT ON FS 409.00+128 LBL INTERIOR BULKHEAD POS, REF CRJ 200 AMM NDTM PART 6, 51-20-06. VERIFIED CRACK. REMOVED AND INSTALLED NESDR SWAA2020092815421Bulkhead Web · crackedCUSTOMER REQUEST: LT STA 663 VAPOR BARRIER CRACKED. ACCOMPLISHED LT HAND STA 663 VAPOR BARRIER REPAIR, IAW B737 SRM 51-70-04-2R-10.SDR SWAA2020091414939Bulkhead Web · crackedCENTER WING REAR SPAR FUSELAGE STA 663 VAPOR BARRIER WEB CRACKED IN RT WHEEL WELL AT RBL 31.83. CRACK MEASURES APROX 4.00', ACTION REQUIRED. REPETITIVE ACTION REQUIRED DO A VISUAL INSPECTION OF THE REPAIR AREA, MAKE SURE THE CRACK AS NOT GROWN PAST THE INTERSDR SWAA2020091015112Bulkhead Web · crackedLEFT WHEEL WELL FORWARD WALL VAPOR BARRIER CRACKED. LEFT WHEEL WELL FORWARD WALL VAPOR BARRIER CRACKED. PERFORMED INTERIM REPAIR, PER EA NR 1-A57-13410R1. THIS IS A TIME LIMITED REPAIR TO REINSPECT THE EFFECTED AREA EVERY 100 CYCLES AND TO PERFORM A PERMANESDR SCNA20201007074Stiffener · corrodedCORROSION FOUND WHERE TOP EDGE OF APU AIR INLET PLENUM ATTACHES TO FWD SIDE OF BULKHEAD STA 1088, MARKED. REMOVED AND REPLACED STIFF NEW AT BS 1088 AT PPU AIR INLET PLENUM ATTACH POINT, IAW B737-800 SRM 51-40-02-0G-0 AND BOEING DRAWING 148A0924 REV B.
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