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 DALA2026090404993Skin · damagedSKIN, FRAME 72, STR 24 LT DAMAGED. COMPLIED WITH A330 SRM 53-41-11-283. (9447248) AIRCRAFT WAS GROUNDED.SDR SWIA2026082976966Skin · puncturedREFERENCE AML 1973154 INSPECTED DAMAGE AND FOUND A PUNCTURE AND DENT, DEFLECTION DAMAGE MEASURING MAX 20" LONG BY MAX 5" WIDE BETWEEN BS 1051.30 - 1098.20, S19 -22R. (FLIGHT 9915) OPEN.SDR SWIA2026082976965Skin · puncturedREF AML1976305 FOR COMPLYING WITH TEMPORARY REPAIR FOR PUNCTURE DAMAGE TO AIRCRAFT SKIN BETWEEN BS 1051.30 - 1098.20, STR 19R - 22R. WITH REO 670-53-61-2749, REV-.SDR CALA2026083119076Skin · puncturedPUNCTURE BETWEEN AFT CARGO DOOR AND R3 ENTRY DOOR ON THE RIGHT SIDE OF ACFT. DAMAGE LOCATED BTWN BS 1439 & 1461 IAW SRM 53-00-00-0G-0. FOUND DAMAGE TO BE 5.4 INCH LONG BY 2.6 INCH WIDE, ON BS 1439 - 1461, STR 21-22R. DAMAGE IS OUT OF LIMITS IAW SRM 53-00-SDR DALA2026083004889Skin · ground damagePUSH BACK TUG STRUCK NOSE OF A/C NEAR GROUND POWER DOOR. COMPLIED WITH ER/A 636558-14 REV. ORIG. PRI REV. 0, 1, 2, & 3 REPAIR INSTRUCTIONAL STEPS. ENSURED ALL ER/A 636588-14 REV. ORIG. PRI REV. 0, 1, 2, & 3 REPAIR INSTRUCTIONAL STEPS ARE COMPLETED AND MATCH SDR DALA2026091005072Skin · dentedER/A 626742-14 REV B, FUSELAGE SKIN, FR 19-20 AND S32L - 33L DENTED. ACCOMPLISH SECTION IV WITHIN 52,500 FLIGHT HOURS OR 30,000 FLIGHT CYCLES FROM TIME OF SECT. III REPAIR AT 15,018 FH AND 6,946 FC (WITHIN AIRCRAFT TOTAL TIME OF 67,518 FH OR 36,946 FC), WHICSDR AALA202609049341Skin · crackedAIRCRAFT WAS NOT GROUNDED: CRACK INDICATION AT LAP SPLICE STATION 807, STRINGER 14R LAP. MAINTENANCED REMOVED AND FABRICATED AND INSTALLED DOUBLER AND FILLERS PER EA NUMBER 378367.SDR BAGA2026090400002Doubler · corrodedHEAVY CHECK SUBMISIION - AFT FUSELAGE AT FRAME 76 WASTE DOUBLER FOUND CORRODED. WASTE DOUBLER REPAIRED IAW REO.SDR FDEA202608281243Skin · noneEXISTING REPAIR AT FUSELAGE SKIN - MAIN DECK CARGO DOOR CUTOUT - FORWARD LOWER CORNER STATION 623.065, LONGERON 27 LEFT HAND. EXISTING REPAIR AT FUSELAGE SKIN - MAIN DECK CARGO DOOR CUTOUT - FORWARD LOWER CORNER STATION 623.065 LONGERON 27 LEFT HAND EVALUASDR FDEA202608281242Skin · noneEXISTING REPAIR AT FUSELAGE SKIN AT STATION 1894 TO STATION 1914 LONGERON 47 LEFT HAND TO LONGERON 50 RIGHT. FUSELAGE SKIN AT STATION 1894 TO STATION 1914 LONGERON 47 LEFT HAND TO LONGERON 50 RIGHT HAND CARRIED OUT REPAIR IN ACCORDANCE WITH EA 1-5330-T03SDR R61A2026092600268Skin · dentedDURING HEAVY CHECK, MAINTENANCE FOUND REAR FUSELAGE SKIN FOUND TO HAVE 3 DENTS BETWEEN FRAMES 99 AND 100, STR 27R & 28R. PERFORMED SKIN CUT OUT, AND PERMANENT REPAIR DOUBLER IAW ETD2026-170-015273-A.SDR SWIA2026082777026Skin · damagedSCRATCH AND DENT APPROXIMATELY 31 INCHES LONG ON THE RT SIDE BETWEEN FR 17 AND FR 14, BTWN STR 20R AND STR 21R.AT THE DEEPEST 0.125" OPENSDR HNAA2026100900970Skin · corrodedCARGO DOOR CUTOUT, THERE IS CORROSION ON THE LOWER EDGE OF THE DOOR CUTOUT, IN-LINE WITH FR 66. REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT SILL IAW SRM 51-40-02.SDR SWIA2026082677540Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE RA103394-SRM 53-10-01-AD01 MXCODEID113882-PR - COMPLY WITH PERMANENT REPAIR ON RA ID 103394DENT ON LEFT FUSELAGE ABOVE SKYWEST LOGO INSPECTED REPORTED DENT ON LEFT FUSELAGE BETWEEN FR 18 - FR20 STGR12L - STGR 15L FOUND TOSDR DALA2026082604844Doubler · wornFWD CARGO FWD EDGE DOUBLER FOUND AFT EDGE WORN AT STR-40R AND FR20. REWORKED AREA PER ERA 614093-14. (1777498) AIRCRAFT WAS GROUNDED.SDR DALA2026082604840Skin · crackedCRACKED ON EXTERNAL FUSELAGE SKIN ON BS 1086 BTW LONG 13L AND 14L, COMPLIED WITH ER/A 636457-14. (1777167) (AIRCRAFT GROUNDED).SDR DALA2026082604839Skin · crackedCRACKS ON EXTERNAL FUSELAGE SKIN ON BS 1076 BTW LONG 13L AND 14L, COMPLIED WITH ER/A 636463-14. (1777154) (AIRCRAFT GROUNDED).SDR HNAA2026101500989Skin · damagedFOUND RELEVANT INDICATIONS ON FUSELAGE SKIN AT FR 75 AT NEAR STGR 2L. FR 75 REPAIR MEMBERS INSTALLED AS REQUIRED IAW EMB 145 SRM 53-31-01-RE ITEM 11, FIGURE 219 SHEET 1 AND SHEET 2 AS WELL AS EMB 145 SRM 51-40-02 AND PIEDMONT EO1-53-26-0468.SDR DALA2026082604842Skin · crackedCRACKS WERE FOUND AFFECTING THE FUSELAGE SKIN AT APPROXIMATELY BS 1087.060, BTW LONGERONS 13 & 14, COMPLIED WITH ER/A 636457-14. (1776557) (AIRCRAFT GROUNDED).SDR DALA2026082604841Skin · crackedCRACKS WERE FOUND AFFECTING THE FUSELAGE SKIN AT APPROX BS 1076, BTW LONGERONS 13L & 14L, COMPLIED WITH ER/A 636463-14. (1776432) (AIRCRAFT GROUNDED).SDR SWIA2026082477121Repair · out of limitsREMOVED REO 670-53-21-1611 REPAIR DOUBLER AT LT FUSELAGE SKIN BTWN BS 394 - 437, STR 14L - 17L DUE TO CLOSE POXIMITY OF ATG 4 WIFI ANTENNA LOCATION. DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT REPAIR OF DOUBLER AT LH FUSELAGE SKIN IAW REO 670-53-21-2SDR DALA2026082704863Skin · ground damageWHILE IN ATL, MTC REPORTED FUSELAGE DAMAGE DUE TO CONTACT WITH GROUND EQUIPMENT. THE DAMAGE INVOLVES MULTIPLE GOUGES WITH TWO PUNCTURES AND IS LOCATED BETWEEN BS 1197+209 - 1219, S33 - 36R. TRIMMED OUT DAMAGED SKIN MINIMUM AMOUNT TO ENCOMPASS DAMAGED AREA. FABSDR FDEA202608241221Skin · dentedFUSELAGE BTWN BS 1963.8 - 1992.8 DENTED. APPLIED PERMANENT REPAIR AT BS 1963.8 - 1992.8 IAW SRM 53-80- 01-2R, REP 1, DETAIL I, FIG 201, SHEET 1, & SRM 51-70-10-2R, REP 4.SDR DALA2026082504809Skin · crackedCRACKS WERE FOUND AFFECTING THE FUSELAGE SKIN AT STA Y=1037 BETWEEN THE L-13L AND L-14L, COMPLIED WITH ER/A 624765-14. (1774752) (AIRCRAFT GROUNDED).SDR CALA2026082518881Skin · crackedFUSELAGE SKIN HAS AN APPROX 2 .5 IN LONG GOUGE 3 IN FWD OF LAV SERVICE PAN. UPON FURTHER CLEANING AND INSPECTION FOUND ADDITIONAL GOUGE IN SKIN 3 INCHES BELOW ORIGINAL DAMAGE. REMOVED DAMAGE TO SKIN MAX MATERIAL REMOVED .006 AND WITHIN ALLOWABLE DAMAGE LIMITSDR DALA2026082404792Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN STA Y= 1037 BTW LONG 13L AND 14L, COMPLIED WITH ER/A 636303-14. (1773110) (AIRCRAFT GROUNDED).SDR HNAA2026092300901Skin · crackedFUSELAGE SKIN HAD A POSSIBLE CRACK AT A RIVET AT FRAME 78, JUST BELOW STRINGER 4L. REPAIRED CRACKED FUSELAGE SKIN IAW EO1-53-26-0433 AND SRM 53-32-01SDR SWAA2026092491395Access Panel · delaminatedDELAMINATED EXTERNAL SKIN ACCESS PANEL 191CL. REPAIRED EXTERNAL SKIN ACCESS PANEL 191CL IAW SRM 51-70-04-2R-1 REPAIR 1.SDR SWAA2026091621561Skin · corrodedCORROSION EXTERNAL SKIN WATER SERVICE CUT OUT BTW BS 907 TO BS 927 AND BTW STRG 26R TO STRG 27R AT LOWER FUSELAGE. REPAIRED EXTERNAL SKIN WATER SERVICE CUT OUT BTW BS 907 TO BS 927 AND BTW STRG 26R TO STRG 27R AT LOWER FUSELAGE IAW EA 26-153-02413 SUMMARY EA SDR SWIA2026082176992Skin · dentedMULTIPLE DENTS AND ONE CREASE ON FUSELAGE BELLY, FWD OF AFT EQUIPMENT BAY DOOR. REPAIRED MULTIPLE DENTS AND THE CREASE ON THE FUSELAGE FWD OF THE AFT EQUIPMENT BAY DOOR IAW REO 601R-53-61-8627, REV -.SDR SWAA2026082555996Skin · crackedRIGHT FUSELAGE SKIN AT BS 380 WAS CRACKED, STRINGERS 24R - 28R.SDR SWAA2026082552272Skin · crackedRT FUSELAGE UPPER SKIN AT BS 380 STR 24R LAP JOINT HAD A 2 INCH CRACK. REPAIRED IAW EA 26-153-02262. EA-26-153-02262 COMPLIED WITH. NO INSPECTION OR RII REQUIRED ON EA.SDR DALA2026082404794Skin · crackedCRACKS WERE FOUND AFFECTING THE FUSELAGE SKIN AT BS Y=1037, BETWEEN THE L-13L AND L-14L, COMPLIED WITH ER/A 636303-14. (1772642) (AIRCRAFT GROUNDED).SDR FDEA202608211212Skin · dentedDURING INSPECTION FOUND EVIDENCE OF STRIKE AT BS 368, STRINGER 5R, DOOR STA 108 3/4" INBD OF STR 5R, REPAIRED SKIN USING COMPLING WITH EA.H-5330-T0388341P1 (PART 1 OF THIS EA PROVIDES INSTRUCTIONS TO ACCOMPLISH SRM 53-00-01-2R, REPAIR 29, WITH CLARIFICATION SDR VNAA2026082423401Skin · dentedDENT FOUND BELOW AFT CARGO. BETWEEN FS1000.00 AND FS1015.00, STRG 19LH AND STRG 20LH. PERFORMED ALL WORK USING STEPS AND DRAWINGS LISTED IN MHIRJ REO 690-53-61-1772SDR ABXA20260821371Skin · crackedDURING MAINT, PRE FLIGHT MAINT FOUND A SUSPECTED 4" CRACK AT FUSELAGE SECTION 48 AT STA 1660 BETWEEN STRINGER 13R AND 14R ON RIGHT SIDE ABOVE STAB CENTER LINE. MAINT GROUNDED A/C . REMOVED DAMAGED, REPAIRED IAW B767-300 SRM 53-80-010 REPAIR 7 DETAIL . AND RETSDR FDEA202608211199Doubler · crackedNR 1 AIRCON RAM AIR EXHAUST CUTOUT PRODUCTION DOUBLER FOUND CRACKED AT STATION Y= 561.667. PRODUCTION DOUBLER ON NR 1 AIRCON RAM AIR EXHAUST CUTOUT AT STATION Y=561.667 REMOVED IAW SRM 51-31-01-0G. DOUBLER FABRICATED IAW DWG ACA3850 REV AA & INSTALLED IAW SRMSDR U2RA2026091000058Skin · corrodedDURING AIRCRAFT D-CHECK MAINTENANCE DISCOVERED CORROSION ON THE UPPER SKIN OF THE CENTER WING AT STA 1140, BETWEEN LBL 100 AND LBL 110. THE DAMAGE WAS REMOVED PER 747-400BCF SRM AND FOUND TO BE BEYOND PUBLISHED LIMITS.
CORROSION BLENDED OUT AND REPAIR COMPLETSDR DALA2026082604836Skin · damagedACFT SUSTAINED FUSELAGE DAMAGE AFT OF AFT CARGO DOOR, BTWN BS 1329 & 1351, BTWN STR 37 & 39 LT. COMPLIED WITH ER/A 636155-14 REV. (1767817)(AIRCRAFT GROUNDED)SDR DALA2026082004765Skin · dentedDURING LAYOVER IN DFW, THE AIRCRAFT WAS FOUND WITH A DENT ON THE FUSELAGE SKIN FWD FUSELAGE LOWER SKIN BETWEEN FR24-26 AND BETWEEN STR22L-23L. TRIMMED OUT DAMAGED PORTION OF THE SKIN PER ASRP BD 500-J51-00-90-01AAA-018A-A. FABRICATED REPAIR DOUBLERS, FILLERS,SDR SWAA2026092411625Skin · crackedCRACKED INNER CHORD, BS 303.9, STR 17L. REPLACED BTWN BS 270 - 360, STR 17L IAW SRM 51-10-02, ITEM 9, INSTALLED FASTENERS IAW SRM 51-40-02 & DWG 142A0050, SHEET 15, REV -.SDR SWAA2026091139224Skin · crackedCRACK EXTERNAL GROUND ELECTRICAL POWER CUTOUT LOWER AREA AT LOWER FUSELAGE. REPAIRED EXTERNAL GROUND ELECTRICAL POWER DOOR CUTOUT LOWER AREA AT LOWER FUSELAGE IAW SRM 53-10-15-2R-4, REPAIR 4.SDR AALA202608314435Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: LAVATORY SERVICE PANEL PAN CORRODED AROUND THE PERIMETER FASTENERS. MAINTENANCE INSTALLED DOUBLER REPAIR AND FILLER ON FUSELAGE SKIN BETWEEN STA 847 TO 867 AND LBL 22 TO LBL 26 IAW EA 378322 DRAFT #2.SDR AALA202608271103Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: BUBBLED PAINT/ POSSIBLE CORROSION AROUND AFT LAV VENT. CORROSION ON SKIN AT STA 907 TO STA 927, STR 20L TO STR 23 L. MAINTENANCE INSTALLED DOUBLER REPAIR ON SKIN STA 907 TO STA 927, STR 20L TO STR 23 L IAW SRM 53-70-012R PROCEDURESDR CALA2026082518885Skin · crackedREF LOGPAGE 4317946 FOR PREVIOUS REPAIR. NEW LOG IS A REVISED DIP TO ACCOMPLISH BETA INSPECTIONS OF THE EXTERNAL DOUBLER/TRIPLER INTERIM REPAIR INSTALLED ON THE LEFT WING OUTBOARD LOWER SKIN PANEL BETWEEN WSTA 564.5 & 591.5 AT STR L-9 ON A/C 14231 AS GIVEN IN SDR SWIA2026081976951Skin · damagedFOUND LIGHTNING STRIKE ENTRANCE POINT ON RIVET AT STGR27L NEXT TO FRAME 18 (FILED CLOSED)REPLACED 1 DAMAGED RIVET ON LH SKIN @ STGR27L NEXT TO FRAME 18 IN REFERENCE TO ERJ 175 SRM 51-41-02**SEE CP 32576138 FOR LEAK/PRESSURE CHECK SIGN-OFFSDR SWIA2026081976950Skin · damagedFOUND MELTED RIVET ON FR12 1 IN UP OFF 26L 1/2 RADIUS DUE TO LIGHTING STRIKE€? SEE ETD 2026-170-014053 FOR ADDITIONAL INFORMATION. DAMAGE REQUIRES EVALUATION AND DISPOSITION. REPLACED 1 FASTENER ON FUSELAGE SKIN @ FR12 AND STR 26L IN REFERENCE TO SRM 53-0SDR SWIA2026081976949Skin · damagedFOUND 3 BURN MELTED SPOTS ABOVE 25L BY 1/2 IN BETWEEN FR12 AND FR13 ONE IS 1/4 RADIUS ONE IS 1/2 IN RADIUS AND ONE IS 3/4 RADIUS ALL GROUPED TOGETHER IN 1 IN 1/4" LONG DUE TO LIGHTING STRIKE€? SEE ETD 2026-170-014053 FOR ADDITIONAL INFORMATION. DAMAGE REQUIRSDR SWIA2026081976948Skin · damagedFOUND A RIVET ON FR13 JUST ABOVE 25L MELTED DUE TO LIGHTING STRIKE 1/2 RADIUS €ŒSEE ETD 2026-170-014053 FOR ADDITIONAL INFORMATION. DAMAGE REQUIRES EVALUATION AND DISPOSITION. REPLACED 1 FASTENER ON FUSELAGE SKIN @ FR13 JUST ABOVE STR 25L IN REFERENCE TO ESDR SWIA2026081976947Skin · damagedFOUND AN ENTRANCE POINT OF LIGHTING STRIKE, LOOKS WELDED AT 2"BELOW 25L JUST OFF FR13 1/2 IN RADIUS€? SEE ETD 2026-170-014053 FOR ADDITIONAL INFORMATION. DAMAGE REQUIRES EVALUATION AND DISPOSITION. (FILED CLOSED)COMPLIED WITH PERMANENT BLENDING REPAIR OF "
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