JASC 5330
Service difficulty reports · 79,329
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 A6WA202012187465Skin · gougedUPPER FUSELAGE SKIN AT ADF ANTENNA MATING SURFACE HAS SCRIBE MARKS AROUND OUTER EDGE. AIRCRAFT REMOVED FROM SERVICE. BLENDED AREA TO SMOOTH CONTOUR AT FS 409+64 TO FS 409+80, STR 1L TO STR 1R. REMOVED AND REPLACED SOLID FASTENER AT BLENDED AREA, REF ASAP EASDR A6WA202012187464Skin · corrodedUPPER FUSELAGE ADF ANTENNA HAS PITTING CORROSION AROUND OUTER EDGES. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON UPPER SKIN FS 409+64 TO FS 409+80, STR 1L AND STR 1R. REMOVED AND REPLACED SOLID FASTENER AT BLENDED AREA, REF ASAP EA: AWAC-CRJ253-0154SDR DALA2020121404077Skin · dentedDENT ON EXTERNAL SKIN LOCATED BETWEEN FR 81 TO FR 82 AND STR 2L TO STR 3L ON UPPER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED BETWEEN FR 81 TO FR 82 STR 2L TO STR 3L ON UPPER FUSELAGE, AS PER SRM A320 53-51-11.SDR SWIA202055736Skin · gougedFUSELAGE SKIN IS GOUGED 4 PLACES JUST AFT OF PASSENGER DOOR HINGE BETWEEN STR 17L AND 18L. (C-CHECK) RO 2/1/2021 COMPLIED WITH REPAIR OF FUSELAGE SKIN IS GOUGES 4 PLACES JUST AFT OF PASSENGER DOOR HINGE BETWEEN STR 17L AND 18L. IAW MHIRJ REO 601R-53-21-3SDR YENA2020121400593Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION EXTERNAL SKIN VACUUM VALVE BETWEEN FR 60 TO FR 70 RT SIDE LOWER FUSELAGE, REF AEROMAN N/R 2020-375163 WO 2020 88/1. PERFORMED PERMANENT REPAIR ON EXTERNAL FUSELAGE LOCATED BETWEEN FR 69 TO FR 70 AND STR 30R TO STR 33R, IAW SDR DALA2020121104052Skin · crackedDURING ROUTINE MAINTENANCE FOUND A SKIN BULGE AND CRACK NEAR DRAIN PORT AT FS 24 AND STRINGER 44. CORRECTIVE ACTION: ACCOMPLISHED REPAIR, PER ER/A 588926-14.SDR CALA2020121001363Skin · dentedSKIN PROTRUSION ON THE LEFT HAND AIRCRAFT EXTERIOR SKIN 1.2L X 0.8W. LOCATED APPROXIMATELY 4.6" AFT OF FRAME 72 AND 1.2" ABOVE STR 28L. EVALUATED SKIN PROTRUSION ON AIRCRAFT EXTERIOR SKIN. FOUND PROTRUSION TO MEASURE 1.2"(L) X .8" (W) X .030" (D). FOUND TOSDR SWAA2020121035432Skin · gougedGOUGE IN RIGHT HAND SIDE FUSELAGE AFT OF STATION 727H BETWEEN STRINGERS 25R AND 26R. FOUND TO BE OUT OF LIMITS IN AREA B, PER TABLE 107 PER SRM 53-00-01-1A-5. PERMANENT REPAIR REQUIRED WITHIN 50 FLIGHT HOURS. A/C 8674 IS PRE SERVICE BULLETIN 737-21-1149. RSDR 6PMR1024800441210Skin · gougedEXT FUSELAGE SKIN HAS GOUGES AT STA 1680-1690 AT STR 17L. CORRECTIVE ACTION: BLENDED GOUGES, IAW EA PD 57-53-350 PEMCO NON-ROUTINE 10248-0044.SDR SWIA202056173Skin · corroded*FREEZE PLUG IN THE SKIN IS CORRODED BETWEEN FS295 AND FS310, AND STGR25L AND STGR24L. (MARKED) (C-CHECK) RO 2/9/2021 REPAIRED SKIN AREA BETWEEN F.S 295 AND F.S 310, STR25L AND 24L REF. MHIRJ REO 601R-53-21-3376 REV. -- DATED 2021-01-06. COMPLIED WITH TASKSDR SWIA202055325Skin · chafedFOUND FUSELAGE SKIN CHAFED AT FS 984 TO FS 983 IN PREVIOUSLY BLENDED AREA APPROXIMATELY .060 WIDE BY .-05 DEEP BY 3 IN LONG. ALSO PANEL 196DR NUPLATE CHANNEL IS CHAFED AND WILL NEED THE TO REACCOMPLISHED. C-CHECK RO 1/6/2021 REPAIRED DAMAGE, IAW REO 670-53SDR FDEA202012093216Skin · dentedLOWER FWD CARGO COMPT LOWER AFT DOOR FRAME, BY PREVIOUS REPAIRED DOUBLER, SHOW DOOR FRAME EDGE IMPACTED BY EQUIPMENT. REMOVED AND REPLACED EXISTING SRM REPAIR AT NOTED LOCATION, REF SRM 53-00-15-2R FIG 202 SHEET 2.SDR DALA2020121004042Skin · dentedDENT EXTERNAL SKIN LOCATED BETWEEN FR 79 TO FR 80 AND STR 4R TO STR 5R ON UPPER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON SKIN LOCATED BETWEEN FR 79 TO FR 80 AND STR 4R TO STR 5R ON UPPER FUSELAGE, AS PER A320 SRM-53-51-11-300- 002.SDR 2020F00486Skin · chafedREPAIR LOWER SKIN CHAFED FROM ANTI-ICE CROSS-FLOW VALVE. ACCOMPLISHED TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-22175 DATED 07/19/2019, STANDARD REPAIR - 680A ALL S/N LOWER SKIN CHAFE FROM ANTI-ICE CROSS-FLOW VALVE. WITH FAA FORM 8100-9 DATED 07/19/2019SDR DU4R2020120900057Skin · dentedDURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FL FOUND LT FUSELAGE SKIN FR 555+2, STR 29L HAS A DENT. S/O 1930115 N/R 22046.SDR SWIA202057490Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA48156-601R-53-61-6986 MXCODEID46346-PR - LEFT SIDE FUSELAGE AREA BELOW CARGO DOOR SCUFF PLATE HAS 6 DENTS BETWEEN FS 605.00 - FS 621.00 AND STGR 17 - STGR 20. PERFORMED TEMP REPAIR PER REO 601R-53-61-6986 REV -- DATESDR SWIA202056168Skin · corroded* THE LOWER FUSELAGE SKIN'S EXTERNAL SURFACE HAS CORROSION AND CHAFING UNDER ACCESS PANEL 195BB, BETWEEN FS 559+112 AND FS 574, AND BETWEEN STRINGERS 21L AND 21R. (C-CHECK) RO 2/9/2021 REMOVED THE CORROSION AND CHAFFING UNDER ACCESS PANEL 195BB BETWEEN FS.SDR SWIA202055703Skin · corrodedEXTERNAL SKIN - RIVETS/SKIN SHOW EVIDENCE OF CORROSION AS MARKED - BTWN STGRS 26L/26R AND FS'S 559/559+32 (C-CHECK) RO 1/29/2021 REMOVED CORROSION AND REPLACED REQUIRED RIVETS, COMPLIED WITH REO 601R-53-51-546 REV-- DATED: 2021-01-03 STEP 1 TO 5, CRJ 200 SSDR SWIA202055700Skin · corrodedEXTERNAL SKIN - RIVETS/SKIN SHOW EVIDENCE OF CORROSION MULTIPLE AREAS AS MARKED - STGR 23R BTWN FS'S 559+80/+112 (C-CHECK) RO 1/29/2021 REMOVED CORROSION ON EXTERNAL SKIN - RIVETS/SKIN - STGR 23R BTWN FS'S 559+80/+112 TO ACCEPTABLE LIMITS REF. REO 601R-53SDR SWIA202055698Skin · corrodedEXTERNAL SKIN - EXTERNAL AFT LAV DUMP VALVE DOUBLER RIVETS/SKIN CORRODED MULTIPE AREAS AS MARKED - BTWN FS'S 559+80/+112 AND BTWN STGRS 20R/24R (C-CHECK) RO 1/29/2021 REMOVED CORROSION FROM LAV DUMP VALVE DOUBLER FS559+80/+112 BETWEEN STR20R - STR24R REF. SDR SWIA202055697Skin · corrodedEXTERNAL SKIN - RIVETS/SKIN SHOW EVIDENCE OF CORROSION AS MARKED - FS 559+96 AND BTWN STGRS 23R/24R (C-CHECK) RO 1/29/2021 REMOVED CORROSION FROM EXTERNAL SKIN AT FS559+96 BTWN STGRS 23R/24R AND REPLACED REQUIRED FASTENERS REF CRJ200 SRM 51-12-00 & 51-42-0SDR SWIA202055696Skin · corrodedEXTERNAL SKIN - RIVETS/SKIN SHOW EVIDENCE OF CORROSION AS MARKED - FS 559+112 BTWN STGRS 23R/24R (C-CHECK) RO 1/29/2021 REMOVED CORROSION FROM EXTERNAL SKIN - RIVETS/SKIN AT FS 559+112 BTWN STGRS 23R/24R TO ACCEPTABLE LIMITS REF. CRJ200 SRM 51-12-00 AND RSDR SWIA202055695Skin · corrodedEXTERNAL SKIN - RIVETS/SKIN SHOW EVIDENCE OF CORROSION AT MULTIPOLE AREAS AS MARKED - STGR 24R BTWN FS'S 559+80/+121 (C-CHECK) RO 1/29/2021 REMOVED CORROSION FROM MULTIPLE AREAS BETWEEN STR24R FS559+80/+121 FROM THE WING TO FUSELAGE AFT FAIRING SUPPORT BEASDR SWIA202055694Skin · corrodedEXTERNAL SKIN - RIVETS/SKIN SHOW EVIDENCE OF CORROSION AS MARKED - BTWN FS'S 559+80/+112 AND STGRS 26L/26R (C-CHECK) RO 1/29/2021 REMOVED CORROSION FROM EXTERNAL SKIN BTWN FS'S 559+80/+112 AND STGRS 26L/26R REF. CRJ 200 SRM 51-21-06 / EXTERNAL SKIN AT FS5SDR SWIA202055693Skin · corrodedEXTERNAL SKIN - RIVETS/SKIN SHOW EVIDENCE OF CORROSION AS MARKED - STGR 26L BTWN FS'S 559+96/+112 (C-CHECK) RO 1/29/2021 REMOVED CORROSION EXTERNAL SKIN AT STGR 26L BTWN FS'S 559+96/+112, WITHIN LIMITS REF REO 601R-53-51-546 REV-- DATED: 2021-01-03 AND CRJSDR SWAA2020123135300Filler · crackedREPAIR FILLER AT THE AFT SIDE OF THE EXTERNAL POWER DOOR CUTOUT IS CRACKED, MARKED. REMOVED DAMAGE, PER SRM 51-10-2. REPAIRED AS PER EA 20-153-02577 REV IR AND ATS ER 20-03722 REV IR.SDR DALA2020121004039Skin · damagedDURING INSPECTION MAINTENANCE FOUND DAMAGE T: TOOLING MARK ON LOWER EXTERNAL SKIN, STA 1601, RBL 2 WAS CAUSED DURING INTERCOSTAL INSTALLATION. DAMAGE AREA WAS REPAIRED, PER SRM 53-00-01-2R-29.SDR SWIA202055688Doubler · corroded* ANTENNA DOUBLER BETWEEN FS295.00 AND FS310.00/STGR 27 IS CORRODED. FLAGGED (C-CHECK) RO 1/29/2021 REMOVED AND INSTALLED NEW TCAS DOUBLER REF. CRJ 200 SRM 51-42-06 AND DWG 601R31022 REV. NC, COMPLIED WITH TASK CARD 51-900-1003-SKY. ALL ASSOCIATED CHECKS SDR SWAA2021011338510Bear Strap · crackedCRACK INDICATION FOUND ON BEAR STRAP AREA (INTERNAL) AROUND TO FASTENER LOCATED AT BS 294.5 BETWEEN S-8R TO S-9R NEAR TO FITTING LATCH FWD GALLEY DOOR (R1) CRACK LENGTH: 0.750 INCH APPROXIMATE. REPAIRED FUSELAGE SKIN BETWEEN BS 277 TO BS 312 STR 6R TO STR 10RSDR UATA202101073314Skin · crackedAIRFRAME SKIN CRACKED TO THE EDGE ON LT SIDE OF CENTER WING CUTOUT AT FR 5. REMOVED DAMAGE, FABRICATED A FLUSH PATCH AND DOUBLER, IAW CASA SRM APPX II FIG B9.SDR UATA202101073313Skin · crackedAIRFRAME SKIN CRACKED TO THE EDGE ON RT FWD SIDE OF CENTER WING CUTOUT AT FR 5. REMOVED DAMAGE, FABRICATED A FLUSH PATCH AND DOUBLER, IAW CASA SRM APPX II FIG B9.SDR R61A2020122100915Skin · dentedPROTRUDING DENT EXTERNAL SKIN FWD FUSELAGE BETWEEN FR 18 AND FR 19 AND STR 24L AND 25L. REPAIRED DENT, IAW EMB SRM 53-10-01.SDR JJBA20201207007Skin · canningDENT WITH OIL CANNING EFFECT ON LT CENTER FUSE 1, BETWEEN FR 20-21 AND BETWEEN STR 13P-14P. DENT WITH OIL CANNING AT LT CENTER FUSE 1, BETWEEN FR 20-21, AND BETWEEN STR 13P-14P REPAIRED.SDR CALA2020120901349Skin · damagedUPON ARRIVAL ORD, GOUGE WAS BLENDED, PER SRM 53-11-11-283-001 AND HFEC ACCOMPLISHED PER NTM 51-10-08 WITH NO CRACKS FOUND. ULTRA SOUND WAS ACCOMPLISHED, PER NTM PT4-00-04-02 AND MEASURMENTS ISSUED ON MATRIX. BLEND IS LOCATED APPROXIMATELY 11.5" AFT OF STATIC SDR SWIA202056316Skin · dentedMULTIPLE DENTS FOUND ON RT SIDE OF FUSELAGE BETWEEN LE OF WING AND AFT OF SERVICE DOOR JUST ABOVE FLOOR LINE. ALL DENTS MARKED. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECSDR SWIA202054716Skin · chafedFUSELAGE CHAFE DAMAGE DISCOVERED BETWEEN THE PYLON TRAILING EDGE FAIRING CAUSED BY THE RUB STRIP RIGHT HAND SIDE OUT OF LIMITS IN NUMEROUS AREAS BETWEEN FS 700 AND FS 755 AND STR 9-12. COMPLY WITH REO MAJOR REPAIR. COMPLIED WITH REO FOR FUSELAGE CHAFE DAMAGESDR R61A2020122100914Skin · dentedPROTRUDING DENT LOCATED BETWEEN FR 19 AND FR 19A STR 23L AND 24L. REPAIRED DENT IAW EMB SRM 53-10-01.SDR SIMA20201206005Skin · damagedCENTER FUSELAGE I SKIN DAMAGED FRAME 23-24, STRINGERS 22R-25R. C/A: REPAIRED DAMAGE TO CENTER FUSELAGE I SKIN FRAME 23-24 STRINGERS 22R-25R, IAW ENVOY ERS-EJ-53MR-4224.SDR FDEA202012063050Skin · damagedLOWER FUSELAGE SKINS BETWEEN STA 1540 AND STA 1640 STRINGERS S-30 TO S-26L HAS NUMEROUS PLACES OF DAMAGE. COMPLIED WITH EA F-5330-T0358203 TITLED: FUSELAGE-SECTION 46 LOWER SECTION-REPAIR OF FUSELAGE SKIN INPACT DAMAGE AT STA 1624; S-29L AND EA F-5330-T035820SDR MASA20201229148Doubler · corrodedAWR HIDDEN DAMAGE IN REF NRC S/N 00252, AFTER INTERNAL PRODUCTION DOUBLER REMOVAL, CORROSION ON INTERNAL FUSELAGE SKIN WAS FOUND ON DOUBLER SETTLEMENT AREA. CORRECTIVE ACTION: AFTER INTERNAL PRODUCTION DOUBLER REMOVAL, ON INTERNAL FUSELAGE SKIN WAS FOUND ON DSDR SIMA20201205004Skin · damagedFUSELAGE EXTERNAL SKIN DENTED AND GOUGED BETWEEN FR 23/24 AND STR 22R/25R. MAJOR REPAIR. C/A: ACCOMPLISED REPAIR TO CENTER FUSELAGE 1 SKINS BETWEEN FRAMES 23-24 AND STRINGERS 22R-25R, IAW ERS-EJ-53MR-4224.SDR SIMA20201205003Skin · damagedFUSELAGE EXTERNAL SKIN DENTED AND GOUGED BETWEEN FR 25/27 AND STR 26L/27R. MAJOR REPAIR. C/A: ACCOMPLISHED REPAIR TO CENTER FUSELAGE I SKINS BETWEEN FRAMES 25-26 AND STR V26L-27R, IAW ERS-EJ-53MR-4225.SDR HNAA2020121200351Skin · deformedFUSELAGE EXTERNAL SKIN DEFORMED BETWEEN FR 12A/13 STR 6R/7R. ACCOMPLISHED REPAIR OF FUSELAGE EXTERNAL SKIN AT UPPER AFT CORNER OF RT DV WINDOW BETWEEN FR 12A-13 STGR 6R-7R, IAW PIEDMONT EO1--53-20-0422.SDR UIEA2020111002376Skin · damagedREF DMI 127742 LP 1158798. CORROSION DAMAGE ON SKIN PANEL (P/N 146T3230-1) NEAR STA 1329, S-35L-CATEGORY-C TIME LIMITED REPAIR CW PART 3 OF EO 6753A851 PERMANENT REPAIR. COMPLIED WITH INSTALLATION OF PERMANENT REPAIR AT STA 1324-1460 STR 33L-39L, PER PART 3 SDR DALA2024022902863Skin · damagedSHIP 5646 LIGHTNING STRIKE DAMAGE TO THE 143N3121-4 UPPER SKIN IN THE S-4L LAP AT BS 822. CORRECTIVE ACTION: REF ERA 483952-14. (1670263)SDR DALA2023062805194Unknown · unknownSHIP 679 ERA 588672-14 SECTION I ISSUED FOR 2 DENTS FOUND BTWEEN 500-520 BETWEEN S27L AND 28L. CORRECTIVE ACTION: SUMMARY OF NR 00259. AREA WAS REPAIRED PER ER/A 588672-14 REV A SECTION III: PERMANTENT REPAIR. (1670742)SDR MASA20201228143Skin · corrodedHIDDEN DISCREPANCY IN REF NRC S/N 00733 DURING LOWER TCAS ANTENNA REMOVAL CORROSION ON EXTERNAL FUSELAGE SKIN WAS FOUND (SETTLEMENT ON ANTENNA AREA). CORRECTIVE ACTION: CORROSION ON EXTERNAL FUSELAGE SKIN (SETTLEMENT ON ANTENNA AREA) WAS REPAIRED PER REO 670SDR HALA2020121000143Skin · corrodedAFT FUSELAGE SKIN BETWEEN FR 77-FR 80, BETWEEN STRINGER 40L AND STRINGER 43L FOUND MULTIPLE FASTENER HEADS CORRODED. CORRECTIVE ACTION: REFER TO NRC 100-017 SVO: 37226895 FOR PAINTING STRIPPING CARRIED OUT. ALL CORRODED FASTENERS REMOVED AND REPLACED, AS PERSDR HALA2020120900118Skin · corrodedCORROSION, AFT FUSELAGE SKIN AT FR 76, BETWEEN STRINGER 48L AND STRINGER 51L FOUND MULTIPLE FASTENER HEADS CORRODED. CORRECTIVE ACTION: REFER TO NRC 100-017 SVO: 37226895 FOR PAINT STRIPPING CARRIED OUT. ALL CORRODED FASTENERS REMOVED, AS PER SRM. INSPECTIOSDR DALA2020120804000Skin · corrodedDURING INITIAL INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AT AFT LAVATORY SERVICE DOOR FUSELAGE SKIN BETWEEN STA 1701-1681.80 & S-29R TO S-26R. REPAIRED PER ERA.
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