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 IPXA2026051573404Bracket · crackedFWD CARGO COMPARTMENT AFT BULKHEAD LT LINNING UPPER SUPPORT BRACKET AT Y953 IS CRACKED. REMOVED BRACKET AT FR 38.2 Y953 IAW A300 SRM 51-40-21. INSTALLED NEW BRACKET AT FR 38.2 Y953 IAW A300 SRM 51-40-21-001.SDR IPXA2026043075328Plate · corrodedFAULT-STR-ZONE 200. LH MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR21 Y0-Y450 METAL RIVETED FLOOR PANEL HAS CORROSION. REMOVED CORROSION AT LH MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR21 Y0-Y450 METAL RIVETED FLOOR PANEL, ORIGINAL THICKNESS IS .129", MATERIAL LOSDR SWAA2026051289001Panel · delaminatedPANEL 194CL HAS DELAMINATION DAMAGE. REPAIRED IAW SRM 51-70-05-2R-2-B00319, REPAIR 2. REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH (12.70 MM) IN DIAMETER TO ONE SKIN AND THE HONEYCOMB CORE .SDR IPXA2026042973327Adapter · corrodedMDC FLOOR STR, FROM FR 23 TO FR 27, Y0, R/H BASE CLS ADAPTER TRACK AND CLS ADAPTERS, 6 SPOTS WITH CORROSION. DOT 73-125. REMOVED MINOR CORROSION AT - Z200 - MDC FLOOR STR, FROM FR 24 TO FR 27, Y0, R/H BASE CLS ADAPTER TRACK AND ADAPTER IAW A300-600 SRM 51-74-1SDR DALA2026041702447Cusp Web · crackedAFTER CRACK REMOVAL ON CUSP WEB STA Y=655-684 RH SIDE, AT PASSENGER COMPARTMENT. REPAIRED PER B717-200 SRM 53-00-55 (1542990) (AIRCRAFT GROUNDED)SDR DALA2026041702446Cusp Web · corrodedCORROSION ON RH FLOOR CUPS WEB AREA (UPPER/ LOWER SURFACES) STA 229, BTW-X =55.5 -X=44.5 APROX AT PAX CABIN. REPAIRED PER B717-200 SRM 53-00-55 (1542943) (AIRCRAFT GROUNDED)SDR CALA2026041515376Channel · corrodedFWD CARGO COMPARTMENT LT ZEE CHANNEL POSSIBLE CORROSION BTW STA 500C TO STA 500E. REMOVED AND REPLACED LT ZEE CHANNEL FWD CARGO COMPARTMENT BTW BS 500C TO 500E IAW SRM 53-00-53-2R-6.SDR AALA202604143132Channel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT ZEE CHANNEL BETWEEN STA 500 AND STA 500I AT LBL 23. REPLACED ZEE CHANNEL PER SRM 51-40-02.SDR AALA202604143012Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL FROM STA 727 TO STA 727E AT S24L. REPLACED TRANSITION PANEL PER SRM 51-40-02-0G.SDR CALA2026041415345Channel · corrodedFWD CARGO COMPARTMENT RH- Z CHANNEL POSSIBLE CORROSION BTW STA 500A TO STA 500I. REMOVED AND REPLACED RH- Z CHANNEL ON FWD CARGO COMPARTMENT BTW STA. 500A TO STA. 500I. IAW B737-800 SRM 53-00-53-2R-6.SDR N6WA2026041305Intercostal · corrodedCORROSION FOUND ON INTERCOSTAL UNDER SERVICE DOOR BETWEEN FS 310-FS 349. INSTALLED NEW INTERCOSTAL UNDER SERVICE DOOR BETWEEN FS310-FS349, IAW CRJ SRM 51-42-06 AND CRJ SRM 51-42-21.SDR SWIA2026041276857Cap · crackedRIGHT WING WHEEL WELL, FIRST BATT RIB IN MLG CUTOUT CRACKED AT TWO LOCATIONS. REMOVED AND INSTALLED NEW SERVICEABLE CAP ON R/H WING WHEEL WELL, FIRST BATT RIB IN L/G CUTOUT IAW CRJ 200 SRM 51-42-21.SDR SWIA2026041276854Channel · crackedLEFT MLG WHEEL WELL, SECOND BATT RIB OTBD, BRACKET CRACKED ON FWD END OF RIB. PERFORMED A MAJOR REPAIR BY REPLACING 2ND BATT RIB CHANNEL , AND ATTACHING ANGLES, OTBD IN LT MLG WHEEL WELL. IAW SRM 51-40-11, 51-42-21, & 51-42-06 COMPLETED SKYWEST RII TASK CASDR SWIA2026041276298Floor Support · corrodedPASSENGER DOOR FLOOR SILL ANGLE BETWEEN BS 310 TO BS 349 HAS MULTIPLE SPOTS OF CORROSION. INSTALLED NEW MID CAP ANGLE TO PAX DOOR LOWER SILL ANGLE REF DWG. SH670-31810 REV AE, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01.SDR VNAA202606120061Stiffener · corrodedCORROSION ON ANGLE BTW STGR 25LH/25RH AT BTW 55.265% AND 67.50 % SPAR DATUM. ANGLE (STIFFENER) BTW STGR 25LH/25RH AT BTW 55.265% AND 67.50 % SPAR DATUM WAS REPLACED PER SRM 51-42-06-001-001-A01.SDR HNAA2026052000391Floor Support · corrodedRIGHT FLOOR SILL 3 HAVE CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED RT FLOOR SILL 3 IAW SRM 51-40-02.SDR HNAA2026052000390Floor Support · corrodedLEFT FLOOR SILL 4 HAVE CORROSION IN MULTIPLE AREAS. R & R LT FLOOR SILL 4 IAW SRM 51-40-02.SDR HNAA2026052000389Floor Support · corrodedLEFT FLOOR SILL 6 HAVE CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED LT FLOOR SILL 6 IAW SRM 51-40-02.SDR HNAA2026050500377Bracket · crackedCRACKED BRACKET IN ZONE 155 JUST AFT OF PANEL 155BZ THAT HOLDS SYSTEM 1 PRESSURE AND RETURN HYDRAULIC TUBES. REMOVED AND REPLACED WITH NEW BRACKET IN ZONE 155 JUST AFT OF PANEL 155BZ IAW SRM 51-40-02-PR.SDR ASAA2026041265822Support · corrodedFWD PIT LOWER AFT BULKHEAD SUPPORT MIDDLE PIECE IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED FWD PIT LOWER AFT BULKHEAD SUPPORT MIDDLE I.A.W. B737-800 SRM 51-40-02-0G-0 STEP 4.B AND 7.CW- 1" O- .063" R- 0" L- 2" D- .063".SDR ASAA2026041265821Web · crackedFWD PIT SILL WEB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED FWD PIT SILL WEB IAW B737-800 SRM 51-40-02-0G-0W: 1" O: .045" R: .039" L: 2" D: .006".SDR ASAA2026041265813Web · corrodedAFT PIT SILL WEB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED AFT PIT SILL WEB IAW B737-800 SRM 51-40-02-0G-0W: 1" O: .050" R: .043" L: 2" D: .007.SDR ASAA2026041265808Plate · corrodedAFT PIT L/H SIDEPLATE HAS CORROSION AT STA 727-747. GROUNDED - YES. REMOVED AND REPLACED AFT PIT L/H SIDEPLATE FROM STA 727 TO 747 IAW BOEING SRM 53-00-53-2R-5WI: 1" OT: 0.040" RT: 0.027" L: 0.013" D: 0.007".SDR AALA202604302016Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON INTERCOSTAL FITTING LOCATED AT LEVEL DOOR STOP N7 ON FR 16RH AT FWD GALLEY AREA. MEASURE IS D=0.087 INCH. MAINTENANCE REPLACED INTERCOSTAL FITTING AND FASTENERS LOCATED AT LEVEL DOOR STOP #7 AT FR16 RH SIDE IAW A31SDR IPXA2026042468432Floor Support · brokenFAULT-STR-ZONE 200 MAIN CABIN DECK, FLOOR SUPPORT STRUCTURE LH SIDE NEXT TO FLOOR SUPPORT Y-1959 BTW FR12A AND FR14 WITH A BRACKET BROKEN DOT 53-118. REMOVED DAMAGE BRACKET ON MAIN CABIN DECK, AT FLOOR SUPPORT STRUCTURE R/H SIDE NEXT TO FLOOR SUPPORT Y-1959 SDR IPXA2026042162642Fitting · chafedFOUND L1 ENTRY DOOR CUTOUT AFT LOWER FITTING CHAFING. REQUEST PERFORM OK TO CLOSE CHECK FOR L1 DOOR AFT SIDE LOWER SIDEWALL PANEL.SDR MASA20260420094Doubler · corrodedDURING HEAVY CHECK INSPECTIONS ON FWD FUSE FLOOR STRUCTURE, CORROSION FOUND ON RH DOUBLER B ETWEEN FR 12-14. RH DOUBLER BETWEEN FR 12-14 REMCVEJ AND REPLACED IAW SRM 51-41-02 AND 51-43-03 REV 46 DEC 03/21 MR YQG NRC4502583-2000-0162SDR DALA2026041402365Cusp Web · crackedCRACK ON CUSP WEB BTW STA Y= 715/719 AND BTW STA X= 44/46 WING BOX AREA AT C. PAX . CUSP WEB BTW STA Y= 715/719 AND BTW STA X= 44/46 WING BOX AREA AT C. PAX WAS REPAIRED PER SRM 53-00-55-2R REPAIR 4 FIGURE 221. (1541206) (AIRCRAFT GROUNDED)SDR DALA2026041402356Support Fitting · corrodedWHILE PREPARING FOR CIC IN ZONE 240, CORROSION WAS FOUND ON THE LAV E SUPPORT FITTING (REF. A220 ASRP 53-61-43-06AAA-041A-A ITEM 24). COMPLIED WITH ER/A 633268-14 PRI REV 0, REV1, REV2 AND FINAL ER/A 633268- 14 REV ORIGINAL. (LP# 1541085)SDR HNAA2026052000386Floor Support · corrodedLEFT FLOOR SILL 7 AROUND NUT-PLATES HOLES HAVE CORROSION. REMOVED AND REPLACED LT FLOOR SILL 7 IAW SRM 51-40-02.SDR SWAA2026051289397Scuff Plate · crackedACD AFT CORNER SCUFF PLATE CRACKED. REMOVED AFT CORNER SCUFF PLATE IAW AMM 53-11-02-020-801. REMOVED AND REINSTALLED ACD AFT CORNER SCUFF PLATE IAW AMM 53-11-02-020-801 AND AMM 53-11-02-420-801.SDR IPXA2026050659214Support Bracket · gougedLEFT MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR 70 Y450 BEAM LOWER SUPPORT BRACKET GOUGED. REMOVED AND REPLACED LOWER SUPPORT AT ZONE 200. LT MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR 70 Y450 IAW A300-600 SRM 51-40-21-001.SDR IPXA2026050255146Angle · crackedAVIONIC COMPARTMENT FR C10 L\H- Y1456 FWD UPPER ANGLE CRACKED. REMOVED AND REPLACED ANGLE P/N A53612356200, B/N 0004482008 AT AVIONIC COMPARTMENT FR10 L/H Y1456 FWD UPPER IAW SRM 51-40-21-001.SDR IPXA2026050255069Angle · crackedAVIONIC COMPARMENT FR C10 L\H -Y1456 AFT UPPER ANGLE CRACKED. REMOVED ANGLE AT AVIONIC COMPARMENT FR 10 L/H Y1456 AFT UPPER IAW SRM 51-40-21-001. INSTALLED NEW ANGLE P/N UPA53612218200 AT AVIONIC COMPARMENT FR 10 L/H Y1456 AFT UPPER IAW SRM 51-40-21-001.SDR IPXA2026042359094Web · crackedLEFT MAIN CABIN FLOOR STRUCTURE FR 78 LT OTBD WEB IS CRACKED. INSPECTED THE INSTALLATION OF NEW WEB ASSY. INSTALLED NEW WEB AT FR 78 LT OTBD IAW SRM 51-40-21-001.SDR REXA2026050400422Buttstrap · corrodedCORROSION ON JOIN APPROX BS 280 BTW RBL25-LBL25 AT PASSENGER CABIN. CORROSION ON JOIN APPROX BS 280 BTW RBL25-LBL25 AT PASSENGER CABIN WAS REPAIRED PER REO 690-53-21-2118 REV. - -SDR IPXA2026041353887Strap · corrodedCORRODED EXISTING FILLER REPAIR AT FS 1825 RBL 3R TO 6R EXISTING MIDDLE STRAP REPAIR ON APU AIR INTAKE INLET CUTOUT AFT STRAP. REMOVE THE EXISTING REPAIR OF APU INLET DOOR MIDDLE STRAP P/N: 148N3138-8000 INSTALLED AT STA 1825 BETWEEN S-3R AND S-6R AND ACCOMPLISDR IPXA2026042959026Floor Support · crackedLEFT MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR 78-79 O/B Z-PROFILE HAS (2EA) CRCKS. Z-PROFILE WAS REMOVAL STR-ZONE 200. LH MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR 78-79 O/B I.A.W A300-600 SRM 51-40-21. INSTALLED NEW Z-PROFILE AT ZONE 200, LH MAIN CABIN COMSDR IPXA2026042759042Profile · crackedMDC FLOOR S, FR 74, -Y2127.5, Z PROFILE WITH CRACK. REMOVED Z-PROFILE FROM MDC FLOOR STR, AT FR74, -Y2127.5 RT IAW SRM 51-40-21. INSTALLED NEW Z PROFILE AT Z200 - MDC FLOOR STR, FR 74, -Y2127.5, IAW SRM 51-40-21-001.SDR IPXA2026041355642Intercostal · corrodedSTR LH WING, WING TO BODY PANEL AREA AT LH W/W STA 1040 TO 1060 T-CHORD IS EXFOLIATED. REMOVED T-CHORD AT WTB L/H W/W 1040 TO 1060 PER SRM 51-40-02-0G. INSTALLED NEW T-CHORD AT LH WING, WING TO BODY PANEL AREA AT LH W/W STA 1040 TO 1060. INSPECTED AND VERIFISDR IPXA2026042355714Angle · crackedFWD CARGO STA 520 CEILING AREA, STRUCTURAL CLIP IS CRACKED. REMOVED STRUCTURAL CLIP AT FWD CARGO STA 520 CEILING AREA IAW SRM 51-40-02-0G-0. INSTALLED NEW PART IAW B757-200, SRM 51-40-02-0G-0.SDR JJBA20260423021Gusset · corrodedCORROSION BEYOND LIMITS ON CENTER FUSELAGE IV FLOOR STRUCTURE, LATERAL SILLS BETWEEN FR61-FR33, GUSSET BEAN HAY BETWEEN FR59 AND FR62 BEAM LH. REPLACED THE GUSSET AND SILLS.SDR CALA2026041515374Stiffener · crackedFOUND CRACK RIGHT VAPOR BARRIER STIFFENER RBL 25 STA 663.75 O/B OF RAM AIR EXIT EXHAUST DUCT. INSTALLED NEW STIFFERNER AT BS 663.75 RBL 25" IAW 51-40-02-0G-0 AND DWG 111A1308-16.SDR DALA2026041402353Angle · crackedCRACKED ANGLE AT WING CENTER, STA 663 RBL 11. REPAIRED ANGLE ATWING CENTER, STA 663 RBL 11 PER B737 SRM 57-10-10-2R-5. (LOG 1539059 - AIRCRAFT WAS GROUNDED).SDR DALA2026041402352Angle · crackedCRACKED ANGLE AT WING CENTER, STA 663 LBL 11. REPAIRED ANGLE AT WING CENTER STA 663 LBL 11 PER SRM 57-10-10-2R-5. (LOG 1539055 - AIRCRAFT WAS GROUNDED).SDR CALA2026041315309Shield · corrodedAFT CARGO SHIELD CORRODED BS 797 - 767, RBL 24. REMOVED CORROSION ON SHIELD, EVALUATED AREA FOUND TO BE OUT OF LIMITS , REMOVED AND REPLACED SHIELD ON AFT CARGO BS 767 - 797, RBL 24 IAW SRM 51-10-02-0G-0, SRM 53-00-53-1A-2, SRM 51-40-02-0G-0, PL 146A0081, RSDR CALA2026041315307Baffle · crackedFWD CARGO BAGGLE UNDER Z CHANNEL AT STA 500B TO 500C RT SIDE IS CRACKED. REMOVED AND REPLACED DAMAGE BAFFLE AT FWD CARGO BTW BS 500B - 500C IAW SRM 51-40-02-OG-0.SDR CALA2026041315303Baffle · damagedFWD CARGO BAFFLE UNDER Z CHANNEL AT STA 500D TO 500W RT SIDE IS BENT/DAMAGED. REMOVED AND REPLACED DAMAGE BAFFLE AT FWD CARGO BTW STA 500D TO STA500E R/H SIDE I.A.W B737-800 SRM 51-40-02-0G-0.SDR CALA2026041315301Baffle · damagedFWD CARGO BAFFLE UNDER Z CHANNEL AT STA 500E TO 500F RT SIDE IS BENT/DAMAGED. REMOVED AND REPLACED DAMAGE BAFFLE AT FWD CARGO BTW BS 500E AND STA 500F R/H SIDE I.A.W B737-800 SRM 51-40-02-0G-0.SDR AALA202604131140Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE BETWEEN STA 500G AND STA 500H AT RBL 25. REPLACED BAFFLE PER AARD 51-00-05-1.
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