JASC 5320
Service difficulty reports · 216,159
Reports filed under 5320 · Fuselage Miscellaneous Structure, 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 = '5320' 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 = '5320' 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 DALA2024093009525Floor Support · corroded(LOG 0581025) PASSENGER COMPARTMENT FLOOR STRUCTURE, STA, 958, RBL 49, WL 208 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT DAMAGED AND REPLACED BTW STA 947.50 TO STA 967 RBL 49 WL 208 PER B737-SRM 51-40-02-0G AND DWG# 147A5650 REV-A.SDR AALA202409306133Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON FLOOR STRUCTURE ON SECTION CONNECTION LOCATED AT FR 66 AT LEVEL STR 23R IN AFT GALLEY AREA. REPLACED SECTION CONNECTION PER SRM 51-42-11-801.SDR VNAA202409270002Web · crackedTWO SMALL DENTS WITH CRACKS IN FLIGHT DECK FLOOR WEB BETWEEN CO-PILOT'S INBOARD AND OUTBOARD SEAT RAILS, COMPLIED WITH ALL THE STEPS OF REO 670-53-11-1989 REV-- DATED 2024-07-18. CUT AWAY DAMAGE SECTION OF COCKPIT FLOOR WEB, FABRICATED, LOCATED AND WET INSTASDR SWIA202411270926Floor Support · corrodedCOCKPIT FLOORBOARD SUPPORT ANGLE IS CORRODED. FWD SIDE OF FS280 BEAM (C-CHECK RO 11/26/2024) REMOVED AND REPLACED COCKPIT FLOORBOARD SUPPORT ANGLE REF CRJ 700 SRM51-42-06-001-001-A01 REV 38 DATE JUL 25/2020, DWG NO. CC670-34010 REV -K AND DWG NO. CC670-SDR SWAA2024110542674Angle · crackedCRACK ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN 2024-597135<[01] REPLACED ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0 AND DWG 146A7901 SHEET 66 REV A.;[02] REPLACED ANGLE LOCATED BS 867 BETWEENSDR VNAA20241103012Plate · corrodedCORROSION ONUPPER/LOWER FACE OF PLATES LBL 3.4 (PLATE 1) BTW FS533.00 AND FS 549.00 (PLATE 2) BTW FS 645.00 AND FS 661.00 AT FWD CARGO COMPARTMENT. PLATES LBL 3.4 (PLATE 1) BTW FS533.00 AND FS 549.00 (PLATE 2) BTW FS 645.00 AND FS 661.00 AT FWD CARGO COMPARTSDR VNAA20241103010Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RH SIDE (BELOW ADG SUPPORT DOUBLER) FS193. CRACK ON ELECTRICAL BAY FLOOR WEB RH SIDE (BELOW ADG SUPPORT DOUBLER) FS193 WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01SDR VNAA20241102006Angle · corrodedCORROSION ON MID CAP ANGLE AND LOWER ANGLE KICK PLATE ON STGR 18LH BTW FS 310.00 TO FS 349.00 AT PASSENGER DOOR FUSELAGE FRAME. MID CAP ANGLE AND LOWER ANGLE KICK PLATE ON STGR 18LH BTW FS 310.00 TO FS 349.00 AT PASSENGER DOOR FUSELAGE FRAME WERE EVALUATED SDR SWAA2024103042493Plate · corrodedCORROSION SPOTS AFT CARGO DOOR CUTOUT LOWER SILL WEB PLATE BETWEEN STA 787 & 807 MKD DOTS.<[01] THIS FAULT WILL BE ACCOMPLISHED ON TTG8Q00W3JB3;[02] VERIFIED STEP 1SDR SWAA2024102242283Angle · corrodedFWD CARGO L/H TRANSITION ANGLE CORROSION BETWEEN STA 500E AND 500D<[01] BLENDED AREAS; REMOVED .007' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] 02 - INSPECTED PER [SRM 53-00-53-1A-2-B00297 (PERMANENT (NON-DENT DAMAGE TYPES))];[03] REMOVED SDR SWAA2024102242273Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION BETWEEN STA 500I AND 500H<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE WITHIN LIMITS . TRANSITION ANGLE TO BE REPLACED. REFERENCE TTG8Q00W4L4E DUE TO THE TRANSITION ANGLE BEING PART OF TRANSITION ANGLE STA 5SDR SWAA2024102242276Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION BETWEEN STA 500G AND 500F<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE WITHIN LIMITS . TRANSITION ANGLE TO BE REPLACED. REFERENCE TTG8Q00W4L4E DUE TO THE TRANSITION ANGLE BEING PART OF TRANSITION ANGLE STA 5SDR SWAA2024102242282Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION BETWEEN STA 500E AND 500D<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE WITHIN LIMITS . TRANSITION ANGLE TO BE REPLACED. REFERENCE TTG8Q00W4L4E DUE TO THE TRANSITION ANGLE BEING PART OF TRANSITION ANGLE STA 5SDR SWAA2024102242284Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION BETWEEN STA 500D AND 500C<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE WITHIN LIMITS . TRANSITION ANGLE TO BE REPLACED. REFERENCE TTG8Q00W4L4E DUE TO THE TRANSITION ANGLE BEING PART OF TRANSITION ANGLE STA 5SDR SWAA2024102242289Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION BETWEEN STA 500C AND 500B<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE WITHIN LIMITS . TRANSITION ANGLE TO BE REPLACED. REFERENCE TTG8Q00W4L4E DUE TO THE TRANSITION ANGLE BEING PART OF TRANSITION ANGLE STA 5SDR SWAA2024102242583Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION STA 500-480<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE WITHIN LIMITS . TRANSITION ANGLE TO BE REPLACED. REFERENCE TTG8Q00W371U DUE TO THE TRANSITION ANGLE BEING PART OF TRANSITION ANGLE STA 500 THRU 500A;[SDR SWAA2024102242292Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION BETWEEN STA 500A AND 500<[01] REMOVED CORROSION DAMAGE PER SRM 53-00-53-1A-2;[02] REMOVED CORROSION DAMAGE PER SRM 53-00-53-1A-2 FOUND TO BE OUT OF LIMITS ; TRANSITION ANGLE REQUIRES REPLACMENT BETWENN STA 480 THRU 500ASDR SWAA2024102242290Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION BETWEEN STA 500B AND 500A<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2. FOUND TO BE OUT OF LIMITS TRANSITION ANGLE REQUIRES REPLACEMENT BETWEEN STA 500A THRU STA 500B;[02] CORRECT PART NUMBER FOR TRANSITION ANGLE 143A75SDR SWAA2024102242278Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION BETWEEN STA 500F AND 500E<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE OUT OF LIMITS . TRANSITION ANGLE TO BE REPLACED. REFERENCE TTG8Q00W4L4E DUE TO THE TRANSITION ANGLE BEING PART OF TRANSITION ANGLE STA 5SDR SWAA2024102242275Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION BETWEEN STA 500H AND 500G<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE OUT OF LIMITS . TRANSITION ANGLE TO BE REPLACED. REFERENCE TTG8Q00W4L4E DUE TO THE TRANSITION ANGLE BEING PART OF TRANSITION ANGLE STA 5SDR IPXA2024101716614Support Bracket · crackedAFT CARGO AT PRESSURE BULKHEAD FR 54 FOUND 6EA FLOOR SUPPORT BRAKETS CRACKED. DOT 60-006. INSTALLED 6EA BRACKET AT AFT CARGO PRESSURE BULKHEAD FR54 RIVET PN: MS20470AD5-8 BATCH: 0004235393 IAW A300 SRM 51-40-21.SDR SWIA20241017926Shear Panel · damagedELONGATED HOLE FOUND AFTER REMOVAL OF PANEL R/H END OF FR88 FOR R/H SHEAR PANEL ATTACHMENT (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED ELONGATED HOLE BY DRILLING TO SPECIFIC DIAMETER TO REMOVE DAMAGE. INSTALLED BUSHING.SEE CONTINUATION CARD FOR WORK PERFORMED.SDR FDEA202409261468Profile · crackedMAIN DECK FLOOR STRUCTURE FOUND T-PROFILE CRACK AT FR80/82,-Y1580 AREA. REMOVED CRACK T-PROFILE AND INSTALLED NEW T-PROFILE I.A.W A300-600F SRM 51-72-10-001, PAGE2 AND 51-40-21-001 PARA6 PAGE7B-23. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AT MAIN DESDR HNAA2024101000958Profile · cracked53-2168 CARGO ENTRY, FLOOR STRUCTURE PROFILE CRACKED. RAR PROFILE IAW SRM 51-40-02SDR CALA2024100302540Web · crackedLOWER FUS R/H FWD EXTERNAL POWER COMPARTMENT FUS CUTOUT LOWER EXTERIOR SMALL DOUBLER CRACKED MKD DOT 037 REF AAR N/R 9903162 ACCOMPLISHED INSTALLATION REPAIR PARTS AT LOWER FUS R/H EXTERNAL POWER COMPARTMENT IN REF B737-900ER SRM 53-10-15-2R-4 WORK ACCOMPLISHESDR CALA2024093002511Angle · damagedAFT CARGO COMPARTMENT AT STATION 727L, STRINGER 25L, BRACKET ASSY PAYLOADS CARGO LINERS BENDED REF AAR N/R 9903178 REMOVED AND REPLACED AFT CARGO SUPPORT ANGLE AT 727L STA 25L PER SRM 51-40-02-0G-0 AND DWG 146A9403 WORK ACCOMPLISHED BY V948628SDR CALA2024093002509Threshold · damagedFWD CARGO COMP DOOR THRESHOLD WEB HAS SEVERAL ELONGATED HOLES REF AAR N/R 9903363 REMOVED AND REPLACED FWD CARGO DOOR THRESHOLD WEB PER SRM 51-40-02-0G-0 REF DWG 143198120.SDR CALA2024093002508Web · corrodedSUPPORT TASK: AFT CARGO COMPARTMENT DOOR SURROUND LOWER SILL WEB IS GOUGED. REMOVED CORROSION,BEGINNING MAT''L THICKNESS .045, REMOVED 146A8123 REV -. LOCATED AND DRILLED,INSTALLED WEB IAW BAC DWG .015, REMAINING MAT''L .030, OUT OF LIMITS IAW B737-800 SRM 1SDR CALA2024093002513Web · corrodedPASSENGER CABIN FLOOR WEB HAS CORROSION F.S. 1030 LBL. 24" REF AAR N/R 9902846 REMOVED AND REPLACED WEB AT PASSENGER CABIN FLOOR F.S 1030 LBL 24" REF 51-40-02-0G-0 WORK ACCOMPLISHED BY V948050SDR CALA2024093002512Channel · disconnectedAFT CARGO COMPARTMENT FLOOR Z-CHANNEL NOT ATTACHED TO STRUCTURE AT STATION 727H DOT 243-006 REF AAR N/R 9903124 REMOVED AND REPLACED AFT CARGO COMP FLOOR R/H Z-CHANNEL FROM STA 727 TO STA 727I+5 RBL 21 PN SRM 51-40-02-0G-0, DWG 146A7500SDR AALA202409270998Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT, AFT BULKHEAD LOWER LOBE CENTER SUPPORT AT STA 500I, LBL 24. REPLACED SUPPORT PER SRM 51-40-02-0G.SDR IPXA2024092620567Web · crackedLH SIDE OF THE E&E BAY HAS A CRACKED WEB BETWEEN FR 11 - 12 DOT 07586-01. INSTALLED WEB NEW P/N: UP513100-1.IAW A300-600 SRM 51-40-21.SDR DALA2024092709481Profile · scratchedSHIP 3143 CORROSION PROFILE LOCATED BETWEEN FR65 AND STR38L TO STR38R AFT CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS PER ER/A 559065-14MA. (0577644)SDR DALA2024092709480Profile · scratchedSHIP 3143 CORROSION PROFILE LOCATED BETWEEN FR56 TO FR58 AND STR38L AFT CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS SECTION I AS PER ER/A 559065-14MA. (0577626)SDR DALA2024092709479Profile · scratchedSHIP 3143 SCRATCH PROFILE LOCATED FR24A AND +Y765 TO +Y12.92 FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS SECTION I AS PER ER/A 559065-14MA. (0577598)SDR DALA2024092709475Web · corrodedSHIP 3144 CORROSION FLOOR STRUCTURE WEB LOC Y1162.5 AND BTW FR69 TO FR70 AT AFT GALLEY ARE. CORRECTIVE ACTION: REPLACED FLOOR STRUCTURE WEB LOC Y1162.5 AND BTW FR69 TO FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11-911-001 AND A319 SRM 51-42-11-801. (0577889SDR DALA2024092709474Web · corrodedSHIP 3144 CORROSION FLOOR STRUCTURE WEB LOC -Y1162.5 AND BTW FR68 TO FR70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR STRUCTURE WEB LOC -Y1162.5 AND BTW FR68 TO FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11-911-001 AND A319 SRM 51-42-11-801. (0577SDR DALA2024092709487Profile · scratchedSHIP 3143 SCRATCH ON PROFILE LOCATED FR24A AND FROM STR35L TO STR38R FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS PER EA/A 559065-14MA. (0577604)SDR AALA202409276084Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR STRUCTURE SECTION-CONNECTING AT FR 66 AND S23L. REPLACED SECTION-CONNECTING PER SRM 51-72-11.SDR SWAA2024110541817Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS 867 AND S-26L AFT CARGO COMPARTMENT 2024-597107<[01] MEASURE OF CRACK: 1.080 INCHES TOOL USED DIGITAL CALIPER P/N:500-197-30 S/N: A21043111 DUE DATE:08-AUG-25. REPLACED ANGLE - SUPPORT LOCATED BS 867 AND S-26L AFT CARGO COMPARTSDR SWAA2024110541820Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS947.5 AND S-26L AFT CARGO COMPARTMENT 2024-597108<[01] REPLACED ANGLE SUPPORT LOCATED ON BS947.5 AND S-26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G AND DWG 149A8103 SHEET 7 REV A. SEE INDIVIDUAL SIGN OFF BELLOW.;[02] CSDR SWAA2024110142078Floor Support · crackedCRACK WEB INTERCOSTAL LOCATED BETWEEN STA277 TO STA294.5 AND BL0 FWD GALLEY AND LAV 2024-600309<[01] REPLACED WEB INTERCOSTAL LOCATED BETWEEN STA277 TO STA294.5 AND BL0 FWD GALLEY AND LAV AND FASTENERS IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141SDR SWAA2024110142080Floor Support · crackedCRACK WEB INTERCOSTAL LOCATED BETWEEN STA344 TO STA360 AND LBL11 FWD GALLEY AND LAV 2024-600315<[01] REPLACED WEB INTERCOSTAL LOCATED BTW BS344 TO BS360 LBL11 AT FWD GALLEY AREA I.A.W. B737-800 SRM 51-40-02 AND DWG 141A5400 SHEET 46 REV. A AND SHEET 16 REV. B<SDR SWAA2024103041755Web · crackedCRACK ON WEB LOCATED AT BILGE AREA BETWEEN STA 500 TO STA 500A AND LBL 21 AT FWD CARGO COMPARTMENT. 2024-588541<[01] REPLACED WEB AND FASTENERS LOCATED AT BILGE AREA BETWEEN STA 500 TO STA 500A AND LBL 21 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEMSDR SWAA2024103041757Web · crackedCRACK ON WEB LOCATED AT BILGE AREA BETWEEN STA 500B TO STA 500C AND RBL 21 AT FWD CARGO COMPARTMENT. 2024-588543<[01] REPLACED WEB AND FASTENERS LOCATED AT BILGE AREA BETWEEN STA 500B TO STA 500C AND RBL 21 AT FWD CARGO COMPARTMENT.IAW B737-700 SRM 51-40-02 SRSDR SWAA2024103042022Plate · corrodedCORROSION ON SIDEPLATE-CHANNEL LOCATED AT RBL 21 AND FROM STA 727D TO STA 767 AND WL156 BILGE AREA AFT CARGO COMPARTMENT 2024-588568 CORROSION ON SIDEPLATE SUPPORT ZEE LOCATED AT RBL 21 AND FROM STA 727D TO STA 767 AND WL156 BILGE AREA AFT CARGO COMPARTMENT<[0SDR SWAA2024103042023Web · corrodedCORROSION ON WEB LOCATED BETWEEN RBL 3.00 AND RBL 8.10 AND BETWEEN STA 767 TO STA 787 AND WL 150 BILGE AREA AT AFT CARGO COMPARTMENT 2024-588569<[01] REPLACED WEB LOCATED BETWEEN RBL 3.00 AND RBL 8.10 AND BETWEEN STA 767 TO STA 787 AND WL 150 BILGE AREA AT AFTSDR SWAA2024103042024Shear Web · corrodedCORROSION SHEAR-WEB LOCATED BETWEEN BS847 TO BS867 RBL21 AND WL165 AT AFT CARGO COMPARTMENT 2024-588570<[01] REPLACED SHEAR-WEB LOCATED BETWEEN BS847 TO BS867 RBL21 AND WL165 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 146A00SDR SWAA2024103042021Angle · crackedCRACK ANGLE LOCATED BS867 LBL11 AND WL165 AT AFT CARGO COMPARTMENT 2024-588567<[01] REPLACED ANGLE LOCATED BS867 LBL1<BR>AND WL165 AT AFT CARGO COMPARTMEN (AW B737-700 SRM 51-40-02 AND SRM<BR>51-10-02 ITEM 9. MEASURE OF CRAK IS: 0.712 IN TOOL USED CALIPER PIN:SDR IPXA2024102994141Web · corrodedSTA. 1681 LBL20 SUB.FLOOR WEB HAS CORROSION AND CRACKED ATA53. ACCOMPLISHED REPAIR PER 757-200PF SRM 53-60-51-2R-6 REPAIR 6 REV 121. REVIEW COMPLETE
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