# Service difficulty reports: N939SW

A list on [N939SW](https://openairdocs.org/aircraft/N939SW.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 4 · 191 reports

- [SDR SWIA2024111501252](https://openairdocs.org/sdr/SWIA2024111501252.md): Anti-Skid Sys · warning message · Nov 14, 2024 · N939SW · Cndair CL6002B19 · Brake Anti-Skid Section
  > ON TO, AFTER MOVING LANDING GEAR LEVER UP, ANTI SKID OUTBOARD CAUTION MESSAGE. FOLLOWED 20-30 SECONDS LATER BY A GEAR DISAGREE WARNING. NOSEHWEEL UP, MAINS DOWN. RAN THE QRH SLOWED FROM 250 TO 200, TURNED ON HYDRAULIC PUMP 2 AND 3B MESSAGE PERSISTED. AS WE WER
- [SDR SWI2024F00492](https://openairdocs.org/sdr/SWI2024F00492.md): Floor Panel · damaged · Jun 16, 2024 · N939SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > D: SINGULAR FLOOR PANEL IN CARGO BAY IS SLIGHTLY DAMAGED (INDENTS A FEW INCHES WHEN STEPPED UPON AND SHOWING VERY SMALL HOLES IN THE MIDDLE) STILL STRUCTURALLY SOUNDC: MEL 25-52-1CAT C DUE 6/26/24SINGULAR FLOOR PANEL IN CARGO BAY IS SLIGHTLY DAMAGED (INDENTS A
- [SDR SWIA2024032000212](https://openairdocs.org/sdr/SWIA2024032000212.md): Structure · chafed · Feb 12, 2024 · N939SW · Cndair CL6002B19 · Fuselage Main, Structure
  > RH MLG WHEEL WELL AT WING BOX LOWER PLANK AFT EDGE BL45.00 AND STR3 HAS SIGN OF CHAFFING (C-CHECK RO 3/19/2024) PERFORMED REPAIR ON R/H MLG WHEEL WELL AT WING BOX LWR PLANK AFT EDGE ON LBL 45.00 STR 3 IAW CRJ 200 REO 601R-57-21-3824. PERFORMED NDT ET INSPE
- [SDR SWIA20240320201](https://openairdocs.org/sdr/SWIA20240320201.md): Structure · chafed · Feb 1, 2024 · N939SW · Cndair CL6002B19 · Fuselage Main, Structure
  > LEFT MAIN LDG GEAR WHEEL WELL OB CORNER FS511.0 AND WS50.54 AREA EVAL CHAFFING (C-CHECK RO 3/19/2024) PERFORMED REPAIR ON DAMAGE AREA AT L/H MLG WHEEL WELL O/B CORNER ON LWR WING PLANK LBL 45.00 STR #3 IAW CRJ 200 REO 601R-57-21-3824, AND CRJ 200 SRM 57-21
- [SDR SWI2024F00251](https://openairdocs.org/sdr/SWI2024F00251.md): Seat Track · corroded · Jan 28, 2024 · N939SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > L/H FLOOR SEAT TRACK AT FS 559.00 + 80- FS 559.00 + 96 AT LBL27 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMOVED ANN INSTALLED NEW L/H FLOOR SEAT TRACK AT FS559.00+80 - FS559.00+96 AT LBL27 IAW CRJ200 AMM 53-00-49TORQUE DRIVER: AV-1623 CAL DUE: JAN202
- [SDR SWI2024F00250](https://openairdocs.org/sdr/SWI2024F00250.md): Seat Track · corroded · Jan 28, 2024 · N939SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > L/H FLOOR SEAT TRACK AT FS 559.00 + 80- FS 559.00 + 96 AT LBL9 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMOVED AND REPLACED LH SEAT TRACK AT FS559.00 + 80 - FS559.00 + 96 AT LBL9, WET SEALED AND TORQUED IAW CRJ 200 AMM 53-00-49CAL TOOL: AV-1623CAL D
- [SDR SWI2024F00249](https://openairdocs.org/sdr/SWI2024F00249.md): Seat Track · corroded · Jan 28, 2024 · N939SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > R/H FLOOR SEAT TRACK AT FS 559.00 + 80- FS 559.00 + 96 AT RBL9 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMOVED AND REPLACED RH FLOOR SEAT TRACK AT FS 559.00 + 80 - FS 559.00 + 96 AT RBL 9 IAW CRJ AMM 53-00-49 CALIBRATED TOOL: AJ-1336DUE: JANUARY 2025
- [SDR SWI2024F00248](https://openairdocs.org/sdr/SWI2024F00248.md): Seat Track · corroded · Jan 28, 2024 · N939SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > R/H FLOOR SEAT TRACK AT FS 559.00 + 80 - FS 559.00 + 96 AT RBL27 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMOVED AND INSTALLED NEW RH SEAT TRACK AT FS559.00+80 TO FS559.00+96 AT RBL27 IAW CRJ200 AMM 53-01-11
- [SDR SWI2024F00247](https://openairdocs.org/sdr/SWI2024F00247.md): Seat Track · corroded · Jan 28, 2024 · N939SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > R/H FLOOR SEAT TRACK AT FS 559.00 + 96- FS- 559 + 112 AT RBL27 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) INSTALLED RH FLOOR SEAT TRACK @ FS559.00+96 TO FS559.00+112 IAW CRJ200 AMM 53-00-49-400-801.
- [SDR SWI2024F00246](https://openairdocs.org/sdr/SWI2024F00246.md): Seat Track · corroded · Jan 28, 2024 · N939SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > R/H FLOOR SEAT TRACK AT FS 559.00 + 96 - FS 559 + 112 AT RBL9 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMOVED AND INSTALLED NEW RH SEAT TRACK FROM FS559.00+96 TO FS559.00+112 AT RBL9 IAW CRJ200 AMM 53-01-11
- [SDR SWI2024F00245](https://openairdocs.org/sdr/SWI2024F00245.md): Seat Track · corroded · Jan 28, 2024 · N939SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > L/H FLOOR SEAT TRACK AT FS 559.00 + 96- FS 559 + 112 AT LBL9 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMMOVED AND INSTALLED FLOOR SEAT TRACK AT LH FS 559.00 +112 AT LBL 9 IAW CRJ200 AMM 53-01-11
- [SDR SWI2024F00244](https://openairdocs.org/sdr/SWI2024F00244.md): Seat Track · corroded · Jan 28, 2024 · N939SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > L/H FLOOR SEAT TRACK AT FS 559.00 + 96 - FS 559 + 112 AT LBL27 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMOVED AND REPLACED LH FLOOR SEAT TRACK AT F.S 559.00+96 TO F.S 559.00+112 AT LBL27 IAW CRJ 200 SRM 51-40-11CAL TOOL: TD S/N AV1623 CAL DATE 01/25
- [SDR SWI2024F00243](https://openairdocs.org/sdr/SWI2024F00243.md): Seat Track · corroded · Jan 28, 2024 · N939SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > L/H FLOOR SEAT TRACK AT FS 559 + 112- FS 621 AT LBL27 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMOVED AND REPLACED LH FLOOR SEAT TRACK AT FS 559+112 - FS 621 AT LBL 27 IAW CRJ 200 AMM 53-00-49.CAL TOOLS: TORQUE DRIVER AJ 1336 CAL DATE JAN 2025
- [SDR SWI2024F00242](https://openairdocs.org/sdr/SWI2024F00242.md): Seat Track · corroded · Jan 28, 2024 · N939SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > L/H FLOOR SEAT TRACK AT FS 559 + 112- FS 621 AT LBL9 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMOVED AND INSTALLED NEW LH SEAT TRACK AT FS559.00+112 TO FS621.00 AT LBL9 IAW CRJ200 AMM 53-01-11CAL TOOLS: TW AV 1627 CAL DATE 01/25
- [SDR SWI2024F00241](https://openairdocs.org/sdr/SWI2024F00241.md): Seat Track · corroded · Jan 28, 2024 · N939SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > R/H FLOOR SEAT TRACK AT FS 559 + 112- FS 621 AT RBL9 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMOVED AND REPLACED SEAT TRACK FROM FS559+112 - FS621 AT RBL9 IAW CRJ 200 AMM 53-00-49CAL TOOL: TORQUE DRIVER AV-1623CAL DUE: JAN 25
- [SDR SWIA20240320128](https://openairdocs.org/sdr/SWIA20240320128.md): Seat Track · corroded · Jan 28, 2024 · N939SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > R/H FLOOR SEAT TRACK AT FS 559 + 112- FS 621 AT RBL27 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) RH FLOOR SEAT TRACK AT FS 559.+112-FS621 AT RIB 27L REPLACED IAW CRJ 200-AMM 53-00-49
- [SDR SWIA20240320127](https://openairdocs.org/sdr/SWIA20240320127.md): Angle · cracked · Jan 27, 2024 · N939SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND ANGLE CRACK AT AFT PRESS BULKHEAD REAR FS625.0 STR12R (C-CHECK RO 3/19/2024) REMOVED AND REPLACE NEW INTERCOSTAL P/N 601-35012-52 AT AFT PRESS BULKHEAD REAR FS 625.0 STR 12R IAW CRJ 200 SRM 51-42-20
- [SDR SWIA20240320117](https://openairdocs.org/sdr/SWIA20240320117.md): Skin · dented · Jan 17, 2024 · N939SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > UPPER AFT FUSELAGE FS672.00 TO F.S. 682.20 AT STR 3 HAS DENT (C-CHECK RO 3/19/2024) PERFORMED PERMANENT REPAIR ON UPPER AFT FUSELAGE F.S 672.00 TO F.S 682.00 STGR 3 LH IAW MHIRJ REO 601R-53-61-8148 REV -- DATED 2024-01-25 NDT PERFORMED BY BARRON NDT FAA C
- [SDR SWIA20240320115](https://openairdocs.org/sdr/SWIA20240320115.md): Skin · damaged · Jan 15, 2024 · N939SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ADM# N939SW-8619 BETWEEN STGR 15L/16L F.S. 404.00. 7/8" LONG BY 3/8 WIDE WITH A DEPTH OF.0040" DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED. ELIMINATE EVIDENCE OF DAMAGE USING STANDARD ACFT PRACTICES. (C-CHECK RO 3/19/2024
- [SDR SWIA202264099](https://openairdocs.org/sdr/SWIA202264099.md): None · malfunctioned · Feb 4, 2022 · N939SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > DURING A GO AROUND AFTER RETRACTING THE GEAR RECEIVED A €ŒGEAR DISAGREE€?. NOSE WHEEL SHOWED NOT UP AND LOCKED. AFTER ABOUT 1 MINUTE, NOSE WHEEL SHOWED UP AND LOCKED AND DISAGREE EXTINGUISHED. RAN QRH PROCEDURE, NO FURTHER ISSUES. (FLIGHT 5452 - FILED C
- [SDR SWIA202163097](https://openairdocs.org/sdr/SWIA202163097.md): None · cracked · Dec 14, 2021 · N939SW · Cndair CL6002B19 · Window/Windshield System
  > UPON BOARDING AIRPLANE CAPTAINS FRONT WINDSHIELD IS CRACKED. (FILED CLOSED)REPLACED CAPTAINS WIND SHIELD IN REFERENCE TO TASK CARD 56-220-1000-SKY AND CRJ 200 MM 56-11-01, OPS CHECK GOOD
- [SDR SWIA202054611](https://openairdocs.org/sdr/SWIA202054611.md): Skin · chafed · Dec 9, 2020 · N939SW · Cndair CL6002B19 · Ailerons
  > LT AILERON UPPER LEADING EDGE SKIN CHAFED IN 2 EA PLACES ON BOTTOM SIDE OF SKIN ABOVE THE CENTER HINGE NUTS. FILED CLOSED. LT AILERON UPPER LEADING EDGE SHROUD FOUND OUT OF LIMITS, REF CRJ 200 SRM AND INSTALLED A NEW LEADING EDGE SHROUD, REF DRAWING AND CRJ
- [SDR SWIA202054610](https://openairdocs.org/sdr/SWIA202054610.md): Skin · bent · Dec 9, 2020 · N939SW · Cndair CL6002B19 · Ailerons
  > RT AILERON LEADING EDGE SKIN IS BENT UP AT THE CENTER HINGE. FILED CLOSED. REMOVED DAMAGED RT AILERON LEADING EDGE UPPER SHROUD, REF CRJ 200 SRM AND INSTALLED A NEW SHROUD, REF CRJ 200 SRM AND DRAWING AND REO.
- [SDR SWIA202054556](https://openairdocs.org/sdr/SWIA202054556.md): Hinge Fitting · corroded · Nov 22, 2020 · N939SW · Cndair CL6002B19 · Elevator Structure
  > RT ELEVATOR HINGE FITTING PN 600-24043-1 NEEDS REPLACING DUE TO PITTING. C-CHECK RO 12/05/2020. INSTALLED NEW RT ELEVATOR HINGE FITTING PN 600-24043-1 P/O 7742-00008/136, REF BOMBARDIER DWG CRJ 200 SRM.
- [SDR SWIA202054555](https://openairdocs.org/sdr/SWIA202054555.md): Hinge Fitting · corroded · Nov 22, 2020 · N939SW · Cndair CL6002B19 · Elevator Structure
  > LT ELEVATOR HINGE FITTING PN 600-24043-1 NEEDS REPLACING DUE TO PITTING. C-CHECK RO 12/05/2020. INSTALLED NEW LT ELEVATOR HINGE FITTING PN 600-24043-1 PO 7742-00008/135, REF BOMBARDIER DWG AND CRJ 200 SRM.
- [SDR SWIA202054554](https://openairdocs.org/sdr/SWIA202054554.md): Structure · bent · Nov 19, 2020 · N939SW · Cndair CL6002B19 · Ailerons
  > LT AILERON LEADING EDGE AT THE CENTER HINGE POINT, IS BENT UPWARD. C-CHECK RO 12/05/2020. REPLACED WITH NEW LT AILERON LEADING EDGE AT THE CENTER HINGE POINT, REF DWG, CRJ 200SRM. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD.
- [SDR SWIA202054553](https://openairdocs.org/sdr/SWIA202054553.md): Fairing · chafed · Nov 11, 2020 · N939SW · Cndair CL6002B19 · Aerodynamic Fairings
  > RIGHT WING TRAILING EDGE TO FUSELAGE APRON CHAFED, MARKED. C-CHECK RO 12/05/2020. REPAIRED RIGHT WING TRAILING EDGE TO FUSELAGE APRON, REF REO. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD.
- [SDR SWIA202054552](https://openairdocs.org/sdr/SWIA202054552.md): Floor Support · damaged · Nov 10, 2020 · N939SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL FROM FS 559+84.9-FS 562.69 REQUIRES REPLACEMENT. C-CHECK RO 12/05/2020. REPLACED RT FLOOR SILL (P/N 601R31133-102) BETWEEN FS 559.00+84.9 AND FS 562.69, REF CRJ200 SRM AND DWG. COMPLIED WITH TASK CARD. LEAK CHECK SATISFACTORY.
- [SDR SWIA202054551](https://openairdocs.org/sdr/SWIA202054551.md): Intercostal · corroded · Nov 10, 2020 · N939SW · Cndair CL6002B19 · Fuselage Main, Structure
  > INTERCOSTAL DD1 IS CORRODED IN SEVERAL LOCATIONS (NOTED AFTER INTERNAL SKIN WAS REMOVED). C-CHECK RO 12/05/2020. PAX DOOR MID DD1 INTERCOSTAL ORIGINAL MATERIAL THICKNESS IS 0.050", IAW CRJ 200 SRM. EXFOLIATED CORROSION AT MULTIPLE LOCATION AND MORE TWO ELEM
- [SDR SWIA202054550](https://openairdocs.org/sdr/SWIA202054550.md): Intercostal · corroded · Nov 10, 2020 · N939SW · Cndair CL6002B19 · Fuselage Main, Structure
  > INTERCOSTAL DD2 IS CORRODED IN SEVERAL LOCATIONS (NOTED AFTER INNER SKIN WAS REMOVED). C-CHECK RO 12/05/2020. PAX DOOR MID DD2 INTERCOSTAL ORIGINAL MATERIAL THICKNESS IS 0.050", IAW CRJ 200 SRM. EXFOLIATED CORROSION AT MULTIPLE LOCATION AND MORE TWO ELEMENT
- [SDR SWIA202054549](https://openairdocs.org/sdr/SWIA202054549.md): Intercostal · corroded · Nov 10, 2020 · N939SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DD1 INTERCOSTAL IS CORRODED. C-CHECK RO 12/05/2020. PAX DOOR AFT DD1 INTERCOSTAL ORIGINAL MATERIAL THICKNESS IS 0.050", IAW CRJ 200 SRM. EXFOLIATED CORROSION AT MULTIPLE LOCATION AND MORE TWO ELEMENT AT GIVEN CROSS-SECTION OUT OF LIMITS, IAW CR
- [SDR SWIA202054548](https://openairdocs.org/sdr/SWIA202054548.md): Skin · damaged · Nov 10, 2020 · N939SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > WHILE REMOVING PANEL 132AL FOUND EXISTING DAMAGE AROUND SCREW HOLE. C-CHECK RO 12/05/2020. BLENDED OUT TOOLING DAMAGE ON SKIN RING AT PANEL 132AL, REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS. SUBMITTED AND RECEIVED ENGINEERING REF REO, ALL STE
- [SDR SWIA202054547](https://openairdocs.org/sdr/SWIA202054547.md): Door Frame · corroded · Nov 7, 2020 · N939SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR FRAME FS 313.56 AND CLEAT HAS CORROSION. C-CHECK RO 12/05/2020. REMOVED FS 313.56 PAX DOOR FRAME & CLEAT. BLENDED CORROSION TO A SMOOTH CONTOUR. REMAINING MATERIAL ON FS 313.56 FRAME WITHIN LIMITS & CLEAT WAS NOT. REINSTALLED FS 313.56 PAX DOOR F
- [SDR SWIA202054546](https://openairdocs.org/sdr/SWIA202054546.md): Intercostal · corroded · Nov 4, 2020 · N939SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD4 CORRODED, MARKED. C-CHECK RO 12/05/2020. PAX DOOR MID DD4 ORIGINAL MATERIAL THICKNESS IS 0.050", IAW CRJ 200 SRM. EXFOLIATED CORROSION AT MULTIPLE LOCATION AND MORE TWO ELEMENT AT GIVEN CROSS-SECTION OUT OF LIMITS, IAW CRJ 200 SRM.
- [SDR SWIA202054545](https://openairdocs.org/sdr/SWIA202054545.md): Attach Angle · corroded · Nov 4, 2020 · N939SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD UPPER ATTACH CORNER ANGLE FOR DD6 IS CORRODED, MARKED. C-CHECK RO 12/05/2020. REMOVED AND INSTALLED NEW PAX DOOR ANGLE COMON TO FWD DD6 INTERCOSTAL, IAW CRJ 200 SRM AND BOMBARDIER DWG.
- [SDR SWIA202054544](https://openairdocs.org/sdr/SWIA202054544.md): Intercostal · corroded · Nov 4, 2020 · N939SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD3 CORRODED, MARKED. C-CHECK RO 12/05/2020. PAX DOOR MID DD3 ORIGINAL MATERIAL THICKNESS IS 0.050", IAW CRJ 200 SRM. EXFOLIATED CORROSION AT MULTIPLE LOCATION AND MORE TWO ELEMENT AT GIVEN CROSS-SECTION OUT OF LIMITS, IAW CRJ 200 SRM.
- [SDR SWIA202054543](https://openairdocs.org/sdr/SWIA202054543.md): Intercostal · corroded · Nov 4, 2020 · N939SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL 4TH FROM TOP ON AFT SIDE IS CORRODED, MARKED (NOTED AFTER INNER SKIN WAS LIFTED). C-CHECK RO 12/05/2020. PAX DOOR AFT DD4 INTERCOSTAL ORIGINAL MATERIAL THICKNESS IS 0.050", IAW CRJ 200 SRM. EXFOLIATED CORROSION AT MULTIPLE LOCATION AND
- [SDR SWIA202054542](https://openairdocs.org/sdr/SWIA202054542.md): Former · corroded · Nov 4, 2020 · N939SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER CORRODED IN SEVERAL OF THE UPPER BAYS ON THE INNER SIDE, MARKED (NOTED AFTER INNER SKIN WAS LIFTED). C-CHECK RO 12/05/2020. PAX DOOR AFT FORMER ORIGINAL MATERIAL THICKNESS IS 0.063", IAW CRJ 200 SRM. EXFOLIATED CORROSION AT MULTIPLE LOCA
- [SDR SWIA202054541](https://openairdocs.org/sdr/SWIA202054541.md): Former · corroded · Nov 4, 2020 · N939SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD FORMER CORRODED IN SEVERAL OF THE UPPER BAYS ON THE INNER SIDE, MARKED (NOTED AFTER INNER SKIN WAS LIFTED). C-CHECK RO 12/05/2020. PAX DOOR FWD FORMER ORIGINAL MATERIAL THICKNESS IS 0.063", IAW CRJ 200 SRM. EXFOLIATED CORROSION AT MULTIPLE LOCA
- [SDR SWIA202054574](https://openairdocs.org/sdr/SWIA202054574.md): Anchor Fitting · corroded · Nov 3, 2020 · N939SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR FWD COUNTERBALANCE ANCHOR FITTING HAS CORRODED ATTACHMENT HARDWARE. C-CHECK RO 12/05/2020. REMOVED AND INSTALLED NEW SERRATED PLATE AND ANCHOR FITTING, PER REFERENCE CRJ 200 AMM. ADJUSTMENT CHECK GOOD.
- [SDR SWIA202054573](https://openairdocs.org/sdr/SWIA202054573.md): Anchor Fitting · corroded · Nov 2, 2020 · N939SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT ANCHOR FITTING SERRATE PLATE IS CORRODED. C-CHECK RO 12/05/2020. REPLACED THE ORIGINAL PAX DOOR AFT ANCHOR PLATE WITH NEW, REF CRJ 200 AMM. TORQUE WRENCH: TUC5660, CAL DUE: 31-JAN-21. NEW PARTS INSTALLED AS FOLLOWS: 1 EA PLATE, 10 EA NUT, 4 EA
- [SDR SWIA202054540](https://openairdocs.org/sdr/SWIA202054540.md): Attach Angle · cracked · Nov 2, 2020 · N939SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 484.00 RBL 27 RT SILL, FLIGHT CONTROL CABLES ROLLER GUIDE BRACKET BOTH ATTACH ANGLES CRACKED, MARKED. C-CHECK RO 12/05/2020. REMOVED INBOARD AND OUTBOARD ANGLE AT FS 484, RBL 27-RBL 36, REF CRJ200 SRM. REPLACED WITH NEW INBOARD AND OUTBOARD REPAIR ANGLE
- [SDR SWIA202054539](https://openairdocs.org/sdr/SWIA202054539.md): Bracket · cracked · Nov 2, 2020 · N939SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 484.00 LBL 27 LT SILL, FLIGHT CONTROL CABLES ROLLER GUIDE BRACKET OUTBOARD ATTACH ANGLE CRACKED, MARKED. C-CHECK RO 12/05/2020. REMOVED AND INSTALLED NEW OUTBOARD REPAIR ANGLE AT FS 484, LBL 27-LBL 36, REF REO. COMPLIED WITH TASK CARD. PRESSURE CHECKS G
- [SDR SWIA202054538](https://openairdocs.org/sdr/SWIA202054538.md): Floor Support · damaged · Nov 2, 2020 · N939SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL INTERCOSTAL FROM FS 559.00-FS 559+16 HAS 100% MATERIAL LOSS AND REQUIRES REPLACEMENT. C-CHECK RO 12/05/2020. REMOVED RT FLOOR SILL INTERCOSTAL AND 3 EA ATTACHING ANGLES FROM FS 559.00-FS 559.00+16, REF CRJ200 SRM. INSTALLED NEW RT FLOOR SILL I
- [SDR SWIA202054572](https://openairdocs.org/sdr/SWIA202054572.md): Cover Plate · corroded · Nov 1, 2020 · N939SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL COVER PLATE HAS CORROSION. C-CHECK RO 12/05/2020. REPLACED DOOR SILL PLATE P/N 601R38957-31. LOCATED NEW HOLES, INSTALLED 6 NEW 8-32 DOME NUTS, IAW CRJ200 DWG 601R38957 REV F CRJ200 SRM SOLID RIVETS AND CRJ200 SRM HOLE PREPERATION.
- [SDR SWIA202054537](https://openairdocs.org/sdr/SWIA202054537.md): Intercostal · corroded · Nov 1, 2020 · N939SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BETWEEN FS 295.00 AND FS 310.00, BETWEEN STGR 17L AND 18L CORRODED. C-CHECK RO 12/05/2020. REMOVED CORRODE INTERCOSTAL AND INSTALLED A NEW INTERCOSTAL AT FS 295 TO FS 310 AT SRINGER 17L AND 18L, REF CRJ 200 SRM AND DRAWING. PRESSURE CHECKS AND O
- [SDR SWIA202054536](https://openairdocs.org/sdr/SWIA202054536.md): Stringer · cracked · Nov 1, 2020 · N939SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STGR 3L CRACKED AT FS 379.00. C-CHECK RO 12/05/2020. REMOVED FASTENERS, CUT OUT BETWEEN FS 379.0 & FS 394.0 AND DISCARDED STR 3L DAMAGED SECTION, REF CRJ 200 SRM. FABRICATED REPAIR PARTS. INSTALLED REPAIR PARTS AT STR 3L BETWEEN FS 379.0 & FS 394.0 AND APP
- [SDR SWIA202054560](https://openairdocs.org/sdr/SWIA202054560.md): Attach Angle · cracked · Oct 31, 2020 · N939SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CLIP ATTACHED TO RT INTERCOSTAL ON FS 621 BULKHEAD CONNECTING TO FRAME AT FS 625, STGR 13R IS CRACKED. C-CHECK RO 12/05/2020. RECEIVED NEW INTERCOSTAL CLIP P/N 601-35012-52. REMOVED DAMAGED CLIP AT FS 625.00 AT STR 13R, IAW CRJ200 SRM. LOCATED AND DRILLED
- [SDR SWIA202054559](https://openairdocs.org/sdr/SWIA202054559.md): Attach Angle · cracked · Oct 31, 2020 · N939SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CLIP ATTACHED TO LT INTERCOSTAL ON FS 621 BULKHEAD CONNECTING TO FRAME AT FS 625, STGR 13L IS CRACKED. C-CHECK RO 12/05/2020. RECEIVED NEW INTERCOSTAL CLIP P/N 601-35012-51. REMOVED DAMAGED CLIP AT FS 625.00 AT STR 13L, IAW CRJ200 SRM. LOCATED AND DRILLED
- [SDR SWIA202054535](https://openairdocs.org/sdr/SWIA202054535.md): Angle · cracked · Oct 31, 2020 · N939SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CLIP ATTACHED TO LT INTERCOSTAL ON FS 621 BULKHEAD CONNECTING TO FRAME AT FS 625, STGR 14L IS CRACKED. C-CHECK RO 12/05/2020. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL P/N 601-35012-53 AT FS 625 STGR 14L, REF DWG, CRJ200 SRM.

Next page: https://openairdocs.org/aircraft/N939SW/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 = 'N939SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N939SW/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.