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 DALA2025101307480Support Angle · corrodedCORROSION ON AFT LAV SUPPORT STRUCTURE CLIP PT 146T3248-8. REPLACED CLIP REF BAC DWG 146T3244 (1233342)SDR DALA2025101307479Support · corrodedCORROSION ON AFT LAV SUPPORT STRUCTURE DOOR SUPPORT PN 148T3248- 7. REPLACED DOOR SUPPORT REF BAC DWG 146T3244 (1233340)SDR DALA2025101307490Angle · corrodedCORROSION ON AFT LAV SUPPORT STRUCTURE CLIP PT # 146T3248-15. REPLACED CLIP REF BAC DWG 146T3244 (1233344)SDR CALA2025100909837Baffle · corrodedFWD CARGO BAY, STRINGER 26L BETWEEN BS 500F - 500G BAFFLE IS CORRODED ON UPPER FLANGE. AFTER INVESTIGATION, DAMAGED AREA AT WAS CONCLUDED THAT THE MATERIAL IS FOUND TO BE 100% OUT OF LIMITS DUE TO EVIDENT EXPOLATION IAW SRM 53-00-53-1A-2, FIG 103. LOCATEDSDR CALA2025100809791Angle · corrodedFWD PIT, LEFT SUPPORT ASSY CORRODED AT LOWER AREA AT BS 500L APPROX. AT LBL-24. REMOVED SUPPORT ASSY (ANGLE) IAW SRM 51-40-02 AND REMOVAL DAMAGE CORROSION. MAT. REMAINED .037" FOUND WITHOUT LIMITS OF .056". LOCATED & DRILLED 1EA NEW SUPPORT ASSY (ANGLE) IASDR CALA2025100709737Intercostal · corrodedMAIN CABIN AFT WET AREA STA 952, RBL26, INTERCOSTAL ANGLE HAS CORROSION. REMOVED AND REPLACED INTERCOSTAL PER BAC DWG 147A5660 ID:0014 REV:- T05867-173.SDR CALA2025100709735Floor Support · corrodedMAIN CABIN FLOOR SUPPORT INTERCOSTAL FLOOR BOARD FASTENER HOLES 2EA HAVE CORROSION IN THE BORE BETWEEN STA 294.5 AND 312 AT APPROX LBL12. MAIN CABIN FLOOR STA 294.5 - 312 LBL 11.1 BLENDED AFFECTED AREA ON INTERCOSTAL TO REMOVED CORROSION, REMAINING MATERIALSDR HALA20251006303Support Bracket · brokenETOPS - FOUND HP FUEL FILTER SUPPORT BRACKET BROKEN WHILE CARRYING OUT TASK CARD # 330-783201-R2-1-1. REMOVED AND REPLACED SUPPORT BRACKET PER AMM SUBTASK 73-11-42-420-052-A. A/C OK TO CONTINUE SERVICE.SDR DALA2025100607265Web · corrodedUPPER FUSELAGE, PAX CABIN ON FR 68 AND ON STGR-23L(LEVEL) SILL WEB WITH CORROSION. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR AT AFT L/H PASSENGER CREW DOOR SILL BEAM BETWEEN FR68-190.5 MM AND FR68+63.5 MM, Y1242.5 IAW A319 SRM TASK 53-41-14-300-001. (12342SDR DALA2025100607242Floor Support · corroded(LOG 1234689) CORROSION ON FLOOR SUPPORT STA 800,809,843 BETWEEN S26R TO DOOR JAMB (BILGIE AREA) CARGO COMPARMENT C2. CARGO COMPARMENT C2 WAS FABIRCATED AND REPLACED PER DWG 146A8128 REV. B AND B737-800 SRM 51-40-02-0G.SDR DALA2025100607240Shield · corroded(LOG 1234618) CORROSION ON RH SHIELD BTW STA 847 TO 867 BTW STRG 25R/26R AT AFT CARGO COMPARMENT. RH SHIELD BTW STA 847 TO 867 BTW STRG 25R/26R AT AFT CARGO COMPARMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR FDEA202510041887Web · crackedMAIN DECK UNDERFLOOR WEB CRACKED AT FR47 BETWEEN -Y953 AND -Y1456 REPLACED THE CRACKED WEB ON MAIN DECK UNDERFLOOR AT FR47 BETWEEN -Y953 AND -Y1456 WITH FABRICATED PART PER A300-600F SRM51-40-21 AND DWG: A53832103(ISSUE: E). THIS IS CATEGORY A REPAIR. MAJORSDR FDEA202510041886Web · crackedMAIN DECK UNDERFLOOR WEB CRACKED AT FR47 BETWEEN Y953 AND Y1456. REPAIRED THE CRACKED WEB ON MAIN DECK UNDERFLOOR AT FR47 BETWEEN Y953 AND Y1456 PER A300-600F SRM53-15-15-201-C2. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER SRSDR CALA2025100609658Floor Support · corrodedFLOOR STRUCTURE PANEL SUPPORT AT STA 312-4" RBL12" IS CORRODED AT BOLT HOLE. REMOVED AND INSTALLED NEW FLOOR PANEL SUPPORT AT STA 312-4" RBL 12" PER SRM 51-40-02-0G-0 AND DWG 141A5410SDR SWI2025F01862Floor Support · corrodedEXFOLIATING CORROSION FOUND ON RH PRESSURE FLOOR SILL STRAP AT FS559.00, WL73.00 BETWEEN RBL36.00 AND RBL45.00. REMOVED AND REPLACED THE RH PRESSURE FLOOR SILL STRAP AT FS559.00, WL73.00 BETWEEN RBL36.00 AND RBL45.00 IN REFERENCE WITH THE SRM 53-41-43 AND SRMSDR SWIA202512221003Floor Support · corrodedDURING INSPECTION AND CORROSION REMOVAL OF THE LH PRESSURE FLOOR SILL ASSY, FOUND 2 CRACKED NUTPLATE HOLES ON LH PRESSURE FLOOR SILL ASSY APPROX. FS 449.85 - FS 461.50 IN BETWEEN LBL 36.00 - 45.00. (C-CHECK RO 12/19/2025)PERFORMED REPAIR OF LH PRESSURE FLOOR SDR SWIA20251124003Floor Support · corrodedRIGHT FLOOR SUPPORT RBL 9 HAS CORROSION APPROXIMATELY BETWEEN BS 501 TO BS 565. REPAIRED THE FLOOR SUPPORT IAW REO 670-53-31-1112 REV -. TASK CARD 51-900-1002-SKY.SDR SWAA2025110521056Support Bracket · crackedCRACK SUPPORT BRACKET LOCATED BS540 AT LEVEL RBL 6 AT RT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET AND FASTENERS LOCATED BS540 AT LEVEL RBL 6 AT RT AIR CONDITIONING BAY IAW SRM 51-10-02 Ï¿½TEM 9; 51-40-02 AND DWG:212A1116 SHEET:1.SDR SWAA2025110520966Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABINREPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO 3R AT PASSENGER CABIN IAW B737-800 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 146A7901 SHEET:66 REV:A.SDR SWAA2025110521063Support Angle · crackedCRACK SUPPORT ANGLE LOCATED BODY STA 663.75 AND LBL 10 AT AIR CONDITIONING BAY. REPLACED SUPPORT ANGLE IAW SRM 51-10-02; SRM 51-40-02. AND DRAWING 111A1000; SHEET 31; REV A.SDR SWAA2025110521062Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BODY STA 663.75 RBL 35 AT AIR CONDITIONING BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02; SRM 51-40-02 AND DRAWING 111A1000; SHEET 31; REV A.SDR SWAA2025110520967Support Angle · crackedCRACK ON SUPPORT ANGLE BTW BS 380 - 400, LBL 13, WL 208.1. REPLACED SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, DWG 143A5400, SHEET 138, REV -, & DWG 143A5400, SHEET 142, REV -.SDR SWAA2025110520965Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 52 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 52 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-01, DWG 143A5400, SHEET 14, REV -, & DWG 143A5400, SHEESDR SWAA2025110520968Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 39 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 39 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-02; DWG 143A5400; SHEET 140; REV- AND DWG 143A5400, SHEESDR SWAA2025110321085Support · corrodedCORROSION SUPPORT ZEE BETWEEN BS 727 - 767, S25R, WL 156. REPLACED SUPPORT ZEE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 146A7500, SHEET 113, REV-, AND DWG 146A7502, SHEET 49, REV-.SDR SWAA2025110331271Support · corrodedCORROSION SUPPORT ZEE BETWEEN BS 727 - 767, S25R, WL 156. REPLACED THE SUPPORT ZEE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 146A7500, SHEET 113, REV-, AND DWG 146A7502, SHEET 49, REV-.SDR SWAA2025103021090Web · crackedCRACK WEB CEILING AREA, BS 847 TO 867, LBL 19, AFT CARGO BAY. REPLACED WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 149A8100, SHEET 1 REV -.SDR SWAA2025103021086Shield · corrodedCORROSION SHIELD WEB FLOOR STRUCTURE BS 767 TO 794.5, S25R, WL156, AFT CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS IAW SRM 51-10-02, ITEM 9, AND INSTALLED FASTENERS IAW SRM 51-40-02, AND DRAWING 146A0081, SHEET 37, REV -.SDR SWAA2025103020975Support Bracket · crackedCRACKED SUPPORT BRACKET, BS 947.5, LBL 10 IN THE AFT CARGO COMPARTMENT. REPLACED SUPPORT BRACKET AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 149A8103, SHEET 7, REV A.SDR SWAA2025103020977Angle · crackedCRACK ANGLE LOCATED BS 867, LBL 10 IN THE AFT CARGO COMPARTMENT. REPLACED ANGLE LOCATED BS 867, LBL 10 IAW SRM 51-10-02, ITEM 9, AND INSTALLED FASTENERS IAW SRM 51-40-02, AND DRAWING 149A8102, SHEET 17, REV-. MEASUREMENT OF CRACK IS 0.550 INCH.SDR IPXA2025101379065Angle · crackedAVIONICS COMPARTMNT FR9 ANGLE CRACKED AT Y950. FABRICATED AND DRILLED NEW ANGLE FITTING FROM 2024-T3 .063C", B/N:0004276732. IAW SRM 53-12-15 FIG.7ITEM #80 AND UPS GMM-09.08.01.03, FOLLOW #4. INSTALLED NEW ANGLE FITTING IAW SRM 51-40-21.SDR SWAA2025102721109Support Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED STA695 AND LBL24.75 PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON FLOOR STRUCTURE IAW SRM 51-40-02-0G-0, & DWG 273A9111, SHEET 6, REV A, AND DWG 111A6000, SHEET 178, REV-.SDR IPXA2025101379032Angle · crackedAVIONICS COMPARTMNT FR9 ANGLE CRACKED AT -Y950 JP-110. REMOVED WEB CRACKED RH SIDE IAW A300/600 SRM 51-40-21. INSTALLED NEW ANGLE FITTING IAW A300-600 SRM 51-40-21.SDR AALA202510237549Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT STA 312, LBL 43. REPLACED INTERCOSTAL PER AARD 51-00-05-1.SDR AALA202510237031Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT STA 312, LBL 10. REPLACED INTERCOSTAL PER AARD 51-00-05-1.SDR AALA202510201195Web · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE WEB AT BS 990, LBL 37. REPAIRED WEB PER EA 368782.SDR IPXA2025101571181Floor Support · corrodedMAIN CABIN COMPARTMENT FLOOR STRUCTURE, BS 1720, LBL 25 HAS (1EA) PLATE EXFOLIATED. REMOVED PLATE 1 EA AT MAIN CABIN COMPARTMENT FLOOR STRUCTURE STA 1720 LBL 25 IAW B757-200 SRM 51-40-02. INSTALLED NEW ANGLE FROM MAIN CABIN COMPARTMENT FLOOR STRUCTURE, STA 17SDR AALA202510152986Fitting · damagedAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLES ON RIGHT AFT PASSENGER / CREW DOOR CUT OUT LOWER CENTER FITTING BETWEEN FR 66 AND FR 68 AT S23R. REPLACED CENTER FITTING PER SRM 51-42-11.SDR DALA2025101307482Strap · corrodedCORROSION ON AFT LAV SUPPORT STRUCTURE STRAP. REPLACED STRAP REF BAC DWG 146T3244 (1232946)SDR DALA2025101307489Stiffener · corrodedCORROSION ON AFT LAV PAN SUPPORT STRUCTURE RH STIFFNER PT# 146T3248-2. REPLACED STIFFNER REF BAC DWG 146T3244 (1232945)SDR DALA2025101307488Stiffener · corrodedCORROSION ON AFT LAV PAN SUPPORT STRUCTURE LH STIFFENER PT # 146T3248-1. REPLACED STIFFENER REF BAC DWG 146T3244 (1232943)SDR DALA2025101307487Stiffener · corrodedCORROSION ON AFT LAV SUPPORT STRUCTURE 2EA STIFFENER SUPPORTS PN 146T3259-1. REPLACED SUPPORTS REF BAC DWG 146T3244 (1231990)SDR DALA2025101307485Angle · corrodedSHIP 185 CORROSION ON AFT LAV PAN SUPPORT STRUCTURE "L- ANGLE" PT # 146T0207-2. CORRECTIVE ACTION: REPLACED ANGLE REF BAC DWG 146T3244 (1232941)SDR AALA202510139781Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM BS 277 TO BS 294.5 AT RBL 2. REPLACED INTERCOSTAL PER AARD 51-00-05-1.SDR AALA202510078435Shield · corrodedAIRCRAFT WAS GROUNDED: CORROSION ON AFT CARGO COMPARTMENT SHIELD BETWEEN BS 767 AND BS 787 AT S25L. REPLACED SHIELD PER AARD 51-00-05-1.SDR AALA202510064945Splice · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT GALLEY AREA INBOARD UPPER SPLICE AT FR 68 AND +Y1162. REPLACED SPLICE PER SRM 51-42-11.SDR CALA2025100609650Floor Support · corrodedMAIN CABIN AFT WET AREA CORROSION AT FLOOR SUPPORT STA 986.5+7" RBL 38". INSTALLED FLOOR SUPPORT AT AFT WET AREA STA 986.5 +7 RBL 38" IAW SRM 51-40-02-0G-0 AND DWG 147A5700.SDR CALA2025100609649Web · corrodedMAIN CABIN AFT WET AREA CORROSION AT FLOOR WEB STA 986.5+2" LBL 34". REMOVED AND REPLACED WEB AT LT AFT WET AREA BETWEEN STA 986.5" TO STA 1016" PER B737-800 SRM 51-40-02-0G-0 AND DWG 147A8501 AND DWG 147A5700.SDR CALA2025100609645Fitting · corrodedTORSION-BOX COVER SHEET AT FR58 AFT COVER SHEET SUPPORT FITTING HAS CORROSION ON LOWER SURFACE. REMOVED AND REPLACED SUPPORT FITTING AT AFT CARGO DOOR TOSION BO X COVER SHEET FR 58 IAW A319 SRM 51-42-11-001.SDR 2025FA0000679Support Angle · corrodedDURING A FUSELAGE EXTERIOR INSPECTION FOUND CORROSION AND THE SUPPORT ANGLE BELOW THE AFT ENTRY DOOR THRESHOLD AROUND THE FASTENER NUTPLATES.
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