# Service difficulty reports: N439SW

A list on [N439SW](https://openairdocs.org/aircraft/N439SW.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 · 189 reports

- [SDR SWIA2020013148032](https://openairdocs.org/sdr/SWIA2020013148032.md): Panel · cracked · Jan 15, 2020 · N439SW · Cndair CL6002B19 · Emergency Exits
  > CREW ESCAPE HATCH PANEL HAS CRACKED SCREW HOLE (C-CHECK) RO 1/28/2020 REPAIRED CRACKED SCREW HOLE IN CREW ESCAPE HATCH PANEL USING SATTO-20-21 PER BOMBARDIER, C/W ALL STEPS OF REO.
- [SDR SWIA2020013148031](https://openairdocs.org/sdr/SWIA2020013148031.md): Pressure Deck · cracked · Jan 12, 2020 · N439SW · Cndair CL6002B19 · Fuselage Main, Structure
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA - THE PRESSURE FLOOR SKIN AT FS 461.00 HAS TWO CRACKS 2 INCHES LONG ONE BTWN BL0.0 AND LBL9 AND 1 BTWN BL0.0 AND RBL9. REPAIRED PER REO PER NDT MANUAL, PART NUMBER: -, SERIAL NUMBER: 7578, POSITION: (C-CHECK) R
- [SDR SWIA2020013148030](https://openairdocs.org/sdr/SWIA2020013148030.md): Bulkhead · cracked · Jan 12, 2020 · N439SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > PRESSURE BULKHEAD F/S 621 L/H AFT SIDE STIFFENER P/N 601R36008-51 IS CRACK (C-CHECK) RO 1/28/2020 REMOVED CRACK STIFFENER IAW CRJ 200 SRM 51-42-06. INSTALLED NEW BULKHEAD STIFFENER IAW CRJ 200 SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA2020013148029](https://openairdocs.org/sdr/SWIA2020013148029.md): Skin · worn · Jan 8, 2020 · N439SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT OUTBOARD FLAP, UPPER SURFACE, TRAILING EDGE PREVIOUSLY INSTALLED CHERRY MAX RIVETS FS245 TO FS235 APPEAR TO BE WORN AND HAVE RECESSED BELOW THE UPPER SURFACE OF THE FLAP SKIN. (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED 10EA. BLIND RIVETS ON THE T/E
- [SDR SWIA2020013148028](https://openairdocs.org/sdr/SWIA2020013148028.md): Vertical Beam · cracked · Jan 3, 2020 · N439SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *FOUND POSSIBLE CRACK ON OTBD SIDE AT LWR END OF VERTICAL BEAM (POST) AT FS409+128 LBL 27. (C-CHECK) RO 1/28/2020 VERIFIED CRACK AND REMOVED AND REPLACED O/B VERTICAL POST AT F.S.409+128 LBL27 IN REF REO, DWG, AND CRJ200 SRM. COMPLIED WITH TASK CARD. SEE C
- [SDR SWIA2020013148027](https://openairdocs.org/sdr/SWIA2020013148027.md): Fastener · loose · Jan 3, 2020 · N439SW · Cndair CL6002B19 · Trailing Edge Flaps
  > *MULTIPLE LOOSE FASTENERS ON L/H OTBD FLAP UPPER SURFACE AT THE MID SECTION. MARKED WITH RED GREASE PENCIL. (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED MULTIPLE RIVETS ON THE LH OTBD FLAP UPPER SKIN REF REO. ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CAR
- [SDR SWIA2020013148026](https://openairdocs.org/sdr/SWIA2020013148026.md): Angle · cracked · Dec 29, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Structure
  > *RIGHT HAND - CRACK IN STRUCTURE BELOW THE WINSHIELD POST. (MARKED & FLAGGED) (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED ANGLE. REF CRJ200 SRM, DRW. COMPLIED WITH SKYCARD. SEE CONTINUATION FOR DETAILS.
- [SDR SWIA2020013148025](https://openairdocs.org/sdr/SWIA2020013148025.md): Frame · cracked · Dec 26, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Frame
  > * STRGR 3L CRACKED AT FRAME 379 MARKED (C-CHECK) RO 1/28/2020 CUT AWAY DAMAGED SECTION OF STRINGER 3L BETWEEN FS 379 AND 394 REF CRJ 200 SRM. INSTALLED STRINGER 3L REPAIR PARTS REF CRJ 200 SRM. WEIGHT OF PART REMOVED IS.12LBS AND WEIGHT OF REPAIR PARTS
- [SDR SWIA2020013148024](https://openairdocs.org/sdr/SWIA2020013148024.md): Frame · cracked · Dec 26, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Frame
  > * SUSPECTED CRACK AT FS 333 LBL 5 MARKED (C-CHECK) RO 1/28/2020 VERIFIED CRACK, REMOVED CRACKED FRAME SECTOR AT FS 333 LBL 5 REF CRJ 200 SRM. - INSTALLED NEW FRAME SECTOR PN 601R32004-41 AT FS 333 REF DRAWINGS AND CRJ 200 SRM. RESTORED FINISH AND APPLIED
- [SDR SWIA2020013148023](https://openairdocs.org/sdr/SWIA2020013148023.md): Floor Support · corroded · Dec 26, 2019 · N439SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *LH FLOOR SILL ANGLE HAS SEVERAL AREAS OF CORROSION (MARKED) (C-CHECK) RO 1/28/2020 REPAIRED LH FLOOR PRESSURE SILL ANGLE REF REO. ALL STEPS COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS. PRESSURE CHECK IS GOOD.
- [SDR SWIA2020013148022](https://openairdocs.org/sdr/SWIA2020013148022.md): Spar · corroded · Dec 26, 2019 · N439SW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > RH HORIZONTAL STAB REAR SPAR HAS CORROSION FWD OF OUTBOARD HINGE FITTING (C-CHECK) RO 1/28/2020 REMOVED CORROSION, RH HORIZONTAL STAB REAR SPAR NEAR OUTBOARD HINGE FITTING, REFERENCE CRJ200 SRM. CORROSION REMOVAL STRUCTURALLY ACCEPTABLE REFERENCE REO.
- [SDR SWIA2020013148021](https://openairdocs.org/sdr/SWIA2020013148021.md): Floor Support · corroded · Dec 26, 2019 · N439SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *LH PRESSURE FLOOR SILL HAS SEVERAL AREAS OF CORROSION (MARKED) (C-CHECK) RO 1/28/2020 REPAIRED LH FLOOR PRESSURE SILL REF REO. ALL STEPS APPLICABLE STEPS COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2020013148020](https://openairdocs.org/sdr/SWIA2020013148020.md): Floor Support · corroded · Dec 26, 2019 · N439SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *RH PRESSURE FLOOR SILL HAS SEVERAL AREAS OF CORROSION ( MARKED) (C-CHECK) RO 1/28/2020 REPAIRED RH FLOOR PRESSURE SILL REF REO. ALL STEPS COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS. NO WEIGHT CHANGE AS THESE WERE MINIMAL BLENDS.
- [SDR SWIA2020013148019](https://openairdocs.org/sdr/SWIA2020013148019.md): Frame · corroded · Dec 26, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *FS 605 FRAME CORRODED ON FWD SIDE LOWER FLANGE STR 26R-23L (C-CHECK) RO 1/28/2020 BLENDED CORROSION ON FRAME AT FS 605 BETWEEN STGR 26R AND STGR 23L. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW FS 605.00 FRAME LOWER SECTOR AND REINFORCING ANGLE
- [SDR SWIA2020013148018](https://openairdocs.org/sdr/SWIA2020013148018.md): Frame · corroded · Dec 26, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *FS 589 FRAME ON FWD SIDE LOWER FLANGE CORRODED FROM STR 25R-23L (C-CHECK) RO 1/28/2020 REPAIRED FRAME AT FS 589. REF BOMBARDIER REO AND BOMBARDIER DWG. REFERENCE THE CONTINUE CARD FOR DETAILS. PRESSURE LEAK CHECKS GOOD.
- [SDR SWIA2020013148017](https://openairdocs.org/sdr/SWIA2020013148017.md): Floorbeam · cracked · Dec 24, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS280 FLOORBEAM CLIP RBL9 INBOARD IS CRACKED (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED FS280 FLOORBEAM CLIP RBL9 INBOARD REF. CRJ 200 SRM AND REO. C/W TASK CARD.
- [SDR SWIA2020013148016](https://openairdocs.org/sdr/SWIA2020013148016.md): Floorbeam · cracked · Dec 24, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS280 FLOORBEAM CLIP RBL9 OUTBOARD IS CRACKED (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED FS280 FLOORBEAM CLIP RBL9 OUTBOARD REF. CRJ 200 SRM AND REO. C/W TASK CARD.
- [SDR SWIA2020013148015](https://openairdocs.org/sdr/SWIA2020013148015.md): Floorbeam · cracked · Dec 24, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS280 FLOORBEAM CLIP LBL9 INBOARD IS CRACKED (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED FS280 FLOORBEAM CLIP LBL9 INBOARD REF. CRJ 200 SRM AND REO. C/W TASK CARD. NOTE: REO PREVIOUSLY COMPLIED WITH, AND USED FOR FABRICATION AND INSTALLATION ONLY.
- [SDR SWIA2020013148014](https://openairdocs.org/sdr/SWIA2020013148014.md): Floorbeam · cracked · Dec 24, 2019 · N439SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS280 FLOORBEAM CLIP LBL9 OUTBOARD IS CRACKED (C-CHECK) RO 1/28/2020 REMOVED CRACKED FLOOR BEAM CLIP FS280 LBL9 OUTBOARD REF. CRJ 200 SRM. - INSTALLED NEW FLOOR BEAM CLIP FS280 LBL9 OUTBOARD P/N 601R-53-11-3529-1 REF. REO. PERFORMED FUNCTIONAL TEST OF
- [SDR SWIA2020013148013](https://openairdocs.org/sdr/SWIA2020013148013.md): Strap · corroded · Dec 24, 2019 · N439SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH FLOOR STRAP AT FS559.00 CORROSION SPOTS MARKED (C-CHECK) RO 1/28/2020 REMOVED CORROSION FORM LH FLOOR STRAP AT FS559 CRJ 200 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW LH FLOOR STRAP AT FS559.00 REF CRJ200 SRM AND DWG. PRESSURE CHECK GOOD
- [SDR SWIA2020013148012](https://openairdocs.org/sdr/SWIA2020013148012.md): Seat Track · corroded · Dec 24, 2019 · N439SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO SEAT TRACK STRUCTURE BETWEEN FS574.00 - FS621.00, LBL27 CORROSION AROUND SCREWHOLES MARKED (C-CHECK) RO 1/28/2020 REMOVED CORROSION AT CARGO SEAT TRACK STRUCTURE BETWEEN FS574.00 - FS621.00, LBL27 REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AN
- [SDR SWIA2020013148011](https://openairdocs.org/sdr/SWIA2020013148011.md): Seat Track · corroded · Dec 24, 2019 · N439SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO SEAT TRACK STRUCTURE BETWEEN FS559+112 - FS574.00, LBL27 CORROSION AROUND SCREWHOLES MARKED (C-CHECK) RO 1/28/2020 LBL 27 FLOOR BEAM CAP FOR THE SEAT TRACK CORRODED 100% THRU FLANGE AND INSTALLED A NEW FLOORBEAM CAP FROM APPRX FS 559+10 TO FS 583 REF
- [SDR SWIA2020013148010](https://openairdocs.org/sdr/SWIA2020013148010.md): Angle · cracked · Dec 24, 2019 · N439SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > OTBD CLIP AT FS484.00 RH SIDE PRESSURE FLOOR CRACKED, FLAGGED AND MARKED (C-CHECK) RO 1/28/2020 REMOVED CRACKED CLIP REF CRJ 200 SRM. INSTALLED NEW CLIP REF CRJ 200 SRM WITH REO FOR FASTENERS SIZE AND TYPE. PRESSURE LEAK CHECKS GOOD.
- [SDR SWIA2020013148009](https://openairdocs.org/sdr/SWIA2020013148009.md): Angle · cracked · Dec 24, 2019 · N439SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INBD CLIP AT FS484.00 RH SIDE PRESSURE FLOOR CRACKED, FLAGGED AND MARKED (C-CHECK) RO 1/28/2020 REMOVED CRACKED AND INSTALLED NEW CLIP REF CRJ 200 SRM WITH REO FOR FASTENERS SIZE AND TYPE.
- [SDR SWIA2020013148008](https://openairdocs.org/sdr/SWIA2020013148008.md): Angle · cracked · Dec 24, 2019 · N439SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INBD CLIP AT FS484.00 LH SIDE PRESSURE FLOOR CRACKED, FLAGGED AND MARKED (C-CHECK) RO 1/28/2020 REMOVED CRACKED AND INSTALLED NEW CLIP REF CRJ 200 SRM WITH REO FOR FASTENERS SIZE AND TYPE.
- [SDR SWIA2020013148007](https://openairdocs.org/sdr/SWIA2020013148007.md): Angle · cracked · Dec 24, 2019 · N439SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > OTBD CLIP AT FS484.00 LH SIDE PRESSURE FLOOR CRACKED, FLAGGED AND MARKED (C-CHECK) RO 1/28/2020 REMOVED CRACKED CLIP REF CRJ 200 SRM AND CRJ 200 SRM. INSTALLED NEW CLIP REF CRJ 200 SRM WITH REO FOR FASTENERS SIZE AND TYPE.
- [SDR SWIA2020013148006](https://openairdocs.org/sdr/SWIA2020013148006.md): Skin · corroded · Dec 23, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION ON SKIN DOUBLER FOR ANTENNA BETWEEN FS295.00 - FS310.00, STGR27 - STGR26R, MARKED (C-CHECK) RO 1/28/2020 REMOVED CORROSION FROM SKIN DOUBLER FOR TCAS ANTENNA BETWEEN FS295.00- FS310.00, STGR27-STGR26R REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. IN
- [SDR SWIA2020013148005](https://openairdocs.org/sdr/SWIA2020013148005.md): Frame · corroded · Dec 23, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION FWD SIDE FRAME FLANGE ON FRAME AT FS319.70 BETWEEN STGR24L - STGR25R, MARKED (C-CHECK) RO 1/28/2020 REPAIRED FRAME FS319.70 BETWEEN STGR24L TO STGR25R PER COMPLIED WITH ALL STEPS OF BOMBARDIER REO.
- [SDR SWIA2020013148004](https://openairdocs.org/sdr/SWIA2020013148004.md): Floorbeam · corroded · Dec 23, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAM SUPPORT ANGLE FS349.00 LH SIDE AT WINDSCREEN TIEDOWN POST, MARKED (C-CHECK) RO 1/28/2020 CORROSION ON FLOOR BEAM SUPPORT ANGLE 100% EXFOILIATED, FABRICATED NEW ANGLE AND INSTALLED IT REF DRAWING, AND COMPLIED WITH SKYCARD STRUCTURAL
- [SDR SWIA2020013148003](https://openairdocs.org/sdr/SWIA2020013148003.md): Floor Support · corroded · Dec 23, 2019 · N439SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL CORROSION SPOTS AROUND SCREWHOLES FROM FS349.00 - FS379.00, MARKED (C-CHECK) RO 1/28/2020 REMOVED BAD AND INSTALLED REPLACEMENT RH FLOOR SILL FROM FS349.00 €“ FS409.00 WITH REPLACEMENT HARDWARE REF CRJ200 SRM. COMPLIED WITH TASK CARD. SEE CO
- [SDR SWIA2020013148002](https://openairdocs.org/sdr/SWIA2020013148002.md): Floorbeam · corroded · Dec 23, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS280.00 BEAM HAS CORROSION AROUND SCREW HOLES, COCKPIT ENTRYWAY, MARKED (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED AFT COCKPIT FLOOR SUPPORT AT FS280 REF. CRJ 200 SRM, BOMBARDIER DWG, AND REO. COMPLIED WITH TASK CARD.
- [SDR SWIA2020013148001](https://openairdocs.org/sdr/SWIA2020013148001.md): Floorbeam · corroded · Dec 23, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > COCKPIT ENTRYWAY AFT FLOOR SILL ANGLE CORROSION, MARKED, FS280.00 (C-CHECK) RO 1/28/2020 REPAIRED CORRODED COCKPIT ENTRYWAY AFT FLOOR SILL ANGLE FS280.00 REF. REO, ALL STEPS COMPLIED WITH.
- [SDR SWIA2020013148000](https://openairdocs.org/sdr/SWIA2020013148000.md): Mount · corroded · Dec 23, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > BOTH INBD FWD AND AFT FLOOR MOUNT BOLT HOLES FOR THE GALLEY HAVE CORROSION, MARKED (C-CHECK) RO 1/28/2020 REMOVED CORROSION ON THE GALLEY INBD FWD AND AFT FLOOR MOUNT PLATES PER CRJ 200 SRM. CHECKED AND FOUND AFT PLATE WITHIN LIMIT PER CRJ 200 SRM, ORIGINA
- [SDR SWIA2020013147999](https://openairdocs.org/sdr/SWIA2020013147999.md): Mount · corroded · Dec 23, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > BOTH INBD FWD AND AFT FLOOR MOUNT BOLT HOLES FOR THE WARDROBE HAVE CORROSION, MARKED (C-CHECK) RO 1/28/2020 REMOVED CORROSION ON BOTH IB= FWD AND IB-AFT WARDROBE MOUNT PLATES PER CRJ 200 SRM.,CHECKED AND FOUND IB- FWD PLATE WITHIN LIMIT PER CRJ 200 SRM. OR
- [SDR SWIA2020013147998](https://openairdocs.org/sdr/SWIA2020013147998.md): Cup · corroded · Dec 23, 2019 · N439SW · Cndair CL6002B19 · Passenger/Crew Doors
  > *PAX DOOR FWD AND AFT HANDRAIL CUPS CORRODED (C-CHECK) RO 1/28/2020 BLENDED OUT CORROSION ON THE FWD AND AFT PAX DOOR HANDRAIL CUPS REF CRJ 200 SRM, AFT CUP IN LIMITS AND FWD CUP OUT OF LIMITS REF CRJ 200 SRM, REPLACED FWD CUP REF CRJ 200 SRM AND DRAWING.
- [SDR SWIA2020013147997](https://openairdocs.org/sdr/SWIA2020013147997.md): Shear Tie · corroded · Dec 23, 2019 · N439SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *FS 394 FRAME LOWER FLANGE ON FWD SIDE HAS CORROSION BETWEEN STR 25R-25L (C-CHECK) RO 1/28/2020 REMOVED CORROSION ON FRAME FS394 LOWER FWD FLANGE BETWEEN STGR25R TO STGR25L REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM. MEASURED THICKNESS.039
- [SDR SWIA2020013147996](https://openairdocs.org/sdr/SWIA2020013147996.md): Frame · corroded · Dec 23, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *FS 349 FRAME OPPER FLANGE HAS CORROSION AT STR 26R (C-CHECK) RO 1/28/2020 REMOVED CORROSION ON FRAME AT FS349 UPPER FLANGE STGR26R CRJ200 SRM, REPAIRED FRAME REF REO. COMPLIED WITH ALL STEPS OF REO, SEE CONTINUATION CARDE FOR DETAILS.
- [SDR SWIA2020013147995](https://openairdocs.org/sdr/SWIA2020013147995.md): Skin · corroded · Dec 19, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > *FS559.00 €“ FS574.00 BETWEEN STRG 26L AND 26R EXTERNAL SKIN CORROSION AT NUMEROUS AREAS (MARKED) (C-CHECK) RO 1/28/2020 BLENDED CORROSION BETWEEN FASTENER ROWS @ FS.559 TO FS.559+32, FS.559+32 TO FS559+80, AND FS.559+80 TO FS.574 ON STRG 26L TO STRG 26R
- [SDR SWIA2020013147994](https://openairdocs.org/sdr/SWIA2020013147994.md): Skin · cracked · Dec 19, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > * THE NLG WHEEL WELL SKIN CUTOUT ON LH SIDE JUST BEHIND THE AFT NLG DOOR IS CRACKED. (C-CHECK) RO 1/28/2020 REPAIRED THE CRACK AT THE NLG CUTOUT (LH) SIDE. REF BOMBARDIER REO AND REO. REFERENCE THE CONTINUE CARD FOR DETAILS.
- [SDR SWIA2020013147993](https://openairdocs.org/sdr/SWIA2020013147993.md): Rib · corroded · Dec 19, 2019 · N439SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > *AT WS 50.00 BATT RIB HAS CORROSION AT CANNON PLUG CONNECTIONS R/H INSIDE WHEEL WELL (C-CHECK) RO 1/28/2020 BLENDED CORROSION AT RIGHT BATT RIB.AT WS 53.60 FOUND TO BE WITHIN LIMITS REF REO. COMPLIED WITH ALL APPLICABLE STEPS ON REO. COMPLIED WITH TASK
- [SDR SWIA2020013147992](https://openairdocs.org/sdr/SWIA2020013147992.md): Vane · chafed · Dec 17, 2019 · N439SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * L/H INBD FLAP VANE OUTBD L/E CAP IS CHAFFED, (FLAGGED) (C-CHECK) RO 1/28/2020 BLEND LEFT I/B FLAP VANE O/B CAP REF REO. FOUND TO BE OUT OF LIMITS REF REO. REMOVED AND REPLACED VANE CAP REF CRJ200 SRM, BOMBARDIER DRAWING. COMPLIED WITH SKY CARD.
- [SDR SWIA2020013147991](https://openairdocs.org/sdr/SWIA2020013147991.md): Skin · chafed · Dec 17, 2019 · N439SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * L/H INBD FLAP VANE MIDDLE L/E CAP IS CHAFFED, (FLAGGED) (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED WITH NEW 1EA. L/H I/B FLAP MIDDLE L/E VANE CAP (P/N 601R14303-51S). REF CRJ200 SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA2020013147990](https://openairdocs.org/sdr/SWIA2020013147990.md): Vane · chafed · Dec 17, 2019 · N439SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * R/H INBD FLAP VANE OUTBD L/E CAP IS CHAFFED, (FLAGGED) (C-CHECK) RO 1/28/2020 BLENDED RH INBOARD FLAP VANE OUTBOARD LE CAP CHAFE REF. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW RH INBOARD FLAP VANE OUTBOARD LE CAP REF BOMBARDIER DWG AND CRJ200
- [SDR SWIA2020013147989](https://openairdocs.org/sdr/SWIA2020013147989.md): Vane · chafed · Dec 17, 2019 · N439SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * R/H INBD FLAP VANE MIDDLE L/E CAP IS CHAFFED, (FLAGGED) (C-CHECK) RO 1/28/2020 BLENDED RH INBOARD FLAP VANE MIDDLE LE CAP CHAFE REF REO. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW RH INBOARD FLAP VANE MIDDLE LE CAP REF BOMBARDIER DWG AND CRJ200
- [SDR SWIA2020013147988](https://openairdocs.org/sdr/SWIA2020013147988.md): Vane · chafed · Dec 17, 2019 · N439SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * R/H INBD FLAP VANE INBD L/E CAP IS CHAFFED, (FLAGGED (C-CHECK) RO 1/28/2020 BLENDED RH INBOARD FLAP VANE INBOARD LE CAP CHAFE REF REO. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW RH INBOARD FLAP VANE INBOARD LE CAP REF BOMBARDIER DWG AND CRJ2
- [SDR SWIA2020013147987](https://openairdocs.org/sdr/SWIA2020013147987.md): Bulkhead Web · cracked · Nov 12, 2019 · N439SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER TR, TO APPENDIX B€“
- [SDR SWIA201744149](https://openairdocs.org/sdr/SWIA201744149.md): Cleat · corroded · Dec 12, 2017 · N439SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL CLEAT IS CORRODED. REMOVED AND REPLACED THE CLEAT IAW SRM 51-42-06.
- [SDR SWIA201744148](https://openairdocs.org/sdr/SWIA201744148.md): Intercostal · corroded · Dec 12, 2017 · N439SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL HAS CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM.
- [SDR SWIA201744147](https://openairdocs.org/sdr/SWIA201744147.md): Intercostal · corroded · Dec 12, 2017 · N439SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL HAS CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM.
- [SDR SWIA201744146](https://openairdocs.org/sdr/SWIA201744146.md): Intercostal · corroded · Dec 12, 2017 · N439SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL HAS CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM.

Next page: https://openairdocs.org/aircraft/N439SW/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 = 'N439SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N439SW/reports

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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.