# Service difficulty reports: N980SW

A list on [N980SW](https://openairdocs.org/aircraft/N980SW.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 5 · 202 reports

- [SDR SWI2025F00326](https://openairdocs.org/sdr/SWI2025F00326.md): Windshield · arced · Mar 5, 2025 · N980SW · Cndair CL6002B19 · Flight Compartment Windows
  > CA WINDSHIELD CRACKED AND CAUSING ARCING. REMOVED CA WINDSHIELD IN REFERENCE TO AMM 56-11-01. REFERENCE CP 29735053-1 FOR INSTALLATION.
- [SDR SWI2025F00284](https://openairdocs.org/sdr/SWI2025F00284.md): Window · arced · Mar 5, 2025 · N980SW · Cndair CL6002B19 · Flight Compartment Windows
  > CA WINDSHIELD CRACKED AND CAUSING ARCING. (FILED OPEN) REMOVED CA WINDSHIELD IN REFERENCE TO AMM 56-11-01. REFERENCE CP 29735053-1 FOR INSTALLATION.
- [SDR SWIA2025021900018](https://openairdocs.org/sdr/SWIA2025021900018.md): Switch · malfunctioned · Feb 18, 2025 · N980SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > ENGINE 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 DI
- [SDR SWI202501240078](https://openairdocs.org/sdr/SWI202501240078.md): Indication Sys · false activation · Jan 21, 2025 · N980SW · Cndair CL6002B19 · Auto Flight System
  > AT 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 RE
- [SDR SWI202408210700](https://openairdocs.org/sdr/SWI202408210700.md): Skin · dented · Jun 2, 2024 · N980SW · Cndair CL6002B19 · Spoilers
  > TRANSFER 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
- [SDR SWI202408210699](https://openairdocs.org/sdr/SWI202408210699.md): Skin · dented · Jun 2, 2024 · N980SW · Cndair CL6002B19 · Ailerons
  > TRANSFER 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
- [SDR SWI202408210698](https://openairdocs.org/sdr/SWI202408210698.md): Skin · dented · Jun 2, 2024 · N980SW · Cndair CL6002B19 · Ailerons
  > TRANSFER 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 27-900-1
- [SDR SWI202408210697](https://openairdocs.org/sdr/SWI202408210697.md): Skin · dented · Jun 2, 2024 · N980SW · Cndair CL6002B19 · Drag Control System
  > TRANSFER 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
- [SDR SWI202408210696](https://openairdocs.org/sdr/SWI202408210696.md): Skin · dented · Jun 2, 2024 · N980SW · Cndair CL6002B19 · Trailing Edge Flaps
  > TRANSFER 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
- [SDR SWIA2024082100602](https://openairdocs.org/sdr/SWIA2024082100602.md): Skin · dented · Jun 2, 2024 · N980SW · Cndair CL6002B19 · Trailing Edge Flaps
  > TRANSFER 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 CA
- [SDR SWI2024082100696](https://openairdocs.org/sdr/SWI2024082100696.md): Skin · dented · Jun 2, 2024 · N980SW · Cndair CL6002B19 · Trailing Edge Flaps
  > TRANSFER 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
- [SDR SWI2024F00280](https://openairdocs.org/sdr/SWI2024F00280.md): Warning Message · illuminated · Apr 6, 2024 · N980SW · Cndair CL6002B19 · Detection System
  > AT 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 LOO
- [SDR SWIA20240317](https://openairdocs.org/sdr/SWIA20240317.md): Skin · bent · Mar 17, 2024 · N980SW · Cndair CL6002B19 · Ailerons
  > RH 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 ONT
- [SDR SWIA20240222](https://openairdocs.org/sdr/SWIA20240222.md): Doubler · cracked · Feb 22, 2024 · N980SW · Cndair CL6002B19 · Passenger/Crew Doors
  > CRACK 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. COMPLIE
- [SDR SWIA20240216](https://openairdocs.org/sdr/SWIA20240216.md): Floor Support · corroded · Feb 16, 2024 · N980SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > NUMEROUS 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
- [SDR SWI2024F00273](https://openairdocs.org/sdr/SWI2024F00273.md): Seat Track · corroded · Feb 16, 2024 · N980SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > SEAT 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 AMM53-01-11-400-802
- [SDR SWI202400270](https://openairdocs.org/sdr/SWI202400270.md): Floorbeam · corroded · Feb 16, 2024 · N980SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CABIN 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 SRM
- [SDR SWI2024F00272](https://openairdocs.org/sdr/SWI2024F00272.md): Floor Support · corroded · Feb 16, 2024 · N980SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > NUMEROUS 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 W
- [SDR SWI2024F00271](https://openairdocs.org/sdr/SWI2024F00271.md): Floor Support · corroded · Feb 16, 2024 · N980SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > NUMEROUS 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 WI
- [SDR SWI2024F00270](https://openairdocs.org/sdr/SWI2024F00270.md): Crossbeam · corroded · Feb 16, 2024 · N980SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CABIN 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 SRM
- [SDR SWI2024F00279](https://openairdocs.org/sdr/SWI2024F00279.md): Door Sill · corroded · Feb 15, 2024 · N980SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION 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-53-61-59
- [SDR SWI2024F00278](https://openairdocs.org/sdr/SWI2024F00278.md): Stringer · corroded · Feb 15, 2024 · N980SW · Cndair CL6002B19 · Fuselage Main, Keel
  > CORROSION 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 601
- [SDR SWI2024F00277](https://openairdocs.org/sdr/SWI2024F00277.md): Drain Mast · worn · Feb 15, 2024 · N980SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION 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 CH
- [SDR SWI2024F00276](https://openairdocs.org/sdr/SWI2024F00276.md): Hinge · worn · Feb 15, 2024 · N980SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > COMPLY 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 NEW
- [SDR SWIA20240215](https://openairdocs.org/sdr/SWIA20240215.md): Hinge · worn · Feb 15, 2024 · N980SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > COMPLY 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. COMPLIE
- [SDR SWIA20240214](https://openairdocs.org/sdr/SWIA20240214.md): Skin · dented · Feb 14, 2024 · N980SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PROTRUDING 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 CONTO
- [SDR SWIA20240211](https://openairdocs.org/sdr/SWIA20240211.md): Stringer · gouged · Feb 11, 2024 · N980SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > EVALUATE 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 5
- [SDR SWIA20240207](https://openairdocs.org/sdr/SWIA20240207.md): Seal · corroded · Feb 7, 2024 · N980SW · Cndair CL6002B19 · Service Doors
  > BOTTOM 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-SKY
- [SDR SWIA20240201](https://openairdocs.org/sdr/SWIA20240201.md): Skin · dented · Feb 1, 2024 · N980SW · Cndair CL6002B19 · Trailing Edge Flaps
  > DENT 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 FULL
- [SDR SWI2024F00274](https://openairdocs.org/sdr/SWI2024F00274.md): Fairing · chafed · Jan 27, 2024 · N980SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RH 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 COND
- [SDR SWI2024F00275](https://openairdocs.org/sdr/SWI2024F00275.md): Vane · chafed · Jan 27, 2024 · N980SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LH 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-
- [SDR SWIA202266353](https://openairdocs.org/sdr/SWIA202266353.md): None · failed · Aug 29, 2022 · N980SW · Cndair CL6002B19 · Air Conditioning System
  > ON 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)
- [SDR SWIA202265930](https://openairdocs.org/sdr/SWIA202265930.md): None · odor · Jun 14, 2022 · N980SW · Cndair CL6002B19 · Air Conditioning System
  > STRONG 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 F
- [SDR SWIA202052768](https://openairdocs.org/sdr/SWIA202052768.md): Heat Shield · cracked · Sep 23, 2020 · N980SW · Cndair CL6002B19 · APU Exhaust System
  > APU 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.
- [SDR SWIA2020041750177](https://openairdocs.org/sdr/SWIA2020041750177.md): Doubler · damaged · Apr 13, 2020 · N980SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PAX 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.
- [SDR SWIA2020041750176](https://openairdocs.org/sdr/SWIA2020041750176.md): Hinge Fitting · worn · Apr 3, 2020 · N980SW · Cndair CL6002B19 · Elevator Structure
  > UPON 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 FITTI
- [SDR SWIA2020041750175](https://openairdocs.org/sdr/SWIA2020041750175.md): Retainer · chafed · Apr 2, 2020 · N980SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX 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 DW
- [SDR SWIA2020041750174](https://openairdocs.org/sdr/SWIA2020041750174.md): Hinge Fitting · worn · Apr 2, 2020 · N980SW · Cndair CL6002B19 · Elevator Structure
  > UPON 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 L
- [SDR SWIA2020041750173](https://openairdocs.org/sdr/SWIA2020041750173.md): Angle · cracked · Mar 26, 2020 · N980SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RHS 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.
- [SDR SWIA2020041750172](https://openairdocs.org/sdr/SWIA2020041750172.md): Door Frame · corroded · Mar 25, 2020 · N980SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER 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 40
- [SDR SWIA2020041750171](https://openairdocs.org/sdr/SWIA2020041750171.md): Intercostal · corroded · Mar 25, 2020 · N980SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER 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 20
- [SDR SWIA2020041750170](https://openairdocs.org/sdr/SWIA2020041750170.md): Intercostal · corroded · Mar 25, 2020 · N980SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER 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. INSTA
- [SDR SWIA2020041750169](https://openairdocs.org/sdr/SWIA2020041750169.md): Intercostal · corroded · Mar 25, 2020 · N980SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER 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 CRJ
- [SDR SWIA2020041750168](https://openairdocs.org/sdr/SWIA2020041750168.md): Former · corroded · Mar 25, 2020 · N980SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER 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 DETAILS
- [SDR SWIA2020041750190](https://openairdocs.org/sdr/SWIA2020041750190.md): Skin · corroded · Mar 24, 2020 · N980SW · Cndair CL6002B19 · Passenger/Crew Doors
  > WHILE 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.
- [SDR SWIA2020041750167](https://openairdocs.org/sdr/SWIA2020041750167.md): Stiffener · cracked · Mar 22, 2020 · N980SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BOTTOM 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.
- [SDR SWIA2020041750166](https://openairdocs.org/sdr/SWIA2020041750166.md): Angle · cracked · Mar 19, 2020 · N980SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LH 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.
- [SDR SWIA2020041750165](https://openairdocs.org/sdr/SWIA2020041750165.md): Skin · worn · Mar 19, 2020 · N980SW · Cndair CL6002B19 · Wing, Plate/Skin
  > * 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.
- [SDR SWIA2020041750164](https://openairdocs.org/sdr/SWIA2020041750164.md): Skin · worn · Mar 19, 2020 · N980SW · Cndair CL6002B19 · Wing, Plate/Skin
  > * 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. SEE
- [SDR SWIA2020041750163](https://openairdocs.org/sdr/SWIA2020041750163.md): Skin · worn · Mar 19, 2020 · N980SW · Cndair CL6002B19 · Wing, Plate/Skin
  > * 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 AND

Next page: https://openairdocs.org/aircraft/N980SW/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N980SW/reports

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