JASC 5312
Service difficulty reports · 20,044
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 SWAA2023041814199Bulkhead · delaminatedPREVIOUS REPAIR STARTS TO DELAM AT LOWER L/H COMPOSITE BULKHEAD AT BS663 LBL33 WL161.<[01] IDENTIFIED IAW SRM 57-10-10-0I-2 FIGURE 2 TABLE 2 ITEM 4 <BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PAR.4 D(5)<BR><BR>DAMAGE TO BE REPAIRED IAWSDR SWAA2023041213891Stringer · crackedFOUND CRACK ABOVE FED BS 312 WL 285 BETWEEN STRINGERS 5-6<[01] REPAIR TO BE COMPLETED ON CARD # M-22-153-01244 (2371);[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLESDR SWAA2023040509784Tie Clip · crackedCRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2023-142627<[01] REPLACED TIE CLIP LOC. ON BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET 18 AND REV -.<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02SDR QXEA2023030100031None · noneFR 90 CROSSBEAM AT INTERSECTION OF RH LONGITUDINAL BEAM HAS CORROSION. REMOVED AND REPLACED FR 90 CROSSBEAM AT INTERSECTION OF RH LONGITUDINAL BEAM REF SRM 51-40-08.SDR QXEA2023030100030None · noneRH UPPER SHEET JUST FORWARD OF FR 86 HAS CORROSION. REMOVED AND REPLACE RH UPPER SHEET JUST FORWARD OF FR 86 PER SRM 51-40-08, RESTORED SURFACE PROTECTION PER SRM 51-23-06.SDR DALA2023022401397Angle · corroded(LOG 2640806) DURING INSPECTION FOUND CORROSION ON BULKHEAD SUPPORT ANGLE STA. 947 RBL 17 LOWER SIDE WL.150. REMOVED AND REPLACED BULKHEAD SUPPORT ANGLE STA 947, RBL 17, WL 150 IAW B737 SRM 51-40-02, B737 SRM 51-40-05 AND BOEING DWG # 149A8118.SDR Q5QA20230222003Doubler · crackedDURING AN INSPECTION OF THE TAIL SECTION OF N36TA, THE AFT-MOST FUSELAGE BULKHEAD ASSEMBLY, FS 272.0, WAS NOTED CRACKED AT THE LEFT LOWER AND RIGHT LOWER RADII ONLY ON THE DOUBLER P/N 002-440024-11 (SEE ATTACHED PHOTO).SDR LR7A2023020803269Bulkhead Web · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND RH AFT UPPER BULKHEAD WEB CRACKED AT FS968, RBL 61, WL270. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-50-06. NR# 1000896572. / PSE# 53-50-09, AD 2012-06-09SDR LR7A2023020803268Fitting · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND RH SIDE BULKHEAD FITTING CRACKED AT FS921, RBL62, WL260. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000896191. / PSE# 53-50-07, AD 2012-06-09SDR LR7A2023020803267Web · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND BULKHEAD ASSEMBLY WEB CRACKED AT FS924, RBL61-68, WL270. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000896190. / PSE# 53-50-07, AD 2012-06-09SDR Q5QA20230215001Bulkhead · crackedDURING AN INSPECTION OF THE TAIL SECTION OF N2143J, THE AFT-MOST FUSELAGE BULKHEAD ASSEMBLY, FS 272.0, WAS NOTED CRACKED AT THE LEFT LOWER AND RIGHT LOWER RADII.SDR DALA2023021301104None · noneSHIP 1201 TASK-HFEC SURFACE INSPECTION FOUND 01 EA CRACK APPROX 0.60 INCH IN LENGTH AT THE 5TH FASTENER HOLE ON RH BS1809.5 FORWARD OUTER CHORD INBOARD FLANGE BELOW THE EDGE OF SPLICE FITTING, ACCOMPLISH SECTION 08(RH). CORRECTIVE ACTION: DAMAGE AREA REPAIRED SDR QXEA2023020700016Not Reported · not reportedFWD SVC DOOR GIRT BAR FITTING SPRING BROKEN. REMOVED AND REPLACED FWD SVC DOOR AFT GIRT BAR FITTING SPRING REF AMM 53-10-25.SDR DALA2023020600884Support Fitting · corroded(LOG 2609787) DURING INSPECTION FOUND CORROSION ON AFT BULKHEAD FLOOR SUPPORT STA 500L BTW STR 26RH TO 26LH AT FWD CARGO COMPARTMENT. BULKHEAD FLOOR SUPPORT STA 500L BTW STR 26RH TO 26LH AT FWD CARGO COMPARTMENT (C1) WAS REPLACED PER B737-900ER SRM 51-40-02-0GSDR UIEA2023012400074Frame · crackedFUS - LH STA 1000 BULKHEAD CHORD BETWEEN S-38 AND S-39 FOUND 1EA CRACKED.(<P>FUS - STA 1000 BULKHEAD CHORD BETWEEN STR 38L AND STR 39L CRACK AREA MODIFICATED IAW EO 4453A506 PART 3.</P>)SDR DALA2023013000758Pressure Panel · crackedSHIP 3209 SEVERAL HOLES WERE FOUND CRACKED ON PRESSURE PANEL AT FR36. CORRECTIVE ACTION: COMPLIED WITH ERA 563935-32. (2603943)SDR CALA2023013000242Angle · crackedLOWER FUS.CENTER WING BOX AFT BULBKHEAD VAPOR BARRIER UPPER CHORD ATTACHED ANGLE CRACKED R/H A/C BAY STA 663.75 APPROX RBL7 (REF AAR NR 9667466) ACCOMPLISHED REPAIR 5 AT LOWER FUSELAGE CENTER WING BOX VAPOR BARRIER FWD ANGLE STA663 RBL7. ACCOMPLISHED BY V91319SDR DALA2023012500626Pressure Panel · corrodedCORROSION WAS FOUND AT CEILING MLG WHEELWELL R/H, STA 1100, RBL 41 TO RBL 50. CORROSION ON RH MLG WHEEL WELL PRESSURE DECK WEB, LOWER SURFACE ON STA 1094 TO 1113 AND RBL 45.7 TO RBL 70.5 WAS ATTENDED PER ER/A 605362-14 REV. ORIGINAL SECTION I: PERMANENT REPASDR AALA202301252612Bulkhead Web · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT WHEEL WHEEL FORWARD BULKHEAD 1ST BAY OUTBOARD OF KEEL BEAM CRACKED LOCATED AT STA 663.75 AND RIGHT BUTT LINE 32.53. PERFORMED BONDED REPAIR PER AARD.SDR SWAA2023013091939Support Angle · corrodedCORROSION VAPOR VARRIER AIR CONDITIONING PACK EXHAUST LOWER SUPPORT ANGLE BTW LBL 15 TO LBL 25 AT MAIN WHEEL WELL COMPARTME 2022-691952<[01] TOOLS USED: POWER PACK P/N: FMK0003223; S/N: PE0412/63335; DUE DATE: 26-JAN-23; MULTIMETER P/N: FLUKE 87-5; S/N: 179300SDR SWAA2023012491838Vapor Barrier · crackedLEFT HAND 663 VAPOR BARRIER WEB UPPER EDGE REQUIRES REPAIR AT LBL 44<[01] EVALUATED 6' CRACK IN L/H 663 VAPOR BARRIER AT LBL 44. AND FOUND TO BE REPAIRABLE. IAW B737-700 SRM 57-10-10-2R-2 PAR 1& NOTE. CLEAN AND PREP. IAW B737-700 SRM 51-70-04-2R-10 PAR 4 A-C. SDR UIEA2023011930039Seal · leakingSECTION48, PRESSURE DOME, CONTROL CABLES E1B AND E1A, AIR PRESSURE SEALS WITH EVIDENCE OF AIR LEAK(<P><SPAN DIR="LTR" ROLE="PRESENTATION">SECTION48, PRESSURE DOME, CO-</SPAN><SPAN DIR="LTR" ROLE="PRESENTATION">NTROL CABLES E1B AND E1A, AIR PRESSURE </SPAN><SPASDR SWAA2023012491837Web · cracked1 EA CRACK FOUND IN 663 WEB AT (WL 167) BS 663 LBL 44'<[01] EVALUATED 6' CRACK IN L/H 663 VAPOR BARRIER AT LBL 44. AND FOUND TO BE REPAIRABLE. IAW B737-700 SRM 57-10-10-2R-2 PAR 1& NOTE. CLEAN AND PREP. IAW B737-700 SRM 51-70-04-2R-10 PAR 4 A-C. VERIFIED MATERSDR SWAA2023011791750Vapor Barrier · crackedREAR RT WING SPAR VAPOR BARRIER CRACK CENTER WING REAR SPAR VAPOR BARRIER CRACK RBL 27- RBL 34 (11IN. LONG)<[01] C/W;[02] REPAIRED CRACK (8IN) FROM RBL 34 TO RBL 40 PER SRM 51-70-04 REPAIR 10. CONTINUE TO CARRY REMAINDER OF CRACK (11IN) (RBL 27 TO RBL 33) ON TSDR SWAA2023012490995Attach Angle · cracked2 EA CRACKS FOUND ON UPPER ATTACH ANGLE (WL167) STA 663 AT LBL 8 & LBL 40<[01] VERIFIED ITEM 6 OF STEP 3 AND ITEM 4 OF STEP 4;[02] VERIFIED ITEM 5 OF STEP 4;[03] VERIFIED ITEM 2 OF STEP 7 (FASTENER INSTALL COMMON TO FUEL TANK);[04] VERIFIED ITEM 1 OF STEP 8;[0SDR SWAA2023012691177Bulkhead Web · crackedCENTER WING REAR SPAR VAPOR WEB LEFT SIDE LWR AREA CRACKED<[01] MEASUREMENTS;[02] PERFORMED VISUAL INSPECTION ON L/H VAPOR BARRIER AND FOUND CRACK OF 11' PER B737 NDTM 51-05-01.;[03] PERFORMED STOP DRILL SIZE 0.25 DIAMETER AT THE END OF THE CRACK PER B737 SRM SDR A6WA202301608430Stiffener · missingAFT PRESSURE BULKHEAD FS621 IS MISSING ALL REINFORCEMENT ANGLES, AIRCRAFT REMOVED FROM SERVICE. INSTALLED REINFORCEMENT ANGLES TO AFT PRESSURE BULKHEAD FS621. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMSDR SWIA20230100005None · damagedREAR PRESSURE BULKHEAD FORWARD FACE - SIX OF THE PICKET FENCE REPAIR PLATES HAVE DAMAGE FROM LINER SCREWS WL103.00. (MARKED) (C-CHECK RO 2/26/2023) COMPLIED WITH REO 601R-53-61-7951 REV-- DATED 2023-01-22 FOR REAR PRESSURE BULKHEAD FORWARD FACE REPAIR MSDR LR7A2023010403238Bulkhead Web · puncturedDURING SCHEDULED B-3 CHECK UNDER JOB CARD HB5302, FOUND RH WHEEL WELL FS617 SIDE BULKHEAD WEB WITH A PUNCTURE AT RBL65, WL190. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-40-09. NR# 1000771888.SDR AALA202301251539Flange · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER FLANGE AT BULKHEAD OF FORWARD CARGO. LOCATED AT STA 500I, AND RIGHT BUTT LINE 24 TO LEFT BUTT LINE 24. REMOVED AND BLENDED CORROSION PER SRM.SDR SWAA2023011087188Vapor Barrier · crackedUPPER VAPOR BARRIER ANGLE IN ECS BAY IS CRACKED AT STA 663; WL 167; LBL 41.<[01] REMOVED VERTICAL STIFFENER AT LBL 39 AND HORIZONTAL U-CHANNEL IAW SRM 51-40-02-0G-0.;[02] VERIFIED ITEM 1 OF STEPS 3; 4; 6 AND 7;[03] VERIFIED ITEM 5 OF STEP 7 AND ITEM 1 OF STEP SDR SWAA2023011087182Vapor Barrier · crackedUPPER VAPOR BARRIER ANGLE IN ECS BAY IS CRACKED AT STA 663; WL 167; RBL 41.<[01] VERIFIED ACTION STEP 1 OF STEPS 1; 2 AND 3;[02] VERIFIED ITEM 1 OF STEPS 4; 6; AND 7;[03] VERIFIED ITEM 5 OF STEP 7 AND ITEM 1 OF STEP 8;[04] VERIFIED ITEM 3 OF STEP 8;[05] VERIFISDR 2023F00012Bulkhead · crackedAPPROX 2" CRACK ON INBD FLANGE OF VERTICAL CHORD RADIUS, LBL 5.7 WL 184 ON STA 178 BULKHEAD.SDR SWAA2023012786577Pressure Blkhd · corrodedCORROSION ON PASSENGER CABIN PRESSURE WEB AT LBL 35 BS 693.<[01] REMOVED CORROSION ON PASSENGER CABIN PRESSURE WEB AT LBL 35 BS 693 IN AN AREA OF 0.8X0.85 IAW SRM 51-10-02-0G-0;[02] REMOVED 1EA FASTENER AT B.S 693 LBL 35 IAW SRM 51-40-02-0G-0;[03] VERIFIED CORSDR SWAA2023011786323Bulkhead Web · crackedTWO CRACKS AT BS 663, WL 164, LBL 17, AND 18. FOUND WITH NDT INSPECTION PT6 51-00-00 PROCEDURE 16. CONFORMED SPLICE ANGLE IAW SRM 57-10-10-2R-5, SPLICE ANGLE, FABRICATED IAW SRM 57-10-10-2R-5. REMOVED DAMAGE FROM BS663 LBL 6-32 WL 164 AND PERFORMED DVI ONSDR IPXA2023011189786Structure · crackedINSPECTION TYPE: C13, MAJOR REPAIR. CRACK ON BS 1809.5 BULKHEAD HORIZONTAL INNER CHORD AT APPROXIMATELY WL 257, RBL 28. SRM 53-80-08 REPAIR 10 REV.85.01 AND EO B767-5310-85604-ASDR DALA2022123008497Support Fitting · corroded(LOG 2559259) DURING INSPECTION FOUND CORROSION ON AFT BULKHEAD SUPPORT BTW LH/RH STGR 25 FROM STA 500L AT FWD ARGO COMPARTMENT. AFT BULKHEAD SUPPORT BTW LH/RH STGR 25 FROM STA 500L WAS REPLACED IAW SRM 51-40-02-0G.SDR AALA202212292647Intercostal · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT PRESSURE BULKHEAD HAS AREA OF LIGHT CORROSION LOCATED AT STA 1016 AND RIGHT BUTT LINE 35. REMOVED CORROSION BY MECHANICAL MEANS AND OUT OF SRM LIMITS. REMOVED AND REPLACED INTERCOSTALSDR AALA202212291749Intercostal · corrodedAIRCRAFT IN BASE MAINTENANCE: UPON REMOVAL OF AFT BULKHEAD LOWER SEAL AT AFT PRESSURE BULKHEAD LOWER INTERCOSTAL ATTACHMENT FOUND TO BE CORRODED. REMOVED CORROSION BY MECHANICAL MEANS AND OUT OF SRM LIMITS. FABRICATED NEW INTERCOSTAL AND REPLACED.SDR SWAA2023011185421Doubler · crackedDOUBLER COMMON TO THE FWD SIDE OF THE VAPOR BARRIER IS CRACKED AT BS 663, LBL 25, WL 177. FOUND TO BE OUT OF LIMITS. FABRICATED AND APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON A NEW DOUBLER IAW DWG 111A1000, DWG 111A1511, SRM 51-40-05-0G-0, SRM 51-30-SDR DALA2022122908492Structure · crackedSHIP 182 DURING PERFORM W/C 5310-01376-0703 STEP 3 , HFEC INSPECTION FOUND 01 CRACK IN REMOVED CHORD AND THE CRACK IS FROM THE SEVENTH FASTENER COUNT FROM TOP. CORRECTIVE ACTION: ACCOMPLISHED REPAIRED THE DAMAGED AREA AS PER AMDS W/C 5310-01376-0705. (2554266)SDR DALA2022122908491Fastener · crackedSHIP 182 EO TASK - BY STEP 3 LFEC INSPECTION FOUND 02EA FASTENERS CRACKED ON THE LOWERMOST ROW OF INSPECTION AREA 2,ACCOMPLISH SECTION 07(LH) PRIOR TO FURHER FLIGHT. CORRECTIVE ACTION: ACCOMPLISHED REPAIRED THE DAMAGED AREA AS PER AMDS W/C: 5310-01376-0705 (25SDR SWAA2023020785201Angle · crackedCRACK ANGLE LOCATED BS867; LBL10 AT LEVEL FLOOR STRUCTURE AFT CARGO COMPARTMENT 2022-707319<[01] REPLACED ANGLE LOC. BS867; LBL10 AT LEVEL FLOOR STRUCTURE AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 149A8102 REV: ?.<BR>SEESDR REXA2022123002729Bulkhead Web · corrodedLEFT AFT LOWER BS 280 WEB WAS CORRODED. COMPLIED WITH STEPS B, 1-3 AND FABRICATED NEW LOWER WEB AND BUTTSTRAP IAW SRM 53-11-10-201-004-A01.SDR AALA202212239370Intercostal · crackedAIRCRAFT IN BASE MAINTENANCE: UPON REMOVAL OF AFT BULKHEAD LOWER SEAL FOUND CRACK AT AFT PRESSURE BULKHEAD LOWER INTERCOSTAL ATTACHMENT AT APPROXIMATELY STA 1047 AND LEFT BUTT LINE 29 TO LEFT BUTT LINE 20. REMOVED AND REPLACED INTERCOSTAL PER SRM 10-40-02-0G.SDR 2022FA0000772Bulkhead · crackedCRACKS IN THE BULKHEAD ASSY - TAILCONE STA 325.5.SDR CALA2022122103453Attach Angle · crackedLOWER FUS BS 663.75 BULKHEAD RT VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT FASTENER HEAD, RBL 6. CUT OUT DAMAGE AREA, FABRICATED AND INSTALLED REPAIR IAW SRM 57-10-10-2R-5 FIG 202.SDR SWAA2023020783292Tie Clip · crackedCRACK TIE CLIP LOCATED BS277 AT LEVEL STR10R AT PASSENGER CABIN 2022-697148<[01] REPLACED TIE CLIP AND FASTENERS LOCATED BS277 AT LEVEL STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 DWG: 141A1110; SHEET: 18 REV: -. SEE INDIVIDUAL SIGNSDR SWAA2023011883353Bulkhead · crackedCRACK BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT. FABRICATED NEW BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW AMM 25-52-01-201-801, AND DRAWING 453A2510 SHEET 4.SDR SWAA2023011183521Bulkhead · crackedCRACKED LOWER LT COMPOSITE BULKHEAD AT BS 663, LBL 49, WL 154. EXCEED ALLOWABLE LIMITS IAW SRM 57-10-10-1A-2 PARA 4. D. REPAIRED IAW SRM 51-70-04-2R-10, SRM 57-10-10-2R-2 PARA 1. B.
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