N957SW

Service difficulty reports · 264

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 = 'N957SW' 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 SWIA2026091777216Pressure Panel · scratchedTRANSFER FROM EAML 1993541 TRANSFERRED FROM CAMP 33010415 IDENTIFIED A GOUGE ON LT PRESSURE FLOOR STRUCTURE PANEL AT FS549 APPROXIMATELY 12 X 132 X 003 FLIGHT 1. BLENDED SURFACE SCRATCH ON THE PAINTED LH PRESSURE FLOOR SILL STRUCTURE PANEL AT FS549 IAW SRM 5Sep 17, 2026 · N957SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA20241027Skin · gougedTRANSFER FROM EAML 1458910 : IN REFERENCE TO EAML# 1458203, 1458228. DAMAGE DESCRIPTION AFTER INSPECTION.MULTIPLE GOUGES/NICKS (MAXIMUM OF 100-OFF LOCATIONS, REF)AND DENTS (9-OFF LOCATIONS, REF) TO FUSELAGE SKIN (DWG: 601R35005, 0.058€? +/-0.002€? THK PAD UPOct 27, 2024 · N957SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWI2024F00017Floor Support · corrodedLH FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM F.S. 409.00 +128 TO F.S. 559.00. (C-CHECK RO 1/22/2024) REMOVED CORROSION FROM LH FLOOR SILL FROM F.S. 409.00 +128 TO F.S. 559.00. NDT INSPECTED NO DEFECTS NOTED, APPLIED FINISHES, FOUND TO BE STRUCTURALLDec 20, 2023 · N957SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2024012320Hinge · gougedLH AILERON, #1 HINGE, INBD BUSHING BORE IS GOUGED. (C-CHECK RO 1/22/2024) REPAIRED INBD BUSHING BORE AT LH AILERON, #1 HINGE. REF - MHIRJ REO 601R-57-51-1040, REV -A, DATED 2024-01-04 STEPS 1 THROUGH 9.COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.Dec 20, 2023 · N957SW · Cndair CL6002B19 · AileronsSDR SWIA202401230015Bulkhead · crackedREAR PRESSURE BULKHEAD FS625.00, STRINGER 13 HAS A CRACKED ANGLE. (C-CHECK RO 1/22/2024) LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL ANGLE P/N 601-35012-52 AT FS625 / STGR 13R. REF: CRJ200 SRM 51-42-21 REV 39 DATED 07/20/2022 AND DWG 601-35012, REV: D.Dec 15, 2023 · N957SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2024012314Door · corrodedSERVICE DOOR FWD LOWER CORNER AND SPLICE PLATE CORRODED. (C-CHECK RO 1/22/2024) REMOVED AND INSTALLED NEW SERVICE DOOR LOWER FWD CORNER IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-13 AND CRJ 200 SRM 51-42-21 AND DWG 601R38304 REV. BN. COMPLIED WITH Dec 14, 2023 · N957SW · Cndair CL6002B19 · Galley DoorsSDR SWI2024F00016Skin · dentedFS589.00 STRG 26LH - STRG 27, EXTERIOR SKIN DENT (MARKED) (C-CHECK RO 1/22/2024) COMPLIED WITH REO 601R-53-61-8133 REV --, DATED 2023-12-18 STEPS 1 THRU 10, AND ENSURED ALL OTHER REQUIREMENTS OF REO 601R-51-00-309 REV A DATED 2017-08-23 WERE MET.Dec 13, 2023 · N957SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWI2024F00015Skin · dentedFS574.00 - FS605.00 STRG 24LH - 26LH, 5EA INTERIOR DENTS PROTRUDING EXTERNALLY ON THE FUSELAGE SKIN (MARKED) (C-CHECK RO 1/22/2024) COMPLIED WITH REO 601R-53-61-8133 REV--, DATED 2023-12-18, STEP 1 THRU 10, ENSURED ALL OTHER REQUIREMENTS OF REO 601R-51-00Dec 13, 2023 · N957SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWI2024F00014Door · corrodedSERVICE DOOR LOWER AFT CORNER IS CORRODED. FLAGGED (C-CHECK RO 1/22/2024) REMOVED AND INSTALLED NEW SERVICE DOOR LOWER AFT CORNER IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-13 AND CRJ 200 SRM 51-42-21 AND DWG 601R38304 REV. BN. COMPLIED WITH 51-90Dec 13, 2023 · N957SW · Cndair CL6002B19 · Service DoorsSDR SWIA2024012313Skin · chafedR/H SIDE INBOARD FLAP VANE SKIN INBOARD HAS CHAFE (MARKED) (C-CHECK RO 1/22/2024) FOUND DAMAGE ON RH SIDE INBOARD FLAP VANE IB SKIN OUT OF LIMITS REF CRJ 200 SRM 57-00-31 AND INSTALLED A NEW VANE SKIN REF CRJ 200 SRM 51-42-13 AND DRAWING 601R14302 REV E.Dec 13, 2023 · N957SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWI2024F00013Window Post · crackedL/H SIDE WINDSHIELD POST AFT LOWER ATTACHMENT CLIP HAS CRACK AT RADIUS. (C-CHECK RO 1/22/2024) REMOVED AND REPLACED L/H SIDE WINDSHIELD POST, AFT LOWER ATTACHMENT CLIP FITTING REF CRJ200 SRM 51-42-21 AND DWG#601R33007 REV-U. COMPLIED WITH 51-900-1003-SKY (Dec 12, 2023 · N957SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI2024F00012Seat Track · wornPILOTS INBOARD AND OUTBOARD SEAT TRACKS HAVE WEAR GROOVES WORN INTO TRACK. (C-CHECK RO 1/22/2024) INSTALLED NEW PILOT INBOARD/OUTBOARD SEAT TRACK REF CRJ200 SRM 51-42-21 AND DWG NO 600-33100 REV AE.Dec 12, 2023 · N957SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA20240123012Skin · wornL/H AILERON HAS WARE AND GOUGES ON L/E INBD TO JUST PAST CENTER (MARKED WITH RED) (C-CHECK RO 1/22/2024) REMOVED AND REPLACED L/H AILERON L/E UPPER SKIN WITH NEW REF. CRJ 200 SRM 51-42-21, 51-42-13, 51-42-06 AND DWG #601R1300 REV. P. COMPLIED WITH SKYWEST Dec 12, 2023 · N957SW · Cndair CL6002B19 · AileronsSDR SWIA20240123010Hinge · damagedDURING AUDIT OF 1C TASK CARD 52-840-101 (DETAILED INSPECTION OF THE RIGHT OVERWING EMERGENCY-EXIT EES), FOUND EMERGENCY EXIT DOOR LOWER FWD. DOOR HINGE FITTING I/B SIDE HAS IMPACT DAMAGE (C-CHECK RO 1/22/2024) BLENDED OUT DAMAGE ON RH EMERGENCY EXIT DOOR LDec 10, 2023 · N957SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA202401230001Skin · dentedADM# N957SW-7273 - RIGHT SIDE OF UPPER CENTER SKIN PANEL ON FUSELAGE NOSE BETWEEN FS169.00 TO 193.00. SINGLE DENT MEASURING 1.75 IN L X 1.5 IN W X 0.04 IN D. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDec 1, 2023 · N957SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202310170015Unknown · warning messageOXY LO PRESS CAUTION MSG IN FLIGHT €” 29,000FT/-40*C/1390 PSI. RAN QRH & DESCENDED. PSI HELD STEADY AT 1360 PSI AT LOWER ALTITUDE. CAUTION MSG REMAINED ON THROUGHOUT FLT. ACFT WAS SVC€™D AT SGF, PRIOR TO DEPARTURE. INDICATED 1510 PSI AT 11*C AT GATE. ON Oct 15, 2023 · N957SW · Cndair CL6002B19 · Crew Oxygen SystemSDR SWIA202155644Floor Panel · corrodedLT PRESSURE FLOOR SILL PANEL CORROSION HAS BEEN FOUND TO BE OUT OF ALLOWABLE LIMITS, PER REO 601R-53-41-666 REV -C DATED 2012-11-06 AT 4 EA LOCATIONS BETWEEN FS 424 AND FS 529 DUE TO THE DISTANCE BETWEEN ADJACENT BLENDS. PERMANENT REPAIR REQUIRED. C-CHECK ROJan 8, 2021 · N957SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA202155635Washer · scratchedLT MAIN LANDING GEAR WING TO FUSELAGE SIDE BRACE FITTING AT LBL 13, FS 513.00 HAS SCRATCHES IN LOWER CORNER BELOW ATTACHMENT BOLT. C-CHECK RO 1/28/2021. REPAIRED LT MLG WING TO FUSE SIDE BRACE FITTING AT LBL 13 FS 513.00, IAW REO 601R-57-21-3999 REV- DATED 2Jan 4, 2021 · N957SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA202055656Nut Plate · elongatedLT FLOOR SILL 1.5" AFT OF FS 559.00 HAS 1 EA ELONGATED NUTPLATE HOLE. C-CHECK RO 1/28/2021. REMOVED AND REPLACED LT FLOOR SILL AFT OF FS 559, IAW CRJ 200 SRM-51-42-06 AND 51-42-21 REV 38, DATED 7/10/19. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY CODec 30, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202055655Former · corrodedPAX DOOR FORMER AT FS 329.76 CORRODED. C-CHECK RO 1/28/2021. REMOVED AND REPLACED FORMER, IAW CRJ200 SRM 51-42-06 REV 38, B DATED 25 NOV 2020. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CDec 30, 2020 · N957SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202055643Stiffener · crackedCRACKED STIFFNER AT FS 621.00/STGR 16L. C-CHECK RO 1/28/2021. REMOVED AND REPLACED STIFFENER, IAW CRJ200 SRM 51-42-06 REV 38B DATED 25 NOV 2020. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATIONDec 30, 2020 · N957SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202055642Web · corrodedPAX DOOR AFT WEB FOUND TO BE CORRODED AND CRACKED IN MULTIPLE PLACES. C-CHECK RO 1/28/2021. REPLACED PAX DOOR AFT WEB, IAW CRJ 200 SRM 51-40-11.Dec 30, 2020 · N957SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202055641Web · corrodedPAX DOOR FWD WEB FOUND TO BE CORRODED AND CRACKED IN MULTIPLE PLACES. C-CHECK RO 1/28/2021. REPLACED PAX DOOR FWD WEB, IAW CRJ 200 SRM 51-40-11.Dec 30, 2020 · N957SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202055654Panel · chafedRIGHT WING LOWER WING PLANK IS CHAFED AT RBL 45 APPROXIMATLY FS 513 FROM CONTACT WITH MLG FAIRING. C-CHECK RO 1/28/2021. REPAIRED RT WING LOWER PLANK CHAFE AT RBL 45 FS 513, IAW REO 601R-57-21-880 REV -D DATED 2017-03-06. COMPLETED TASK CARD 51-900-1003-SKYDec 23, 2020 · N957SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202055662Bracket · crackedFS 621 TO FS 625 OBLIQUE ANGLE AT STR 14R IS CRACKED. C-CHECK RO 1/28/2021. REMOVED AND REPLACED ANGLE AT FS 621 TO FS 625, IAW CRJ200 SRM 51-42-20. REFER TO CONTINUATION CARD FOR WORK PERFORMED.Dec 21, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202055661Bracket · crackedFS 621 TO FS 625 OBLIQUE ANGLE AT STR 15 IS CRACKED. C-CHECK RO 1/28/2021. REMOVED AND REPLACED OBLIQUE ANGLE LOCATED ON STGR 15L AT FS 621 TO FS 625, IAW CRJ200 SRM51-42-21. REFER TO CONTINUATION CARD FOR WORK PERFORMED.Dec 21, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202055660Bracket · crackedFS 621 TO FS 652 OBLIQUE ANGLE AT STR 14 IS CRACKED. C-CHECK RO 1/28/2021. REMOVED AND REPLACED FS 621-625 OBLIQUE ANGLE AT STR 14L, IAW CRJ200 SRM 51-42-20, 51-40-11 AND 51-20-00. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.Dec 21, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202055629Intercostal · crackedFS 621 TO FS 625 INTERCOSTAL IS CRACKED AT STR 16L. C-CHECK RO 1/28/2021. REMOVED AND REPLACED INTERCOSTAL AT STR 16L AT FS 621-FS 625, IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHDec 21, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202055630Fitting · gougedLEFT EMERGENCY EXIT DOOR UPPER FORWARD LATCH FITTING IS GOUGED IN CORNER. C-CHECK RO 1/28/2021. REPAIRED LT EMERGENCY EXIT UPPER FORWARD LATCH FITTING, IAW REO 601R-52-21-122 REV-, DATED 12/30/2020. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLEDec 19, 2020 · N957SW · Cndair CL6002B19 · Emergency ExitsSDR SWIA202055659Angle · crackedSTANDOFF ANGLE CRACKED AT FS 589.00 BETWEEN STR 26R AND STR 25R. C-CHECK RO 1/28/2021. REMOVED AND INSTALLED SERVICABLE STANDOFF ANGLE AT FS 589.00 BETWEEN STR 26R AND STR 25R, IAW CRJ 200 SRM 51-42-06. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERDec 18, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202055653Bulkhead · misinstalledLT INLET PANDOWN IS INSTALLED INCORRECTLY. WHILE C/W NDT TASK 54-430-602, NOTED A REPAIR DOUBLER IN THE INSPECTION AREA PREVENTING THE INSPECTION FROM BEING ABLE TO BE DONE AS WRITTEN. AFTER INVESTIGATION, FOUND THAT PANDOWN IS INSTALLED WITH THE MOUNTING FLDec 17, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202055677Hinge Fitting · corrodedUPPER RUDDER HINGE FITTING CONNECT HARDWARE HAS CORROSION. C-CHECK RO 1/28/2021. RECEIVED NEW SERVICEABLE HARDWARE, SEE CAMP 21748747 FOR INSTALL.Dec 16, 2020 · N957SW · Cndair CL6002B19 · Rudder/Tab, Attach FittingsSDR SWIA202055631Skin · dentedVERTICAL STAB, RT SKIN HAS MULTIPLE DENTS. C-CHECK RO 1/28/2021. DISCREPANCY HAS A TYPOGRAPHICAL ERROR, SHOULD READ LT SIDE SKIN. REPAIRED SKIN MHIRJ REO 601R-55-31-368 REV-, DATED 12/29/2020. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED ADec 16, 2020 · N957SW · Cndair CL6002B19 · Vertical Stabilizer, Plate/SkinSDR SWIA202055652Bracket · corrodedINTERCOSTAL AT STR 20 FORM FS 310-FS 333 IS CORRODED. C-CHECK RO 1/28/2021. REMOVED AND REPLACED INTERCOSTAL AT STR 20 AT FS 310-FS 333, IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CDec 15, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202055651Intercostal · corrodedPAX DOOR INTERCOSTAL DD3 IS CORRODED BETWEEN FS 347 AND FS 320. C-CHECK RO 1/28/2021. REMOVED AND REPLACED INTERCOSTAL, IAW CRJ200 SRM 51-42-06 AND 51-42-21 REV 38B DATED 25 NOV 2020. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHEDec 13, 2020 · N957SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202055650Intercostal · corrodedPAX DOOR INTERCOSTAL DD4 IS CORRODED BETWEEN FS 347 AND FS 338. C-CHECK RO 1/28/2021. REMOVED AND REPLACED INTERCOSTAL IAW CRJ200 SRM 51-42-06 AND 51-42-21 REV. 38B DATED 25 NOV 2020. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHEDec 13, 2020 · N957SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202055645Frame · crackedFS 333 FRAME IS CRACKED AT STGR 1L. C-CHECK RO 1/28/2021. REMOVED AND REPLACED FS 333 FRAME AT STGR 1L, IAW CRJ 200 SRM 51-42-06, DRAWING 601R32004 AND 51-42-21 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE AND FORM 337 IS ATTACHED. REF ATTACHED CONTINUATIODec 13, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202055640Skin · corrodedPAX DOOR INTERSKIN IS CORRODED BETWEEN DD5-DD6 AND FS 347-FS 338. C-CHECK RO 1/28/2021. REMOVED AND REPLACED PAX DOOR INNER SKIN, IAW CRJ 200 SRM 51-42-06 AND 51-42-13.Dec 13, 2020 · N957SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202055636Intercostal · corrodedPAX DOOR INTERCOSTAL DD6 IS CORRODED BETWEEN FS 311 AND FS 347. C-CHECK RO 1/28/2021. REMOVED AND REPLACED INTERCOSTAL, IAW CRJ200 SRM TASKS 51-42-06 AND 51-42-21 REV 38B DATED 25 NOV 2020. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ADec 13, 2020 · N957SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202055676Seat Track · corrodedRT SIDE SEAT TRACK FS 547-FS 559+80 SEGMENT IS CORRODED. C-CHECK RO 1/28/2021. TECH REPLACED RT SIDE SEAT TRACK BETWEEN FS 547-FS 559+80, IAW CRJ 200 AMM 53-01-11-400-802.Dec 12, 2020 · N957SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202055675Seat Track · corrodedLT SIDE SEAT TRACK FS 547-FS 559+80 SEGMENT IS CORRODED. C-CHECK RO 1/28/2021. TECH REPLACED LT SIDE SEAT TRACK BETWEEN FS 547-FS 559+80, IAW CRJ 200 AMM 53-01-11-400-802.Dec 12, 2020 · N957SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202055674Strap · corrodedLT FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN LBL 27 AND LBL 45 HAS MULTIPLE SPOTS OF CORROSION. C-CHECK RO 1/28/2021. REMOVED AND REPLACED LT FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN LBL 27 AND LBL 45, IAW CRJ-200 SRM 51-42-06 AND 51-42-10.Dec 10, 2020 · N957SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202055673Strap · corrodedRT FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN RBL 27 AND RBL 45 HAS MULTIPLE SPOTS OF CORROSION. C-CHECK RO 1/28/2021. REMOVED AND REPLACED RT FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN RBL 27 AND RBL 45, IAW CRJ-200 SRM 51-42-06 AND 51-42-10.Dec 10, 2020 · N957SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202055658Fitting · crackedFS 484.00 RT INTERCOSTAL CLIP CRACKED BETWEEN RBL 27 AND RBL 36. C-CHECK RO 1/28/2021. REMOVED AND REPLACED FS 484.00 RT INTERCOSTAL CLIP BETWEEN RBL 27 AND RBL 36, IAW CRJ 200 SRM 51-42-21. REFERENCE ATTACHED CONTINUATION CARD FOR WORK PERFORMED.Dec 10, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202055657Fitting · crackedFS 484.00 LT INTERCOSTAL CLIP CRACKED BETWEEN LBL 27 AND LBL 36. C-CHECK RO 1/28/2021. REMOVED AND REPLACED FS 484.00 LT INTERCOSTAL CLIP CRACKED BETWEEN LBL 27 AND LBL 36, IAW CRJ 200 SRM 51-42-02. SEE ATTACHED CONTINUATION CARD FOR WORK PERFORMED.Dec 10, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202055649Nut Plate · corrodedMINOR CORROSION AROUND NUTPLATE ON FLOORBEAM AT RBL 9 BETWEEN FS 409.00 TO FS 409.00 +16. C-CHECK RO 1/28/2021. REMOVED AND REPLACED FLOORBEAM CAP, IAW REO 601R-53-31-1166 REV- DATED 2021-01-08. COMPLIED WITH TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETEDDec 10, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202055648Floor Support · corrodedRT FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS 409.00 +128 TO FS 559.00. C-CHECK RO 1/28/2021. REPAIRED IAW REO 601R-53-41-666 REV C DATED 2012-11-06. MAJOR REPAIR TASK CARD 51-900-1003-SKY & FORM M337 COMPLETED. NO MEASUREABLE WEIGHT CHANGE, REFER Dec 10, 2020 · N957SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202055639Floor Support · corrodedLT FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS 409.00 +128 TO FS 559.00. C-CHECK RO 1/28/2021. REPAIRED IAW REO 601R-53-41-666 REV C DATED 2012-11-06. MAJOR REPAIR TASK 51-900-1003-SKY & FORM M337 COMPLETED AND ATTACHED. NO MEASUREABLE WEIGHT CHANGEDec 10, 2020 · N957SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202055638Angle · corrodedRT FLOOR SILL ANGLE HAS MULTIPLE SPOTS OF CORROSION FROM FS 409.00 +128 TO FS 559.00. C-CHECK RO 1/28/2021. REPAIRED RT FLOOR SILL ANGLE CORROSION FROM FS 409.00+128 TO FS 559.00, IAW BOMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06, REF ATTACHED CONTINUDec 10, 2020 · N957SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202055634Floorbeam · corrodedFLOOR BEAM AT RBL 9 HAS MULTIPLE SPOTS OF MINOR CORROSION FROM FS 409.00 +128 TO FS 559.00. C-CHECK RO 1/28/2021. REPLACED FLOORBEAM CAP AT RBL 9 AT FS 409+128 TO FS 559, IAW MHIRJ REO 601R-53-41-2835 REV- DATED 2021-01-17. COMPLETED TASK CARD 51-900-1003-SDec 10, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
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