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 SWAA2025090403537Scuff Plate · crackedCRACK ON FWD CORNER SCUFF PLATE LOCATED AT FWD CARGO COMPARTMENT. REPAIRED FWD CORNER SCUFF PLATE LOCATED AT FWD CARGO COMPARTMENT IAW SRM 53-30-15-2R-1 REPAIR 1.SDR JJBA20250904003Support · corrodedRIGHT SIDE SILL BTW FR 22-24 FOUND CORRODED. CF1, RH SIDE SILL BTW FR 22-24 BLENDED OUT OF LIMIT. SILL REMOVED AND REPLACED.SDR ASAA2025081260448Transition Panel · corrodedAFT CARGO COMPARTMENT LT FLOOR TRANSITION PANEL, BS 727I+9 TO TO 847, LBL.21. UPPER AND LOWER SURFACE HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION, ORIGINAL THICKNESS .040, REMOVED .040, REMAINING .000. FOUND TO BE OUT OF LIMITS IAW SRM 53-SDR ASAA2025081260446Transition Panel · corrodedAFT CARGO COMPARTMENT, RT FLOOR TRANSITION PANEL TO BS 727 TO 727I+9, RBL21, UPPER AND LOWER SURFACE HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION, ORIGINAL THICKNESS .040, REMOVED .040, REMAINING .000. FOUND TO BE OUT OF LIMITS IAW SRM 53-00SDR ASAA2025081260445Transition Panel · corrodedAFT CARGO COMPARTMENT LT FLOOR TRANSITION PANEL TO BS 727 TO 727I+9, LBL21 UPPER AND LOWER SURFACE HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION, ORIGINAL THICKNESS .040, REMOVED .040, REMIANING .000. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-SDR ASAA2025081260444Transition Panel · corrodedAFT CARGO COMPARTMENT RT FLOOR TRANSITION PANEL BS 7271+9 TO BS 767, RBL21 UPPER AND LOWER SURFACE HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION, ORIGINAL THICKNESS .040, REMOVED .040, REMAINING .000. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1SDR ASAA2025081260443Threshold Web · corrodedAFT CARGO HAS CORROSION AT DOOR THRESHOLD. GROUNDED - YES. REMOVED CORROSION ON AFT CARGO DOOR THRESHOLD WEB ORIGINAL MAT. THICKNESS .050, MATERIAL REMOVED .026 MATERIAL REMAINING .024. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15. REPLACED AFT CARGO THRESHOLD SDR IPXA2025090236564Tee Angle · corrodedBODY FAIRINGS AREA T-COURD AT STA 900 WITH CORROSION. NSTALLED NEW T-CHORD AND SPLICES AT STA 900, IAW B757-200PF SRM 51-70-12-0G-0 PAG 7 FIGURE 1.SDR IPXA2025090233389Bracket · corrodedAFT CARGO BULKHEAD LOWER STRUCTURE OF MDC BETWEEN BS 1700 TO 1720 HAVE 5 BRACKETS OF THE NUTPLATE WITH CORROSION. INSTALLED 5EA BRACKETS AT AFT CARGO BULKHEAD LOWER STRUCTURE OF MDC BETWEEN BS 1700 TO 1720 IAW SRM 51-40-02.SDR AALA202508291773Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED BAFFLE CLIP AT FORWARD SIDE OF BS 500G LEFT HAND. INSTALLED NEW CLIP. PERB AARD 53-00-01-6SDR AALA202508293364Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED BAFFLE CLIP AT AFT SIDE OF BS 500H LEFT HAND SIDE. INSTALLED NEW BAFFLE CLIP. PER AARD 53-00-01-6SDR ASAA2025081260379Shield · corrodedAFT CARGO COMPARTMENT R/H FLOOR SHIELD BS.767 TO BS.787+6 RBL.21 UPPER AND LOWER SURFACE HAS AREAS OF CORROSION. GROUNDED - YES. EVALUATED R/H SHIELD STA 767 TO STA 787, ORIGINAL THICKNESS .050 REMOVED .010 REMAINING .040 FOUND TO BE OUT OF LIMITS IAW B737-900SDR IPXA2025082337065Tee Fitting · corrodedLEFT LOWER FUSELAGE, STA 1200-1260 LBL 70 T-CHORD HAS (2EA) AREAS WITH DELAMINATION. INSTALLED NEW T-CHORD IN LH LOWER FUSELAGE STA 1200-1260 LBL 70 T-CHORD IAW B757-200 SRM 51-40-02-0GSDR IPXA2025082135811Stiffener · corrodedCORROSION BETWEEN BS 1120 - 1140, LT CHANNEL UNDER PANEL 197EL. INSTALLED A NEW STIFFENER BETWEEN BS 1120-1140 LEFT.SDR AALA202508254688Bracket · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN AFT CARGO COMPARTMENT VACUUM WASTE TANK ENCLOSURE SUPPORT BRACKET LOCATED AT BS 867, FROM S26L TO S27L. REPLACED BRACKET PER AARD 51-00-05-1.SDR IPXA2025081621930Web · crackedCRACKED WEB, AFT LOWER CARGO COMPT ENTRYWAY AT STA 1329 LBL 2.2. .I.A.W AMM 20-11-00-910-802 REV.145 REMOVED BALL PANEL SUPPORT FITTING.FABRICATE P/N: 451T2603-65 PER BOEING DWG NO: 451T2603 SH. 11 REV."-"; PL REV."AP"; PSDL REV."-" AND ORIGINAL PART AS A SASDR DALA2025081306042Floor Support · corrodedSHIP 6716 THE INTERCOSTAL/ FLOOR SUPPORT WEB IS CORRODED THROUGH ON THE I/ B AND O/B SIDES, BELOW THE ALC FLOOR, JUST FWD OF FRAME STA.1420 , JUST O/B OF STR.28L. #19553. CORRECTIVE ACTION: REMOVED AND REPLACED INTERCOSTAL FLOOR SUPPORT WEB BELOW THE ALC FLOORSDR F3LA202508120273Floor Support · corrodedREFERENCE LTPR NR 5001415390-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND FLOOR BEAM Y-756 AT FR66-FR70 CORRODED. REQUIRES REPLACEMENT AS PER SRM 51-72-11 REV 44. FLOOR BEAM Y-765 AT FR66-FR70 WAS REPLACED AS PER SDR F3LA202508120272Shear Plate · crackedREFERENCE LTPR NR 5001415392-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND R/H SHEARPLATE FR 69-70 CRACKED. REQUIRES REPLACEMENT AS PER SRM 51-72-11 REV 44. CORRECTIVE ACTION: R/H SHEARPLATE WAS REPLACED AS PER SRM 5SDR F3LA202508120271Shear Plate · crackedREFERENCE LTPR NR 5001415391-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND LH SHEAR PLATE FR 69 TO FR 70 CRACKED, REPLACEMENT IS REQUIRED AS PER 51-72-11 REV 44. PERFORMED REPLACEMENT OF LH SHEAR PLATE AS PER SRM 51-SDR SWI2025F01445Floor Support · corrodedWHILE PERFORMING REINSPECT OF R/H PRESSURE FLOOR SILL. FOUND CORROSION AT PREVIOUSLY BLENDED LOCATION F.S. 475.00 SILL PANEL. AREA WAS PREVIOUSLY REPAIRED I.A.W. REO 601R-53-41-666 REV.C, DATED 2012-11-06. REFERENCE EXPRESSJET W/O: 390949, MACON AIR CENTER C/OSDR SWIA2025102000811Floor Support · corrodedWHILE PERFORMING REINSPECT OF R/H PRESSURE FLOOR SILL, F.S. 409.00+128 TO F.S. 559.00, FOUND (2EA) PREVIOUS BLEND LOCATIONS THAT ARE CORRODED AROUND NUTPLATES. ONE DAMAGE LOCATION AT F.S. 535.00 APPROX. AND ONE DAMAGE LOCATION AT F.S. 555.00 APPROX. DAMAGE AT SDR SWAA2025092303340Scuff Plate · crackedCRACK AFT CORNER SCUFF PLATE IN AFT CARGO BAY. REPAIRED AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4. B, STEPS 2 AND 4 - 7.SDR AALA202509157112Shield · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SHIELD LOCATED FROM BS 767 TO BS 787 AT RBL 24. REPLACED SHIELD PER AARD 51-00-05-1.SDR SWAA2025090903062Intercostal · crackedFED CUTOUT SURROUND STRUCTURE; INTERCOSTAL IS CRACK AT BS 312 S-6L REPAIR PER EA#M-22-153-01244 REV: B.SDR SWAA2025090803345Scuff Plate · crackedAFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED. WELDED THE CORNER SCUFF PLATE PER SRM 53-60-15-2R-1 STEP 4.B.(4). REFERRED TO BAC 5975.SDR SWAA2025090803346Scuff Plate · crackedACB AFT CORNERR SCUFF PLATE IS CRACKED. WELDED THE CORNER SCUFF PLATE PER SRM 53-60-15-2R-1 STEP 4.B.(4). REFERRED TO BAC 5975.SDR JJBA20250904006Channel · corrodedCF1, SERVICE DOOR CUTOUT, ENTRANCE CHANNEL FOUND CORRODED. CF1, SERVICE DOOR CUT OUT, ENTRANCE CHANNEL BLENDED OUT OF LIMIT. CF1, SERVICE DOOR CUTOUT, ENTRANCE CHANNEL REMOVED FOR REPLACEMENT. CF1, SERVICE DOOR CUT-OUT, ENTRANCE CHANNEL REPLACED.SDR IPXA2025090214639Web · corrodedEVIDENCE OF CORROSION ON WEB LOWER SECTION STA 1180 TO STA 1240 R/H. INSTALLED WEB LOWER SECTION STA 1180 TO STA 1240 R/H IAW B757-200 SRM 51-40-02. FASTENERS INSTALLED.SDR IPXA2025083014616Tee Angle · corrodedEVIDENCE OF CORROSION ON TEE ANGLE UPPER SECTION STA 1220 RT. INSTALLED TEE ANGLE UPPER BS 1220 RT SIDE UPPER SECTION IAW B757-200 SRM 51-40-02.SDR JJBA20250827058Gusset · corrodedCENTER FUSELAGE IV, CENTER GUSSET BTW FRAME 59-61 CORRODED OUT OF LIMITS CENTER FUSELAGE IV, CENTER GUSSET BTW FR59-61 REPLACED.SDR JJBA20250827057Gusset · corrodedCENTER FUSELAGE IV, RH GUSSET BTW FRAME 59-61 CORRODED. R/H GUSSET BLENDED OUT OF LIMITS. TH GUSSET BTW FR59-61 REMOVED FOR REPLACEMENT. CENTER FUSELAGE IV, R/H GUSSET BTW FR 59-61 REPLACED.SDR IPXA2025082315088Tee Fitting · corrodedEVIDENCE OF CORROSION ON VERTICA LT-CHORD STA 1220 RT. INSTALLED NEW T-CHORD IN STA 1200 R/H IAW B757-200 SRM 51-40-02-0GSDR AALA202508273563Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT CARGO RIGHT HAND TRANSITION PANEL CORRODED HAS LOOSE RIVET BS 727E. INSTALLED NEW RIGHT HAND TRANSITION PANEL ON TASK CARD NUMBER: 08C14053016/001.SDR CALA2025082608119Intercostal · corrodedMAIN E&E COMP LT CORROSION AT INTERCOSTAL BETWEEN BS 294.5-312 STR 23L. COMPLETED INSTALLATION NEW WEB BETWEEN BS 294.5 & 312 S23L IAW SRM 51-40-02-G-0 AND DWG# 141A8131.SDR CALA2025082608118Intercostal · corrodedMAIN E&E COMP LT CORROSION AT INTERCOSTAL BETWEEN BS 344-3" S23L. INSTALLED NEW WEB AT E&E COMP LT BETWEEN BS 330 & 344, S23L IAW SRM 51-40-02-0G-0 AND DWG# 141A8131.SDR ASAA2025081160263Transition Panel · corrodedAFT CARGO LT TRANSITION PANEL HAS CORROSION BS 727 TO 787. GROUNDED - YES. REMOVED DAMAGE TRANSITION PANEL FOUND TO BE OUT LIMITS. REMOVED AND REPLACED TRANSITION PANEL IAW SRM 53-00-53-2R-5 W= 2 O= 0.3040 R= 0 L= 2 D= 0.040.SDR COEA2025081904734Support · crackedCAPTAIN SEAT L/H BOTTOM SUPPORT CRACKED. REPLACED WITH NEW SEAT REF. C408 MM 25-10-05.SDR AALA202508189162Bracket · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN AFT CARGO COMPARTMENT VACUUM WASTE TANK ENCLOSURE VERTICAL SUPPORT BRACKET LOCATED AT BS 867, LBL 20. REPLACED BRACKET PER AARD 51-00-05-1.SDR AALA202508126930Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER AFT CORNER SHAPE FITTING AT FR 68 AND S23R. REPLACED AFT CORNER SHAPE FITTING PER SRM 51-72-11.SDR JR2R20250811972Gusset · corrodedAFT WET AREA TEXAS GUSSET AT FR90 RBL24 CORRODED. REPLACEDSDR FDEA202508111406Profile · crackedMAIN DECK FLOOR STRUCTURE WAS FOUND PROFILE-Z CRACK AT FR80/82, Y1448. REPLACED THE CRACK PROFILE-Z WITH NEW PART.LOCATE AT MAIN DECK FLOOR FR80/82 Y1448.I.A.W A300-600F SRM 51-72-10-001 PAGE 2 AND 51-40-21-001 PARA 6 PAGE 7B~PAGE 23.REPAIR CLASSIFIED AS SDR HNAA2025091400631Floor Support · corrodedLH #7 FLOOR SILL IS CORRODED. R&R LH #7 FLOOR SILL IAW EMB 145 SRM 51-40-02.SDR AALA202509147411Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL LOCATED FROM BS 500 TO BS 500I AT S25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.SDR AALA202509146141Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL LOCATED FROM BS 500C TO BS 500I AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.SDR HNAA202509110064Floor Support · corrodedLH #6 FLOOR SILL IS CORRODED. R&R LH #6 FLOOR SILL IAW EMB 145 SRM 51-40-02.SDR SWAA2025090800284Support Angle · corrodedAFT CARGO BULKHEAD SUPPORT ANGLE AT BS 947.5, LBL 4, WAS CORRODED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 149A8117, REV -.SDR SWAA2025090800176Support · corrodedAFT CARGO ZEE ANGLE SUPPORT AT RBL 21 FROM STA 727 TO STA 767 HAS CORROSION IN VARIOUS LOCATIONS. REMOVED AND REPLACED THE FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02, AND DWG 146A7500 0085, REV A.SDR SWAA2025090800175Support · corrodedAFT CARGO ZEE ANGLE SUPPORT AT LBL 21 FROM BS 727 - 847 HAD CORROSION IN VARIOUS LOCATIONS. REMOVED AND REPLACED THE FLOOR TO SIDEWAL SUPPORT IAW SRM 51-40-02, AND DWG 146A7500 0061, REV-.SDR SIMA20250810001Floor Support · corrodedRH FWD SILL HAS CORROSION BETWEEN FR 13 AND FR 14 @ Y=+48" (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED CORROSION ON FWD RH SILL AT FR13-FR14 AND Y=+48" PER EMB 175 SRM 51-10-03. BLENDED AREA MEASURES (L: 3" W: 1" D: .015".) AREA MEASURED USING DEPTH GAUGE AND I
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