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 DALA2026021901202Web · crackedAIRCRAFT 9500, CRACK ON WEB WAS FOUND FROM STA 465 TO STA 475, AFTER REMOVAL OF RT OUTB SEAT TRACK. CRACK ON WEB STA 465 TO STA 475 OF RH OUTB SEAT TRACK WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. (LP 1457705)SDR SWAA2026032472094Scuff Plate · crackedCRACKED FWD CORNER SCUFF PLATE. REPAIRED BY WELDING FWD CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, & BAC 5975.SDR SWAA2026032372089Support · crackedCRACKED SUPPORT ZEE, BTWN BS 747 - 847, STRINGER 25L. REPLACED THE SUPPORT ZEE SECTION IAW SRM 51-40-02, SRM 53-00-53-2R-5, SRM 51-10-02, ITEM 9, AND DWG 146A7502, SHEET 29, REV -, DWG 146A7500, SHEET 85, REV A.SDR SWAA2026032372078Gusset · crackedCRACKED GUSSET, BS 500D, STRINGER 19L. REPLACED GUSSET AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, STEP 9, AND DWG 143A7902, SHEET 174, REV -.SDR SWAA2026032372079Angle · crackedCRACKED ANGLE, AFT FACE OF FRAME BS 500, STRINGER 26L, REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 143A7505, SHEET 82, REV -.SDR QXEA2026031800061Shear Web · corrodedAFT WET AREA RH SHEAR WEB IS CORRODED AT FRAME 87.BLENDED AREA AND FOUND OUT OF LIMITS AFTER EVALUATION. REPLACED SHEAR WEB IAW E175 SRM 51-40-08, RESTORED FINISH.SDR QXEA2026031800060Gusset · corrodedAFT WET AREA GUSSET AT FRAME 90 RBL 11 IS CORRODED. BLENDED OUT CORROSION AND MATERIAL LOSS WAS 100% . REPLACED GUSSET IAW E175 SRM 51-40-08SDR QXEA2026031800059Gusset · corrodedAFT WET AREA GUSSET AT FRAME 90 RBL 24 IS CORRODED.BLENDED CORROSION AND MATERIAL LOSS WAS 100% AND OUT OF LIMITS. REPLACED GUSSET IAW E175 SRM 51-40-08.SDR IPXA2026031281437Web · chafedRIGHT WING, MLG CYLINDER DOOR CUTOUT (WING SIDE), AFT I/B SKIN PLATE WITH CHAFFING. DOT 73-019. REWORKED CHAFING WITH HAND ABRASION ON R/H WING, MLG CYLINDER DOOR CUTOUT (WING SIDE), AFT I/B SKIN IAW A300-600 SRM 51-73-10-001. REMOVED WEB AT R/H WING, MLG CYLISDR CALA2026030314257Transition Panel · corrodedFWD CARGO BAY LT TRANSITION PANEL FROM BS 500C+15 - 500L, LBL 21 CORRODED. THE CORRODED AREA ON THE TRANSITION PANEL FROM BS 500C+15 - 500K, LBL 21 FOUND TO BE 100% MATERIAL LOSS IN MULTIPLE AREAS IAW SRM 53-00-53-1A-2, FIG 103, REMOVED DAMAGED TRANSITION PASDR AALA202603021155Support Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SUPPORT ANGLE AT BS 992 BETWEEN LBL 33 AND LBL 44. REPLACED SUPPORT PER AARD 51-00-05-1.SDR CALA2026030214147Floor Support · corrodedFWD WET AREA FLOOR SUPPORT BS 294.5-312, RBL 10 WITH CORROSION AT FASTENER HOLES. REMOVED AND REPLACED THE FLOOR SUPPORT AT FWD WET AREA FLOOR STRUCTURE BETWEEN BS 294.5 TO BS 312, RBL 10 IAW SRM 51-40-02-0G-0 AND DWG 141A5410.SDR AALA202602263839Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM BS 312 TO BS 328 AT LBL 46. REPLACED INTERCOSTAL PER AARD 51-00-05-1.SDR AALA202602265667Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM STA 328 TO STA 342 AT LBL 46. REPLACED INTERCOSTAL PER AARD 51-00-05-1.SDR CALA2026022013933Floor Support · corrodedFWD WET AREA FLOOR SUPPORT BS 312-328, RBL 10 CORRODED AT FASTENER HOLES. REMOVED & REPLACED FLOOR SUPPORT BETWEEN BS 312 - 328, RBL 10, SRM 51-40-02-0G-0, AND DWG 141A5410.SDR DALA2026021901210Strap · crackedCRACKED STABILIZATION STRAP BTW BS 1380, RBL 47 AT CEILING STRUCTURE OF AFT CARGO COMPARTMENT. THE STABILIZATION STRAP BS 1380, RBL 47 AT CEILING STRUCTURE OF AFT CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-51-2R PROCEDURE 12. (1456046)SDR AALA202602198233Shield · corrodedAIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO COMPARTMENT RIGHT HAND FLOOR TRANSITION SHIELD UPPER SURFACE HAS AREAS OF CORROSION BETWEEN BS 420 AND BS 440, AT RBL 25. REPLACED TRANSITION SHIELD PER SRM 51-40-05.SDR DALA2026021901181Floor Support · corrodedCORROSION FLOOR SUPPORT -Y765 LOCATED BTW FR 67 TO FR 68 AT AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT -Y765 AND FASTENERS LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11 AND DWG D53472816. (LP 1457078)SDR CALA2026021913914Strap · gougedL1 DOOR CUTOUT UPPER SILL INBOARD STRAP GOUGED BY DOOR SURROUND LINER HARDWARE. REPLACED L1 DOOR UPPER SILL INBOARD STRAP REF SRM 51-40-02 AND BOEING DWG 141N8321 SHEET 1.SDR CALA2026021913912Bracket · displacedGROUND CLIP BRACKET AT BS 500C RT SIDE REQUIRES RELOCATION DUE TO GROUND CLIP BEING DISPLACED AND FASTENER HOLES PLUGGED ON UAL ECRA 2500--16443 REV ORIGINAL FOR EA 2500-13122 REV ORIGINAL OPS 007.SDR JR2R20260218692Support · corrodedAFT WET AREA ANGLE SUPPORT AT RBL 11, FR 90 - 90A CORRODED. REPLACED.SDR JR2R20260218700Floor Support · corrodedAFT WET AREA FLOOR SUPPORT FWD OF FR 87 AT RBL 24 CORRODED. REPLACEDSDR ASAA2026021765188Plate · corrodedAFT CARGO SIDEPLATE HAS CORROSION FROM BS 727D TO 827 LT SIDE. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO SIDEPLATE IAW SRM 53-00-53-2R-5.SDR ASAA2026021765115Web · corrodedAFT CARGO SILL WEB CORROED. GROUNDED - YES. R & R THE SILL WEB IAW SRM 51-40-02-0G-0.SDR ASAA2026021765114Plate · corrodedFWD CARGO, RT SIDE PLATE CORRODED, BS 500C - 500D. GROUNDED - YES. R & R THE SIDE PLATE IAW SRM 51-40-02-0G-0.SDR ASAA2026021765112Web · corrodedFOWARD CARGO SILL WEB CORRODED. GROUNDED - YES. R & R THE SILL WEB, IAW SRM 51-40-02-0G-0.SDR SWAA2026032371793Angle · corrodedCORRODED ANGLE, BS 270, RBL 4, WL 208.1. REMOVED THE CORROSION ON THE ANGLE IAW SRM 53-10-51-1A-1, PARAGRAPH 4 B (2).SDR SWAA2026031971751Scuff Plate · crackedCRACK ON AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED BY WELDING AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.SDR SWAA2026031971752Scuff Plate · crackedCRACK ON FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED BY WELDING FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.SDR QXEA2026031800063Support · corrodedFORWARD WET AREA SILL AT FRAME 12-14 RH CORRODED. REPLACED SILL IAW E175 SRM 51-40-08.SDR IPXA2026031355302Support Strap · corrodedAPU INTAKE SUPPORT STRUCTURE FWD STRAP CORRODED FWD O/B SIDE. 61-016 ATA 53-80 INSTALLED 1EA UPPER SUPPORT ANGLE P/N: 148N3152-2, 1EA LOWER SUPPORT ANGLE P/N: 148N3152-1 APU INTAKE SUPPORT STRUCTURE BETWEEN STA 1787.45 AND STA 1825.00 STR 3R AND STR 6R IAW 757SDR AALA202603092870Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON CORNER FITTING LOCATED AT FR66 AT LEVEL STR 23RH AFT GALLEY AREA MEASURES OF CORROSION ARE: L=4.067IN, W= 1.013IN D =0.005IN. MAINTENANCE REPLACED CORNER FITTING AND FASTENERS LOCATED BTW FR66 AT LEVEL STR 23RH AFTSDR CALA2026022313974Floor Support · scratchedSCRATCH - FWD WET AREA FLOOR STRUCTURE FLOOR SUPPORT STA 328 - 344 LBL 11 WITH SCRATCH ON UPPER SURFACE. REF AAR N/R 100007400 REMOVED AND REPLACED FWD WET AREA FLOOR SUPPORT STA328 TO STA344, LBL11, REF. SRM 51-40-02-0G-0, DWG #141A5400.SDR SWAA2026022071395Scuff Plate · crackedFWD SERVICE DOOR THRESHOLD HAD A THREE INCH CRACK ON AFT EDGE. R & R FWD SERVICE DOOR SCUFF PLATE IN REF WITH AMM 53-11-01.SDR CALA2026021913910Angle · interferenceGROUND CLIP AT STATION 559 R/H SIDE REQUIRES RELOCATION DUE TO GROUND CLIP BEING DISPLACED AND FASTENER HOLES PLUGGED ON UAL ECRA 2500-16443 REV ORIGINAL FOR EA 2500-13122 REV ORIGINAL OPS 009SDR CALA2026021913907Shear Web · damagedSHEAR WEB LOWER FASTENER HOLE HAS A CRACK INDICATION, FRAME 61, S37L. REMOVED, FABRICATED, & INSTALLED THE SHEAR WEB IAW SRM 51-72-11-911-001, CAT A.SDR DALA2026021801177Cusp Web · crackedAIRCRAFT 9511, CRACK WAS FOUND ON CUSP WEB AT X=-44 BTW BS 636 - 655 AT PAX CABIN. CRACKED ON CUSP WEB AT X=-44 BTW STA Y=636 - 655 AT PAX CABIN WAS REPAIRED PER SRM 53-00-55-2R, PROCEDURE 4, REPAIR 4, PAR 5 (19), FIGURE 221. (LP 1454694)SDR DALA2026021801142Floor Support · corrodedCORROSION OUT OF LIMITS, IN REF TO NRC 00453: CORROSION ON LOWER SILL LH SIDE UPPER SURFACE STA 732 AT FLOOR STRUCTURE LEVEL IS OUT OF LIMITS PER B757-300 SRM 53-30-15-1A PROCEDURE 1 AD 1. FIG. 101 DETAIL VI SECTION B-B. NEW LOWER SILL LH UPPER SURFACE STA 6SDR REXA2026080301394Fitting · corrodedCORROSION ON MACHINED FITTING LOCATED ON FS847 BETWEEN STRG 25L TO STRG 25R (INTERNAL FUSELAGE). MACHINED FITTING LOCATED ON FS847 BETWEEN STRG 25L TO STRG 25R (INTERNAL FUSELAGE) WERE REPAIRED PER REO 670-53-41-834 REV --SDR REXA2026080301393Fitting · corrodedCORROSION ON MACHINED FITTING LOCATED ON FS847 BETWEEN STRG 25L TO STRG 25R (INTERNAL FUSELAGE). MACHINED FITTING LOCATED ON FS847 BETWEEN STRG 25L TO STRG 25R (INTERNAL FUSELAGE) WERE REPAIRED PER REO 670-53-41-834 REV --SDR SWIA2026021675983Intercostal · corrodedINTERCOSTAL LEFT OF STRINGER 27 BETWEEN FS 349.00 AND 379.00 IS CORRODED. REMOVED AND REPLACED THE INTERCOSTAL LEFT OF STGR 27 BETWEEN FS349 - FS364, NEW SERVICEABLE L/H INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND SRM51-42-21-001-001-A01.SDR SWAA2026032371373Rub Strip · wornWORN RUB STRIP, BODY FAIRING BS 540 + 10. RBL 41. REPAIRED IAW SRM 57-10-13-2R-3, REPAIR 3, & SRM 51-40-02.SDR HNAA2026031800226Angle · crackedRIGHT OVERWING FAIRING 1ST ANGLE CRACKED. REPAIRED ANGLE IAW SRM 57-20-01RESDR HNAA2026031700217Angle · crackedLT OVERWING FAIRING 1ST ANGLE CRACKED. REMOVED, FABRICATED ANGLE, AND INSTALLED IAW SRM 57-20-01SDR HNAA2026031100207Angle · crackedLEFT OVERWING FAIRING 4TH ANGLE CRACKED. REPAIRED ANGLE IAW SRM 57-20-01 ITEM 3 (FIG 205)SDR SWAA2026030371345Support Angle · crackedCRACKED SUPPORT ANGLE, BS 907 - 927, S25R - S27R. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 147A7221, SHEET 24, REV - .SDR SWAA2026022771167Bracket · crackedSUPPORT STANDOFF FWD OF AE0104A DISCONNECT BRACKET IS CRACKED. REMOVED AND REPLACED SUPPORT STANDOFF FWD OF AE0104A DISCONNECT BRACKET (NUTSPACE) IAW SRM 51-40-02-0G-0 AND AIPC 25-50-51-45A DETAIL F.SDR HNAA2026022400156Angle · crackedRIGHT OVERWING FAIRING 2ND ANGLE CRACKED. RAR ANGLE IAW SRM 51-40-02SDR DALA2026021801136Strap · crackedCRACK ON STABILIZATION STRAP (1EA) BTW STA 580 LBL 19 AT CEILING STRUCTURE OF FWD CARGO COMPARTMENT. CRACK ON STABILIZATION STRAP (1EA) BTW STA 580 LBL 19 AT CEILING STRUCTURE OF FWD CARGO COMPARTMENT WAS REPAIRED PER B757-300 SRM 53-00-51-2R-12- REPAIR 12.SDR CALA2026021713845Drain · cloggedDURING WALK AROUND IT WAS NOTICED SMOKE COMING OUT FROM FUSELAGE CLOSE TO RT STAB, PERFORMED INTERNAL VISUAL INSPECTION OF AFT UNPRESSURIZED AREA AND TAIL CONE AREA IAW AMM 05-41-03. NO HYDRAULIC LEAKS FOUND. FOUND TAIL CONE AREA DRAIN POINT TOTALLY CLOGGED A
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