JASC 5320
Service difficulty reports · 216,095
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 AALA202504074441Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT STA 500G, S26L. REPLACED BAFFLE CLIP PER AARD 51-00-05-1.SDR IXXA20250404003Stiffener · corrodedRH WHEEL WELL STA1095 OUTER FRAE OF WHEEL WELL CORRODEDSDR SWI2025F01173Bracket · bentFORWARD BAGGAGE BRACKET, IS BENT ON FRAMES , BS 565.00 AT STGR27. REMOVED 1 EACH DAMAGE BRACKETS AT BS 565, S27 IAW SRM 51-42-06-001-001-A01. INSTALLED NEW BRACKET P/N SH670-34082-3 AT FS565.00 STGR27 IAW SRM 51-42-06-001-001-A01 AND DWG SH670-33600 REV-AD.SDR SWIA2025090200017Bracket · bentFORWARD BAGGAGE BRACKET, IS BENT ON FRAMES , FS 581.00 AT STGR27. REMOVED 1 EACH DAMAGE BRACKETS AT 581.00 AT STGR27 IAW SRM 51-42-06-001-001-A01. INSTALLED NEW BRACKET AT FS581.00 STGR27 IAW SRM 51-42-06-001-001-A01 AND DWG SH670-33600 REV- AD. COMPLIEDSDR VNAA20250525025Cap · corrodedAFTER REMOVAL MID CAP IN REFERENCE TO NRC 00214, CORROSION ON MID CAP AND FWD CAPANGLE WAS FOUND. CORROSION ON MID CAP AND FWD CAPANGLE WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-23-101-001-A01 WERE REPLACED AND MUST BE INSTALLED UNDER NRC0214.SDR VNAA20250525021Intercostal · corrodedCORROSION ON INTERCOSTALS (1 EAS) STGR 21LH BTW FS310 TO FS333 AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL AT STGR 21LH BTW FS310 TO FS333 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ 70SDR VNAA20250525019Diaphragm · wornCRACK ON DIAPHRAGM LBL17.63 BTW FS 939.00 TO FS 909.00 AT AFT FUSELAGE. DIAPHRAGM LBL17.63 BTW FS 939.00 TO FS 909.00 AT AFT FUSELAGE WAS REPAIRED PER REO 670-53-82-478 REV. -A.SDR VNAA20250525008Fitting · corrodedCORROSION ON 8 EA. FITTINGS BTW FS280 TO FS 310 FROM LBL38 TO RBL38. EXCESSIVE DAMAGE FOUND OUT OF LIMITS 8EA. BTW FS280 TO FS310 FROM LBL38 TO RBL38 REPLACED PER CRJ 700 SRM 51-42-21-001-AO1SDR VNAA20250525007Diaphragm · corrodedCRACK ON DIAPHRAGM RBL17.63 BTW FS 939.00 TO FS 909.00 AT AFT FUSELAGE. DIAPHRAGM RBL17.63 BTW FS 939.00 TO FS 909.00 AT AFT FUSELAGE WAS REPAIRED PER REO 670-53-82-478 REV. -A.SDR VNAA202504018Angle · corrodedCORROSION ON ANGLE KICKPLATE OF PASSENGER DOOR SURROUND STRUCTURE FROM FS 310 TO FS EN 349 AT PAX CABIN. ANGLE KICKPLATE OF PASSENGER DOOR SURROUND STRUCTURE AT PAX CABIN WAS EVALUATED OUT OF LIMITS PER CRJ700 53-21-23-101-001-A01 AND WAS REPLACED PER CRJ70SDR VNAA202504016Intercostal · corrodedCORROSION ON INTERCOSTAL AND CLEATS (3 EAS) AT STGR 20R BTW FS319.70 TO FS 349.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERCOSTAL WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-23-101-002-A02 AND CORROSION ON CLEATS (3 EAS) AT STGR 20R BTW FS319.70 SDR IPXA2025040322399Transition Panel · corrodedAFT CARGO TRANSITION PANEL R/H SIDE BETWEEN STA 1440-1460 HAS CORROSION UNDER NUTPLATE DOT#21-5. INSTALLED FLOOR PANEL SUPPORT IAW B757 SRM 51-40-02.SDR SWAA2025042921482Web · corrodedCORROSION ON LOWER SILL WEB UPPER SURFACE FROM BS 624 TO BS 632; RBL68; WL208<[01] 'THE DAMAGE WAS REWORKED PER 737-700 SRM 53-40-15-1A-1 (ALLOWABLE DAMAGE 1) AND EA 25-153-00920';[02] CARD COMPLETESDR SWAA2025041421088Strip · corroded4 EA. AFT CARGO L/H CAP STRIPS HAVE MULTIPLE AREAS OF CORROSION<[01] PROCURED SERVICEABLE REPLACEMENT CAP STRIPS FROM STOCK. CAP STRIPS TO BE INSTALLED ON TASK# 2552-E-17151-MAX (REPL - CARGO COMPARTMENT SIDEWALL STANDARDIZATION) TTG8Q00SYSZJ;[02] CHAD DUNN (TSDR SWAA2025041421089Strip · corroded3 EA. (#1;2;3) AFT CARGO R/H CAP STRIPS HAVE MULTIPLE AREAS OF CORROSION<[01] PROCURED SERVICEABLE REPLACEMENT CAP STRIPS FROM STOCK. CAP STRIPS TO BE INSTALLED ON TASK# 2552-E-17151-MAX (REPL - CARGO COMPARTMENT SIDEWALL STANDARDIZATION) TTG8Q00SYSZJ;[02] CHASDR CALA2025040703594Plug · corroded(B737-53-3-0740) AFT PASSENGER COMPARTMENT WET AREA AT STA951 DR AIN PLUG INTERCOSTAL HAS CORROSION AT MULTIPLE PLACES. TRANSCRIB ED FROM HAECO GSO NRC 9284552. REMOVED AND REPLACED INTERCOSTAL P/N: 147A5762U13 P.O. 1116947.6 IAW BACDWG 147A5762 REV L AND B737SDR CALA2025040703582Intercostal · corrodedCORROSION ON AFT CARGO COMP INTERCOSTAL CHORD BTW STA 1480-1500 STRG 126-127. REF: NRC 124913. INTERCOSTAL ANGLE WAS REMOVED, NEW IN TERCOSTAL ANGLE WAS RECIEVED WITH TRAVELER#T25/1805770 AND NEW I NTERCOSTAL ANGLE WAS INSTALLED I.A.W. B757-200 SRM 51-40-02.SDR AALA202504040462Retainer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND WHEEL WELL CUT OUT SEAL RETAINER AT BS 727, RBL 39. REMOVED, FABRICATED, AND INSTALLED WHEEL WELL CUT OUT SEAL RETAINER PER SRM 51-40-02-0G.SDR AALA202504041148Retainer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND WHEEL WELL CUT OUT AFT SEAL RETAINER AT BS 727, RBL 57. REMOVED, FABRICATED, AND INSTALLED WHEEL WELL CUT OUT SEAL RETAINER PER SRM 51-40-02-0G.SDR IXXA202504030011Support · corrodedCORROSION F/S 1856 TO 1862 RBL 14 - LBL 18 THREE AREAS CORRODED UNDER WEB ON SUPPORT CHORD.SDR WRXR20250403004Strap · corrodedCORROSION FOUND ON SUBSTRUCTURE AT FS 847.00+32.00 - FS 847.00+62.00 LH BL 18.00 ALONG BOTTOM STRAP. REMOVED CORROSION ON SUBSTRUCTURE AT FS 847.00+32.00 - FS 847.00+62.00 LH BL 18.00 ALONG BOTTOM STRAP IAW CRJ900 SRM 51-21-06-001-001-A01.SDR IXXA20250403006Web · corrodedLH WHEEL WELL STA1103 LBL0 KEEL WEB AT FITTING CORRODEDSDR IXXA20250403002Support Angle · corrodedEWIS CLAMP AND SUPPORT ANGLE CORRODED AT LEFT WING FUEL TANK REAR SPAR JUST ABOVE O/B REACTION LINK ATTACH POINTSDR VNAA20250602003Fitting · corrodedCORROSION AND MISSING NUT ON GALLEY FLOOR SUPPORTS (2EAS) LOCATED BTW FS 280.00 - FS 295.00 AT FUSELAGE FLOOR STRUCTURE RH. CORROSION LOCATED BTW FS 280.00 - FS 295.00 AT FUSELAGE FLOOR STRUCTURE RH WAS EVALUATED DUE TO EXCESIVE DAMAGE ON SUPPORT (1EA) PER CRSDR VNAA20250602002Fitting · corrodedCORROSION ON SETTLEMENT FITTING (1EA) BTW FS 379 AND FS 394, RBL12 OF FWD LAVATORY AT FUSELAGE FLOOR STRUCTURE. CORROSION ON SETTLEMENT FITTING (1EA) BTW FS 379 AND FS 394, RBL12 OF FWD LAVATORY AT FUSELAGE FLOOR STRUCTURE WAS EVALUATED DUE TO EXCESIVE DAMAGSDR VNAA20250524010Bracket · corrodedCORROSION ON HYD PLATES ON LH/RH MAIN WHEEL WELL AND RH/LH MLG HYDRAULIC LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) AT MLG WHEEL WELL AREAS, RBL40, RBL 45 AND LBL45, RBL40. CORROSION ON HYD PLATES ON LH/RH MAIN WHEEL WELL AND RH/LH MLG HYDRAULIC LINES SUPPOSDR SWAA2025052220787Vapor Barrier · crackedCRACK VAPOR BARRIER WEB LOCATED BS 663.75 RBL 25 AT MAIN WHELL WELL COMPARTMENT 2025-242107.SDR SWAA2025042955184Strap · corrodedCORROSION ON TENSION STRAP @ BS1016+13; LBL3 WL 208<[01] THE CORROSION ON TENSION STRAP @ BS1016+13; LBL3 WL 208 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM FOR THIS ITEM AND IT IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02; REMOVED AND REPSDR SWAA2025042955148Scuff Plate · crackedFCB AFT CORNER SCUFF PLATE IS CRACKED.<[01] EDITED STEP 5; WRITTEN IN ERROR;[02] CRACKED FCB AFT CORNER SCUFF PLATE IS REPAIRED BY WELDING IAW SRM 53-30-15-2R-1.;[03] OK TO INSTALL;[04] REPAIRED THE CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1.;[05] VERIFIED ACTIOSDR SWAA2025042955147Scuff Plate · crackedFCB FWD CORNER SCUFF PLATE IS CRACKED.<[01] CRACKED FCB FWD CORNER SCUFF PLATE IS REPAIRED BY WELDING IAW SRM 53-30-15-2R-1.;[02] REPAIR THE CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1.;[03] VERIFIED ACTION 2.<BR>JOB COMPLETE.SDR SWAA2025042955187Angle · corrodedMULTIPLE AREAS OF CORROSION ON AED MOPSILL BETWEEN BS967-BS986; LBL 45; WL 208<[01] REMOVED AND REPLACED AED MOP SILL IAW SRM 51-40-02 AND DWG# 147A8501 REV:-;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[03] VERIFIED CORRECTIVE ACTION COMPLETESDR SWAA2025042850947Angle · crackedHFEC CRACK INDICATION ON THE FOURTH FROM O/B SPAR CHORD HOLE COMMON TO THE LEFT VAPER BARRIER ANGLE REPAIR. ACCOMPLISHED EA 25-157-00870 WIP1 AND WIP2 ON DISCREPANT HOLE.SDR IPXA2025042807149Tee Angle · corrodedCORROSION ON T CHORD STA 1150-1200 BL 70. INSTALLED (14EA NUT PLATES AND 3EA FASTENERS) AT AREA I.A.W B757-200 RM 51-40-02-OG.SDR SWAA2025042321200Scuff Plate · crackedAFT CARGO COMPARTMENT; AFT CORNER SCUFF PLATE IS CRACKED. <[01] WELDED THE CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1594362-1 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(4). REFERRED TO BAC5975 EQUIPMENT USED; WELDING MACHINE ID# E10583 CAL DUE DATE 01/2SDR SWAA2025042321202Structure · corrodedCORROSION ON CREASE BEAM INNER CHORD UPPER SURFACE; STA 687-727; RBL65 WL208. <[01] REMOVED AND REPLACED INNER CREASE BEAM CHORD BS 675-732 RBL 65 WL 208 P/N 144A5910U10 LOT 1601385-1 I.A.W SRM 51-40-02-0G-0 AND DWG 144A5900; [02] REMOVED AND REPLACED INNER CRSDR SWAA2025042321203Panel · crackedCRACKED PANEL BREAK BS 540 BL0-LBL25; WL208 <[01]. INSTALLED NEW PANEL BREAK BS 540 BL0-LBL25; WL208 PER SRM 51-40-02; 51-40-05 AND DWG 143A0060 REV A.; [02] VERIFIED ACTION 1. JOB COMPLETE.SDR SWAA2025042321204Panel · crackedCRACKED PANEL BREAK BS 540 BL0-RBL25; WL208 <[01]. REMOVED AND REPLACED PANEL BREAK BS 540 BL0-RBL25; WL208 PER SRM 51-40-02; 51-40-05 AND DWG 143A0060 REV A.; [02] VERIFIED ACTION 1. JOB COMPLETE.SDR IPXA2025040207006Tee Angle · corrodedCORROSION ON T CHORD AT STA 1180-1220 BL 57.50. INSTALLED NEW T-CHORD FROM STA 1180 TO 1220 LBL 57. NUTPLATES-BACN11P3B6CG, BATCH 0004386857, QTY 17. RIVETS-MS20426AD3-6, BATCH 0004370829, QTY 34. MS20470AD6-6, BATCH 0004377267, QTY 52. HI-LOKS-BACB30MY6K5X,SDR SWAA2025041420672Scuff Plate · crackedACB AFT CORNER SCUFF PLATE IS CRACKED.<[01] WELDED THE CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1594362-1 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(4). REFERRED TO BAC5975.SDR JJBA20250410052Floor Support · corrodedCF3 ON CENTER OMEGA BEAM LOWER FLANGE BTW FR 46-52 FOUND CORRODED. REPAIR DOUBLER ON CF III ENTER OMEGA BEAM ON LH HORIZONTAL FLANGE BTW FR 51-52 CARRIED OUTSDR AALA202504077985Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT STA 500E, LBL 26. REPLACED BAFFLE CLIP PER AARD 51-00-05-1.SDR DALA2025040402567Shear Plate · crackedAIRCRAFT 3084, CRACK SHEAR PLATE LOCATED STR 23 R FROM FR69 TO FR70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SHEAR PLATE AND FASTENERS ON AREA LOCATED STR 23 R BTW FR69 TO FR7O AT AFT GALLEY AREA AS PER A321 SRM 51-42-11, A321 SRM 51-72-11 AND DWG D5347SDR DALA2025040402566Shear Plate · crackedAIRCRAFT 3084, CRACK SHEAR PLATE LOCATED STR 23 L FROM FR69 TO FR70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SHEAR PLATE AND FASTENERS LOCATED STR 23 L FROM FR69 TO FR70 AT AFT GALLEY AREA AS PER A321 SRM 51-42-11. A321 SRM 51-72-11. DWG D53474180 ISSUESDR AALA202504031746Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM STA 500A TO STA 500I AT S24R. REPLACED TRANSITION PANEL PER SRM 51-40-02-0G.SDR AALA202504039391Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM STA 480 TO STA 500I AT S24R. REPLACED TRANSITION PANEL PER SRM 53-00-53.SDR CALA2025040303495Floor Support · corrodedPAX CABIN AFT WET AREA FLOOR STRUCTURE HAS CORROSION ALONG THE L-2 DOOR INNER CHORD. REF BY AAR N/R9961928. ESFR COMPLETED AND SUBMITTED. REMOVED AND REPLACED NEW INNER CHORD AS PER SRM 51-40-02-0G-0 AND DWG: 147A8501. REF ESFR NR645.SDR CALA2025040303493Angle · crackedW/W RH STA 663 RBL 7" VAPOR BARRIER UPPER ANGLE CRACKED REF AAR N/R 9954772 ESFR CREATED AND SUBMITTED. CORRECTIVE ACTION: REMOVED AND REPLACED UPPER ATTACH ANGLE ON R/H VAPOR BARRIER SIDE AS PER SRM 51-40-02-0G-0 AND DWG # 111A1000 REF ESFR NRO.644.SDR CALA2025040303490Angle · cracked{ B737-06-3-0030 } W/W LH STA 663 LBL 7" VAPOR BARRIER UPPER ANGLE CRACKED REF AAR N/R 9954773 ESFR INFORMATION ADDED. ACCOMPLISHED REPAIR AT L/H VAPOR BARRIER STA 663 LBL 7 AS PER SRM 57-10-10-2R-5 AND APPLIED CIC TO REPAIR AREA AS PER AMM 51-21-91-620-802. RSDR DALA2025040302495Angle · corrodedCORROSION ON ANGLE OF AFT CARGO DOOR JAMB AREA BTW STA Y=956 AND LONGERON 27R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00300: CORROSION LEVEL 2. ANGLE OF AFT CARGO DOOR JAMB AREA BTW STA Y=956 AND LONGERON 27R AT AFT CARGO COMPARTMENT WAS REPLACED AND INSTALLESDR VNAA202504020033Floor Support · crackedCRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). CRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR
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