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 AALA202502147208Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL LOCATED FROM STA 344 TO STA 360 AT BL 0. REPLACED INTERCOSTAL PER AARD 51-00-05-1.SDR JJBA20250213018Gusset · corrodedCENTER FUSELAGE IV, CENTER GUSSET BTW FRAME 59-61 FOUND CORRODED. CF4, CENTER GUSSET BTW FR 59-61 CORRODED OUT OF LIMITS. GUSSET REMOVED FOR REPLACEMENT. GUSSET CENTER BTW FR 59-61 REPLACEDSDR VNAA202502110012Plate · corrodedCORROSION ON KICKPLATE AT PASSENGER DOOR. KICKPLATE AT PASSENGER DOOR WAS EVALUATED ARE OUT OF LIMITS PER CRJ/900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.SDR DALA2025021000997Floor Support · corrodedSHIP 6705 CORROSION OUT OF LIMITS: IN REF NRC 297. CORROSION ON FLOOR SUPPORTS AT AFT CARGO COMP RBL=16.10, 7.55 AND 2.90 ALSO LBL= 16.10, AND 2.90. BTW STA= 1320-1340 FOUND OUT OF LIMITS PER B757-200 SRM 53-00-53-1A PROCEDURE 1. CORRECTIVE ACTION: SUMMARY OF SDR CALA2025020600308Floor Support · corroded(SUPPORT TASK) R/H LONGITUDINAL EAM HAS 2EA SPOTS OF CORROSION AT -Y1162.5 BETWEEN FR68 AND FR69. REMOVED AND REPLACED LONGITUDINAL BEAM LOCATED BETWEEN FR68 TO FR70 AT -71162.5 PER A320 SRM 51-42-11/001 AND AIRBUS DWG D53472040, ISSUE A,SDR AALA202502097598Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.SDR DALA2025020600941Sill Drain · corroded(LOG 0796948) L2 AFT MOP SILL HAS SPOTS (3) OF LIGHT SURFACE CORROSION. FABRICATED NEW WEB FROM .040 7075-T6 AND REPLACED SUPPORT WITH NEW SUPPORT IAW B737 SRM 51-40-02, B737 SRM 51-30-01, B737 SRM 51-40-05 AND B737 SRM 53-70-15-1A.SDR DALA2025020600938Plate · corroded(LOG 0797747) CORROSION ON SIDE PLATE LH SIDE, S-26L FROM STA 727 B TO STA 727C ON AFT CARGO C2. SIDE PLATE LH SIDE, S-26L FROM STA 727 B TO STA 727C WAS REPAIRED PER B737-800 SRM 53-00-53 2R PROCEDURE 6 REPAIR 6.SDR DALA2025020600935Support Angle · corroded(LOG 0797537) ACB SHIELD SUPPORT ANGLE AT BS 767-787 RBL 21 WL 156 IS CORRODED. REMOVED OLD PART AND RECEIVED, LOCATED AND INSTALLED NEW SHIEL SUPPORT ANGLE FROM ACB BS 5767 RBL 21 WL 156 IAW BOEING 146A8123 DWG ID: 0016 REV: - AND B737-900 SRM 51-10-02-0G.SDR DALA2025020600934Shield · corroded(LOG 0797501) CORROSION ON FWD SHIELD AT ACB BS767 - BS787 RBL21 WL157. REMOVED OLD SHIELD, RECEIVED NEW SHIELD LOCATED AND DRILLED IAW BOEING 1460081 DWG ID: 0049 REV: A AND B737-900 SRM 51-10-02-0G.SDR DALA2025020600933Support · corroded(LOG 0797496) CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS767 - BS727B RBL21 WL156. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT BS727 TO BS 767 RBL21, PER DWG# 146A7500. REV - SHEET 225. AND B-737-960 SRM 51-40-02-0G.SDR DALA2025020600931Floor Support · cracked(LOG 0797437) MAIN CABIN FLOOR STRUCTURE SUPPORT HAS A CRACK AT RADIUS, LOWER SURFACE BS.540 APROX RBL.2. REMOVED AND REPLACED MAIN CABIN FLOOR STRUCTURE SUPPORT PN# 143A5240U12 AND PN 143A5240-10 AT BS.540 AT APPROXIMATELY BL 0 TO RBL.24 IAW B737 SRM 51-40-02SDR DALA2025020600930Floor Support · corroded(LOG 0797399) MAIN CABIN R1 DOOR AREA, FLOOR STRUCTURE HAS CORROSION ON UPPER SURFACE AT STA 313 AND 325 RBL 60. REMOVED AND REPLACED CHORD ASSY 654A0004-106 IAW B 737 SRM 51-40-02.SDR J6BA202502060005Floor Support · damagedFLOOR BEAM FLOOR BOARD LANDING BETWEEN FS 409.00 TO FS 409.00 + 37 AT RBL 9.0 BEYOND LIMITS OF REO 601R-53-00-005. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESSSDR N6WA2025020503Intercostal · corrodedCORROSION ON INTERCOSTAL BELOW PAX DOOR AFT OF FS333 BY STR20L. REPLACED INTERCOSTAL BELOW PAX DOOR AFT FS333 BY STR20L IAW CRJ SRM 51-42-20.SDR IXX2025F00005Stiffener · corrodedLH WHEEL WELL STA1140 LBL74 LOWER PANEL SUPPORT SUPPORT CORRODEDSDR AALA202502059252Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN INTERCOSTAL UPPER ANGLE FROM STA 380 TO STA 400 AT RBL 0. REPLACED ANGLE PER AARD 51-00-05-1.SDR SWI2025F01022Channel · corrodedCORROSION ON AFT WATER DRAIN MAST CHANNEL (C-CHECK RO 07/18/2025)INSTALLED AFT DRAIN MAST CHANNEL REF SRM 51-42-06-001-001-A01,DWG:MM670-43200 REV NC. PRESSURE CHECK AND OPS CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.SDR SWIA2025062400204Floor Support · crackedDURING AUDIT OF 48MO TASK CARD 53-140-505(DETAILED INSPECTION OF THE CABIN FLOOR SUPPORT STRUCTURE FROM FS280.0 TO FS409.0 (CPCP)) FOUND CRACKED CLIP ON AFT SIDE OF 280 AT RBL9. (C-CHECK RO 06/23/2025)REPLACED CRACKED FLOOR SUPPORT CLIP AT FS 280 & RBL 9.0 ASDR SWAA2025031095377Vapor Barrier · crackedTHE L/H B.S. 663 VAPOR BARRIER HAS AN ALUMINUM FOIL PREVIOUS REPAIR LOCATED AT APPROXIMATELY LBL 55 <[01]. PREVIOUS ALUMINUM FOIL REPAIR ON L/H B.S. 663 VAPOR BARRIER LOCATED AT APPROXIMATELY LBL 55 WAS REMOVED; AND PERMANENT REPAIR WAS ACCOMPLISHED IAW SRM 5SDR SWAA2025031092940Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN BS727 TO BS847 LBL21 AND WL156 AFT CARGO COMPARTMENT 2025-110533 <[01]. REPLACED SUPPORT ZEE LOCATED BETWEEN BS727 TO BS847 LBL21 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 146ASDR SWAA2025031092941Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN BS727D TO BS787 RBL21 AND WL156 AFT CARGO COMPARTMENT 2025-110534 CORROSION SUPPORT ZEE LOCATED BETWEEN BS727D TO BS767 RBL21 AND WL156 AFT CARGO <[01]. REPLACED SUPPORT ZEE LOCATED BETWEEN BS727D TO BS767 RBL21 AND WL156SDR REXA2025030600274Angle · corrodedDURING SILL REMOVAL IN REF NRC 093, CORROSION ON ANGLE MID CAP WAS FOUND CORROSION ON ANGLE MID CAP WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-002-A02 THEREFORE WAS REPLACED ON NRC 0093SDR SWAA2025030493141Panel · crackedCRACKED PANEL BREAK AT MIDCABIN BS 540; RBL 1; WL 208. <[01] REMOVED PANEL BREAK AT BS 540 RBL 1 WL 208 PER SRM 51-40-02 AND INSTALLED NEW PANEL BREAK AT BS 540 RBL 1 WL 208 PER DWG: 143A0060 REV: - AND SRM 51-40-02; [02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2025030393142Panel · crackedCRACKED PANEL BREAK AT MID CABIN BS 540; LBL 1; WL 208. <[01] REMOVED PANEL BREAK AT BS 540 LBL 1 WL 208 PER SRM 51-40-02 AND INSTALLED NEW PANEL BREAK AT BS 540 LBL 1 WL 208 PER DWG: 143A0060 REV: - AND SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTION 1.SDR IPXA2025022863373Sidewall Panel · no discrepancyREMOVE L3 DOOR FOR STR. MAINT. REMOVED UPPER CARGO STA 1281 L/H SIDEWALL PNL PER MD11 AMM 25-23-02-000-801. REMOVED L3 DOOR PER MD11 AMM 52-12-12-000-801.REINSTALLED L3 DOOR PER MD11 AMM 52-12-12-400-801.SDR IPXA2025022863391Sidewall Panel · not reportedREMOVE R3 DOOR FOR STR. MAINT. REMOVED UPPER CARGO R/H STA 1281 SIDEWALL PNL PER MD11 AMM 25-23-02-000-801. REMOVED R3 DOOR PER MD11 AMM 52-12-12-000-801.REINSTALLED R3 DOOR PER MD11 AMM 52-12-12-400-801.SDR R61A2025022600108Support · corrodedCFIII, FR85-87, CORRODED LWR BEAM SUPPORT. CFIII, FR85-87, CORRODED LWR BEAM SUPPORT REMOVED AND REPLACED IAW SRM 51-41-01.SDR R61A2025022600103Support Angle · crackedWHEEL WELL AREA, CENTER TANK EXTERNAL LOWER SKIN L ANGLE SUPPORT FOR RIB FR52 IS CRACKED. WHEEL WELL AREA, CENTER TANK EXTERNAL LOWER SKIN L ANGLE SUPPORT FOR RIB FR52 WAS REPLACED IAW SRM 51-43-03SDR ASAA2025020456235Angle · corrodedFWD CARGO PIT, R/H FROM STA 500C TO 500I, TRANSITION ANGLE HAS CORROSION ON TOP SURFACE. GROUNDED - YES. EVALUATED & REMOVED DAMAGE ON FWD CARGO PIT R/H TRANSITION @ STA 500C -500I, ORIGINAL: .040 , REMOVED: .040, REMAINING: .000 AND FOUND TO BE OUT OF LIMITS SDR SWAA2025022692936Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] CORROSION WAS FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED SHIELD AS PER SRM 51-40-02-0G-0 AND DRAWING 146A7500 REV: -SDR SWAA2025022692934Support · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] CORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT LIMITS. REMOVE AND REPLACE L/H FLOOR TO SIDEWALL SDR SWAA2025022692935Support Plate · corrodedCORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] CORROSION WAS FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED FLOOR TO SUPPORT AS PER SRM 51-40-02 AND DRAWING 146A7500 REV: -SDR ASAA2025020456160Channel · corrodedFWD CARGO PIT, L/H AT STA 500C TO 500I, TRANSITION ANGLE HAS CORROSION ON TOP SURFACE AT FASTENER HOLES, MARKED. GROUNDED - YES. REMOVED CORROSION ORIGINAL THICKNESS .040, REMOVED .040, REMAINING .000. FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2. SDR ASAA2025020456159Angle · corrodedFWD CARGO PIT, STA 500I AT AFT BULKHEAD TO FLOOR PANEL ANGLE HAS CORROSION AT FASTENER HOLES FOR PANEL. GROUNDED - YES. EVALUATED ORIGINAL MATERIAL THICKNESS .071, REMOVED .071, REMAINING .000 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-30SDR ASAA2025020456154Door Sill · corrodedFWD CARGO PIT, CARGO DOOR SILL STRUCTURE ON TOP HAS CORROSION MARKED. GROUNDED - YES. EVALUATED AREA AND REMOVED DAMAGE, ORIGINAL: .045, REMOVED: .012, REMAINING: .033 & IS FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 51-60-15-1A-1. REMOVED DAMAGED THRESHOLD WEBSDR ASAA2025020456149Angle · corrodedFWD CARGO PIT, R/H AT STA 500A TO 500C, TRANSITION ANGLE HAS CORROSION AT FASTENER HOLES, MARKED. GROUNDED - YES. EVALUATED AND REMOVED DAMAGE ON FWD CARGO PIT R/H TRANSITION @ STA 500A-500C , ORIGINAL : .040 , REMOVED : .040, REMAINING: .000 AND FOUND TO BE OSDR CALA2025022400420Stiffener · crackedLOWER FUS. CENTER WING REAR SPAR STIFFENER LOWER RADIUS CRACKED AT LBL 25 STA 663.75 O/B OF L/H RAM AIR EXIT EXHAUST REF AAR N/R 9933669 REMOVED AND REPLACED LOWER FUS. CENTER WING REAR SPAR STIFFENER AT LBL 25 STA 663.75 O/B OF L/H RAM AIR EXIT EXHAUST AS PESDR IPXA2025021570871Support · corrodedAFT CARGO CEILING SUPPORT AT FR 54 HAS 1(EA) FASTENER HOLE WITH CORROSION DOT 07586-01. REMOVE AND REPLACE 1 EACH SUPPORT (P/N: A53410767204) PER PRODUCTION DRAWING REQUIREMENTS AND SRM CHAPTER 51 REQUIREMENTS. USE ORIGINAL PART AS SAMPLE IN ACCORDANCE WITH SDR JJBA20250213026Support · corrodedREAR FUSELAGE I, LH SILL BTW FRAME 61-65 FOUND CORRODED. LH SILL BTW FR 64-65 BLENDED OUT OF LIMIT. REAR FUSELAGE I, LH CARBON BULKHEAD REMOVED FOR ACCESS. RF I, L SILL BTW FR 61-65 REMOVED FOR REPLACEMENT. RF1, LH SILL BTW FR61-65 INSTALLED. RD1, LH CARBON BUSDR JJBA20250213022Support · corrodedCENTER FUSELAGE II, RH SILL BTW FRAME 29-35 FOUND CORRODED. CENTER FUSELAGE II, RH SILL BTW FR 29-35, CORROSION BLENDED OUT OF LIMIT. RH SILL BTW FR 29-35 REMOVED FOR REPLACEMENT. AT CF2, RH SILL BTW FR29-35 REPLACEDSDR JJBA20250213020Tee Angle · corrodedREAR FUSELAGE 1, LH T-POST AT FR61 FOUND CORRODED. RF1, LH T-POST AT FR61 BLENDED OUT OF LIMITS. LH T-POST AT FR61 REMOVED FOR REPLACEMENT. LH T-POST NEW PART INSTALLED.SDR IPXA2025021170871Support · corrodedOPEN. AFT CARGO CEILING SUPPORT AT FR 54 HAS 1(EA) FASTENER HOLE WITH CORROSION DOT 07586-01 INSTALLED SUPPORT IAW A300 SRM 51-40-21. PN: CCR264SS3-04, BN: 0004364298 MS20426AD5-9, BN: 0004233085SDR JJBA20250210015Angle · crackedCENTER FUSELAGE 1, AT FRAME 14 AND STR 16L, REINFORCEMENT ANGLE FOUND CRACKED. AT CF1, AT FR 14 STR 16L REINFORCEMENT ANGLE REMOVED FOR REPLACEMENT. AT CF1 AT FR14 STR 16L REINFORCEMENT ANGLE REPLACEDSDR UIEA2025020300116Web · damagedDURING HFEC INSPECTION ON NOSE WHEEL WELL SIDE AND TOP PANEL, WEB AND STIFFENER AT STA 265-280, WL 140 FOUND TWIN FASTENER AND UNABLE TO SCAN AROUND(<P>FASTENER REMOVED AND REPLACED IAW B747-400F SRM 51-40-02 REV 102. WORK ACCOMPLISHED IAW EN 1008-25 REV 0. NOSDR DALA2025020600929Transition Panel · corroded(LOG 0795520) TRANSITION PANEL AT STA.500 (R/H SIDE) INSIDE FWD CARGO COMPARTMENT HAS (1) AREA OF CORROSION. REPAIRED IAW B737 SRM 53-00-53-2R-5.SDR U2RA2025020400001Support Bracket · wornDURING AIRCRAFT HEAVY CHECK IN XMV, HAECO MAINTENANCE DISCOVERED 1EA EXISTING REPAIR DOUBLER WAS INSTALLED ON REF. /A/ L1 MED FWD FRAME WEB. THE EXISTING DOUBLER WAS FOUND WORN DAMAGE DUE TO INTERFERENCE WITH THE REF. /C/ DOOR CUTOUT FWD FRAME SUPPORT BRACKET.SDR REXA2025020500128Angle · corrodedPAX DOOR UPPER MID SILL ANGLE IS CORRODED REMOVED UNSERVICEABLE PAX DOOR UPPER MID SILL ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-41-02-001-001-A01.INSTALLED NEW PAX DOOR UPPER MID SILL ANGLEP/N SH670-31825-9S IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-41SDR REXA2025020500127Angle · corrodedPAX DOOR UPPER FWD SILL ANGLE IS CORRODED. REMOVED UNSERVICEABLE PAX DOOR UPPER FWD SILL ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR UPPER FWD SILL ANGLE P/N SH670-31821-5S IAW CRJ900 SRM 51-42-06-001-001-A01.SDR REXA2025020500124Bracket · chafedR/H WHEEL WELL FWD WHEEL BIN ATTACHMENT BRACKET AFT FACE IS CHAFED. REMOVED AND EPLACED WHEEL BIN BRACKET CC670-39221-4: LOCATED 13 HOLES FOR HI-LITES IAW CRJ700 SRM 51-40-11-001-001-A01 INSTALLED 13 HI-LITES IAW CRJ700 SRM 51-42-21-001-001-A01 LOCATED 8 HOLES
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