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.

SDR SWAA2026062906011Support Angle · crackedCRACKED SUPPORT ANGLE LOCATED BS 294.5 AT LEVEL STR 13L AT FWD GALLEY AREA. REPLACED THE SUPPORT ANGLE AND FASTENERS LOCATED BS 294.5 AT LEVEL STR 13L AT FWD GALLEY AREA IAW SRM 51-10-02-0G-0 ITEM 9, SRM 51-40-02-0G-0, AND DWG 141A1311, SHEET 1, REV C.May 23, 2026 · N260WN · Boeing 7377H4SDR SWAA2026062505863Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED FWD FACE BS 695 BL 0 WL 208.1 REPLACED SUPPORT ANGLE AND FASTENERS LOCATED FWD FACE BS 695 BL 0 WL 208.1 RT SIDE AT PASSENGER CABIN IAW SRM 51-40-02-0G-0 AND DWG 273A9110, SHEET 6, REV A.May 23, 2026 · N260WN · Boeing 7377H4SDR SWAA2026062505868Angle · crackedCRACK ON ANGLE LOCATED FWD FACE BS 500C AT LEVEL STR 26L AT FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS LOCATED FWD FACE BS 500C AT LEVEL STR 26L IAW SRM 51-40-02-0G-0 AND DWG 143A7505; SHEET 82; REV.-.May 23, 2026 · N260WN · Boeing 7377H4SDR SWAA2026062506013Tie Clip · crackedCRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA. REPLACED TIE CLIP AND FASTENERS, BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0; DWG 141A1110 SHEET: 18 REV: - AND DWG 141A8380, SHEET: 21 REV:-May 23, 2026 · N260WN · Boeing 7377H4SDR SWAA2026062505865Gusset · crackedCRACKED GUSSET ANGLE LOCATED BS 500D AT LEVEL STR 19L AT FWD CARGO BAY. REPLACED GUSSET ANGLE AND FASTENERS LOCATED BS 500D STR 19L AT FWD CARGO BAY IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A7902; SHEET: 174; REV - .May 23, 2026 · N260WN · Boeing 7377H4SDR SWAA2026061105657Angle · crackedAFT CARGO COMPARTMENT BS 867, LBL 13, ANGLE BRACKET FOR PANEL 141QW PILLAR IS CRACKED. REMOVED AND REPLACED AFT CARGO COMPARTMENT BS 867, LBL 13.May 23, 2026 · N8540V · Boeing 7378H4SDR ASAA2026052366544Transition Panel · crackedFWD CARGO RT TRANSITION PANEL BS 500B TO 500H HAS MULTIPLE CRACKED AREAS. GROUNDED - YES. REMOVED AND REPLACED RT TRANSITION PANEL AND SPLICE BS 500B TO 500H IAW SRM 53-00-53-2R-6.May 23, 2026 · N409AS · Boeing 737990ERSDR MASA20260608148Shear Panel · corrodedDURING HEAVY CHECK, INSPECTIONS OF THE CFIII, AFT WET AREA, CORROSION ON LT SHEAR PANEL AT FR 87, LBL 13 TO LBL 46 REMOVED BY BLENDING IAW SRM 51-10-03, MAX MATRL REMOVED .002". FOUND TO BE WITHIN LIMITS IAW SRM 53-23-10 AD 03.10X MAG C/OUT, NO FAULT FOUND. BMay 23, 2026 · N88335 · Emb ERJ170200LRSDR AALA202606027001Baffle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT BAFFLE AT STA 771 AND RBL 34. REPLACED BAFFLE PER SRM 51-10-02.May 23, 2026 · N800NN · Boeing 737823SDR FDEA202605230659Floor Support · corrodedMAIN DECK - FWD COURIER AREA FR11-FR14 Y1456 LONGITUDINAL FLOOR SUPPORT CORRODEDMay 23, 2026 · N660FE · Airbus A300F4605RSDR FDEA202605230649Web · crackedMDC - UNDER FLOOR WEB CRACKED AT FR47 Y-953 - Y-1456. REPAIRED THE CRACKED WEB ON MDC - UNDER FLOOR AT FR47 Y-953 - Y-1456 PER A300-600F SRM53-15-15-201 FIG.201. THIS IS A CATEGORY B REPAIR AND IT MUST BE INSPECTED AT DEFINED INTERVAL PER A300-600F SRI53-1May 23, 2026 · N660FE · Airbus A300F4605RSDR FDEA202605230636Web · crackedMDC - UNDER FLOOR WEB CRACKED AT FR47 Y0 - Y-450. REPAIRED THE CRACKED WEB ON MDC - UNDER FLOOR AT FR47 Y0 - Y-450 PER A300-600F SRM53- 15-15-201 FIG.201. THIS IS A CATEGORY B REPAIR AND IT MUST BE INSPECTED AT DEFINED INTERVAL PER A300-600F SRI53-15-15-2-May 23, 2026 · N660FE · Airbus A300F4605RSDR UIEA2026040400123Support Bracket · damagedAPU COMPT LH STA 2674.85 FRAME ATT WIRE SUPPORT BRACKET FOUND DETACH AND RIVET HOLES ELONGATED(<P>FRAME REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026040500124Floor Support · crackedM/D STA 1200, RH O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED(<P>INTERCOSTAL WEB CRACK AREA REPAIRED SRM 53-40-51-2R-9 REPAIR 9 AND RI-53-40-18156 REV A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026040500125Floor Support · crackedBS 346 LB '0' INTERCOSTAL FOUND 2EA CRACKS(<P>INTERCOSTAL CRACK AREA REPAIRED AS PER RI-53-10-18208 REV B. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026041500194Bracket · corrodedU/D - LBL 23 BS 480 FLR SUPPORT BRACKET FOUND CORROSION(<P>CORROSION BRACKET REPLACED AS PER SRM 51-10-02 AND NEW BRACKET HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW BRACKET INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026041700209Web · corrodedU/D LBL 10 TO 20 BS 480 TO 500 FLOOR SUPPORT WEB FOUND CORROSION(<P>WEB FABRICATED AS PER DWG 141U5421 AND PL, WEB REPLACED AS PER SRM 51-10-02, AND NEW WEB HOLES TRANSFERRED AS EPR SRM 51-40-05, AND NEW WEB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOMay 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026041700210Doubler · corrodedU/D LBL 10" - LBL 14" BS 480-500 FLOOR SUPPORT WEB ATT. DOUBLER CORROSION(<P>DOUBLER FABRICATED AS PER DWG 141U5422, AND PL DOUBLER REPLACED AS PER SRM 51-10-02, AND NEW DOUBLER HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW DOUBLER INSTALLED AS PER SRM 51-40-May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026041800212Web · crackedLH BS 1480 WEB CRACKED 1/4" ADJACENT LONGERON FITTING LOWER AREA(<P>WEB REAIRED AS PER SRM 53-40-08-2R-1 REPAIR 1 FIG 201 AND RI-53-40-18137 REV A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026042400246Web · crackedU/D LBL 10 TO LBL 35 BS 500 - BS 540 FLOOR SUPPORT SHEAR WEB CORROSION(<P>SHEAR WEB FABRICATED AS PER BOEING DWG 141U5421 AND PL, AND NEW SHEAR WEB HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW SHEAR WEB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTEDMay 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026042600248Floor Support · crackedM/D BS 1860 - 1880 RHS O/B RBL 116" FLOOR SUPPORT L ANGLE FOUND CRACK.(<P>FLOOR SUPPORT CRACK AREA REPAIRED AS PER RI-25-21-18246 REV A. NO FURTHER DEFECTS NOTED.May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026042800258Web · crackedFX RH BS 1480 WEB CRACK 5/8" ADJACENT LONGERON EXTENSION FITTING LOWER AREA(<P>WEB CRACK AREA REPAIRED AS PER ATLAS AIR EO 4453A818 REV 20 PART 8 AND RI-53-20-1823 REV A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026050100282Panel · crackedCOCKPIT LHS FLOOR FLIGHT KIT STOWAGE BASE PNL FOUND CRACK(<P>BASE PNL CRACK AREA REPAIR AS PER RI-25-10-18213 REV A. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026050400289Liner · tornBULK CARGO STA 2160 LINER FOUND TORN AT SEVERAL LOCATION(<P>CARRY OUT REPAIR AS PER RI-25-54-18224 REV C. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR UIEA2026050600304Panel · damagedM/D LHS BS 1920 - 2020 DADO PANEL FOUND DAMAGED(<P>DADO PANEL FWD CUTOUT GOUGE AND AFT CUTOUT DEFORM AREA REPAIRED AS PER RI-25-21-18165 REV B. NO FURTHER DEFECTS NOTED</P>)May 23, 2026 · N477MC · Boeing 74747UFSDR IPXA2026052425094Stiffener · crackedCRACKED STIFFENER, FLOOR SUPPORT STRUCTURE STA 785.9 LBL 55. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2 REV. 95 AND EGAT WORK SHEET NO: 60432 AND EO-58151-REQ001 REV1.May 23, 2026 · N341UP · Boeing 767300SDR IPXA2026052425098Stiffener · crackedCRACKED STIFFENER, FLOOR SUPPORT STRUCTURE STA 785.9 RBL 55. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2 REV. 95 AND EGAT WORK SHEET NO: 60430 AND EO-58151-REQ001 REV1.May 23, 2026 · N341UP · Boeing 767300SDR DALA2026052403136Web · corrodedLEVEL 2 CORROSION, ON WEB LOCATED AT LEVEL S23R BTW FR 69 TO FR 70 AFT GALLEY AREA. REPLACED WEB AND FASTENERS LOCATED AT LEVEL S23R BTW FR 69 TO FR 70 AFT GALLEY AREA IAW SRM 51-42-11, DWG D53474180, ISSUE: E. (LP: 1609209) AIRCRAFT WAS GROUNDED.May 23, 2026 · N369NB · Airbus A319114SDR DALA2026052403135Web · corrodedLEVEL 2 CORROSION, ON WEB LOCATED AT LEVEL S23R BTW FR 69 TO FR 70 AFT GALLEY AREA. INSTALLED WEB, BRACKET (1 EA) AND FASTENERS LOCATED AT LEVEL STR23RH BTW FR69 TO FR70 AFT GALLEY AREA AS PER A319 SRM 51-42- 11,DWG: D53474180 ISSUE: E. (LP: 1609200) AIRCRAFMay 23, 2026 · N369NB · Airbus A319114SDR DALA2026052403134Floor Support · corrodedLEVEL 3 CORROSION, EVIDENCE OF REWORK FLOOR SUPPORT +Y254 LOC. FR 16 TO FR 20 AT FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT Y254 AND FASTENERS LOCATED BTW FR12 TO FR24 AT FWD GALLEY AREA IAW SRM 51-42-11 AND DWG D53112816, ISSUE : G00, DWG D53110984 ISSUE: CMay 23, 2026 · N369NB · Airbus A319114SDR DALA2026052403133Cover Plate · damagedELONGATED HOLES ON COVER SHEET LOCATED FROM FR55A TO FR59 IN AFT CARGO COMPARTMENT. REPLACED COVER SHEET LOCATED FROM FR55A TO FR59 IN AFT CARGO COMPARTMENT IAW SRM 51-42-11, SRM 51-72-11 AND DWG E53476320, ISSUE: BD. MEASURE OF ELONGATED HOLE IS : D = 0.300May 23, 2026 · N369NB · Airbus A319114SDR SWIA2026052277008Angle · corrodedFOUND LOWER ANGLE PN:601R32200-17 TO BE HEAVILY CORRODED AT FS 409 AFT SIDE BL0 (C-CHECK RO 08/28/2026)REMOVED 2 ANGLES AFT OF FS409 BL0 FOR ACCESS IAW CRJ200 SRM 51-42-06 & 51-42-21.REMOVED CORRODED LOWER ANGLE PN# 601R32200-17 AT FS409 AFT SIDE BL0 IAW CRJMay 22, 2026 · N477CA · Cndair CL6002B19SDR SWAA2026061505699Scuff Plate · crackedCRACKED FWD CORNER SCUFF PLATE AT AFT CARGO BAY. REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO BAY IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4. B, STEPS (2 TO 7), FIGURE 203.May 22, 2026 · N483WN · Boeing 7377H4SDR SWAA2026061505462Crossbeam · crackedBREAK PANEL SUPPORT CRACKED AT BS 540, LBL 1, WL 208.1. REMOVED AND REPLACED BREAK PANEL SUPPORT AT BS 540, WL 208.1, LBL 1 IAW SRM 51-40-02 AND DWG 143A0060, REV A.May 22, 2026 · N7704B · Boeing 7377BDSDR SWAA2026061505456Angle · corrodedCORROSION FOUND AT F.S. 685 + 8 W.L. 200 RBL 63. REMOVED AND REPLACED THE PRESSURE FLOOR ANGLE B.S. 685 + 8 W.L. 200 RBL 63; IAW SRM 51-40-02 AND DWG 144A7700, REV E.May 22, 2026 · N7704B · Boeing 7377BDSDR SWAA2026061505457Stiffener · corrodedCORROSION FOUND AT F.S. 685 +1 W.L. 200; LBL 63. REFER TO FAULT TTG8Q01CB9LV FOR REPAIR RESOLUTION.May 22, 2026 · N7704B · Boeing 7377BDSDR SWAA2026061505458Stiffener · corrodedCORROSION FOUND AT 685+12; W.L. 200; LBL62. STIFFENER BS 685+12; W.L. 200; LBL62 WAS REPAIRED IAW EA 26-153-01440-WIP1; REV-A.May 22, 2026 · N7704B · Boeing 7377BDSDR SWAA2026060305683Web · crackedCRACK ON WEB LOCATED BTW BS 500B TO BS 500C A LEVEL STR26L AT FWD CARGO COMPARTMENT. REPLACED WEB LOCATED BTW BS 500B TO BS 500C A LEVEL STR26L AT FWD CARGO COMPARTMENT.<BR>IAW B737-700 SRM 51-40-02-0G-0 AND DWG#143A7505 SHEET 81 REV-.May 22, 2026 · N253WN · Boeing 7377H4SDR DALA2026052803221Cusp Web · crackedIAW TASK 310-01436-01 STEP 5 AFTER REMOVAL CUSP MEMBRENE CRACK WAS FOUND AT CUSP WEB. FUSELAGE STA 674 LH SIDE. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55 (1606106) (AIRCRAFT GROUNDED)May 22, 2026 · N993AT · Boeing 717200SDR 4VAA202605210010Bracket · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE HYDRAULIC PIPE BRACKET. IT WAS REPLACED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060669.May 21, 2026 · N749SA · Saab 2000SAABSDR REXA2026080401460Latch · brokenBROKEN SPRING LATCH (2 EAS) OF REFUEL/DEFUEL CONTROL PANEL 192AR SPRING LATCH (2 EAS) OF REFUEL/DEFUEL CONTROL PANEL 192AR WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01May 21, 2026 · N146PQ · Cndair CL6002D24SDR REXA2026080401459Access Panel · corrodedCORROSION ON MLG WHEEL WELL ACCESS PANELS NO. 542AZ, 542BZ, 642AZ AND 642BZ CORROSION ON MLG WHEEL WELL ACCESS PANELS NO. 542BZ, 642AZ AND 642BZ WAS REMOVED PER SRM 51-21-06-001-001-A01 AND WERE FOUND WITHIN LIMITS PER SRM 53-00-00-101-001-A01. NEW MLG WHEEL WMay 21, 2026 · N146PQ · Cndair CL6002D24SDR VNAA202608010012Floor Support · crackedCRACK ON CENTER FLOOR BEAM RBL 12.0 BTW 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50) FLOOR BEAM RBL 12.0 BTW 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE WAS REPAIRED PER REO: 690-53-11-21May 21, 2026 · N644NN · Cndair CL6002D24SDR VNA2026F00009Bracket · corrodedCORROSION ON BRACKET'S MACHINED (2EAS) FS 515, (1EA) FS533, (2EAS) FS 565, (2EAS) FS629, (1EA) FS645, AND (2EAS) FS661+8.40 AT CENTER AND FWD BAGGAGE COMPARTMENT. BRACKET'S MACHINED (2EAS) FS 515, (1EA) FS533, (2EAS) FS 565, (2EAS) FS629, (1EA) FS645, AND (2EMay 21, 2026 · N644NN · Cndair CL6002D24SDR VNAA202608010007Bracket · corrodedCORROSION ON BRACKET'S MACHINED (2EAS) FS 515, (1EA) FS533, (2EAS) FS 565, (2EAS) FS629, (1EA) FS645, AND (2EAS) FS661+8.40 AT CENTER AND FWD BAGGAGE COMPARTMENT. BRACKET'S MACHINED (2EAS) FS 515, (1EA) FS533, (2EAS) FS 565, (2EAS) FS629, (1EA) FS645, AND (2EMay 21, 2026 · N644NN · Cndair CL6002D24SDR VNAA202608010006Bracket · corrodedCORROSION ON BRACKET'S MACHINED (2EAS) FS 515, (1EA) FS533, (2EAS) FS 565, (2EAS) FS629, (1EA) FS645, AND (2EAS) FS661+8.40 AT CENTER AND FWD BAGGAGE COMPARTMENT. BRACKET'S MACHINED (2EAS) FS 515, (1EA) FS533, (2EAS) FS 565, (2EAS) FS629, (1EA) FS645, AND (2EMay 21, 2026 · N644NN · Cndair CL6002D24SDR VNAA202608010001Web · corrodedSEVERAL CORRSION ON SETTLEMENT AREA OF FAIRING ACCESS PANEL 194AB (AFT SIDE), ON SETTLEMENT AREA OF ACCESS PANELS 174BZ, 174DZ 173BZ AND 173DZ ALSO IN ANGLE OF KEEL BEAM NEAR FS 669.40 AT MLG WHEEL AREA. CORROSION WERE REMOVED ON SETTLEMENT AREA OF FAIRING ACMay 21, 2026 · N644NN · Cndair CL6002D24SDR VNAA202607310002Angle · corrodedCORROSION ON KICKPLATE ANGLE AND MID CAP ANGLE OF PASSANGER DOOR LOWER SURROUND STRUCTURE. KICKPLATE ANGLE AND MID CAP ANGLE OF PASSANGER DOOR LOWER SURROUND STRUCTURE WAS EVALUTAED AND FOUND TO EXCESSIVE CORROSION IAW SRM 51-10-06-001-001-A01 AND WERE REPLACMay 21, 2026 · N644NN · Cndair CL6002D24SDR ASAA2026052166973Web · corrodedAFT CARGO STRAP INBD OF SILL WEB IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO STRAP INBD OF SILL WEB IAW SRM 51-40-02-0G-0 STEP 7.C., 4.B.May 21, 2026 · N548AS · Boeing 737890SDR ASAA2026052166972Strap · corrodedAFT CARGO STRAP INBD OF SILL WEB IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO STRAP INBD OF SILL WEB IAW SRM 51-40-02-0G-0 STEP 7.C., 4.B.May 21, 2026 · N548AS · Boeing 737890
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