N980SW

Service difficulty reports · 202

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 = 'N980SW' 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 SWI2025F00326Windshield · arcedCA WINDSHIELD CRACKED AND CAUSING ARCING. REMOVED CA WINDSHIELD IN REFERENCE TO AMM 56-11-01. REFERENCE CP 29735053-1 FOR INSTALLATION.Mar 5, 2025 · N980SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWI2025F00284Window · arcedCA WINDSHIELD CRACKED AND CAUSING ARCING. (FILED OPEN) REMOVED CA WINDSHIELD IN REFERENCE TO AMM 56-11-01. REFERENCE CP 29735053-1 FOR INSTALLATION.Mar 5, 2025 · N980SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA2025021900018Switch · malfunctionedENGINE OVER SPEED WARNING ON RIGHT ENGINE DURING CLIMB, THERE WAS AN UNCOMMANDED ACCELERATION FROM 93% N1 TO ABOUT 99% N1. THIS OCCURRED LESS THAN A MINUTE AFTER THRUST HAD BEEN ADJUSTED TO THE CLIMB THRUST SETTING. LEFT ENGINE DID SIMILAR ACCELERATION, BUT DIFeb 18, 2025 · N980SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWI202501240078Indication Sys · false activationAT THE NEXT OVERNIGHT MX, T/S REPEAT WRITE UPS FOR YDMCI TYPE: TROUBLESHOOTING PRIORITY 1UNCOMMANDED YAW MOTION (FLIGHT 5219 - FILED CLOSED) JAN 22, 2025 STATION: GRB--REMOVED AND REPLACED FCC #2 CARD IAW AMM 22-12-14. OPS CHECK GOOD AT THIS TIME. AC REJan 21, 2025 · N980SW · Cndair CL6002B19 · Auto Flight SystemSDR SWI202408210700Skin · dentedTRANSFER FROM EAML 1352997 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1352408 FOUND 30 DENTS ON RH FLIGHT SPOILER UPPER SKIN. (FLIGHT 5057 - FILED CLOSED)REMOVED AND REPLACED RH FLIGHT SPOILER IN REFERENCE WITH AMM 27-64-05. OPS CHECKED GOOD AT Jun 2, 2024 · N980SW · Cndair CL6002B19 · SpoilersSDR SWI202408210699Skin · dentedTRANSFER FROM EAML 1352977 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1352408 FOUND 18 DENTS ON RH AILERON UPPER SKIN. (FLIGHT 5057 - FILED CLOSED)REMOVED AND REPLACED RH AILERON IN REFERENCE WITH AMM 27-15-01 AND TASK CARD 27-900-1001-SKY. OPS Jun 2, 2024 · N980SW · Cndair CL6002B19 · AileronsSDR SWI202408210698Skin · dentedTRANSFER FROM EAML 1352976 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1352408 FOUND 45 DENTS ON LH AILERON UPPER SKIN. (FLIGHT 5057 - FILED CLOSED)REMOVED AND REPLACED LH AILERON ASSEMBLY REFERENCING AMM 27-15-01. COMPLIED WITH TASK CARD 27-900-1Jun 2, 2024 · N980SW · Cndair CL6002B19 · AileronsSDR SWI202408210697Skin · dentedTRANSFER FROM EAML 1352994 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1352408 FOUND 22 DENTS ON LH FLIGHT SPOILER UPPER SKIN. (FLIGHT 5057 - FILED CLOSED)REMOVED AND REPLACED LH FLIGHT SPOILER IN REFERENCE WITH AMM 27-64-05. REFER TO CP 28456843 Jun 2, 2024 · N980SW · Cndair CL6002B19 · Drag Control SystemSDR SWI202408210696Skin · dentedTRANSFER FROM EAML 1352978 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1352408 FOUND 23 DENTS ON ON LH OTBD FLAP UPPER SKIN. (FLIGHT 5057 - FILED CLOSED)REMOVED AND REPLACED LH OUTB FLAP ASSEMBLY IN REFERENCE WITH AMM 27-54-05. COMPLIED WITH TASK Jun 2, 2024 · N980SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2024082100602Skin · dentedTRANSFER FROM EAML 1352982 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1352408 FOUND 74 DENTS ON RH INBD FLAP UPPER SKIN. (FLIGHT 5057 - FILED CLOSED)REMOVED AND REPLACED RH INBD FLAP ASSEMBLY IN REFERENCE WITH AMM 27-54-01. COMPLIED WITH TASK CAJun 2, 2024 · N980SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWI2024082100696Skin · dentedTRANSFER FROM EAML 1352978 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1352408 FOUND 23 DENTS ON ON LH OTBD FLAP UPPER SKIN. (FLIGHT 5057 - FILED CLOSED)REMOVED AND REPLACED LH OUTB FLAP ASSEMBLY IN REFERENCE WITH AMM 27-54-05. COMPLIED WITH TASK Jun 2, 2024 · N980SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWI2024F00280Warning Message · illuminatedAT NEXT MX OVERNIGHT PLEASE TROUBLESHOOT REPEAT WRITE UPS FOR L 10TH DUCT WARNING MSGSMCI TYPE: TROUBLESHOOTING PRIORITY 1 (FLIGHT 5035 FILED CLOSED)APR 06, 2024 STATION: DEN--INSPECTED AND FOUND FIRE LOOPS CONTACTING ONE ANOTHER AND DUCTING. REPOSITIONED LOOApr 6, 2024 · N980SW · Cndair CL6002B19 · Detection SystemSDR SWIA20240317Skin · bentRH AILERON UPPER SKIN IS BENT BETWEEN HINGES #2 AND #3. (C-CHECK RO 4/3/2024) REMOVED DAMAGED RH AILERON UPPER LEADING EDGE SKIN & INSTALLED NEW RH AILERON UPPER LEADING EDGE SKIN IAW CRJ 200 SRM 51-42-21 & DWG NO. CC670-13000 REV. -DINSTALLED BRACKETS ONTMar 17, 2024 · N980SW · Cndair CL6002B19 · AileronsSDR SWIA20240222Doubler · crackedCRACK NOTED ON CARGO DOOR SILL SUPPORT CLIP ATTACHED TO FWD SIDE OF FRAME 589 (MARKED) (C-CHECK RO 4/3/2024) REPLACED LH CARGO DOOR SILL SUPPORT CLIP AT FS 589 WITH NEW FABRICATED CLIP 601R35011-11 REF CRJ 200 SRM 51-42-21 AND DWG 601R35011 REV R. COMPLIEFeb 22, 2024 · N980SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA20240216Floor Support · corrodedNUMEROUS CORROSIONS NOTED ON L/H PRESSURE FLOOR SILL ANGLE BETWEEN FS409.00+128 TO FS559.00 (MARKED) (C-CHECK RO 4/3/2024) REMOVED CORROSION ON NUMEROUS AREAS ON LH PRESSURE FLOOR SILL ANGLE BETWEEN FS409.00+128 - FS559 8 AREAS IN TOTAL. AREAS ARE LABELED Feb 16, 2024 · N980SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWI2024F00273Seat Track · corrodedSEAT RAIL FS364-FS394 LBL9 CORROSION, HN00139361 (C-CHECK RO 4/3/2024) REMOVED AND REPLACED SEAT RAIL FS364 - FS394 LBL9 REF CRJ200 AMM53-01-11-000-802 AND AMM53-01-11-400-802Feb 16, 2024 · N980SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWI202400270Floorbeam · corrodedCABIN FLOOR FS280 CROSS BEAM LBL9- RBL9 HAS AREAS OF CORROSION, HN00139344 (C-CHECK RO 4/3/2024) REMOVED AND REPLACED F.S. 280 CROSS BEAM FGLOOR SUPPORT ANGLE BETWEEN LBL 9 AND RBL 9 WITH NEW, REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21, CRJ 200 SRMFeb 16, 2024 · N980SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI2024F00272Floor Support · corrodedNUMEROUS CORROSIONS NOTED ON R/H PRESSURE FLOOR SILL BETWEEN FS409.00+128 TO FS559.00 (MARKED) (C-CHECK RO 4/3/2024) REMOVED CORROSION ON R/H PRESSURE FLOOR SILL BETWEEN FS409.00+128 TO FS559.00 AT 18 EA AREAS (MARKED) REF CRJ200 SRM 51-21-06. . COMPLIED WFeb 16, 2024 · N980SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F00271Floor Support · corrodedNUMEROUS CORROSIONS NOTED ON L/H PRESSURE FLOOR SILL BETWEEN FS409.00+128 TO FS559.00 (MARKED) (C-CHECK RO 4/3/2024) REMOVED CORROSION ON L/H PRESSURE FLOOR SILL BETWEEN FS409.00+128 TO FS559.00 AT 8 EA AREAS (MARKED) REF CRJ200 SRM 51-21-06. . COMPLIED WIFeb 16, 2024 · N980SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F00270Crossbeam · corrodedCABIN FLOOR FS280 CROSS BEAM LBL9- RBL9 HAS AREAS OF CORROSION, HN00139344 (C-CHECK RO 4/3/2024) REMOVED AND REPLACED F.S. 280 CROSS BEAM FGLOOR SUPPORT ANGLE BETWEEN LBL 9 AND RBL 9 WITH NEW, REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21, CRJ 200 SRMFeb 16, 2024 · N980SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI2024F00279Door Sill · corrodedCORROSION NOTED AT CARGO DOOR SILL (MARKED) (C-CHECK RO 4/3/2024) REMOVED AND REPLACED WITH NEW, CARGO FLOOR LANDING PLATE (FLOOR SILL) 601R35011-63 AND RE-INSTALLED EXISTING REPAIR PARTS REF CRJ 200 SRM 51-42-06 , DWG 601R35011 REV R AND REO 601R-53-61-59Feb 15, 2024 · N980SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F00278Stringer · corrodedCORROSION NOTED ON STRG SUPPORT FITTING ON STRG 27 AFT OF FRAME 559+112 (MARKED) (C-CHECK RO 4/3/2024) STRINGER TIE CLIP SUPPORT ANGLES P/N 601R31057-139 & -140, FABRICATED FROM S6144-33 ANGLE (.050" 7075-T62, RADIUS .12) PO# 5000008296-000010, IAW DWG 601Feb 15, 2024 · N980SW · Cndair CL6002B19 · Fuselage Main, KeelSDR SWI2024F00277Drain Mast · wornCORROSION NOTED INNER BASE PLATE FOR AFT DRAIN MAST AFT OF FRAME 589 BTWN STRG26R-STRG25R (MARKED) (C-CHECK RO 4/3/2024) REMOVED AND REPLACED AFT DRAIN MAST MOUNTING PLATE WITH NEW, REF CRJ 200 SRM 51-42-06 AND DWG 601R43216 REV -D, OPS TEST GOOD, LEAK CHFeb 15, 2024 · N980SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F00276Hinge · wornCOMPLY WITH CUURENT REVISION OF EA RJ3292-52 REPLACEMENT OF PASSENGER DOOR PIANO HINGE OPTION D3 (C-CHECK RO 4/3/2024) REMOVED DOOR HINGE, PERFORMED CUTTING TO CENTER HINGE AND TRIMMED TO FIT 2 EA. FWD AND AFT HINGE SECTIONS. BACK-DRILLED 4 EA HOLES IN NEWFeb 15, 2024 · N980SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA20240215Hinge · wornCOMPLY WITH CURRENT REVISION OF EA RJ3296-53 REPLACEMENT OF PASSENGER DOOR PIANO HINGE OPTION F3 (C-CHECK RO 4/3/2024) COMPLIED WITH E.A. NO. RJ3296-53 REV C DATED: 03/28/2024, REPLACEMENT OF PASSENGER DOOR PIANO HINGE OPTION F3 WITH HINGE REMOVAL. COMPLIEFeb 15, 2024 · N980SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA20240214Skin · dentedPROTRUDING DENT NOTED ON L/H EXTERNAL SKIN 3"-6" BELOW L/H WINDSHIELD SIDE POST AT APPROX. FS235.00 (MARKED) (C-CHECK RO 4/3/2024) CUT AWAY FS 235.0 FRAME UPPER FLANGE AND DRESSED BACK DENT ON FUSELAGE SKIN AT FS 235.0 BETWEEN STR 11L-12L TO ORIGINAL CONTOFeb 14, 2024 · N980SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA20240211Stringer · gougedEVALUATE CRACK ON STRINGER 8R BETWEEN FS280 AND FS295.0 INTERIOR CABIN. PERFORMED REPAIR ON STR 8R BETWEEN FS280.00 TO FS 295.00 IAW CRJ 200 REO 601R-53-21-3688 REV -- DATE:2024-04-29,SRM 53-00-00,SRM 51-26-01,SRM 51-42-21,SRM 51-42-06,SRM 51-21-11 AND SRM 5Feb 11, 2024 · N980SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA20240207Seal · corrodedBOTTOM OF SERVICE DOOR HAS CORROSION MARKED (C-CHECK RO 4/3/2024) REMOVED AND REPLACED SERVICE DOOR CORRODED LWR AFT FORMER WITH NEW, REF CRJ 200 SRM 51-42-06 AND DWG 601R38304 REV BN, PRESSURE LEAK CHECK GOODCOMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKYFeb 7, 2024 · N980SW · Cndair CL6002B19 · Service DoorsSDR SWIA20240201Skin · dentedDENT NOTED AT R/H INBD FLAP EXTERNAL LOWER SKIN AT APPROX. 2" FROM T/E AND 5" FROM INBD EDGE (MARKED) (C-CHECK RO 4/3/2024) R/H I/B FLAP EXTERNAL LOWER SKIN DENT HAS BEEN REPAIRED REF CRJ 200 SRM 57-52-00. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED FULLFeb 1, 2024 · N980SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWI2024F00274Fairing · chafedRH INBOARD FLAP HAS CHAFFING 2 AREAS WHERE CANOE FAIRING 683BB AND 686BB CONTACT LOWER SKIN (C-CHECK RO 4/3/2024) BLENDED-OUT DAMAGE AND EVALUATED LIMITATIONS ON RHS INBOARD FLAP LOWER SKIN AT FLAP-STA-74.718 AND FLAP STA-135.512, THE SUBJECT REWORKED CONDJan 27, 2024 · N980SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWI2024F00275Vane · chafedLH INBOARD FLAP VANE CHAFFED ON OUTBOARD LEADING EDGE (C-CHECK RO 4/3/2024) L/H I/B FLAP VANE, OUTBOARD LEADING EDGE CHAFFING BLENDED IAW CRJ 200 SRM 51-12-00 AND FOUND TO BE BEYOND LIMITS IAW CRJ 200 SRM 57-20-00 AND REO 601R-57-52-004 REV.-D, DATED 2012-Jan 27, 2024 · N980SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202266353None · failedON CLIMB OUT IN TEENS ON ENGINE BLEED SOURCE R PACK HI PRESS CAUTION MESSAGE. RAN QRH, DID NOT RECOVER RIGHT HAND PACK. CONTINUED CLIMB, GOT L PACK HI PRESS CAUTION MESSAGE. RAN QRH. WAS ABLE TO RECOVER LH PACK. RETURNED TO FIELD. (FLIGHT #5593 FILED CLOSED)Aug 29, 2022 · N980SW · Cndair CL6002B19 · Air Conditioning SystemSDR SWIA202265930None · odorSTRONG EXHAUST SMELL IN THE COCKPIT DURING DESCENT. PACK 1 SHOWING TEMPERATURE OUTPUT OF -6C. (FLIGHT 5928 - FILED CLOSED) PERFORMED FIM TASK 21-21-00. FOUND NO DAMAGE OR DEFECTS. RAN BOTH ENGINES REF AMM 71-00-00 AND OPERATED BOTH PACKS ON ENGINE BLEEDS FJun 14, 2022 · N980SW · Cndair CL6002B19 · Air Conditioning SystemSDR SWIA202052768Heat Shield · crackedAPU EXHAUST SHEILD CRACKED AT THE 6 O'CLOCK POSITION. FILED CLOSED (9/23/2020). REMOVED AND REPLASED THE APU EXHAUST SHIELD AND SUPPORT ASSY, IAW AMM.Sep 23, 2020 · N980SW · Cndair CL6002B19 · APU Exhaust SystemSDR SWIA2020041750177Doubler · damagedPAX DOOR SURROUND LOWER FWD CORNER DAMAGED DURING PAX DOOR INSTALL (C-CHECK) RO 4/16/2020 REMOVED DAMAGED DOUBLER AND INSTALLED NEW DOUBLER AND FILLER ON PAX DOOR SURROUND LOWER FWD CORNER REF CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS.Apr 13, 2020 · N980SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2020041750176Hinge Fitting · wornUPON REMOVAL ON JOB 2795595 OP 93 CAMP 20686462, FOUND R/H ELEVATOR L/E HINGE FITTING ASSY P/N 600-24043-1 @ ES16.52 TO BE EXCESSIVELY WORN AT BEARING LOCATION. REPLACE HINGE FITTING ASSY. (C-CHECK) RO 4/16/2020 REMOVED WORN R/H ELEVATOR L/E HINGE FITTIApr 3, 2020 · N980SW · Cndair CL6002B19 · Elevator StructureSDR SWIA2020041750175Retainer · chafedPAX DOOR UPPER CENTER RETAINER SEAL CHAFED/GOUGED (C-CHECK) RO 4/16/2020 BLENDED OUT CHAFE/GOUGE ON PAX DOOR UPPER CENTER SEAL RETAINER. REF CRJ 200 (TR51-44) SRM. PAX DOOR UPPER CENTER SEAL RETAINER ORIGINAL MATERIAL THICKNESS IS 0.050" IAW BOMBARDIER DWApr 2, 2020 · N980SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020041750174Hinge Fitting · wornUPON REMOVAL ON JOB 2795595 OP 92 CAMP 20686457, FOUND L/H ELEVATOR L/E HINGE FITTING ASSY P/N 600-24043-1 @ ES16.52 TO BE EXCESSIVELY WORN AND CORRODED AT BEARING LOCATION. REPLACE HINGE FITTING ASSY. (C-CHECK) RO 4/16/2020 REMOVED WORN L/H ELEVATOR LApr 2, 2020 · N980SW · Cndair CL6002B19 · Elevator StructureSDR SWIA2020041750173Angle · crackedRHS BATT RIB CAP ANGLE CRACKED AT WS48.30 (P/N 600-10389-2). (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED RHS BATT RIB ANGLE AT WS48.30 (P/N 600-10389-2) REF DWG AND CRJ200 SRM.Mar 26, 2020 · N980SW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA2020041750172Door Frame · corrodedPASSENGER DOOR: FRAME LOCATED AT FS313.56 BETWEEN INTERCOSTALS DD4 AND DD5 HAS CORROSION. (MARKED). (C-CHECK) RO 4/16/2020 WHILE REMOVING CORROSION ON FRAME FS313.56 BETWEEN INTERCOSTAL DD4 AND DD5 FOUND SEVERE CORROSION ON 3EA ELEMENTS AND ON MORE THAN 40Mar 25, 2020 · N980SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020041750171Intercostal · corrodedPASSENGER DOOR: INTERCOSTAL DD4 HAS CORROSION (MARKED). (C-CHECK) RO 4/16/2020 CORROSION IS PRESENT ON ALL 3EA ELEMENTS AND COVERS MORE THAN 30% OF PART OUT OF LIMITS REF CRJ200 SRM. REPLACE INTERCOSTAL DD4. REMOVED PAX DOOR MID DD4 INTERCOSTAL IAW CRJ 20Mar 25, 2020 · N980SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020041750170Intercostal · corrodedPASSENGER DOOR: INTERCOSTALL DD3 IS CORRODED (MARKED). (C-CHECK) RO 4/16/2020 CORROSION IS PRESENT ON ALL 3EA ELEMENTS AND COVERS MORETHAN 30% OF THE LENGHT OF PART OUT OF LIMITS REF CRJ200 SRM. REMOVED PAX DOOR MID INTERCOSTAL DD3 IAW CRJ 200 SRM. INSTAMar 25, 2020 · N980SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020041750169Intercostal · corrodedPASSENGER DOOR: INTERCOSTAL DD2 IS CORRODED (MARKED). (C-CHECK) RO 4/16/2020 CORROSION IS PRESENT ON MORE THAN 80% OF THE LENGHT OF PART AND FOUND ON 3EA ELEMENTS. OUT OF LIMITS REF CRJ200 SRM. REMOVED AND REPLACED NEW PAX DOOR MID DD2 INTERCOSTAL IAW CRJMar 25, 2020 · N980SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020041750168Former · corrodedPASSENGER DOOR: FORMER LOCATED AT FS347.27 IS CORRODED (MARKED). (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED PASSENGER DOOR FORMER LOCATED AT FS 347.27 REF BOMBARDIER DWG, CRJ-200-SRM. SEE CONTINUATION CARD FOR DETAILSMar 25, 2020 · N980SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020041750190Skin · corrodedWHILE REMOVING PASSENGER DOOR INNER SKIN FOUND CORROSION ON INNER SURFACE AT MULTIPLES LOCATIONS. (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED PAX DOOR INNER SKIN. REF CRJ 200 SRM.Mar 24, 2020 · N980SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020041750167Stiffener · crackedBOTTOM STIFFENER CRACKED OUTBOARD OF LBL36 ON AFT SIDE OF FS621 BULKHEAD. (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED BOTTOM STIFFENER OUTBOARD OF LBL36 ON AFT SIDE OF FS621 BULKHEAD REF CRJ-200 SRM AND BOMBARDIER DWG. PRESSURIZATION LEAK CHECK GOOD.Mar 22, 2020 · N980SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020041750166Angle · crackedLH BATT RIB ANGEL AT WS48.30 HAS A CRACK ON AFT END (P/N 600-10204-27). (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED DAMAGED BATT RIB ANGLE AT WS48.30 LHS PER DWG AND CRJ200 SRM.Mar 19, 2020 · N980SW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA2020041750165Skin · worn* R/H WING FUEL ACCESS PANEL LOCATION 650CB HAS PITTING ON EDGE (MARKED) (C-CHECK) RO 4/16/2020 BLENDED OUT DAMAGED AREAS AS REQUIRED ON RH WING FUEL ACCESS PANEL LOCATION 650CB PER REO. GAP CHECK AND LEAK CHECK ARE GOOD. SEE CONTINUATION FOR DETAILS.Mar 19, 2020 · N980SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020041750164Skin · worn* L/H WING FUEL ACCESS PANEL LOCATION 510AB INBOARD EDGE HAS PITTING (MARKED) (C-CHECK) RO 4/16/2020 BLENDED OUT DAMAGE AREAS OF LH WING FUEL ACCESS PANEL 510AB PER REO. BLEND OUT IS OUT OF LIMITS. RECEIVED REO. ROTO PEENED AND RESTORED REWORKED AREA. SEEMar 19, 2020 · N980SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020041750163Skin · worn* FUEL ACCESS PANEL LOCATION WING PLANK PERIMETER.550HB HAS PITTING AND DEEP WEAR GROOVE MARKING .(MARKED) (C-CHECK) RO 4/16/2020 BLENDED OUT DAMAGE AREAS OF LH WING FUEL ACCESS PANEL 550HB PER REO. BLEND OUT IS OUT OF LIMITS. RECEIVED REO. ROTO PEENED ANDMar 19, 2020 · N980SW · Cndair CL6002B19 · Wing, Plate/Skin
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