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 SWIA20240817Pressure Blkhd · crackedAFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGER 14R, CLIP/ANGLE CRACKED. (FILED CLOSED) REMOVED AND REPLACED INTERCOSTAL ON AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF RBL 36.20 (CORRECTED LOCATIOSDR SWAA2024100127002Doubler · crackedR/H BS 663 VAPOR BARRIER DOUBLER #111A1511-28 CRACKED<[01] FABRICATED DOUBLER FROM 2024 T3 0.040 LOT 1567370-1 IAW SRM 51-30-01-0G-0 STEP 8 AND DWG 111A1152-28 REV: A<BR>DOULER GOING TO BE IN STALL ON TTG8Q00V8DXP STEP 17;[02] FABRICATED DOUBLER FROM 2024 T3 0SDR SWI202409120803Pressure Blkhd · damagedREAR PRESSURE BULKHEAD FS621.00 FWD FACE HAS SCREW DAMAGE ON DOUBLERS LOCATED AT RBL36.20, 27.50, 18.00, 9.50 AND LBL 9.50, 18.00, 27.50 AND 36.20 @ WL103.50 AS WELL AS RIVETS AT WL87.00 WITH SAME BUTTOCK LINES. (FILED OPEN) COMPLIED WITH REO 601R-53-61-SDR SWIA202408190017Pressure Blkhd · crackedAFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGER 14R, CLIP/ANGLE CRACKED. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESSSDR LR7A2024081603456Pressure Blkhd · crackedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH MLG PRESSURE SKIN TO INTERCOSTAL ATTACH ANGLE CRACKED AT FS507, RBL62, WL160. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-40-10. NR# 1001153492.SDR LR7A2024081603450Pressure Blkhd · corrodedDURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5313, FOUND LH UPPER MLG PRESSURIZED WEB CORRODED AT FS603, LBL62, WL228. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-40-09. NR# 1001138266. / PSE# 53-40-17, AD 2012-06-09SDR LR7A2024081603430Pressure Blkhd · corrodedDURING SCHEDULED C-15 CHECK UNDER JOB CARD HHC5313, FOUND LH MLG PRESSURIZED WEB CORRODED AT FS491, LBL62, WL192. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-40-09. NR# 1001133024. / PSE# 53-40-17, AD 2012-06-09SDR LR7A2024081603429Pressure Blkhd · corrodedDURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5313, FOUND LH MLG PRESSURIZED WEB CORRODED AT FS613, LBL62, WL228. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-40-09. NR# 1001133020. / PSE# 53-40-17, AD 2012-06-09SDR IXXA2024081608Bulkhead · crackedSTA 1809.5 BULKHEAD RH FWD OUTER CHORD LOWER FWD FASTENER HAS CRACK EXTENDING FROM THE 3 O'CLOCK POSITION TO THE END OF THE PART AND UNDER ADJACENT STRUCTURE.SDR SWAA2024082826413Vapor Barrier · elongatedVAPOR BARRIER WEB UNDER VERTICAL LEG OF UPPER CHORD AT LBL 20 HAS TWO ELONGATED FASTENER HOLES<[01] REPAIRED PER EA 24-157-02249;[02] 1. DAVID BASTIAN (TECHNICIAN); 21-AUG-2024 15:59 UTC<BR>REPAIRED PER EA 24-157-02249 RIISDR SWAA2024081626275Vapor Barrier · crackedDURING REINSPECT OF STA 663.75 R/H SIDE LOWER WEB (VAPOR BARRIER) APROX RBL 50; FOUND ADDITIONAL DAMAGE. FOUND CRACK @ STA 663 APPROXIMATELY RBL30.5 - RBL 42.5. REF TTG8Q00T5HM0.<[01] REPAIR ACCOMPLISHED ON TTG8Q00V9DTC.;[02] REPAIR ACCOMPLISHED ON TTG8Q00V9DTSDR SWAA2024081626271Vapor Barrier · cracked6 INCH CRACK FOUND IN LH WHEEL WELL AREA ON REAR VAPOR BARRIER. CRACK IS LOCATED BEHIND SYSTEM A HYDRAULIC PRESSURE MODULE.<[01] COMPLIED WITH EA# M-21-157-00675SDR SWAA2024100125996Vapor Barrier · crackedL/H BS 663 VAPOR BARRIER IS CRACKED AT APROX. LBL 32<[01] CRACK ON BS 663 LBL 32 L/H VAPOR BARRIER WILL BE REPAIRED ON FAULT TTG8Q00VC4WT DUE TO THE PROXIMITY OF DAMAGED AREAS;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024100126212Vapor Barrier · crackedL/H BS 663 VAPOR BARRIER IS CRACKED AT LBL 37.<[01] PERFORMED DETAIL VISUAL INSPECTION AS PER AMM 05-00-00-201-NG (TIME LIMITS/MAINTENANCE CHECKS - MAINTENANCE PRACTICES ) AN D TASK CARD COMPLETED.;[02] DISCREPANCY WILL BE CORRECTED ON TTG8Q00VC4WTSDR SWAA2024100125997Vapor Barrier · crackedR/H BS 663 VAPOR BARRIER IS CRACKED AT APROX. RBL 32<[01] RIGHT/HAND BS 663 VAPOR BARRIER; CRACK AT APPROX. RBL 32; WAS REPAIRED IAW SRM 51-70-04-2R-10.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024100126213Vapor Barrier · crackedR/H BS 663 VAPOR BARRIER CRACKED AT RBL 9.<[01] RIGHT/HAND BS 663 VAPOR BARRIER WITH CRACK AT RBL 9 WAS REPAIRED IAW SRM 51-70-04-2R-10.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024091924847Vapor Barrier · cracked(CUSTOMER REQUEST) CRACK ON RH VAPOR BARRIER LOCATED ON BS663.75 BTW RBL25 TO RBL45.64 AT MAIN LANDING GEAR COMPARTMENT 2024-512103<[01] TOOL USED CALIPER P/N 500-197-30 S/N A18229508 DUE DATE 14 JAN 25;[02] TOOL USED: HOTBONDER P/N: HCS9200B-AV S/N: 18196021 SDR SWAA2024091924848Vapor Barrier · cracked(CUSTOMER REQUEST) CRACK ON LH VAPOR BARRIER LOCATED ON BS663.75 BTW LBL24.92 TO LBL31.83 AT MAIN LANDING GEAR COMPARTMENT 2024-512104<[01] TOOL USED CALIPER P/N 500-197-30 S/N A18229508 DUE DATE 14 JAN 25;[02] TOOL USED: HOTBONDER P/N: HCS9200B-AV S/N: 181960SDR SWI2024F00899Pressure Blkhd · damagedREAR PRESSURE BULKHEAD FORWARD FACE HAS 5 DAMAGED FASTENERS, 11 GOUGES AND ONE SCRATCH ABOUT 4 INCHES LONG (FILED CLOSED) COMPLIED WITH REO 601R-53-61-8215 DATED: 2024-08-22 REV €“ FOR THE BLENDED GOUGES ON FS 621.00 BULKHEAD AND FASTENER REPLACEMENT TO SDR SWAA2024091924030Bulkhead Web · crackedCRACK INTERNAL AREA RT SIDE BODY STATION 663.75 RBL 15; VAPOR WEB (BARRIER) AT MAIN WHEEL WELL COMPARTME 2024-489185<[01] TOOL USED: CALIPER P/N: 500-196-30; S/N: A23048326; DUE DATE: 05 JUN 25.;[02] TOOL USED= HOT BONDER P/N:HCS9200B AV; S/N: 18185781; DUE DASDR SWAA2024091224025Vapor Barrier · crackedTHE BS 663 VAPOR BARRIER IS CRACKED AT MID SPAN<[01] THE BS 663 VAPOR BARRIER DAMAGED MID SPAN LOCATION HAS BEEN REPAIRED IAW SRM 51-70-04-2R-10.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024091923513Vapor Barrier · crackedCRACK BODY STATION 663.75 VAPOR BARRIER LBL 38 AT MAIN WHEEL WELL COMPARTME 2024-503825<[01] TOOL USED CALIPER P/N 500-197-30 S/N A18229508 DUE DATE 14 JAN 25;[02] TOOL USED: HOTBONDER P/N: HCS9200B-AV S/N: 18196021 DUE DATE: 15-FEB-25.;[03] TOOL USED SCALE P/SDR SWAA2024091923514Vapor Barrier · crackedCRACK BODY STATION 663.75 VAPOR BARRIER RBL 38 AT MAIN WHEEL WELL COMPARTME 2024-503828<[01] TOOL USED CALIPER P/N 500-197-30 S/N A18229508 DUE DATE 14 JAN 25;[02] TOOL USED: HOTBONDER P/N: HCS9200B-AV S/N: 18196021 DUE DATE: 15-FEB-25.;[03] TOOL USED SCALE P/SDR SWAA2024091923365Vapor Barrier · crackedR/H BS 663 VAPOR BARRIER IS CRACKED AT MID SPAN<[01] 04 - REPAIRED PER [SRM 51-70-04-2R-10-A00755 (REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES - AIRFRAME - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024091923366Vapor Barrier · crackedL/H BS 663 VAPOR BARRIER IS CRACKED AT MID SPAN<[01] 04 - REPAIRED PER [SRM 51-70-04-2R-10-A00755 (REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES - AIRFRAME - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024082823151Vapor Barrier · crackedR/H AC BAY STA 663 VAPOR BARRIER UPPER CHORD CRACKED AT RBL 37<[01] PARTS DATA UPDATE ONLY;[02] MATCH DRILLED AND DEBURRED NEW CHORD PER SRM 51-40-02/SRM51-10-02.;[03] OK TO INSTALL NEW CHORD (RII);[04] INSTALLED AND DOMED SEALED FASTENERS COMMON TO FUEL TANK SDR SWAA2024082823150Vapor Barrier · crackedL/H AC BAY STA 663 VAPOR BARRIER UPPER CHORD CRACKED AT LBL 37<[01] MATCH DRILLED AND DEBURRED NEW UPPER CHORD PER SRM 51-40-02/SRM51-10-02.;[02] OK TO INSTALL L/H AC BAY STA 663 VAPOR BARRIER UPPER CHORD.;[03] INSPECTION VERIFIED 'OK TO INSTALL L/H AC BAY STASDR AALA202408055432Bulkhead · out of adjustAIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR DIFFICULT TO OPEN IN FLIGHT. ADJUSTED UPPER COCKPIT WALL BETWEEN GALLEY AND FORWARD LAVATORY.SDR SWAA2024091922059Vapor Barrier · crackedCRACK BODY STATION 663.75 VAPOR BARRIER LBL 15 AT MAIN WHEEL WELL COMPARTME 2024-488949<[01] TOOL USED: CALIPER P/N: 500-196-30; S/N: A23048326; DUE DATE: 05 JUN 25.;[02] TOOL USED= HOT BONDER P/N:HCS9200B AV; S/N: 18185781; DUE DATE: 15-FEB-25.;[03] TOOL USEDSDR SWAA2024082722048Vapor Barrier · crackedCRACK FOUND AT FASTENER HOLE LBL 9 EXTERNAL VAPOR BARRIER UPPER ATTACHMENT ANGLE ADJACENT TO CENTER BOX REAR SPAR STA 663<[01] REMOVED; REPAIRED AND RE-INSTALLED LH VAPOR BARRIER UPPER ATTACHMENT ANGLE STA 663 PER SRM 51-40-02-0G-0 AND SRM 57-10-10-2R-5.;[02] SDR DALA2024080707868Pressure Blkhd · damaged(LOG 0480708) DURING INSPECTIONS, OIL CAN WAS FOUND ON THE STA 1016 PRESSURE BULKHEAD WEB, BETWEEN S-3L AND S-5L. DAMAGE WAS REMOVED AND REPAIRED PER 737-800 SRM 53-80-08-2R-8 - REPAIR 8 AND ERA 619759-14AD.SDR SWAA2024090521588Vapor Barrier · crackedTWO PREVIOUS REPAIRS ON RH 663 VAPOR BARRIER ARE CRACKED PREVIOUS REPAIRS ARE LOCATED AT RBL 40 AND RBL 51<[01] REMOVED TWO CRACKED PREVIOUS REPAIRS ON RH 663 VAPOR BARRIER AND ACCOMPLISHED PERMANENT REPAIR IAW SRM 51-70-04-2R-10.;[02] VERIFIED CORRECTIVE ACTISDR SWAA2024090521589Vapor Barrier · crackedPREVIOUS REPAIR ON LH 663 VAPOR BARRIER IS CRACKED PREVIOUS REPAIR IS LOCATED AT LBL 36<[01] CRACKED PREVIOUS REPAIR ON LH 663 VAPOR BARRIER WAS REPAIRED IAW SRM 51-70-04-2R-10.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.SDR U2RA2024081500023Pressure Deck · crackedDURING C CHECK IN GMF, FOUND CRACK ON SKIN AT LH WLG W/W CANTED PRESSURE DECK STA 1241LBL 11.33 CATEGORY B REPAIR WAS ACCOMPLISED IN ACCORDANCE WITH BOEING MESSAGE BOE MUA-MUA 24-0122SDR SWAA2024082721048Vapor Barrier · crackedACCOMPLISH REPAIR OF L/H VAPOR BARRIER AS REQUIRED<[01] LATE ENTRY ; WORK ACCOMPLISHED ON 08-04-24; APPLIED REPAIR AT L/H VAPOR BARRIER STA 663 ON FWD AND AFT SIDE AS PER B737 SRM 51-70 -04-2R-10 PARAG 4F AND 737 SRM57-10-10-2R-2 AND SRM 51-70-04-2R-0 PARAG4-NSDR SWAA2024082721049Vapor Barrier · crackedACCOMPLISH REPAIR OF R/H VAPOR BARRIER AS REQUIRED<[01] LATE ENTRY ;WORK ACCOMPLISHED ON 08-04-2024; APPLIED REPAIR AT R/H VAPOR BARRIER STA 663 ON FWD AND AFT SIDE AS PER B737 SRM 51-70-04-2R-10 PARG 4F AND B737 SRM 57-10-10-2R-2 AND SRM 51-70-04-2R-0 PARAG 4SDR SWAA2024082721045Bulkhead Web · crackedCENTER WING REAR VAPOR WEB STA 663.75;LBL 10 HAS CRACK EVIDENCE NOTED(LOWER # 1 ELECTRIC HYDRAULIC PUMP).<[01] REPAIR OF L/H VAPOR BARRIER WAS ACCOMPLISHED ON BARCODE TTG8Q00UXQ95;[02] FINAL INSPECTION; VERIFIED STEP #1.SDR AALA202408022415Vapor Barrier · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND VAPOR BARRIER IS CRACKED AT BS 663 OUTBAORD OF PACK EXHAUST DUCT, CRACK IS 9 INCHES IN LENGTH. INSTALLED FABRIC PATCH REPAIR AND BOTTOM END IS STOP-DRILLED. PER AARD 57-10-10-9 AND SRM 57-10-10-2R-2.SDR IPXA2024091273020Intercostal · bentFAULT: STR-Z30 THS BAY AFT PRESSURE BULKHEAD BETWEEN FR86 AND FR87 R/H SIDE, INTERCOSTAL IS BENT. MB-60-029. INSTALLED INTERCOSTAL RH BETWEEN FR86 AND FR87 IAW A300-600 SRM 51-40-21 RIVETS PN: MS20470AD5-5, BATCH: 0004301662 AND PN: MS20470AD4-6 BATCH: 0004304SDR EE4Y2024072820517Bulkhead · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 533152-01-7-001, FR 35 BULHEAD FWD FACE LOWER CHORD BETWEEN STGR 38 LH/43 RH WITH (2EA) SPOT CORROSION WAS FOUND.DUE THE DAMAGE IS BEYOND SRM LIMITS TO REPAIR AIRBUS WAS CONTACTED ASKING FOR REPAIR INSTRUCTIONS. AIRBSDR N6WA2024072908Stiffener · crackedCRACKED ANGLE STIFFNER ON LH LOWER BULKHEAD WEB AT FS280.00. REPLACED ANGLE STIFFNER ON LH LOWER BULKHEAD AT FS280.00 BL26 IAW CRJ 550 SRM 51-42-06.SDR N6WA2024072906Bulkhead Web · corrodedLOWER RH WEB AT FS280.0- HAS CORROSION. REPLACED LOWER RH WEB AT FS280.00 IAW CRJ 700 SRM 51-42-06.SDR N6WA2024072905Bulkhead Web · corrodedLOWER LH WEB AT FS280 HAS CORROSION. REPLACED LOWER WEB AT FS280.00 IAW CRJ SRM 51-42-06.SDR N6WA2024072802Angle · crackedCRACKED ANGLE ON LH LOWER BULKHEAD WEB AT FS280.00 BL26.00. REPLACED ANGLE ON LH LOWER BULKHEAD FS280.00 BL26 IAW CRJ 550 SRM 51-42-06.SDR AALA202407251579Rail · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT AFT BULKHEAD LOWER LOBE RAIL ASSEMBLY AT STA 500I, FROM S25L TO S25R. REPLACED RAIL ASSEMBLY PER SRM 51-40-02-0G.SDR SWI202408260778Pressure Blkhd · crackedAFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGER 14L, CLIP/ANGLE CRACKED. (FILED - CLOSED)REMOVED AND REPLACED CLIP/ANGLE ON AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGESDR SWI202408260777Pressure Blkhd · crackedAFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 14R, CLIP/ANGLE CRACKED. (FILED - CLOSED)REMOVED AND REPLACED CLIP/ANGLE ON AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGESDR SWIA2024082600722Pressure Blkhd · gougedREAR PRESSURE BULKHEAD (FS621.00) FWD FACE HAS RIVET HEAD DAMAGE AND GOUGES ON DOUBLERS, LOCATED APPROX. LBL 18.00, 27.50, RBL 36.20, 27.50, 18.00 @ WL 87.50 AND WL 94.50. (FILED - CLOSED)UPON FURTHER INSPECTION FOUND 6 GOUGES LOCATED FS 621 BULKHEAD TOP DOUBLSDR DALA2024072907564Pressure Blkhd · corroded(LOG 0465469) CORROSION ON STA 1016 PRRESSURE BULKHEAD INTERCOSTAL LBL 9-17 WL 210. REMOVED, FABRICATED AND REPLACED PRESSURE BULKHEAD INTERCOSTAL ON STA. 1016 LBL 9-17 WL 210 I.A.W. B737 SRM 51-40-02-0G AND DWG 65-54862 REV. H. AND DWG. 148A0922.SDR VNAA202508200022Bulkhead Web · corrodedAFTER REMOVAL OF CAP ANGLE, CORROSION ON WEB OF BULKHEAD FS 280.00 LH SIDE . EVALUATED, DUE TO EXCESSIVE CORROSION ON WEB OF BULKHEAD FS 280.00 LH SIDE, IT IS OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND REPAIRED PER CRJ-900 SRM 53-11-10-201-004-A01.
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