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 AALA202604131323Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT FORWARD SIDE OF STA 500G, AT RBL 23. REPLACED BAFFLE CLIP PER AARD 51-00-05-1.SDR AALA202604135698Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT AFT SIDE OF STA 500G, AT RBL 23. REPLACED BAFFLE CLIP PER AARD 53-00-01-6.SDR DALA2026041302316Web · corrodedCORROSION WEB LOCATED AT FR 20 LEVEL STR 23L AT FWD GALLEY AREA. REPLACED WEB LOCATED AT FR 20 LEVEL STR 23L AT FWD GALLEY AREA AS PER A320 SRM 51-72-11, SRM 51-42-11 AND DWG D53112545 RELEASE DATE 30-JUN-98 ISSUE: F00 AND DWG D53114392 RELEASE DATE: 01- FEB-SDR DALA2026041202305Floor Support · corrodedCORROSION FLOORBEAM +Y765 LOCATED BTW FR 67 TO FR 68 AT AFT GALLEY A REA (SSI 534147). REPLACED FLOOR BEAM Y765 LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AREA AS PER A320 SRM 51-72-11; A320 SRM 51-42-11 AND DWG D53472815 RELEASE DATE 18-DEC-06. ISSUE G. MEASURSDR IPXA2026051230823Floor Support · crackedAFT CARGO DOOR SILL FLOOR SUPPORT BETWEEN C60 AND C61 HAS CORROSION. SILL FLOOR SUPPORT AFT CARGO ENTRANCE REMOVED AND REPLACED IAW A300-600F SRM 51-72-10-001.SDR SWAA2026051188148Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 51 WL 208.1 AT PASSENGER CABIN REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 51 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02 AND DWG 143A5400 SHEET 183 REV -.SDR SWAA2026051197570Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 51 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 51 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-02 AND DWG 143A5400 SHEET 183 REV -.SDR SWAA2026051188150Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 40 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 40 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02 AND DWG 143A5400 SHEET 140 REV -.SDR SWAA2026051197571Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 40 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 40 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02 AND DWG 143A5400 SHEET 140 REV -.SDR SWAA2026051188146Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENER LOCATED BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-02-0G; SRM 51-10-02-0G-0 AND DWG 143A5400 SHEET 154 REV - MESDR SWAA2026051197572Support Angle · crackedCRACKED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENER LOCATED BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-02-0G; SRM 51-10-02-0G-0 AND DWG 143A5400 SHEET 154 REV - MEASSDR SWAA2026051188147Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-02 AND DWG 143A5400 SHEET 184 REV -.SDR SWAA2026051197573Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-02 AND DWG 143A5400 SHEET 184 REV -.SDR SWAA2026051188149Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 500I TO BS 520 BL 0 WL 208.1 AT PASSENGER CABIN. REPLACED NEW SUPPORT ANGLE LOCATED BTW BS 500I TO BS 520 BL 0 WL 208.1 AT PASSENGER CABIN AND FASTENER IAW SRM 51-40-02-0G; SRM 51-10-02-0G-0 AND DWG 143A5400 SHEET 115 REVSDR IPXA2026041036299Stiffener · crackedSTIFFENER BETWEEN FRAMES 38.1-38.2 R/H SIDE WITH CRACK. INSTALLED FLOOR ANGLE AT MAIN CABIN FR38.1 TO FR38.2 IAW SRM 51-40-21-001 AND REMOVED PROTECTION ELECTRICAL (EWIS) IAW ESPM 20-54-50-02. REPLACED STIFFENER IAW SRM 51-40-21-001.SDR IPXA2026050536213Stiffener · crackedSTIFFENER BETWEEN FRAMES 37-38 R/H SIDE WITH CRACK. REPLACED STIFFENER BETWEEN FRAME 37-38 R/H IAW SRM 51-40-21-001.SDR SCNA20260508189Floor Support · crackedCRACKED PASSENGER FLOOR SUPPORTS (2 EAS) ON STA 540, BTW RBL 2 & LBL 2 WNG BOX AREA. (PAX CAB) - - NEW FLOOR SUPPORTS (2 EAS) ON STA 540, BTW RBL 2 & LBL 2 WNG BOX AREA. (PAX CAB) WERE REPLACED PER B737-800 SRM 51-40-02-0G-0SDR IPXA2026042936056Web · crackedWEB BETWEEN FRAME 79-80 L/H SIDE WITH CRACK. INSTALLED NEW WEB. LT MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR 79-80: I.A.W. A300-600 SRM 51-40-21-001.SDR REXA2026050700524Angle · corrodedCORROSION ON ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR WERE EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 THEREFORE WERE REPLACED PER CRJ900 SSDR REXA2026050700523Angle · corrodedCORROSION ON ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR WERE EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 THEREFORE WERE REPLACED PER CRJ900 SSDR REXA2026050700521Angle · corrodedCORROSION ON ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR WERE EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 THEREFORE WERE REPLACED PER CRJ900 SSDR REXA2026050700520Angle · corrodedCORROSION ON ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR WERE EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 THEREFORE WERE REPLACED PER CRJ900 SSDR REXA2026050700518Angle · corrodedCORROSION ON LOWER SILL ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR. CORROSION ON LOWER SILL ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR WAS REMOVED PER SRM 51-21-06-001-001-A01 EVALUATED OUT OF LIMITS PER CRSDR REXA2026050700517Angle · corrodedCORROSION ON LOWER SILL ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR. CORROSION ON LOWER SILL ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 EVALUATED OUT OF LIMITSDR REXA2026050500468Plate · wornWEAR ON FLAP FITTINGS AND PLATE SUPPORTS OF STUB FAIRINGS 171DL AND 172DR AT MLG WHEEL WELL FLAP FITTINGS AND PLATE SUPPORTS OF STUB FAIRINGS 171DL AND 172DR AT MLG WHEEL WELL WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 AND SRM CRJ-900 51-41-02-001-001-SDR REXA2026050500467Plate · wornWEAR ON FLAP FITTINGS AND PLATE SUPPORTS OF STUB FAIRINGS 171DL AND 172DR AT MLG WHEEL WELL FLAP FITTINGS AND PLATE SUPPORTS OF STUB FAIRINGS 171DL AND 172DR AT MLG WHEEL WELL WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 AND SRM CRJ-900 51-41-02-001-001-SDR REXA2026050500466Fitting · wornWEAR ON FLAP FITTINGS AND PLATE SUPPORTS OF STUB FAIRINGS 171DL AND 172DR AT MLG WHEEL WELL FLAP FITTINGS AND PLATE SUPPORTS OF STUB FAIRINGS 171DL AND 172DR AT MLG WHEEL WELL WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 AND SRM CRJ-900 51-41-02-001-001-SDR REXA2026050500465Fitting · wornWEAR ON FLAP FITTINGS AND PLATE SUPPORTS OF STUB FAIRINGS 171DL AND 172DR AT MLG WHEEL WELL FLAP FITTINGS AND PLATE SUPPORTS OF STUB FAIRINGS 171DL AND 172DR AT MLG WHEEL WELL WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 AND SRM CRJ-900 51-41-02-001-001-SDR HNAA2026050500368Floor Support · corrodedDURING INSPECTION OF DENT ON LH WINDOW #5 FOUND CORROSION FOUND ON RT FLOOR SILL BETWEEN FR 33 - 34, STGR 15 R. REMOVED AND REPLACED WITH NEW RH FLOOR SILL BETWEEN FR 33-39 STR 15R IAW EMB 145 SRM 51-40-02-PRSDR HNAA2026050500367Floor Support · corrodedDURING INSPECTION OF DENT ON CABIN WINDOW LH SIDE #5 FOUND CORROSION FOUND ON LH FLOOR SILL BETWEEN FR 27 - 28. STGR 15L. REMOVED AND REPLACED WITH NEW LH FLOOR SILL BETWEEN FR 27- FR 28 IAW EMB 145 SRM 51-40-02-PRSDR IPXA2026043042646Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR STRINGER HAS CORROSION APPROX BTW BS 1445 AND BS 1497.5, RBL 10.45. REMOVED 1EA DAMAGED FLOOR STRINGER IN AFT CARGO COMPARTMENT BTW BS 1445 AND BS 1497.5, RBL 10.45 IAW SRM 51-40-02-0G-0. INSTALLED NEW REPLACEMENT STRINGER AT AFT CASDR IPXA2026043042676Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR STRINGER HAS CORROSION APPROX BTW BS 1445 AND BS 1497.5, LBL 7.55. REMOVED 1EA DAMAGED FLOOR STRINGER IN AFT CARGO COMPARTMENT BTW BS 1445 AND BS 1497.5, LBL 7.55 REF SRM 51-40-02-0G-0. INSTALLED NEW REPLACEMANT STRINGER AT BTW BS SDR IPXA2026042636124Web · crackedWEB BETWEEN FRAMES 73-74 L/H SIDE WITH CRACK. INSTALLED NEW WEB AT FRAMES 73-74 L/H: IAW SRM 51-40-21-001.SDR AALA202604239948Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-72-11.SDR IPXA2026042142676Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR STRINGER HAS CORROSION APPROX BTW BS 1445 AND BS 1497.5, LBL 7.55,SDR IPXA2026041742646Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR SUPPORT HAS CORROSION APPROX BTW BS 1445 AND BS 1497.5, RBL 10.45SDR CALA2026041515372Web · dentedFOUND LARGE DENT FLIGHT COMPARTMENT FLOOR LBL 15 STA 259. REPAIRED FLIGHT COMPARTMENT FLOOR STRUCTURE WEB APPROX STA 259 LBL 15 AS PER SRM 53-10-51-2R-2.SDR UIEA2026030200074Channel · crackedCRACK FOUND ON LT OF TENSION TIE FWD CHANNEL AT FS 720. REPAIRED LT TENSION TIE AT BS 720 PER SRM 53-20-30-R2-2 REPAIR 2. NO FURTHER DEFECTS NOTED.SDR DALA2026041302337Pan · damagedSECTION I REPAIR TO AFT LAVATORY SERVICE PANEL PAN REQUIRES PART REPLACEMENT PER SECTION II OF ERA 633530-14. (FUSELAGE / ACCESS COVERS / AFT LAV SERVICE PANEL PAN / STA 1681 - STA 1701, S-26R & S-29R / CRACKS). CORRECTIVE ACTION: REF ERA 633530-14. (1537629) SDR DALA2026041002293Structure · corrodedFOUND MID AFT M16 LAV ENDWALL CORROSION AT AFT LOWER SURFACE. REPLACED MID AFT M16 LAV ENDWALL AT AFT LOWER SURFACE AS PER ER/ A 633262-14 (1537386) (AIRCRAFT GROUNDED)SDR 2026F00070Angle · crackedREPAIRED CRACKED CLIP INSIDE EQUIPMENT BAY ON RH SIDE OF CANTED BULKHEAD PER AQRD ERO-988018, REV. IR, TITLED "N317QS- TAILCONE CANTED BULKHEAD RH CLIP CRACKS", DATED APR 06, 2026. F&DT EVALUATION DUE DATE: MAR 31, 2027. NOTE 1: THE FATIGUE AND DAMAGE TOLERANCSDR IXXA20260410001Strap · crackedWHILE PREFORMING INSP AT STA. 1725.5 OF BULKHEAD OUTER CHORD STRAP FOUND CRACK AT STRINGER 6R INTERNAL FWD OF APU INTAKE DOORSDR SCNA20260508188Angle · crackedCRACK ON ANGLE OF VAPOR BARRIER STA 663 AND RBL 2 AT MLG WHELL WELL. - - ANGLE OF VAPOR BARRIER STA 663 AND RBL 2 AT MLG WHELL WELL WAS REPLACED PER B737-800 SRM 51-40-02-0G-0.SDR ASAA2026040965745Shield · corrodedMULTIPLE SPOTS OF CORROSION ON THE SHIELD ON THE RIGHT HAND SIDE OF THE AFT CARGO PIT BETWEEN STATIONS 767 AND 787,18 INCHES FROM THE BUTT LINE. GROUNDED - YES. REMOVED CORROSION FROM THE AFT PIT, FWD SHIELD FROM STA 767 TO 787 IAW B737-800 SRM 53-60-15-1A-1.2SDR R61A2026042600113Doubler · corrodedWHILE IN HEAVY CHECK - LT COCKPIT FLOOR DOUBLER HAS MULTIPLE AREAS OF CORROSION AND MISSING SURFACE PROTECTION. PERFORMED REPAIR SPLICE OF LT COCKPIT FLOOR DOUBLER IAW SRM 53-10-10 R07SDR R61A2026042600112Doubler · corrodedWHILE DURING HEAVY CHECK - RT COCKPIT FLOOR DOUBLER HAS CORROSION AND SURFACE PROTECTION MISSING IN MULTIPLE AREAS. PERFORMED REPAIR SPLICE OF RT COCKPIT FLOOR DOUBLER IAW SRM 53-10-10 R07.SDR MASA20260420095Doubler · corrodedDURING HEAVY CHECK, INSPECTIONS OF THE INTERANAL FWD FUSE, FLOOR SUPPORT STRUCTURE, DOUBLER AT FR 16, LBL 11, CORROSION AT ANCHOR NUT HOLE BLENDED IAW SRM 51-10-03, MAX MATRL REMOVED .002. WITH IN LIMITS IAW SRM 53-10-10, ALLOWABLE LIMITS, FIG 101, SHT 4 10X MSDR MASA20260420087Shear Plate · corrodedDURING HEAVY CHECK, INSPECTIONS OF THE INTERANAL FUSELAGE STRUCTURE AT CFIII, CORROSION FOUND ON R/H SHEAR PLATE, BETWEEN FR 87 AND FR 88 R/H REPLACED IAW ERJ 175 SRM 51-41-02, REV# 45, MAY-28-2021. NRC # 4502583-1000-0056.SDR IPXA2026041121387Profile · corruptedTEE PROFILE AT FRAME 80 RT CORNER WITH CRACK. REMOVED AND REPLACED TEE PROFILE.SDR DALA2026041402342Web · corrodedCORROSION ON RT FLOOR CUPS WEB AREA (UPPER/ LOWER SURFACES) STA 256 BTW-X =55.5 -X=44.5 APROX AT PAX CABIN. REPAIRED IAW SRM 53-00-55-2R (1536178) (AIRCRAFT GROUNDED)
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