N930SW

Service difficulty reports · 233

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N930SW' AND registry_match = 'registration'
  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.

SDR SWIA202164231None · corrodedLH FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS.409.00+128 TO FS.529.00. (C CHECK RO 2-11-2022) REPAIRED LH FLOOR SILL MULITPLE SPOTS OF CORROSION FROM FS 409.00+128 TO FS 529.00 IAW BOMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06 AND SKY CARD 5Nov 28, 2021 · N930SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164230None · corrodedRH FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS.424.00 TO FS.473.15. (C CHECK RO 2-11-2022) COMPLIED WITH BOMBARDIER REO 601R-53-41-666 REV-C DATED: 2012-11-06. COMPLIED WITH SKY CARD 51-900-1003-SKY AND 337 COMPLETED. WEIGHT AND BALANCE NOT EFFECTENov 28, 2021 · N930SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164269None · corrodedCROSSBEAM CAP AT FS 589 HAS MULTILE SPOTS OF CORROSION BETWEEN RBL24 AND RBL45 (C CHECK RO 2-11-2022) REMOVED AND REPLACED CROSSBEAM CAP AT FS 589 RBL24 - RBL 45 IAW CRJ 200 SRM 51-42-15 AND SRM 51-42-06Nov 27, 2021 · N930SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164268None · corrodedCROSSBEAM CAP AT FS 589 HAS MULTIPLE SPOTS OF CORROSION BETWEEN LBL 9 AND LBL 27 (C CHECK RO 2-11-2022) REMOVED AND REPLACED CROSSBEAM CAP AT FS 589 BETWEEN LBL9 AND LBL27 IAW CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21, AND CRJ 200 SRM 51-40-11Nov 27, 2021 · N930SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164259None · corrodedRH SIDE SEAT TRACK BETWEEN FS 499.00 AND FS 559.00+80 IS CORRODED. (C CHECK RO 2-11-2022) REMOVED AND REPLACED RH SIDE SEAT TRACK BETWEEN FS 499.00 AND FS 559.00+80 IAW CRJ 200 AMM 53-01-11-400-802 REFERENCE CONTINUE CARD FOR WORK PERFORMED.Nov 27, 2021 · N930SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164258None · corrodedLH SIDE SEAT TRACK BETWEEN FS 499.00 AND FS 559.00+80 IS CORRODED. (C CHECK RO 2-11-2022) REMOVED AND REPLACED L/H SEAT TRACK BETWEEN FS 499.00 AND FS 559.00+80 IAW CRJ 200 AMM 53-01-11-400-802. REFERENCE CONTINUE CARD FOR WORK PERFORMED.Nov 27, 2021 · N930SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164257None · corrodedRH SIDE SEAT TRACK BETWEEN FS 449.00 AND FS 499.00 IS CORRODED. (C CHECK RO 2-11-2022) REMOVED AND REPLACED R/H SIDE SEAT TRACK BETWEEN FS 449.00 AND FS 499.00 IAW CRJ 200 AMM 53-01-11-400-802. REFERENCE CONTINUE CARD FOR WORK PERFORMED .Nov 27, 2021 · N930SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164256None · corrodedLH SIDE SEAT TRACK BETWEEN FS 449.00 AND FS 499.00 IS CORRODED. (C CHECK RO 2-11-2022) REMOVED AND REPLACED LH SIDE SEAT TRACK BETWEEN FS 449.00 AND FS 499.00 IAW CRJ 200 AMM 53-00-49-000/400-801 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMEDNov 27, 2021 · N930SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164255None · corrodedRH SIDE SEAT TRACK BETWEEN FS 364.00 AND FS 409.00+16 IS CORRODED (C CHECK RO 2-11-2022) REMOVED AND REPLACED RH SIDE SEAT TRACK BETWEEN FS 364.00 AND FS 409.00+16 IAW CRJ200 AMM 53-01-11-000-802 AND 53-01-11-400-802.Nov 27, 2021 · N930SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164254None · corrodedRH SEAT RAIL STRUCTURE TRIM RETAINER BETWEEN FS 409.00+16 AND FS 409.00+64 IS CORRODED. (C CHECK RO 2-11-2022) REMOVED AND REPLACED RH SEAT RAIL STRUCTURE TRIM RETAINER BETWEEN FS 409.00+16 AND FS 409.00+64 BY REMOVING SEAT TRACK THAT HOLD RETAINER IN POSINov 27, 2021 · N930SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164253None · corrodedRH SEAT RAIL STRUCTURE TRIM RETAINER BETWEEN FS 364.00 AND FS 409.00+16 IS CORRODED. (C CHECK RO 2-11-2022) REMOVED AND REPLACED RH SEAT RAIL STRUCTURE TRIM RETAINER BETWEEN FS 364.00 AND FS 409.00+16 IAW CRJ200 AMM 53-01-11-000-802 , 53-01-11-400-802 ANDNov 27, 2021 · N930SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164252None · corrodedLH SEAT RAIL STRUCTURE TRIM RETAINER BETWEEN FS 409.00+64 AND FS 409.00+112 IS CORRODED. (C CHECK RO 2-11-2022) REMOVED CORROSION FROM LH SEAT RAIL RETAINER FROM FS 409+64 -FS 409+112 IAW CRJ 200 SRM 51-21-06 AND FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 5Nov 27, 2021 · N930SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164251None · corrodedLH SEAT RAIL STRUCTURE TRIM RETAINER BETWEEN FS 409.00+16 AND FS 409.00+64 IS CORRODED. (C CHECK RO 2-11-2022) REMOVED CORROSION FROM LH SEAT RAIL RETAINER FROM FS 409+16 - FS 409+64 IAW CRJ 200 SRM 51-21-06 AND FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 5Nov 27, 2021 · N930SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164250None · corrodedLH SEAT RAIL STRUCTURE TRIM RETAINER BETWEEN FS 364.00 AND FS 409.00+16 IS CORRODED. (C CHECK RO 2-11-2022) REMOVED CORROSION FROM LH SEAT RAIL RETAINER FROM FS 364 - FS 409+16 IAW CRJ 200 SRM 51-21-06 AND FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 53-00-0Nov 27, 2021 · N930SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164249None · corrodedLH SIDE SEAT TRACK BETWEEN FS 409.00+112 AND FS 449.85 IS CORRODED. (C CHECK RO 2-11-2022) REMOVED AND REPLACED LH SIDE SEAT TRACK BETWEEN FS 409.00+112 - FS 449.85 IAW CRJ200 AMM 53-01-11-000-802 AND 53-01-11-400-802.Nov 27, 2021 · N930SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164248None · corrodedLH SIDE SEAT TRACK BETWEEN FS 409.00+16 FS 409.00+112 IS CORRODED. (C CHECK RO 2-11-2022) REMOVED AND REPLACED LH SIDE SEAT TRACK BETWEEN FS 409.00+16 - FS 409.00+112 IAW CRJ200 AMM 53-01-11-000-802 AND 53-01-11-400-802.Nov 27, 2021 · N930SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164267None · corrodedSTRINGER 21L CORRODED BETWEEN FS 333.00 AND FS 349.00. (C CHECK RO 2-11-2022) FOUND CORROSION TO BE ON INTERCOSTAL NOT ON THE STRINGER REMOVED AND REPLACED STRINGER 21L INTERCOSTAL BETWEEN FS 333 AND FS 349 IAW CRJ 200 SRM 51-42-21 AND BOMBARDIER DRAWING 6Nov 26, 2021 · N930SW · Cndair CL6002B19 · Fuselage Main, KeelSDR SWIA202164229None · corrodedFRAME CORRODED AT FS 333.00 BETWEEN STGR 26L AND STGR 26R. (C CHECK RO 2-11-2022) REMOVED AND REPLACED FRAME AT FS333.00 STGR 23L AND 23R IAW CRJ 200 SRM 51-42-21, 51-42-06, BOMBARDIER DWG 601R32001 REV W DATED 2005/06/22 AND SKY CARD 51-900-1003-SKY NO WENov 26, 2021 · N930SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202164228None · corrodedFRAME CORRODED AT FS 319.70 BETWEEN STGR 25L AND STGR 27. (C CHECK RO 2-11-2022) REMOVED AND REPLACED FRAME AT FS 319.70 BETWEEN 25L AND STGR 27 IAW CRJ 200 SRM 51-42-06, 51-42-21, BOMBARDIER DRAWING 601R31022 REV NC AND SKY CARD 51-900-1003-SKY NO WEIGHTNov 26, 2021 · N930SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202164227None · corrodedFRAME CORRODED AT FS 310.00 BETWEEN STGR 23L AND STGR 27. (C CHECK RO 2-11-2022) COMPLIED WITH REPLACEMENT OF F.S. 310.00 FRAME BETWEEN STR 23L AND STR 23R IAW CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED CONov 26, 2021 · N930SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202164226None · corrodedFRAME CORRODED AT FS 295.00 BETWEEN STGR 27 AND STGR 25L. (C CHECK RO 2-11-2022) COMPLIED WITH REPLACEMENT OF F.S. 295.00 FRAME BETWEEN STR 24L AND STR 24R IAW CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21, COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED CONov 26, 2021 · N930SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202164225None · elongatedRIGHT HAND WING PANEL 684CB HAS AN ELONGATED FASTENER HOLE IN IT AND IN SUPPPORTING STRUCTURE. (C CHECK RO 2-11-2022) REPAIRED RH INBOARD FLAP AT PANEL 684CB IAW MHIRJ REO 601R-57-2441 REV -- DATED 2022-01-27. ATTACHED COMPLETED MAJOR REPAIR TASK CARD 51-Nov 19, 2021 · N930SW · Cndair CL6002B19 · Wing StructureSDR SWIA202164279None · failedDURING BACKLASH CHECK OF THE R/H I/B FLIGHT SPOILER, FOUND THE MAXIMUM BACKLASH TO BE 0.130 (MAX ALLOWABLE LIMIT IS 0.114) (C CHECK RO 2-11-2022) REMOVED AND REPLACED RH IB FLIGHT SPOILER MOUNTING HARDWARE IAW CRJ 200 AMM 27-62-01-000/400-801 BACKLASH CHECNov 17, 2021 · N930SW · Cndair CL6002B19 · Aileron TabsSDR SWIA202164247None · chafedLH OVERWING EMERGENCY EXIT AFT UPPER LATCH FITTING IS CHAFED (C CHECK RO 2-11-2022) REMOVED AND REPLACE LH OVERWING EMERGENCY EXIT AFT UPPER LATCH FITTING IAW CRJ 200 SRM 51-40-11 AND CRJ 200 AMM 20-21-00-910-801 REF ATTACHED CONTINUATION CARD FOR DETAILS Nov 16, 2021 · N930SW · Cndair CL6002B19 · DoorsSDR SWIA202164246None · chafedLH OVERWING EMERGNCY EXIT STOP FITTING PADS ARE CHAFED. (6 TOTAL) (C CHECK RO 2-11-2022) REPLACED LH OVERWING EMERGENCY STOP FITTING PADS QTY 06 IAW CRJ 200 AMM 52-21-00-400-803Nov 16, 2021 · N930SW · Cndair CL6002B19 · DoorsSDR SWIA202164245None · chafedRH OVERWING EMERGENCY EXIT OPPER FWD LATCH FITTING AND BOTH LOWER HINGE SUPPRT FITTINGS ARE CHAFED/GOUGED. FUSELAGE SIDE (C CHECK RO 2-11-2022) REMOVED AND REPLACED RH OVERWING EMERGENCY EXIT OPPER FWD LATCH FITTING AND BOTH LOWER HINGE SUPPRT FITTINGS FNov 16, 2021 · N930SW · Cndair CL6002B19 · DoorsSDR SWIA202164244None · chafedRH OVERWING EMERGENCY EXIT STOP PADS ARE CHAFED. (6 TOTAL) (C CHECK RO 2-11-2022) REPLACED RH OVERWING EMERGENCY EXIT STOP PADS QTY 06 IAW CRJ 200 AMM 52-21-00-400-803Nov 16, 2021 · N930SW · Cndair CL6002B19 · DoorsSDR SWIA202164282None · wornR/H INBD. GRD. SPOILER HAS EXCESS PLAY AT ATTACH LINK TO ACTUATOR (C CHECK RO 2-11-2022) REMOVED AND REPLACED RH IB GROUND SPOILER ACTUATOR LINK ASSY AND HARDWARE IAW CRJ 200 AMM 27-65-01-000/400-801 OP CHECK GOOD REF ATTACHED CONTINUATION CARD FOR DETAILSNov 12, 2021 · N930SW · Cndair CL6002B19 · Wing StructureSDR SWIA202164281None · wornR/H OUTBD. GRD. SPOILER TO ACTUATOR SHOWS SIGNS OF EXCESSIVE PLAY (C CHECK RO 2-11-2022) REMOVED AND REPLACED RH OUTBD GROUND SPOILER ACTUATOR LINK ASSY AND HARDWARE IAW CRJ 200 AMM 27-65-01-000/400-801 OPS CHECK GOOD REF ATTACHED CONTINUATION CARD FOR DETNov 12, 2021 · N930SW · Cndair CL6002B19 · Wing StructureSDR SWIA202164224None · chafedR/H INBD. FLAP VANE HAS 3 EA. CHAFFES ALONG L/E FROM BUMPER STOPS (C CHECK RO 2-11-2022) REMOVED AND REPLACED O/B, MID, AND I/B VANE SKIN CAPS ON R/H I/B FLAP VANE IAW CRJ200 SRM 51-40-11 AND 51-42-13. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND ATTNov 11, 2021 · N930SW · Cndair CL6002B19 · Wing, Fuselage Attach FittingsSDR SWIA202164280None · damagedLH AND RH OB FLAP CENTER HINGE BEAM (FLAP SIDE) REQUIRED REMOVAL TO ACCESS PANELS 594/694 NB/QB (C CHECK RO 2-11-2022) REMOVED LH AND RH OB FLAP CENTER HINGE BEAM FLAP SIDE IAW CRJ 200 AMM 57-53-02-000-806 REF CAMPS # 23288100 AND 23288103 AND ATTACHED CONAug 13, 2021 · N930SW · Cndair CL6002B19 · Aileron TabsSDR SWIA202164277None · damagedREMOVE AND REPLACE BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C CHECK RO 2-11-2022) REMOVED AND REPLACED BUSHINGS ON RH AILERON WING AFT SPAR IAW CRJ 200 AMM 20-26-00-910-804 REF CAMP # 23288004 FOR REPLACEMENT OF HJul 21, 2021 · N930SW · Cndair CL6002B19 · Wing StructureSDR SWIA202164276None · damagedREMOVE AND REPLACE BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C CHECK RO 2-11-2022) REMOVED AND REPLACED BUSHINGS ON LH AILERON WING AFT SPAR IAW CRJ 200 AMM 20-26-00-910-804 REF CAMP # 23288003 FOR REPLACEMENT OF TJul 21, 2021 · N930SW · Cndair CL6002B19 · Wing StructureSDR SWIA202164223None · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA67065-601R-53-61-7594 N930SW MXCODEID55025-PR - FOUND CHAFE DAMAGE AT F.S. 700.00 ON RIGHT FUSELAGE FRAME BETWEEN STGR 15R AND STGR 16R. PERFORMED TEMPORARY REPAIR TO FRAME SECTOR AT FS700.00, BETWEEN STR 15R AND 16RJul 21, 2021 · N930SW · Cndair CL6002B19 · Nacelle/Pylon, Frame/Spar/RibSDR SWIA202164222None · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA53307-601R-53-21-3196-N930SW MXCODEID49025-DTI - DURING ACCOMPLISHMENT OF REO 601R-53-21-814 REV C TYPE 1 REPAIR TO THE PAX DOOR HINGE (FUSE SIDE), AFT LUGS FOUND OUT OF LIMITS. HINGE FOUND STRUCTURALLY ACCEPTABLE REF Jul 21, 2021 · N930SW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR SWIA202158626Wire Harness · failedGEAR DISAGREE WARNING MESSAGE ABOUT 10 MINUTES AFTER TAKEOFF. NOSE GEAR WAS AMBER ON ED1. MESSAGE CLEARED ON ITS OWN AFTER ABOUT 20 SECONDS. GEAR DEPLOYED NORMALLY UPON SELECTION DOWN FOR LANDING. (FLIGHT 5449 - FILED CLOSED) UPON INVESTIGATION FOUND INJun 4, 2021 · N930SW · Cndair CL6002B19 · Landing Gear System WiringSDR SWIA202156638Frame · chafedFOUND CHAFE DAMAGE AT F.S. 700.00 ON RIGHT FUSELAGE FRAME BETWEEN STGR 15R AND STGR 16R DAMAGE OUT OF LIMITS AND IS CLASSIFIED AS A MAJOR REPAIR PER GMM 3-26 FORM M-337 REQUIRED. FILED CLOSED PERFORMED TEMPORARY REPAIR TO FRAME SECTOR AT FS700.00, BEMar 3, 2021 · N930SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202156007Windshield · crackedCAPTAIN SIDE WINDOW HAS WHAT APPEARS TO BE CRACKS IN THE UPPER RIGHT AND LEFT HAND CORNERS. FLIGHT 5229 - FILED CLOSED REMOVED AND REPLACED LH SIDE WINDOW IAW AMM 56-12-01.LH SIDE WINDOW HEAT OP/C GOOD. PLEASE REFERENCE AML 575890 FOR SEALANT CURE PLEASEFeb 8, 2021 · N930SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA2019100446409Floorbeam · crackedL/H FS280 CENTER FLOOR BEAM OUTBD CLIP CRACKED (C-CHCEK) RO: 10/01/2019 REMOVED CRACKED FS280 LBL9 OTBD CLIP ANGLE AND INSTALLED NEW, FABRICATED, CLIP ANGLE IAW REO.Sep 7, 2019 · N930SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2019100446415Angle · corrodedCORROSION FOUND ON PAX DOOR LOWER SILL ANGLE AROUND NUT PLATE. (C-CHECK) RO: 10/01/2019 REMOVED CORROSION FROM PAX DOOR LOWER SILL ANGLE. REMOVED AND REPLACED THE PAX DOOR LOWER SILL ANGLE IAW SRM. OP CHECKS GOOD.Sep 5, 2019 · N930SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019100446414Frame · corrodedFWD SIDE OF FRAME AT FS605.00 BETWEEN STRG 22-27 LH NUMEROUS CORRODED AREAS (C-CHECK) RO: 10/01/2019 BLENDED CORROSION ON THE FS605 FRAME STR22-27L. REMOVED AND REPLACED THE FS605 FRAME IAW SRM. LEAK CHECKS GOOD.Sep 4, 2019 · N930SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2019100446408Floorbeam · crackedRH FS280.00 CENTER FLOOR BEAM CLIPS ARE BOTH CRACKED. (C-CHECK) RO: 10/01/2019 REMOVED CRACKED ANGLE AND INSTALLED NEW CLIP ANGLE ON R/H SIDE INBD OF FLOOR BEAM AT RBL18 IAW REO.Sep 4, 2019 · N930SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2019100446413Hinge · scratchedPIANO HINGE HALF ON FUSELAGE SIDE HAS MULTABLE LUGS THAT ARE SCRATCHED. (C-CHECK) RO: 10/01/2019 BLENDED AND REPAIRED SCRATCHES ON PAX DOOR PIANO HINGE HALF ON FUSELAGE SIDE IAW REO.Sep 3, 2019 · N930SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA2019100446412Frame · corrodedFS 349 BETWEEN STR 26L-26R FWD AND AFT SIDES OF FRAME HAD CORROSION (C-CHECK) RO: 10/01/2019 BLENDED CORROSION ON FS349 FRAME BETWEEN STR26L - STR26R. / REMOVED AND REPLACED THE FS349 LOWER FRAME SECTOR IAW SRM. LEAK CHECKS GOOD.Sep 3, 2019 · N930SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2019100446411Skin · chafedL/H AILERON PANEL 599CB HAS CHAFING DAMAGE. (C-CHECK) RO: 10/01/2019 BLENDED CHAFE, NDT'ED REPAIR - NO DEFECTS NOTED IAW REO.Aug 27, 2019 · N930SW · Cndair CL6002B19 · AileronsSDR SWIA2019100446410Skin · chafedL/H AILERON PANEL 599BB HAS CHAFING DAMAGE (C-CHECK) RO: 10/01/2019 BLENDED CHAFE, NDT'ED REPAIR - NO DEFECTS NOTED IAW REO.Aug 27, 2019 · N930SW · Cndair CL6002B19 · AileronsSDR SWIA2019031245618Holder · defectiveSMOKE AND SPARKS COMING FROM EXIT ROW LIGHT ON RIGHT SIDE OF ISLE. (FLT 5306) CLOSED FOUND SIDEWALL LIGHT HOLDER AT ROW 7 CD AND 8 CD AFT END TO BE BLACK WITH THE SMELL OF BURNT ELECTRICAL. REMOVED AND WIRED IN NEW SIDEWALL LIGHT HOLDER IAW AMM. SIDEWALL LIGHMar 11, 2019 · N930SW · Cndair CL6002B19 · Passenger Compartment LightingSDR SWIA2018040544461Door · icedCREW REPORTED A LOUD CLUNKING NOISE WHICH INCREASED AFTER GEAR RETRACTED AND INCREASED SPEED. REMOVED HEAVY ICE BUILD UP FROM NOSE GEAR AND NOSE DOORS, PERFORMED GVI OF NOSE GEAR AND DOORS NO OTHER DEFECTS NOTED.Apr 5, 2018 · N930SW · Cndair CL6002B19 · Landing Gear DoorsSDR SWIA201743727Floor Support · corrodedCARGO FLOOR SUPPORT CORRODED BS 611 AND 621, LBL 27. REMOVED THE CORROSION IAW SRM AND REO.Aug 8, 2017 · N930SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201743726Door Sill · corrodedCARGO DOOR SILL CORRODED BS 564 - 621, LBL 43. REMOVED AND REPLACED THE DOOR SILL IAW SRM.Aug 8, 2017 · N930SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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