JASC 5330
Service difficulty reports · 79,281
Reports filed under 5330 · Fuselage Main, Plate/Skin, 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 = '5330' 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 = '5330' 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 DALA2026040302150Skin · dentedTHE FWD RH DENT IS OUTSIDE OF LIMITS DUE TO BEING PARTIALLY WITHIN AN EXCLUDED ZONE AND THE AFT RH DENT IS OUTSIDE OF LIMITS DUE TO THE MAX DEPTH BEING GREAT THAN 0.020. MAINTENANCE CONFIRMS THE DAMAGE TO THE TWO (2) SHEAR TIES. FIRST SHEAR TIE IS AT FRAME 73SDR SWIA2026040176327Doubler · corrodedCORROSION NOTED ON DOUBLER COMMON TO ELECTRICAL CONNECTORS J410 AND J412 AT RT RIB REAR SPAR ASSY. AT WS53.60. REMOVED AND INSTALLED NEW DOUBLER ANGLE ON BATT RIB, WS53.6 PER CRJ200 SRM 51-42-06 AND DWG NO. 601R10203 REV -G. OPS CHECK GOOD. COMPLIED TASK CARD SDR AALA202606026252Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FUSELAGE SKIN INTERNAL SIDE BETWEEN STA 847 AND STA 867, BETWEEN S26R AND S27R. REPAIRED SKIN PER SRM 51-10-02 AND EA 374893.SDR AALA202606024222Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FUSELAGE SKIN INTERNAL SIDE BETWEEN STA 827 AND STA 847, BETWEEN S26R AND S27R. REPAIRED SKIN PER SRM 51-10-02 AND EA 374549.SDR AALA202605226257Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FUSELAGE SKIN INTERNAL SIDE, BETWEEN STA 807 AND STA 827, BETWEEN S26R AND S27R. ACCOMPLISHED DOUBLER REPAIR PER SRM 51-10-01 AND EA 374893.SDR AALA202605221571Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FUSELAGE SKIN INTERNAL SIDE, BETWEEN STA 787 AND STA 807, BETWEEN S26R AND S27R. ACCOMPLISHED DOUBLER REPAIR PER SRM 51-10-02 AND EA 374549.SDR AALA202605223145Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FUSELAGE SKIN INTERNAL SIDE, BETWEEN STA 767 AND STA 787, BETWEEN S26R AND S27R. ACCOMPLISHED DOUBLER REPAIR PER SRM 51-40-02 AND EA 374893.SDR AALA202605224153Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FUSELAGE SKIN INTERNAL SIDE, BETWEEN STA 847 AND STA 855, OUTBOARD SIDE OF S26R. ACCOMPLISHED DOUBLER REPAIR PER SRM 51-10-02 AND EA 374893.SDR CALA2026040815223Repair · delaminatedFOUND A REPAIR WITH DELAMINATION AT STA345 BETWEEN S-33L AND S-34L.SDR MASA20260406062Doubler · corrodedCF III, WASTE BOX CUTOUT DOUBLER, RIVET ROW ON OUTBOARD SIDE OF STGR 28R, BET. FR 88 -FR 89 FOUND CORRODED. CORRODED RIVETS AT CFIII, WASTE BOX CUTOUT DOUBLRE, OUTBOARD SIDE OF STRINGER 28R, BETWEEN FRAME 88-FRAME 89 REPLACED WITH NEW AND INSTALLED IAW SRM 514SDR VNAA202604010041Skin · dentedEXTERNAL FUSELAGE SKIN DENTED BETWEEN FS333 AND FS349 STGR 5R. FUSELAGE DENT WAS REPAIRED IAW REO 670-53-21-2658 REV.-- DATED 2025-10-06.SDR VNAA202604010048Doubler · corrodedONE NUTPLATE DOUBLER IS CORRODED FOR THE FWD WING-TO-FUSELAGE FAIRING, LOCATED BETWEEN FS 597 AND FS 613, BETWEEN STGR 27 AND STGR 26L. REMOVED CORRODED DOUBLER. FABRICATED AND INSTALLED NEW DOUBLER IAW CRJ 700 SRM 51-23-00-001-001-A01 AND CRJ 700 SRM 51-42-SDR VNAA202604010015Doubler · corrodedANTENNA DOUBLER BETWEEN FS 295 AND FS 310 AT BL0 IS CORRODED. REMOVED AND REPLACED DOUBLER IAW CRJ-700 SRM 51-42-06-001-001-A01. SH670-32364-7SDR VNAA202604010058Joint · corrodedF.S. 477 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STGR 25L AND STGR 24R. PERFORMED REPAIR BY COMPLYING WITH MHIRJ REO 670-53-21-2657 REV – DATED 2025-07-25. - DISPOSITION FOR BLENDED CORROSION DAMAGE TO FS477.40 BUTTSTRAP BETWEEN STR 25L AND STR 24R. THE AISDR SCNA20260601233Skin · dentedDENT IS 2 INCHES WIDE, 4 INCHES LONG, 040 DEEP, AT STRINGER 26L STATION 366. ACCOMPLISHED FUSELAGE STRINGER REPAIR, FWD FUSELAGE BETWEEN STA 344 TO STA 400 AND STRINGER 26L AS PER REF B737-800 SRM 53-00-03-2R-1 AND R.E.S # 014817-1-1. CAT A REPAIRSDR K11A2026042700378Skin · chafedAFT CARGO DOOR HAS CHAFFING DAMAGE ON DOOR CUTOUT FWD AND UPPER AREAS INSIDE.SDR SWAA2026040785040Doubler · brokenEGPR CUTOUT LOWER DOUBLER IS BROKEN. ACCOMPLISHED REPAIR IAW SRM 53-10-15-2R-4. ACCOMPLISHED REPAIR IAW B737-8 SRM 53-10-15-2R-4.SDR JJBA20260406001Skin · dentedDENT ON LT SIDE FUSELAGE JUST BELOW STR 12 BETWEEN FRAMES 20 & 21.SDR DALA2026033102109Skin · gougedTWO EACH DENTS WITH GOUGE AND PUNCTURE BETWEEN FR7 AND FR 8 R/H SIDE FUSELAGE SKIN. PERFORMED REPAIR IAW PRI 633376-14 REV 0, 1 AND 2. ALL STEPS COMPLIED WITH. WAITING ON FINAL ERA, (448268). RECEIVED FINAL ER /A APPROVAL FROM ENGINEERING. O.K. FOR SERVICE. (LSDR VNAA2026040920491Skin · dentedDENT OF FUSELAGE. LOCATION FS 485SDR VNAA2026040920489Skin · dentedDENT OF FUSELAGE. LOCATION FS 409-421 STGR 19RHSDR VNAA2026040920488Skin · dentedDENT OF FUSELAGE. LOCATION FS 394-409 STGR 17RH (BELOW WINDOW 2 RH)SDR DALA2026040202137Skin · damagedLOWER EXTERNAL FUSELAGE AT FR 25+160MM, STGR 40L SKIN WITH TOOL MARKS. FOUND DURING PROCESS WITH ORNRC 100-269. REPAIRED LOWER FUSELAGE SKIN PANEL FROM FR25 +66.5MM TO FR25 + 296.6MM BETWEEN STRG 39LH-41LH DUE TO TOOL MARK OUT LIMITS I/A/W A319 SRM 53-21-11-3SDR JJBA20260401027Skin · crackedCRACK FOUND IN LT UPPER FUSELAGE SKIN AT FRAME 75. COMPLETED PERMANENT REPAIR TO CRACKED SKIN.SDR SWIA2026032976238Skin · damagedEVIDENCE OF LIGHTNING DAMAGE IN AREA OF BS 354, S27. REPAIRED DAMAGED AREAS ON EXTERIOR FUSELAGE SKIN AT BS 354, S27 IAW REO 670-53-21-2895, REV --, AND SRM 51-42-06, 53-00-00, 51-40-11, 51-12-00; AMM 05-51-07.SDR SWIA2026032976232Skin · gougedPAX DOOR CUTOUT-FWD LOWER CORNER HAS GOUGE (BS 319.7 AND BS 333, STGR17L AND WL 71) PERFORMED REPAIR AREA ON PAX DOOR CUTOUT FWD LOWER CORNER AT BS 319.7 TO BS 333, STGR17L AND W L71 IAW SRM 51-26-01, 51-11-00. 53-21-01. THIS TEMPORARY REPAIR MUST BE REPLACEDSDR CALA2026040115033Skin · damagedDENT OR POSSIBLE BLENDOUT ON LOWER SKIN AT APPROX BS 950, STR 27L. REMOVED INTERCOSTAL FASTENER ON FUSELAGE SKIN BS 937, 2 INCH INBD OF STR 27L. MEASURED PREVIOUS BLEND OUT TO SKIN AT 0.020" AT DEEPEST SPOT. BLEND IS APPROX 1" LONG BY 1" WIDE. FOUND ADDITISDR SWIA2026032875600Skin · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA110660-REO 670-53-31-1164 N715SK MXCODEID120995-TR - COMPLY WITH TEMPORARY REPAIR ON RA ID: 110660 BLENDED LIGHTNING STRIKE DAMAGE TO CENTER FUSELAGE LOWER SKIN BTW BS 565 - 581 STR24L - STR25L PER REO 670-53-31-1164 SDR N6WA2025033002Skin · damagedDAMAGE TO FUSELAGE SKIN BETWEEN BS 501 - 517, STRINGERS 15 - 16RT. PERFORMED A PERMANENT REPAIR OF THE FUSELAGE SKIN IAW EO C550-53MR-025, REV O.SDR R61A2026032800070Skin · damagedDURING AAI INSP. FOUND - AAI DISCREPANCY ITEM NR 2 REPAIR NR 38 - FR 27-28, STGR 22R-23R, PROVIDES A REPAIR DISPOSITION OF SRM 51-75-11 FOR DAMAGE BETWEEN STGR 22R AND 23R; HOWEVER, SRM 51-75-11 IS NOT APPLICABLE BECAUSE THE DOUBLER CROSSES A RIVET ROW (STGR SDR SWIA2026032777755Skin · corrodedNUMEROUS SPOTS OF CORROSION ON FUSELAGE SKIN AT ATTACHMENT HOLES FOR FAIRING PANEL 195BB. BLENDED AND EVALUATED, FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW REO 601R-53-00-943, REV -, & SRM 53-00-31 PAR 4 B, FIG 101, & FIG 102. COMPLIED WITH TASK CARD 51-900-10SDR SWIA2026032777751Skin · corrodedNUMEROUS SPOTS OF CORROSION ON FUSELAGE SKIN AT ATTACHMENT HOLES FOR FAIRING PANEL 192BB. EVALUATED AND REPAIRED THE AREAS IAW REO 601R-53-31-1372, REV --, & REF CONTINUATION CARD FOR PROCEDURE DETAILS, LEAK CHECKED GOOD IAW AMM 21-50-00-863-801, PRESSURIZATSDR SWIA2026032777749Skin · corrodedNUMEROUS SPOTS OF CORROSION ON FUSELAGE SKIN AT ATTACHMENT HOLES FOR FAIRING PANEL 191BB. EVALUATED & REPAIRED AREAS AS REQUIRED IAW REO 601R-53-31-1372, REV --, REF CONTINUATION CARD FOR PROCEDURE DETAILS, LEAK CHECKED GOOD IAW AMM 21-50-00-863-801, NO WEIGSDR SWIA2026032776274Skin · scratchedMULTIPLE NICKS AND SCRATCHES ON EXTERIOR SKIN BETWEEN BS 1000 TO BS 1051.30 BETWEEN S27R AND S24R. REPAIRED MULTIPLE NICKS AND SCRATCHES ON EXTERIOR SKIN BETWEEN BS 1000 TO 1051.30 BETWEEN S27R AND S24R. IAW REO 670-53-61-2715 REV -.SDR TSAA2026032700002Skin · damagedFELT TAIL STRIKE ON ROTATIONSDR DALA2026040102119Skin · corrodedDURING M2 AND WHILE INSPECTING PER JIC 5320-6010-DE, CORROSION SPOTS FOUND ON FUSELAGE SKIN, INTERNAL SIDE BETWEEN STRGR 31L - STRGR 32L AND FR67 - FR69. AT REV A STAGE II DTE IS COMPLETE. STAGE III PENDING. C/A: *DTE* PER SECTION DTE I, THE REPAIR OF SECTION SDR YENA2026033100362Skin · dentedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / LHS LOWER LATERAL PANEL / BTWN FR5-FR6 / EXISTING REWORKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0027-26 REV. 0 (COVER + PARTS 1-2) /2/ AIRBUS DOSSIER 81764255 /3/ AIRBUS RDAF 81764255/004/20SDR YENA2026033100359Skin · dentedDURING HEAVY MAINTENANCE: DAMAGE ON CAPT SIDE FUSELAGE BTWN FR 5 & 7 LOWER HALF DENTED. ACCOMPLISHED REPAIR OF EXISTING REWORKS NOSE FWD FUSELAGE LT LOWER LATERAL PANEL BTW FR 5 TO 6 IAW EA 53-0027-26, REV 0, & RDAF 81764255/004/2026, ISSUE A, & EC A26-248-SDR DALA2026041302318Skin · dentedDENTED SECTION IN THE BELLY OF THE FUSELAGE FROM A SUSPECTED GROUND IMPACT. REPAIRED PER ERA 625902-14AD. (1513848) (AIRCRAFT GROUNDED)SDR CALA2026040915231Skin · corrodedCORROSION: LOWER FUSELAGE WATER SERVICE DOOR CUTOUT INNER SKIN CORROSION AROUND HINGES. REMOVED AND REPLACED DOUBLER PER REF 51-40-02-0G-0 AND DWG147A7221.SDR EE4Y2026032624179Skin · damagedDURING A STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGE (LSD) WAS IDENTIFIED AT FR03 AND Y=25MM, SEE FIGURE 1. SINCE THE DAMAGE DEPTH EXCEEDED 50% OF THE SKIN THICKNESS, IT WAS REMOVED BY DRILLING THROUGH THE SKIN ONLY. AFTER REMOVING THE FRAME PRODUCTION FASTSDR 2026FA0000218Stiffener · crackedFUSELAGE AFT LWR SKIN, STIFFENER CRACKEDSDR SWAA2026050483123Angle · crackedCRACKED ANGLE, LOCATED BS 500H AT STR26L FWD POSITION AT FWD CARGO COMPARTMENT. REPLACED ANGLE, IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 138, REV - .SDR N6WA2025032706Skin · gougedAFT FUSELAGE SKIN AT BS 977, STRINGER 27 IS GOUGED OUT OF LIMITS. REPAIRED FUSELAGE SKIN AT FS977 STGR27 IAW GOJET EO C550-53MR-108-O.SDR DALA2026032702039Skin · crackedDTA MONITOR INSPECTION LOG REF ERA 632608-14 FUSELAGE SKIN, BS 890 - 900, S26L - S28L CRACKED AND CORRODED. REF ERA 632608-14. (1511712)SDR DALA2026032702036Skin · corrodedCORROSION BTW FUSELAGE SKIN AND TRAY OF LAVATORY SERVICE DOOR. CORROSION LEVEL 2. AREA BTW FUSELAGE SKIN AND TRAY OF LAVATORY SERVICE DOOR WAS REPAIRED PER ER/A 632678- 14 REV ORIGINAL SECTION I. (1512314)SDR DALA2026032702035Skin · corrodedCORROSION ON FUSELAGE SKIN BTW STA. 890 TO 900 ANS BTW S-28L TO S-27L AT FWD CARGO COMPARTMENT. CORROSION LEVEL 2. CORROSION ON FUSELAGE SKIN BTW STA. 890 TO 900 ANS BTW S-28L TO S-27L AT FWD CARGO COMPARTMENT WAS REPAIRED PER PRI 632608-14 REV 7 AND ERA 632SDR DALA2026032702034Skin · mechanic errorMAINTENANCE ERROR: MISDRILLED HOLE ON OUTER SKIN AND STRAP STA 900 AND BELOW S-26L AT LOWER FUSELAGE. AREA ON OUTER SKIN AND STRAP STA 900 AND BELOW S-26L AT LOWER FUSELAGE. WAS REPAIRED PER PRI 632608-14 REV 7 AND ERA 632608-14 REV ORIGINAL SECTION I. (1511SDR DALA2026032702033Skin · mechanic errorMAINTENANCE ERROR IN REF. TO NRC 00608. ELONGATE HOLES (36 EAS) ALONG TO REPAIR AREA BTW STA. 820 TO 900 AND S-28L TO S25L AT EXTERNAL FUSELAGE SKIN. ELONGATE HOLES (36 EAS) ALONG TO REPAIR AREA BTW STA. 820 TO 900 AND S-28L TO S25L AT EXTERNAL FUSELAGE SKINSDR DALA2026032702032Skin · crackedIN REF NRC 00454: AFTER CORROSION WERE REMOVED, CRACK WAS FOUND ON FUSELAGE SKIN BTW STA. 890 TO 900 ANS BTW S-28L TO S-27L AT FWD CARGO COMPARTMENT (AFT BULKHEAD). AREA ON FUSELAGE SKIN BTW STA. 890 TO 900 ANS BTW S-28L TO S-27L AT FWD CARGO COMPARTMENT (AF
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