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 SWIA2026061577145Skin · damaged6 RIVETS ON STGR 24R BETWEEN FS44550 AND FS45700 6 BURNT RIVETS LOCATED ON STGR 24R FS44550-FS45700 REF TABLE 1 OF REO 670-53-00-719 REV-- TABLE 1 DAMAGE 43, 44, 45, 46, 465, 47 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF DIN 27769127 FOR ASSOCIATED CPS REO 670-SDR SWIA2026061577144Skin · damaged5 SKIN BURN MARKS NEAR STGR 24R AND 25R AND BETWEEN FS43525-FS44550 5 SKIN BURN MARKS NEAR STGR 24R AND 25R AND BETWEEN FS43525-FS44550 REF TABLE 1 OF REO 670-53-00-719 REV-- TABLE 1 DAMAGE 39, 40, 41, 42, 48 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF DIN 2776SDR SWIA2026061577142Skin · damaged9 RIVETS ON STGR 25R BETWEEN FS42200 AND FS43700 9 BURNT RIVETS LOCATED ON STGR 25R BETWEEN FS42200-FS43700 REF TABLE 1 OF REO 670-53-00-719 REV-- DATED 2024-02-15 TABLE 1 DAMAGE 30, 31, 32, 33, 34, 35, 36, 37, 38 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF DIN SDR DALA2026061703619Skin · ground damageTUG STRUCK FWD FUSELAGE RT SIDE. COMPLIED WITH ALL STEPS OF PRI 634968 14 REV 0. COMPLETED STR 22R REPAIR PER B737 SRM 53-00-03-2R PROCEDURE 1 REPAIR 1. COMPLETED PRI 634968-14 REV 03. COMPLETED REPAIR PER ERA 634968-14. COMPLETE ALL RII ACCOMPLISHED. (LOG 164SDR DALA2026061603608Panel · corrodedAFTER REMOVAL OF AFT TOILET SERVICE PANEL CORROSION WAS FOUND AROUND FUSELAGE SKIN BS 1540-1560 S-29R TO S-27R AT LOWER FUSELAGE. FUSELAGE SKIN STA 1540- 1560 S-29R TO S-27R AT LOWER FUSELAGE WAS REPAIRED PER ERA 634606-14 REV. ORIGINAL, SECTION I: REPAIR INSDR SWIA2026061476361Skin · damagedFASTENER HOLE ELONGATED EXTERNAL FUSELAGE SKIN FR19-19A STGR 18L-19L. REPAIRED ELONGATED HOLE ON EXTERNAL FUSELAGE SKIN FR19-19A STGR 18L-19L BY PERFORMING BUSHING REPAIR IAW REF SRM 51-10-07 AND ETD2026-170-010476 REV A.SDR SWIA2026061377699Skin · corrodedSKIN INNER SURFACE IS CORRODED FS33300 - 31900 STGR25L -26L CIRCLED IN RED C-CHECK RO 10132026REMOVED CORROSION FROM SKIN INNER SURFACE AT FS33300, STGR25L - STGR26L PER REF CRJ 900 SRM 51-21-06-001-001-A01 REWORKED AREA IS WITHIN LIMITS PER REO 690-53-21-215SDR REXA2026073001322Skin Splice · corrodedCORROSION ON INTERNAL SKIN SPLICE AT FS 280.00 TO FS 282.00 FROM STGR 24RH TO 26LH CORROSION ON INTERNAL SKIN SPLICE AT FS 280.00 TO FS 282.00 FROM STGR 24RH TO 26LH WAS REMOVED PER CRJ-900 SRM SRM 51-21-06-001-001-A01 EVALUATED BTW FS 280.00 TO FS 282.00 FROMSDR IPXA2026061235641Doubler · corrodedTOILET/WASTE PANEL DRAIN VALVE ASSEMBLY, PAN ASSY (INTERNAL AND EXTERNAL DOUBLER) CORRODEDSDR DALA2026061203547Skin · dentedDURING WALK AROUND FOUND DENT ON RH FWD FUSELAGE 30 MM AFT RADOME FRAME. RELEASED PER SRM A330 53-00-11-283-011- FIG002 ITEM 19 // REPAIR DEFERRED FOR 200 FC FROM ACTUAL FLIGHT. (8179330) AIRCRAFT WAS GROUNDED.SDR CALA2026061517108Skin · ground damageLAV SERVICE VEHICLE HIT AFT LOWER FUSELAGE.DAMAGE AT APPROX. STA 747.5 BY STRINGER S-20L. DAMAGED MEASURED 2.5 INCHES IN LENGTH AND WIDTH IS 8 INCHES. PERFORMED ECRA 5330-07773, LH FUSELAGE SKIN PUNCTURE AT STA 747 & S-20L. NO FURTHER DAMAGE FOUND WITHIN THE 1SDR DALA2026061203546Skin · damagedFUSELAGE VIASAT, FR 64, STR 1L, OVERSIZE HOLES & TOOLING DAMAGE. REPAIRED PER ERA 627660-14 REV C. (1641493) AIRCRAFT WAS GROUNDED.SDR SCNA20260715301Skin · corrodedWO SEVERAL CORROSIONS ON UPPER FUSELAGE SKIN BETWEEN S-4L & S-4R AND B STA 1016 & B STA 1088, AREA COVERED PER VERTICAL STABILIZER. - - CORROSION ON UPPER FUSELAGE SKIN BETWEEN S-4L & S-4R AND B STA 1016 & B STA 1088, AREA COVERED PER VERTICAL STABILIZER WAS RSDR DALA2026061503582Skin · corrodedCORROSION FOUND ON EXTERNAL FUSELAGE SKIN AT FR57-61 STR36-L . C/W ER/A 634830-14AD REV ORIGINAL. (LP# 1639893; AIRCRAFT WAS GROUNDED)SDR AALA202606157076Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION AND BULGING ON FUSELAGE SKIN PANEL JUST BELOW APU OUTLET DOOR BETWEEN FR 65 AND FR 66 AT S32R. REPAIRED SKIN PANEL PER SRM 53-41-11 AND EA 376028.SDR AALA202607221642Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT INTERNAL SKIN PANEL BETWEEN FR 59 AND FR 60, BETWEEN S42L AND S43L. REPAIRED SKIN PANEL PER EA 376515.SDR AALA202606156642Skin · crackedAIRCRAFT IN BASE MAINTENANCE: FATIGUE CRACKING ON FORWARD LEFT HAND FUSELAGE SKIN PANEL RADIATING FROM FASTENER HOLE BETWEEN FR 13 AND FR 14 BETWEEN WL Z+780 AND Z+950. REPAIRED SKIN PANEL PER EA 375972SDR AALA202606159346Skin · crackedAIRCRAFT IN BASE MAINTENANCE: FATIGUE CRACKING ON FORWARD RIGHT HAND FUSELAGE SKIN PANEL RADIATING FROM FASTENER HOLE BETWEEN FR 13 AND FR 14 BETWEEN WL Z+780 AND Z+950. REPAIRED SKIN PANEL PER EA 375973SDR DALA2026061103541Doubler · corrodedER/A 635012-14; A220-100 FUSELAGE REAR BARREL SKIN DOUBLER , WASTE ACCESS AND WASTE BOX ASSY / BTW FR75 - FR76, STR 32L - STR 36L / CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH 635012-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 1,000 SDR DALA2026061003517Skin · crackedCRACK ON FUSELAGE SKIN BTW STA Y=1037 & LONG 14R AT AFT FUSELAGE AREA. FUSELAGE SKIN BTW STA Y=1037 & LONG 14R AT AFT FUSELAGE AREA WAS REPAIRED PER PRI 634847-14 REV. 2 AND ER/A 634847-14 REV. ORIGINAL SECTION 1. (LP 1638764 - AIRCRAFT WAS GROUNDED)SDR DALA2026060903483Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN STA 1087 RT LONG 14R. EXTERNAL FUSELAGE SKIN STA 1087 RT LONG 14R WAS REPAIRED PER PRI 634855-14 REV. 1 AND ER/A 634855-14 REV. ORIGINAL. (LP 1637170 - AIRCRAFT WAS GROUNDED)SDR CALA2026061117003Skin · dentedDAMAGE APPROX 21 INCHES AFT OF FWD AVIONICS DOOR. DENT MEASURES 1"W X 1"L X .030" DEEP. AT FR 16R AND 2 RIVETS UP FROM STGR 36R. DENT IS OUT OF LIMITS, IN RESTRICTED AREA REF. SRM 53-11-11-283-012, FRAME 16 INBETWEEN STRINGER 32 AND 31. DENT IS ON RH FRAMESDR DALA2026060903481Skin · crackedAIRCRAFT 9559, CRACK ON EXTERNAL SKIN STA Y= 1133 BTW PROJECTION LONG 2 RH TO LONG 3 RH AT AFT FUSELAGE SECTION. CORRECTIVE ACTION: CRACK ON EXTERNAL SKIN STA Y= 1133 BTW PROJECTION LONG 2 RH TO LONG 3 RH AT AFT FUSELAGE SECTION WAS REPAIRED PER PRI 634850-14 SDR DALA2026060903479Skin · corrodedLEVEL 2 CORROSION, BULGE ON FUSELAGE SKIN LOCATED APROX 24 INCHES UNDER R2 DOOR CENTER LINE. EVALUATED BULGE ON EXTERNAL FUSELAGE SKIN FOUND DAMAGE TO BE EXFOLIATION CORROSION WITH 100% MATERIAL LOSS PERFORMED DAMAGE CUTOUT AND REPAIR AT FR67 AND STGR 31R/H RSDR DALA2026060903454Skin · damagedPERFORM PERMANENT REPAIR ON LOWER FUSELAGE EXTERNAL SKIN AT BS 720.8, STR 28R. LOWER FUSELAGE EXTERNAL SKIN AT STA 720.8 STR 28R WAS REPAIRED PER B757-300 SRM 53-00-01-2R PROCEDURE 29 REPAIR 29. (1636516) AIRCRAFT WAS GROUNDEDSDR DALA2026060903453Skin · damagedPERFORM PERMANENT REPAIR ON LOWER FUSELAGE EXTERNAL SKIN AT STA720.8 STR 28R. LOWER FUSELAGE EXTERNAL SKIN AT STA 720.8 STR 28R WAS REPAIRED PER B757-300 SRM 53-00-01-2R PROCEDURE 29 REPAIR 29. (1636473) AIRCRAFT WAS GROUNDED.SDR SWIA2026060777030Skin · dentedFUSALAGE SKIN HAS A POSABLE PROTRUDING DENT AT APPROXIMATE BS 241 AND IB OF APPROXIMATE STRINGER 26R. COMPLIED WITH REPAIR OF FUSELAGE SKIN AT APPROXIMATE BS 241 AND INBOARD APPROX STRINGER 26R IAW REO 670-53-11-2333 REV -- ALL STEPS COMPLIED WITH. LEAK CHECKSDR DALA2026060903480Skin · crackedAIRCRAFT 9521, CRACK ON EXTERNAL FUSELAGE SKIN STA 1076 RH BTW LONG 14RH. EXTERNAL FUSELAGE SKIN STA 1076 RH BTW LONG 14RH WAS REPAIRED PER PRI 634869-14 REV 0 AND ERA 634869-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP 1634693 - AIRCRAFT WAS GROUNDED)SDR DALA2026061603603Skin · gougedFOUND GOUGE ON RT AFT FUSELAGE SECT 46 BETWEEN STATIONS 727J AND 727H. COMPLIED WITH SRM 53-00-01-2R-36 PARAGRAPH 4. STEPS A-D. DAMAGE REMOVAL. COMPLIED WITH ER/A 635005-14 REV A SEC LL: PERMANENT REPAIR. (LOG 8888894 - AIRCRAFT WAS GROUNDED).SDR DALA2026060703414Skin · corrodedCORROSION LEVEL 2 ON LOWER SILL BTW BS 1380 TO 1440 AT AFT CARGO COMPARTMENT DOOR CUTOUT. REPLACED AFT CARGO COMPARTMENT DOOR CUTOUT LOWER SILL PER SRM 51-40-02-0G PAR 4. B. AND PAR 7. D. (LP 1633682 - AIRCRAFT WAS GROUNDED)SDR ASAA2026060567093Skin · damagedREF LP 61290055, FUSELAGE SKIN PEELED BACK, UPPER RH SIDE BEHIND RADOME. GROUNDED - YES. ACCOMPLISHED CATEGORY "B" MAJOR REPAIR TO FUSELAGE SKIN P/N 141A3721-62 AT STA 178BETWEEN WL220-240 IAW EA M9-53EA-30452 REV 00 DATED 06/25/2026 NEW 8100-9 TO BE ISSUED WISDR ASAA2026060566998Skin · damagedREF LP 61290055, FUSELAGE SKIN PEELED BACK, UPPER RH SIDE BEHIND RADOME. GROUNDED - YES. ACCOMPLISHED CATEGORY "B" MAJOR REPAIR TO FUSELAGE SKIN P/N 141A3721-62 AT STA 178BETWEEN WL220-240 IAW EA M9-53EA-30452 REV 00 DATED 06/25/2026THIS TERMINATES MCT DEFSDR CALA2026061217062Skin · damagedINSPECTION REQUIREMENTS OF THE LATEST VERSION OF ECRA 5310-08928 PRIOR TO JUNE 03, 2027. PERFORM PART 2 - INSPECTION REQUIREMENTS OF THE LATEST VERSION OF ECRA 5310-08928 PRIOR TO JUNE 03, 2027.SDR DALA2026060903494Skin · corrodedDURING C2 + 6 YEAR (HEAVY) CHECK IN MSP, MAINTENANCE WAS ACCOMPLISHING THE EO 5331-01297-01C WORKCARD / SB BD500-530010 MODIFICATION WHEN CORROSION WAS FOUND COMMON TO THE FUSELAGE LOWER AND BOTTOM SKIN PANELS AT THE FWD CARGO DOOR CUTOUT. COMPLIED WITH ER/A 6SDR DALA2026060903492Skin · corrodedDURING C2 + 6Y ( H ) CHECK IN MSP, DAL FOUND CORROSION LOCALIZED AROUND THE SKIN SCUFF PLATE ATTACH HOLES PREVIOUSLY REPAIRED VIA REO 500-53-21-651. MTC REQUIRES ENGINEERING AUTHORITY TO ACCOMPLISH EO WORKCARD 533101297-01B (SB BD500-530010 ISSUE 004 PART B) OSDR DALA2026060903464Skin · damagedFR 24 / STRINGER 4R TO 5R / VIASAT TOOLING DAMAGE. COMPLIED WITH ERA 630752-14. (1631438) AIRCRAFT WAS GROUNDED.SDR DALA2026060903463Bracket · mislocatedFR 23 / S-5R TO S-6R / VIASAT BRACKET MIS-LOCATED AND TOOLING DAMAGE. COMPLIED WITH ERA 630770-14. (1631552) AIRCRAFT WAS GROUNDEDSDR FDEA202606050673Skin · damagedREQUEST A PERMANENT REPAIR ON AFT FUSELAGE SKIN STA 2319 TO STA 2344.5, S-48R TO S-49R.SDR SWIA2026060476190Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN FS 830.40 - FS 847.00 AND STRG 1L - STRG 0 DUE TO THE DEMODIFICATION OF ATG WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR) (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSDR HNAA2026070300569Skin · gougedLT CENTER I LOWER FUSELAGE EXTERIOR SKIN GOUGED BTW FR 19-20 AND BTW STRINGERS 16L-17L. PERFORMED DOUBLER AND FILLER REPAIR ON LT CENTER 1 LOWER FUSELAGE SKIN BETWEEN FR 19-20 AND STRINGERS 16L-17L IAW ETD2026-145-009805 AND EO1-53-26-0282.SDR 1Q2R2026061800001Skin · gougedTWO (2) RIVETS FOUND PULLED THROUGH SKIN ON PATCH AT AFT LOWER FUSELAGE AREA (FS801.25 TO FS977.00, STR27). PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-128886 REV. 0, AND REO 670-53-00-830 REV. --.SDR SWIA2026060476192Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 1000.00 - FS 1015.00 AND STRG 25R - STRG 26R DUE TO THE DEMODIFICATION OF ATG WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR). PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FSDR SWIA2026060476191Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 581.00 - FS 597.00 AND STRG 24R - STRG 25R DUE TO THE DEMODIFICATION OF ATG WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR). PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSDR UIEA2026060300444Skin · dentedDENT ON FUSELAGE AT BS 640, STRINGER 43R - 44R WITHIN SRM LIMITS, ACCOMPLISHED EI T2026A53M-1074 REV 1 AND SRM 53-00-01-2R-10 REPAIR 10 REV 48. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR SWIA2026060277654Skin · gougedAFT FUSELAGE SKIN GOUGED BETWEEN FS91300 - FS92700 STGR27 AS MARKED C-CHECK RO 10132026PERFORMED REPAIR AT AFT FUSELAGE SKIN BETWEEN FS91300 - FS92700 STGR27 REF REO REO 670-53-00-290 REV-F DATE2019-04-26COMPLIED WITH TASK CARD 51-900-1002-SKY NO LEAKS DETECSDR AALA202606245986Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FUSELAGE SKIN PANEL INTERNAL SURFACE AT FR 59 BETWEEN S42L AND S43L. REPAIRED SKIN PANEL PER EA 375970.SDR N6WA2026060306Skin · gougedGOUGED ON SKIN AT FS977 STRINGER 27. PERFORMED PERMANENT REPAIR ON FUSELAGE SKIN AT FS977-FS985 IAW GOJET EO C550-53MR-108 REV O.SDR SWIA2026060276189Skin · dentedINSPECTED SKIN DEFORMATION/DENT OBSERVED BTWN FR10 & FR12, STR 14 THROUGH STR 16, DAMAGED AREA INITIATES APPROX 2.00 IN FWD OF FR10 & EXTENTS AFT TO FR12. OVERALL AFFECTED AREA MESSURES 27.0 IN IN LENGTH & 7 INCHES IN WIDTH, WITH A MAX DEPTH OF 0.204 IN ALONGSDR SWIA2026060177648Skin · damagedLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN 7 EA FROM FS693 TO FS881, STR12L TO STR16L C-CHECK RO 10132026REPAIRED LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN 7 EA FROM FS693 TO FS881, STR12L TO STR16L BY COMPLYING WITH ALL STEPS OF REO 690-53SDR SWIA2026060177290Skin · corrodedDURING AAI AUDIT IT WAS FOUND THAT THERE IS POSSIBLE CORROSION AROUND THE LOWER SIDE OF THE AFT LAVATORY SERVICING POINT. REPAIRED AROUND THE LOWER SIDE OF THE AFT LAVATORY SERVICING POINT IAW REO 601R-53-51-748 REV -. PERFORMED DISPOSITIONS 1 TO 5, ENSU
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