# Service difficulty reports: N979SW

A list on [N979SW](https://openairdocs.org/aircraft/N979SW.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 · 165 reports

- [SDR SWIA20251001928](https://openairdocs.org/sdr/SWIA20251001928.md): Rib · cracked · Sep 28, 2025 · N979SW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > CRACK ON A NUTPLATE HOLE ON THE LH H-STAB RIB NO. 9 SPLICE (DWG: 600-23037 AL ALY ALCD 2024-T3, 0.032" NOM THK, REF) LOCATED ALONG LBL112.00. COMPLIED WITH TEMP REPAIRS PER REO 601-55-11-792. COMPLY WITH PERMANENT REPAIR OF L/H H-STAB RIB 9 SPLICE NUTPLATE HOL
- [SDR SWIA2025F01396](https://openairdocs.org/sdr/SWIA2025F01396.md): Rib · cracked · Sep 28, 2025 · N979SW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA99994-REO 601R-55-11-792 REV-- DATED 5/24/25 MXCODEID110694-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 99994CRACK ON A NUTPLATE HOLE ON THE LH H-STAB RIB NO. 9 SPLICE (DWG: 600-23037 AL ALY ALCD 2024-T3, 0.032" NOM TH
- [SDR SWIA2024012631202](https://openairdocs.org/sdr/SWIA2024012631202.md): Stiffener · cracked · Dec 2, 2023 · N979SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 409+128 BULKHEAD INBD STIFFENER @ BL36L IS CRACKED IN LOWER RADIUS (C-CHECK RO 1/24/2024) INSTALLED NEW INBOARD STIFFENER P/N 601R32208-227 IN FS409+128 BULKHEAD, LBL36 REF. DWG 601R32208 REV-T AND CRJ 200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-10
- [SDR SWIA2024012631201](https://openairdocs.org/sdr/SWIA2024012631201.md): Floorbeam · cracked · Dec 1, 2023 · N979SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280.00 @ RBL 9, O/B SIDE, FLOOR SUPPORT BEAM, UPPER HORIZONTAL SPLICE ANGLE FOUND CRACKED IN RADIUS ON I/B END OF SPLICE (C-CHECK RO 1/24/2024) INSTALLED NEW FLOOR SUPPORT BEAM UPPER HORIZONTAL SPLICE ANGLE AT FS 280.00 @ RBL 9, O/B SIDE, REF CRJ 200 SR
- [SDR SWI2024F00054](https://openairdocs.org/sdr/SWI2024F00054.md): Stiffener · cracked · Nov 30, 2023 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128, LBL 27, VERTICAL STIFFENER CRACKED AT LOWER END IN RADIUS. (C-CHECK RO 1/24/2024) REMOVED AND INSTALLED A NEW INBD STIFFENER REF AT FS409+128 LBL27. CRJ 200 SRM 51-42-06 AND 51-42-22, REO 601R-53-41-3201 REV-- DATED 2023-12-08, DWG 601R32208 RE
- [SDR SWIA2024012631130](https://openairdocs.org/sdr/SWIA2024012631130.md): Angle · cracked · Nov 30, 2023 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280, RBL 9 INBOARD VERTICAL ANGLE CRACKED AT TOP END. (C-CHECK RO 1/24/2024) INSTALLED NEW VERTICAL ANGLE AT FS 280.00, RBL 9 (INBOARD SIDE) REF CRJ 200 SRM 51-42-21-00 AND DWG 601R31113 REV AD. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2024012631120](https://openairdocs.org/sdr/SWIA2024012631120.md): Skin · damaged · Nov 20, 2023 · N979SW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > RH HORIZONTAL STAB TIP HAS EVIDENCE OF LIGHTNING STRIKE (FLAGGED) (C-CHECK RO 1/24/2024) REPAIRED LIGHTNING STRIKE DAMAGE TO RH HORIZONTAL STAB TIP TO MHIRJ REO 601R-55-11-752 REV -A DATED 2023-12-13, SEE CONTINUE CARD FOR DETAILS OF REPAIR.COMPLIED WITH S
- [SDR SWIA2024012631116](https://openairdocs.org/sdr/SWIA2024012631116.md): Window Post · cracked · Nov 16, 2023 · N979SW · Cndair CL6002B19 · Fuselage Main, Structure
  > * CO-PILOT'S WINDSHIELD SIDE POST, LOWER ANGLE BELOW BOTTOM OF WINDSHIELD SILL IS CRACKED, MARKED. (C-CHECK RO 1/24/2024) INSTALLED NEW FRAME SECTION P/N 601R34032-22. REF: CRJ200 SRM 51-42-06 AND DWG 601R34032, REV: V. NO LEAKS NOTED. COMPLIED WITH TASK C
- [SDR SWI2024F00053](https://openairdocs.org/sdr/SWI2024F00053.md): Lintel · cracked · Nov 12, 2023 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *PAX DOOR SURROUND UPPER LINTEL CRACKED AT FS.280.00 (FLAGGED). (C-CHECK RO 1/24/2024) REMOVED AND REPLACED ALL CRACKED PARTS WITH FABRICATED NEW ONES. REF: CRJ-200 SRM 51-42-21, DWG-600-31057 REV-P, CMS6144. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY
- [SDR SWIA2024012631112](https://openairdocs.org/sdr/SWIA2024012631112.md): Bulkhead · cracked · Nov 12, 2023 · N979SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > PREVIOUS BOTTOM REPAIR ANGLE AT BULKHEAD FS280.00 RBL-9 HAS CRACK. (C-CHECK RO 1/24/2024) REMOVED EXISTING REPAIR ANGLE. REF: CRJ-200 S.R.M.51-42-06,51-42-21.INSTALLED NEW REPAIR DOUBLER. REF: CRJ-200 S.R.M. 51-42-06, 51-42-21 AND REO 601R-53-11-171 REV -
- [SDR SWIA2024012631111](https://openairdocs.org/sdr/SWIA2024012631111.md): Cleat · corroded · Nov 11, 2023 · N979SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD HANDRAIL CAP (CLEAT) BETWEEN FS310.00 TOFS319.00 HAS CORROSION (MARKED) (C-CHECK RO 1/24/2024) INSTALLED NEW PAX DOOR FWD HANDRAIL CAP (CLEAT) BETWEEN FS310.00 TOFS319.00. REF CRJ200 SRM 51-42-06 & DWG 601R31527 REV AM. COMPLIED WITH TASK CARD
- [SDR SWI2024F00052](https://openairdocs.org/sdr/SWI2024F00052.md): Floor Support · corroded · Nov 11, 2023 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H FLOOR BEAM AT LBL9 BETWEEN FS394.00 TO FS409.00+128 SEVERAL AREAS HAS CORROSION (MARKED) (C-CHECK RO 1/24/2024) REMOVED AND REPLACED LBL 9 FLOOR BEAM CAP BEWTEEN F.S. 394 AND F.S. 409+128 WITH NEW, REF CRJ 200 SRM 51-42-06, DWG 601R31117 REV E AND REO
- [SDR SWI2024F00051](https://openairdocs.org/sdr/SWI2024F00051.md): Floor Support · corroded · Nov 11, 2023 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H FLOOR BEAM AT RBL9 BETWEEN FS394.00 TO FS409.00+128 SEVERAL AREAS HAS CORROSION (MARKED) (C-CHECK RO 1/24/2024) R/H FLOOR BEAM AT RBL 9 BETWEEN FS 409.00+5 AND FS 409.00+118 FOUND TO BE BEYOND LIMITS IAW CRJ 200 SRM 53-00-00 AND GENERIC REO 601R-53-00-
- [SDR SWI2024F00050](https://openairdocs.org/sdr/SWI2024F00050.md): Cleat · corroded · Nov 11, 2023 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR AFT HANDRAIL CAP (CLEAT) BETWEEN FS333.00 TOFS349.00 HAS CORROSION (MARKED) (C-CHECK RO 1/24/2024) REPLACED OUT OF LIMIT PAX DOOR AFT HANDRAIL CAP & CLEAT. REF CRJ200 SRM 51-42-06 & DWG 601R31527 REV AM. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWI2024F00046](https://openairdocs.org/sdr/SWI2024F00046.md): Floor Support · corroded · Nov 11, 2023 · N979SW · 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 1/24/2024) BLENDED OUT NUMEROUS AREAS OF CORROSIONS L/H PRESSURE FLOOR SILL BETWEEN FS409.00+128 TO FS559.00, EVALUATED AND PERFORMED REO 601R-53-41-
- [SDR SWI2024F00045](https://openairdocs.org/sdr/SWI2024F00045.md): Floor Support · corroded · Nov 11, 2023 · N979SW · 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 1/24/2024) REPAIRED R/H PRESSURE FLOOR SILL BETWEEN FS409.00+128 TO FS559.00 REF REO 601R-53-41-3195 REV -- DATED 2023-11-24 AND REO 601R-53-41-666
- [SDR SWI2024F00044](https://openairdocs.org/sdr/SWI2024F00044.md): Seat Track · corroded · Nov 10, 2023 · N979SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT TRACK RBL9 BETWEEN FS 559.00+64 - 559.00+80. MARKED. (HN00121983) (C-CHECK RO 1/24/2024) REMOVED AND INSTALLED NEW FLOOR SEAT TRACK RBL9 BETWEEN FS 559+64 TO FS 559.00+80 REFCRJ-200 AMM 53-01-11-400-802 AND CRJ-200 AMM 53-01-11-00
- [SDR SWI2024F00043](https://openairdocs.org/sdr/SWI2024F00043.md): Floor Support · corroded · Nov 10, 2023 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON LBL9 FLOOR BEAM BETWEEN FS 589.00 - 605.00. MARKED. (HN00121987) (C-CHECK RO 1/24/2024) COMPLIED WITH PERMANENT REPAIR ON LBL-9 FS589.00 - FS605.00 FLOOR SUPPORT STRUCTURE SPLICE REPAIR. REF CRJ-200 SRM 53-00-43 REPAIR NO.-2 FIGURE 201 AND 203
- [SDR SWI2024F00042](https://openairdocs.org/sdr/SWI2024F00042.md): Floor Support · corroded · Nov 10, 2023 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON RBL9 FLOOR BEAM BETWEEN FS 589.00 - 605.00. MARKED. (HN00121985) (C-CHECK RO 1/24/2024) COMPLIED WITH PERMANENT REPAIR ON FLOOR BEAM SPLICE SUPPORT STRUCTURE AT RBL-9 FS589.00 - FS605.00 REF CRJ-200 SRM 53-00-43, REPAIR NO. 2. COMPLIED WITH SK
- [SDR SWIA2024012631110](https://openairdocs.org/sdr/SWIA2024012631110.md): Floor Support · corroded · Nov 10, 2023 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON RBL9 FLOOR BEAM BETWEEN FS 559.00+64 - 559.00+80. MARKED. (HN00121979) (C-CHECK RO 1/24/2024) REPAIRED RBL9 FLOOR BEAM BETWEEN FS559+64 - FS559+80. PER REO 601R-53-00-883 REV -- DATED 2023-11-21 AND REF CRJ200 SRM 53-00-43. COMPLIED WITH TASK
- [SDR SWI2024F00041](https://openairdocs.org/sdr/SWI2024F00041.md): Door Frame · corroded · Nov 8, 2023 · N979SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR FRAME FS313.56 HAS INTERGRANULAR CORROSION (C-CHECK RO 1/24/2024) INSTALLED NEW PAX DOOR FRAME AT FS 313.56 PN 601R318086-1 REF CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV N. PRESSURE LEAK TEST GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY
- [SDR SWI2024F00040](https://openairdocs.org/sdr/SWI2024F00040.md): Former · corroded · Nov 8, 2023 · N979SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR AFT FORMER FS347.25 HAS INTERGRANULAR CORROSION (C-CHECK RO 1/24/2024) REMOVED AND INSTALLED A NEW PAX DOOR AFT FORMER AT FS347.25. REF CRJ 200 SRM 51-42-06, CRJ-200 SRM 51-42-21, AND DRAWING 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-1003-SK
- [SDR SWI2024F00039](https://openairdocs.org/sdr/SWI2024F00039.md): Former · corroded · Nov 8, 2023 · N979SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR FORWARD FORMER FS311.75 HAS INTERGRANULAR CORROSION (C-CHECK RO 1/24/2024) INSTALLED NEW PAX DOOR FWD FORMER FS 311.75 PN 601R318031-5 REF CRJ 200 SRM 51-42-06 AND SRM 51-42-21 AND DWG 601R31702 REV N. NO LEAKS NOTED. COMPLIED WITH TASK CARD 51-90
- [SDR SWI2024F00038](https://openairdocs.org/sdr/SWI2024F00038.md): Intercostal · corroded · Nov 8, 2023 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR INTERCOSTAL DD4 FS320.00 - FS3338.00 HAS INTERGRANULAR CORROSION (C-CHECK RO 1/24/2024) REMOVED AND INSTALLED A NEW PAX DOOR INTERCOSTAL DD4 AT FS.320-FS.338 REF CRJ-200 SRM 51-42-06, CRJ-200 SRM 51-42-21, AND DRAWING 601R31702 REV N. COMPLIED WIT
- [SDR SWI2024F00037](https://openairdocs.org/sdr/SWI2024F00037.md): Intercostal · corroded · Nov 8, 2023 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR INTERCOSTAL DD3 FS320.00 - FS3338.00 HAS INTERGRANULAR CORROSION (C-CHECK RO 1/24/2024) REMOVED AND INSTALLED A NEW PAX DOOR INTERCOSTAL DD3 AT FS.320-FS.338 REF CRJ-200 SRM 51-42-06, CRJ-200 SRM 51-42-21, AND DRAWING 601R31702 REV N. COMPLIED WIT
- [SDR SWI2024F00036](https://openairdocs.org/sdr/SWI2024F00036.md): Intercostal · corroded · Nov 8, 2023 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR INTERCOSTAL DD5 FS338.00 - FS347.25 HAS INTERGRANULAR CORROSION (C-CHECK RO 1/24/2024) REMOVED AND INSTALLED A NEW PAX DOOR INTERCOSTAL DD5 AT FS.338-FS.347.25 REF CRJ-200 SRM 51-42-06 AND DRAWING 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-10
- [SDR SWI2024F00035](https://openairdocs.org/sdr/SWI2024F00035.md): Intercostal · corroded · Nov 8, 2023 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR INTERCOSTAL DD4 FS338.00 - FS347.25 HAS INTERGRANULAR CORROSION (C-CHECK RO 1/24/2024) REMOVED AND INSTALLED A NEW PAX DOOR INTERCOSTAL DD4 AT FS.338-FS.347.25 REF CRJ-200 SRM 51-42-06 AND DRAWING 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-10
- [SDR SWI2024F00034](https://openairdocs.org/sdr/SWI2024F00034.md): Intercostal · cracked · Nov 8, 2023 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR INTERCOSTAL DD1 FS338.00 - FS347.25 IS CRACKED (C-CHECK RO 1/24/2024) REMOVED AND INSTALLED A NEW PAX DOOR INTERCOSTAL DD1 AT FS.338-FS.347.25 REF CRJ-200 SRM 51-42-06 AND DRAWING 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-1003-SKY PRESSURE L
- [SDR SWIA2024012631108](https://openairdocs.org/sdr/SWIA2024012631108.md): Intercostal · corroded · Nov 8, 2023 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR INTERCOSTAL DD3 FS311.75 - FS320.00 HAS INTERGRANULAR CORROSION (C-CHECK RO 1/24/2024) REMOVED AND INSTALLED A NEW PAX DOOR INTERCOSTAL DD3 FS311.75 - FS320.00. REF CRJ 200 SRM 51-42-06 AND DRAWING 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-1
- [SDR SWIA2024012631107](https://openairdocs.org/sdr/SWIA2024012631107.md): Intercostal · corroded · Nov 7, 2023 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR INTERCOSTAL DD2 FS320.00 - FS338.00 IS CORRODED (C-CHECK RO 1/24/2024) REMOVED AND INSTALLED A NEW PAX DOOR INTERCOSTAL DD2 FS.320-FS.338 REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 AND DWG 601R31702 REV N. PRESSURE CHECK GOOD. COMPLIED WITH TA
- [SDR SWIA2024012631103](https://openairdocs.org/sdr/SWIA2024012631103.md): Rib · cracked · Nov 3, 2023 · N979SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LEFT WING BATT RIB, WS48.30 IS CRACKED. (MARKED) (C-CHECK RO 1/24/2024) REMOVED CRACKED AND INSTALLED NEW LH BATT RIB P/N 600-10389-1 AT WS48.30 REF CRJ 200 SRM 51-42-21 REVISION 39: MAR 10/2021, DRAWINGS 601R10212 REV A AND 601R10204 REV -J FOR FASTENER
- [SDR SWIA2024012630607](https://openairdocs.org/sdr/SWIA2024012630607.md): Attach Fitting · cracked · Jun 7, 2023 · N979SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > *RIGHT WING TO FUSELAGE ATTACHMENT AT RBL45 AND FS513.00 IS CRACKED ON THE UPPER FLANGE. (C-CHECK RO 1/24/2024) REMOVED AND REPLACED RH WING TO FUSELAGE ATTACHMENT FITTING REF. REO 601R-57-11-099 REV. -A DATED 2024-01-04 STEPS 1-20, ALL STEPS COMPLIED WITH
- [SDR SWIA2024012630522](https://openairdocs.org/sdr/SWIA2024012630522.md): Vane · chafed · May 22, 2023 · N979SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING INBD FLAP VANE LEADING EDGE OUTBD CHAFFED MARKED (C-CHECK RO 1/24/2024) LEFT WING I/B FLAP VANE, O/B LEADING EDGE CHAFFE MARKS BLENDED AND FOUND TO BE BEYOND LIMITS IAW CRJ 200 SRM 57-52-00 AND REO 601R-57-52-004 REV-D, DATED 2012-12-19. FLAP VAN
- [SDR SWI2024F00033](https://openairdocs.org/sdr/SWI2024F00033.md): Skin · dented · May 18, 2023 · N979SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > MULTIPLE DENTS AND GOUGES FOUND ALONG THE EDGE OF THE CARGO DOOR HANDLE HOUSING (C-CHECK RO 1/24/2024) HANDLE HOUSING ASSY AT CARGO DOOR STRUCTURE WITH NEW FASTENERS PER CRJ200 SRM 51-42-21 REF. BOMBARDIER DWG. 601R35027 REV. AY. COMPLIED WITH TASK CARD 51
- [SDR SWIA202401260518](https://openairdocs.org/sdr/SWIA202401260518.md): Vane · chafed · May 18, 2023 · N979SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP VANE LEADING EDGE HAS CHAFFING IN 3EA AREAS (C-CHECK RO 1/24/2024) RIGHT I/B FLAP VANE LEADING EDGE CHAFFING IN 3 AREAS BLENDED AND EVALUATED IAW REO 601R-57-52-004 REV.-D DATED 2012-12-19 PERMANENT REPAIR. I/B & CENTER LEADING EDGES ARE
- [SDR SWIA202161095](https://openairdocs.org/sdr/SWIA202161095.md): None · failed · Sep 21, 2021 · N979SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > GEAR DISAGREE WARNING MSG DURING RETRACTION. L MAIN GEAR. PERFORMED QRH. (FLIGHT 5397 - FILED CLOSED) T/S PER FIM 32-60-09. THE ONLY PSEU CODE WAS SHOWING S20 FAR. PERFORMED GEAR SWING AND NOTICED LT GEAR WOULD GO UP AND LOCK INTO THE UPLOCK THE SAME TIME
- [SDR SWIA2019101846544](https://openairdocs.org/sdr/SWIA2019101846544.md): Drag Angle · cracked · Oct 2, 2019 · N979SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE PREVIOUS REPAIR IS CRACKED BEHIND MOTOR PULLEY BRACKET, APPROX 1.5" LONG. (C-CHECK) RO: 10/16/2019 REMOVED AND REPLACED AFT PAX DOOR DRAG ANGLE IAW SRM.
- [SDR SWIA2019101846543](https://openairdocs.org/sdr/SWIA2019101846543.md): Bulkhead Web · gouged · Sep 26, 2019 · N979SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT FACE OF R/H F.S. 280.00 BULKHEAD SKIN IS GOUGED AT 2EA LOCATIONS (C-CHECK) RO: 10/16/2019 REPAIRED IAW REO.
- [SDR SWIA2019101846542](https://openairdocs.org/sdr/SWIA2019101846542.md): Floorbeam · corroded · Sep 26, 2019 · N979SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > F.S. 621.00 FLOOR SUPPORT ANGLE IS CORRODED AT MULTIPLE LOCATIONS BETWEEN LBL 45 AND RBL 27. (C-CHECK) RO: 10/16/2019 REMOVED CORROSION BY COMPLYING WITH REPAIR AT F.S 621 BETWEEN LBL 45 AND RBL 27 FLOOR SUPPORT ANGLE IAW REO.
- [SDR SWIA2019101846541](https://openairdocs.org/sdr/SWIA2019101846541.md): Angle · corroded · Sep 26, 2019 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL ANGLE IS CORRODED AROUND PROX SENSOR AND MULTIPLE NUTPLATE HOLES. (C-CHECK) RO: 10/16/2019 INSTALLED NEW SILL ANGLE IAW SRM.
- [SDR SWIA2019101846540](https://openairdocs.org/sdr/SWIA2019101846540.md): Floorbeam · cracked · Sep 26, 2019 · N979SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL 9 FLOOR BEAM I/B AND O/B ATTACHMENT ANGLES ARE CRACKED AT F.S. 280.00. (C-CHECK) RO: 10/16/2019 REMOVED AND REPLACED RBL 9 I/B AND O/B ATTACHMENT ANGLES AT F.S 280 IAW SRM.
- [SDR SWIA2019101846539](https://openairdocs.org/sdr/SWIA2019101846539.md): Floorbeam · cracked · Sep 26, 2019 · N979SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL 9 FLOOR BEAM I/B AND O/B ATTACHMENT ANGLES ARE CRACKED AT F.S. 280.00. (C-CHECK) RO: 10/16/2019 REMOVED AND REPLACED LBL 9 I/B AND O/B ANGLES AT F.S 280 IAW SRM.
- [SDR SWIA2019101846538](https://openairdocs.org/sdr/SWIA2019101846538.md): Angle · cracked · Sep 25, 2019 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 36 F.S. 484 CLIP IS CRACKED. (C-CHECK) RO: 10/16/2019 REMOVED AND REPLACED CLIP IAW SRM.
- [SDR SWIA2019101846536](https://openairdocs.org/sdr/SWIA2019101846536.md): Angle · cracked · Sep 25, 2019 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 36 F.S. 484 CLIP IS CRACKED. (C-CHECK) RO: 10/16/2019 REMOVED AND REPLACED CLIP IAW SRM.
- [SDR SWIA2019101846535](https://openairdocs.org/sdr/SWIA2019101846535.md): Angle · cracked · Sep 25, 2019 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 27 F.S. 484 CLIP IS CRACKED. (C-CHECK) RO: 10/16/2019 REMOVED DAMAGED CLIP AT LBL 27 F.S. 484.00. LOCATED AND DRILLED 8 EA FASTENER HOLES ON CLIP. INSTALLED NEW SERVICEABLE CLIP IAW SRM.
- [SDR SWIA2019101846534](https://openairdocs.org/sdr/SWIA2019101846534.md): Seat Track · corroded · Sep 25, 2019 · N979SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 FLOOR SEAT RAIL IS CORRODED IN VARIOS LOCATIONS STATRING AT F.S. 409.00 TO F.S. 409.00+128.(C-CHECK) RO: 10/16/2019 REMOVED CORRODED/DAMAGED FLOOR SEAT TRACK AT LBL 9 FROM F.S. 409.00 TO F.S. 409.00+128 AND REPLACED WITH NEW SERVICABLE SEAT TRACK IAW AMM
- [SDR SWIA2019101846533](https://openairdocs.org/sdr/SWIA2019101846533.md): Window Post · cracked · Sep 25, 2019 · N979SW · Cndair CL6002B19 · Fuselage Main, Structure
  > R/H WINDSHIELD SIDE POST AFT BRACKET IS CRACKED. (C-CHECK) RO: 10/16/2019 REMOVED CRACKED R/H WINDSHIELD SIDE POST AFT BRACKET, AND INSTALLED A NEW SERVICEABLE BRACKET IAW SRM.
- [SDR SWIA2019101846532](https://openairdocs.org/sdr/SWIA2019101846532.md): Trunnion · damaged · Sep 18, 2019 · N979SW · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > RH MLG TRUNNION HAS AN INDICATION.1" LONG BY 50% FSH IN THE 2ND TO LAST OUTBD FASTENER HOLE. FAILED NDT INSPECTION. (C-CHECK) RO: 10/16/2019 REPAIRED DAMAGED FASTENER HOLE ON R/H WING LOWER SURFACE AT WS 65.75 IAW REO.
- [SDR SWIA2019101846531](https://openairdocs.org/sdr/SWIA2019101846531.md): Structure · damaged · Sep 17, 2019 · N979SW · Cndair CL6002B19 · Standard Practices/Structures
  > WHILE INCORPORATING SB 601R-57-046 REV C, FOUND 1EA. OVERSIZE (#14) FASTENER HOLE (C-CHECK) RO: 10/16/2019 REPAIRED IAW REO.
- [SDR SWIA2019101846530](https://openairdocs.org/sdr/SWIA2019101846530.md): Bracket · cracked · Sep 17, 2019 · N979SW · Cndair CL6002B19 · Wing, Attach Fittings
  > L/H WHEEL WELL FWD HYD FUSE BRACKET IS CRACKED. (C-CHECK) RO: 10/16/2019 RREMOVED UNSERVICEABLE L/H WHEEL WELL FWD HYD FUSE BRACKET IAW SRM. INSTALLED NEW SERVICEABLE L/H WHEEL WELL FWD HYD FUSE BRACKET IAW SRM.

Next page: https://openairdocs.org/aircraft/N979SW/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 = 'N979SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N979SW/reports

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