# Service difficulty reports: N978SW

A list on [N978SW](https://openairdocs.org/aircraft/N978SW.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 · 205 reports

- [SDR SWIA2026082576960](https://openairdocs.org/sdr/SWIA2026082576960.md): Diaphragm · cracked · Aug 25, 2026 · N978SW · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND DIAPHRAGM UNDER UPPER AFT CORNER COVER OF PAX DOOR CRACKED. REMOVED AND REPLACED DIAPHRAGM UNDER UPPER AFT CORNER COVER OF PAX DOOR IN REF, TO REO 601R-52-11-3131, REV.--, DATED 2026-08-25, COMPLETED TASK CARD 51-900-1003-SKY AND M-337. ALL NDT'S COMPL
- [SDR SWIA2026082476955](https://openairdocs.org/sdr/SWIA2026082476955.md): Cover · cracked · Aug 24, 2026 · N978SW · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND CRACKED IN THE PAX DOOR BETWEEN THE FOLDING STEP & WHEEL SYSTEM. REMOVED AND REPLACED PAX DOOR UPPER AFT CORNER COVER IN REF. TO REO 601R-52-11-3131, REV. --, DATED 2026-08-25, NO DEFECTS NOTED AT THIS TIME.
- [SDR SWIA2026082476944](https://openairdocs.org/sdr/SWIA2026082476944.md): Door Seal · dented · Aug 24, 2026 · N978SW · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND DENT AND SEPERATION OF DOUBLER ON PAX DOOR SEAL SURROUND AFT SIDE IN FRONT OF UPPER PIN STOP FITTING. REMOVED AND REPLACED DOUBLER ON PAX DOOR SEAL SURROUND AFT SIDE IN FRONT OF UPPER PIN STOP FITTING IN REFERENCE TO TO GREO 601R-53-22-033 REV-D 2014/02/
- [SDR SWIA2025120900001](https://openairdocs.org/sdr/SWIA2025120900001.md): Apu · faulted · Dec 1, 2025 · N978SW · Cndair CL6002B19 · APU Oil System
  > APU OIL TEMP CAUTION AT CRUISE. (FLIGHT 5116) REF AML 1760814, REF AML 1760819, REF AML 1760821, DEFERRING APU IAW MEL 49-10-1A. REMOVED & REPLACED APU ASSY, & APU GENERATOR. OPS CHKD GOOD. APU OIL TEMP CAUTION NO LONGER DISPLAYED. DMI CLEARED AND PLACAR
- [SDR SWIA2025120200001](https://openairdocs.org/sdr/SWIA2025120200001.md): Oil System · warning message · Dec 1, 2025 · N978SW · Cndair CL6002B19 · APU Oil System
  > APU OIL TEMP CAUTION IN CRUISE. MEL 49-10-1ACAT C, ODI EVENT, (FLIGHT 5116) REFERENCE AML 1760814, REFERENCE AML 1760819, REFERENCE AML 1760821. DEFERRING APU IAW MEL 49-10-1A. MAINTENANCE PROCEDURES COMPLIED WITH. PLACARD INSTALLED.
- [SDR SWIA20251202130](https://openairdocs.org/sdr/SWIA20251202130.md): Oil System · warning message · Nov 30, 2025 · N978SW · Cndair CL6002B19 · APU Oil System
  > APU OIL TEMP CAUTION AT CRUISE. (FLIGHT 5116) REFERENCE AML 1760814, REFERENCE AML 1760819, REFERENCE AML 1760821. DEFERRING APU IAW MEL 49-10-1A. MAINTENANCE PROCEDURES COMPLIED WITH. PLACARD INSTALLED.
- [SDR SWIA2025120111301](https://openairdocs.org/sdr/SWIA2025120111301.md): Warning Message · illuminated · Nov 30, 2025 · N978SW · Cndair CL6002B19 · APU Oil System
  > APU OIL TEMP CAUTION AT CRUISE. (FLIGHT 5116)
- [SDR SWIA2024081900013](https://openairdocs.org/sdr/SWIA2024081900013.md): Oil System · low pressure · Aug 13, 2024 · N978SW · Cndair CL6002B19 · Engine Oil Pressure
  > AT CRUISE APPROX 25 MIN FROM XWA GOT L ENG OIL PRESS WARNING MESSAGE. RAN QRH. IT CALLED FOR SHUTTING THE ENGINE DOWN. RAN QRH FOR SHUTTING LEFT ENGINE DOWN. LANDED SAFELY. FLIGHT 5461. REPLACED LEFT ENGINE ATS, IDG, #6 AND #7 CARBON SEALS AND EXHAUST FRAME
- [SDR SWIA2024081400013](https://openairdocs.org/sdr/SWIA2024081400013.md): Oil System · low pressure · Aug 13, 2024 · N978SW · Cndair CL6002B19 · Engine Oil Quantity
  > AT CRUISE APPROX 25 MIN FROM XWA GOT L ENG OIL PRESS WARNING MESSAGE. RAN QRH. IT CALLED FOR SHUTTING THE ENGINE DOWN. RAN QRH FOR SHUTTING LEFT ENGINE DOWN. LANDED SAFELY. (FLIGHT 5461 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWI2024061800493](https://openairdocs.org/sdr/SWI2024061800493.md): Bpsu · failed · Jun 17, 2024 · N978SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECEIVED FLAPS FAIL CAUTION MESSAGE AT CRUISE ALTITUDE. RAN QRH AND RETURNED TO ORD. (FLIGHT 5722 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28399576 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CP 28400569 FOR TROUBLESHOOTING OF FLA
- [SDR SWIA2023090831](https://openairdocs.org/sdr/SWIA2023090831.md): Unknown · dented · Aug 31, 2023 · N978SW · Cndair CL6002B19 · Wing Structure
  > RH WING LEADING EDGE PANE 620 JL HAS A SMALL DENT ON THE INBOARD SIDE (TOP) 27104415 (C-CHECK RO 9/6/2023) REPAIRED R/H WING LEADING EDGE PANEL REF REO 601R-57-41-1165 REV -- DATED 2023-09-01. COMPLIED WITH 51-900-1003-SKY AND VISUALLY INSPECT FOR ANY
- [SDR SWIA202309080729](https://openairdocs.org/sdr/SWIA202309080729.md): Unknown · cracked · Jul 29, 2023 · N978SW · Cndair CL6002B19 · Fuselage Structure (General)
  > *FS333.00 STRG 0 - STRG 1LH, FRAME POSSIBLY CRACKED AT LOWER MACHINE HOLE (MARKED) 26957001 (C-CHECK RO 9/6/2023) REPAIRED FS333.00 STRG 0 - STRG 1LH, FRAME REO 601R-53-21-3642 REV -- DATE 2023-08-11. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION C
- [SDR SWI20230908319](https://openairdocs.org/sdr/SWI20230908319.md): Unknown · cracked · Jul 26, 2023 · N978SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L IS CRACKED JUST FORWARD OF FRAME 379.00 AT IS CONNECTION POINT WITH THE PASSENGER DOOR UPPER SILL FITTING. (MARKED) (C-CHECK RO 9/6/2023) REPAIRED STRINGER 3L JUST FORWARD OF FRAME 379.00 REF CRJ-200-SRM 53-00-03. COMPLIED WITH 51-900-1003-
- [SDR SWI2023F00319](https://openairdocs.org/sdr/SWI2023F00319.md): Unknown · cracked · Jul 26, 2023 · N978SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L IS CRACKED JUST FORWARD OF FRAME 379.00 AT IS CONNECTION POINT WITH THE PASSENGER DOOR UPPER SILL FITTING. (MARKED) (C-CHECK RO 9/6/2023) REPAIRED STRINGER 3L JUST FORWARD OF FRAME 379.00 REF CRJ-200-SRM 53-00-03. COMPLIED WITH 51-900-1003-
- [SDR SWIA20230908725](https://openairdocs.org/sdr/SWIA20230908725.md): Unknown · cracked · Jul 25, 2023 · N978SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CRACK ON COCKPIT FLOOR SUPPORT ANGLE,FWD OF FS 280 FLOOR BEAM. (C-CHECK RO 9/6/2023) REPLACED CRACK COCKPIT FLOOR SUPPORT ANGLE,FWD OF FS 280 FLOOR BEAM WITH NEW ANGLE PN 600-34017-351 PO# T-69724 REF CRJ 200 SRM 51-42-06 AND DWG 600-34017 REV A
- [SDR SWIA202309080723](https://openairdocs.org/sdr/SWIA202309080723.md): Unknown · corroded · Jul 23, 2023 · N978SW · Cndair CL6002B19 · Empennage Structure
  > AFTER REMOVAL OF R/H ELEVATOR FITTING AT BL15.25, FITTING WAS DIS-ASSEMBLED TO EVALUTE PRIOR TO NEW BEARING INSTALLATION AND FOUND CORROSION AND PITTING INSIDE BOTH SIDES OF BEARING BORE. (C-CHECK RO 9/6/2023) R/H ELEVATOR FITTING LOCATED AT BL 15.25 HA
- [SDR SWI2023F00322](https://openairdocs.org/sdr/SWI2023F00322.md): Unknown · corroded · Jul 22, 2023 · N978SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT HAND PRESSURE FLOOR SILL HAS CORROSION IN MULTIPLE AREAS BETWEEN FS409+128 TO FS559.00. (MARKED) (C-CHECK RO 9/6/2023) REPAIRED LEFT HAND PRESSURE FLOOR SILL BETWEEN FS409+128 TO FS559.00 BY COMPLYING WITH ALL STEPS OF REO 601R-53-41-666 REV -C DAT
- [SDR SWI202309008321](https://openairdocs.org/sdr/SWI202309008321.md): Unknown · corroded · Jul 22, 2023 · N978SW · Cndair CL6002B19 · Empennage Structure
  > UPON REMOVAL ON JOB HN103215 CAMP #26917265, FOUND L/H ELEVATOR L/E HINGE FITTING ASSY P/N 600-24043-1 AT ES16.52 TO HAVE PITTING CORROSION IN BEARING BORES OF BOTH FITTING HINGE HALVES. REPLACE HINGE FITTING ASSY P/N 600-24043-1. (C-CHECK RO 9/6/2023)
- [SDR SWI20230908320](https://openairdocs.org/sdr/SWI20230908320.md): Unknown · cracked · Jul 22, 2023 · N978SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND 2 CRACKED AREAS AT LBL 12 AND 1 CRACKED AREA AT RBL 12.0 ON FS 280 FLOOR SUPPORT BEAM. (C-CHECK RO 9/6/2023) REPAIRED BULKHEAD WEB FS280 FLOOR SUPPORT BEAM BY COMPLYING WITH ALL STEPS OF REO 601R-53-11-926 REV -B DATED 2006/05/10. NO DEFECTS NOTED
- [SDR SWI2023F00320](https://openairdocs.org/sdr/SWI2023F00320.md): Unknown · cracked · Jul 22, 2023 · N978SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FOUND 2 CRACKED AREAS AT LBL 12 AND 1 CRACKED AREA AT RBL 12.0 ON FS 280 FLOOR SUPPORT BEAM. (C-CHECK RO 9/6/2023) REPAIRED BULKHEAD WEB FS280 FLOOR SUPPORT BEAM BY COMPLYING WITH ALL STEPS OF REO 601R-53-11-926 REV -B DATED 2006/05/10. NO DEFECTS NOTED
- [SDR SWI2023F0000316](https://openairdocs.org/sdr/SWI2023F0000316.md): Unknown · corroded · Jul 21, 2023 · N978SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH FLOOR SILL AFT OF FS 449.85 HAS CHIPPED PAINT AND LIGHT CORROSSION AT FASTNER HOLE MARKED (C-CHECK RO 9/6/2023) REPAIRED LH FLOOR SILL AFT OF FS449.85 BY COMPLYING WITH REO 601R-53-41-666 REV -C DATED 2012-11-06. COMPLIED WITH SKYWEST TASK CARD 51-90
- [SDR SWI2023F00315](https://openairdocs.org/sdr/SWI2023F00315.md): Unknown · corroded · Jul 21, 2023 · N978SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS574.0 STGR24R-STGR27 HAS AREAS OF CORROSION (C-CHECK RO 9/6/2023) INSTALLED NEW FRAME SECTOR AT FS574.00 PER CRJ200 SRM 51-42-06 AND 51-42-21 AND 51-42-22.DWG# 601R35031 REV-AG AND DWG# 601R35226 REV-P AND DWG# 601R36024 REV-N.COMPLIED WITH A
- [SDR SWIA202309080720](https://openairdocs.org/sdr/SWIA202309080720.md): Unknown · cracked · Jul 20, 2023 · N978SW · Cndair CL6002B19 · Fuselage Structure (General)
  > PRESSURE FLOOR FS481.00 INBOARD AFT ATTACH ANGLE ON BRACKET BETWEEN RBL27 & RBL43 IS CRACKED. (MARKED) (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED NEW ATTACH ANGLE BRACKET REF CRJ200 SRM 51-42-21 AND REO 601R-53-41-059 REV-C DATED: 2020-03-11 USED FOR
- [SDR SWIA20230908719](https://openairdocs.org/sdr/SWIA20230908719.md): Unknown · cracked · Jul 19, 2023 · N978SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING TRAILING EDGE UNDER OUTBOARD GROUND SPOILER WS137.0 CRACKED (C-CHECK RO 9/6/2023) REPAIRED CRACK TO TRAILING EDGE RIB AT WS130.10 RHS PER R.E.O. 601R-57-51-1020 REV. -- DATED 2023-07-21. COMPLIED WITH ALL APPLICABLE STEPS SEE CONTINUE CARD FO
- [SDR SWIA202309080718](https://openairdocs.org/sdr/SWIA202309080718.md): Unknown · gouged · Jul 18, 2023 · N978SW · Cndair CL6002B19 · Empennage Structure
  > RH ELEVATOR INBD HINGE GOUGED (C-CHECK RO 9/6/2023) REMOVED GOUGE FROM RH ELEVATOR INBD HINGE, WITHIN LIMITS. RECEIVED AND COMPLIED WITH MHIRJ REO 601R-55-11-748 REV --A, DATED 2023-08-18. SEE CONTINUATION FOR FURTHER DETAILS. COMPLIED WITH 51-900-1003
- [SDR SWIA20230908715](https://openairdocs.org/sdr/SWIA20230908715.md): Unknown · corroded · Jul 15, 2023 · N978SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL AT DD7 BETWEEN FS 320.10 AND FS329.50 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD7 REF CRJ200 SRM 51-42-06 AND DWG 601R31702 REV N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD. S
- [SDR SWIA20230908712](https://openairdocs.org/sdr/SWIA20230908712.md): Unknown · gouged · Jul 12, 2023 · N978SW · Cndair CL6002B19 · Emergency Exits
  > *LH EMER DOOR, BOTH THE FWD AND AFT BOTTOM DOOR HOOKS (ON DOOR) ARE GOUGED AND AREAS OF ROLLED METAL (MARKED) (C-CHECK RO 9/6/2023) REPAIRED DAMAGE AT LH OVERWING EMERGENCY EXIT DOOR FWD AND AFT LOWER FITTINGS PER REO 601R-52-21-147 REV -- DATE 2023-07
- [SDR SWIA2023090800708](https://openairdocs.org/sdr/SWIA2023090800708.md): Unknown · cracked · Jul 8, 2023 · N978SW · Cndair CL6002B19 · Fuselage Main, Frame
  > LEFT SIDE FS235.00 UPPER FRAME SECTOR IS CRACKED. (MARKED) SRM 53-11-15 (C-CHECK RO 9/6/2023) REPLACED LH SIDE FS235.00 UPPER FRAME SECTOR/ANGLE P/N: 601R34032-21, NEW CLIP P/N: 601R34032-31 AND NEW ATTACHMENT ANGLE P/N:601R34032-19. REF CRJ200 SRM 51-4
- [SDR SWI2023F00306](https://openairdocs.org/sdr/SWI2023F00306.md): Unknown · damaged · Jul 7, 2023 · N978SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN JUST AFT OF THE PASSENGER DOOR HINGE HAS DAMAGE. (MARKED) (C-CHECK RO 9/6/2023) REPAIRED FUSELAGE SKIN JUST AFT OF THE PASSENGER DOOR HINGE REF REO 601R-53-21-3643 REV -- DATED 2023-08-07. COMPLIED WITH 51-900-1003-SKY AND LEAK CHECK GOO
- [SDR SWIA20230707](https://openairdocs.org/sdr/SWIA20230707.md): Unknown · corroded · Jul 7, 2023 · N978SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DATUM 1 INTERCOSTAL BETWEEN APPROX FS320 - FS338 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED NEWLY DRILLED INTERCOSTAL D1 BETWEEN FS320 - FS338 REF CRJ200 SRM 51-42-06 REF CRJ200 SRM 51-42-21 AND DWG 601R31702 REV-N. COMPLIED WITH 51-900-1
- [SDR SWI2023F0000317](https://openairdocs.org/sdr/SWI2023F0000317.md): Unknown · bent · Jul 6, 2023 · N978SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FORWARD TRACK SUPPORT LOWER CHANNEL IS BENT. (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED THE NEW CHANNEL AT THE AFT CARGO DOOR FORWARD TRACK SUPPORT THE LOWER CHANNEL PART # 601R35050-119 REF. CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21 AND
- [SDR SWI2023F00318](https://openairdocs.org/sdr/SWI2023F00318.md): Unknown · bent · Jul 6, 2023 · N978SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FORWARD TRACK SUPPORT UPPER CHANNEL IS BENT. (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED A NEW REPLACEMENT CARGO DOOR FORWARD TRACK SUPPORT UPPER CHANNEL (PART#601R35050-21) REF CRJ 200 SRM 51-42-06 AND DRAWING 601R35050 REV AC. COMPLIED WITH
- [SDR SWI2023F00317](https://openairdocs.org/sdr/SWI2023F00317.md): Unknown · bent · Jul 6, 2023 · N978SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FORWARD TRACK SUPPORT LOWER CHANNEL IS BENT. (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED THE NEW CHANNEL AT THE AFT CARGO DOOR FORWARD TRACK SUPPORT THE LOWER CHANNEL PART # 601R35050-119 REF. CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21 AND
- [SDR SWI2023F00313](https://openairdocs.org/sdr/SWI2023F00313.md): Unknown · corroded · Jul 5, 2023 · N978SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DATUM 2 INTERCOSTAL BETWEEN APPROX FS338 - FS347 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND REPLACED INTERCOSTAL D2 BETWEEN FS338 - FS347 REF CRJ200 SRM 51-42-06, AND DWG 601R31702 REV-N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOODS. SE
- [SDR SWI2023F00312](https://openairdocs.org/sdr/SWI2023F00312.md): Unknown · corroded · Jul 5, 2023 · N978SW · Cndair CL6002B19 · Fuselage Structure (General)
  > DATUM 4 INTERCOSTAL BETWEEN APPROX FS320 - FS338 HAS CORROSION (C-CHECK RO 9/6/2023) INSTALLED NEWLY DRILLED INTERCOSTAL D4 BETWEEN FS320 - FS338 REF CRJ200 SRM 51-42-06 REF CRJ200 SRM 51-42-21 AND DWG 601R31702 REV-N. COMPLIED WITH 51-900-1003-SKY AND
- [SDR SWI2023F00311](https://openairdocs.org/sdr/SWI2023F00311.md): Unknown · corroded · Jul 5, 2023 · N978SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DATUM 3 INTERCOSTAL BETWEEN APPROX FS320 - FS338 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED NEW PAX DOOR DATUM 3 INTERCOSTAL BETWEEN FS 320 -FS338 REF CRJ-200-SRM 51-42-06, CRJ-200-SRM 51-42-21 AND DRAWING 601R31702 REV N. COMPLIEDWITH 5
- [SDR SWI2023F00310](https://openairdocs.org/sdr/SWI2023F00310.md): Unknown · corroded · Jul 5, 2023 · N978SW · Cndair CL6002B19 · Fuselage Main, Frame
  > AFT FORMER @ APPROX. FS347 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND REPLACED AFT FORMER @ FS347 REF CRJ200 SRM 51-42-06 REF CRJ200 SRM 51-42-21 DWG 601R31702 REV-N. NO DEFECTS NOTED. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (STRUCTURAL MAJ
- [SDR SWIA20230705](https://openairdocs.org/sdr/SWIA20230705.md): Unknown · corroded · Jul 5, 2023 · N978SW · Cndair CL6002B19 · Fuselage Structure (General)
  > DATUM 5 INTERCOSTAL BETWEEN APPROX FS338 - FS347 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND REPLACED INTERCOSTAL D5 BETWEEN FS338 - FS347 REF CRJ200 SRM 51-42-06, DWG 601R31702 REV-N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD. SEE CONT
- [SDR SWI2023F00309](https://openairdocs.org/sdr/SWI2023F00309.md): Unknown · corroded · Jul 5, 2023 · N978SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DATUM 4 INTERCOSTAL BETWEEN APPROX FS338 - FS347 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND REPLACED INTERCOSTAL D4 BETWEEN FS338 - FS347 REF CRJ200 SRM 51-42-06 DWG 601R31702 REV-N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD. SEE CONTI
- [SDR SWI2023F00308](https://openairdocs.org/sdr/SWI2023F00308.md): Unknown · corroded · Jul 5, 2023 · N978SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DATUM 1 INTERCOSTAL BETWEEN APPROX FS338 - FS347 HAS CORROSION (C-CHECK RO 9/6/2023) REPLACED INTERCOSTAL D1 BETWEEN FS338 - FS347 REF CRJ200 SRM 51-42-06. DWG 601R31702 REV-N. PRESSURE LEAK CHECK GOOD. SEE CONTINUE CARD FOR ALL WORK PERFORMED. COMPLIE
- [SDR SWI2023F00307](https://openairdocs.org/sdr/SWI2023F00307.md): Unknown · corroded · Jul 5, 2023 · N978SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FWD FORMER @ APPROX. FS311 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED NEW FWD PASSENGER DOOR FORMER REF CRJ-200-SRM 51-42-06, CRJ-200-SRM 51-42-21, AND DRAWING 601R31702 REV N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD. SE
- [SDR SWIA202309080701](https://openairdocs.org/sdr/SWIA202309080701.md): Unknown · worn · Jul 1, 2023 · N978SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR PIANO HINGE ON AIRCRAFT SIDE HAS WORN HINGE PIN HOLES (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED NEW HINGE (FUSELAGE SIDE) REF. CRJ 200 SRM 53-21-23, DWG 601R31527 REV AM AND REO 601R-53-21-656 REV. A DATED 2017/03/06. LEAK CHECK GOOD. COMPL
- [SDR SWIA20230908630](https://openairdocs.org/sdr/SWIA20230908630.md): Unknown · chafed · Jun 30, 2023 · N978SW · Cndair CL6002B19 · Ailerons
  > LEFT INBOARD FLAP VANE INBOARD LEADING EDGE PANEL IS CHAFED. (C-CHECK RO 9/6/2023) EVALUATED FOUND OUT OF LIMITS, REMOVED AND INSTALLED NEW LEFT INBOARD FLAP VANE INBOARD LEADING EDGE PANEL REF CRJ200 SRM 51-42-13 & DWG 601R14303 REV J. COMPLIED WITH S
- [SDR SWIA20230908628](https://openairdocs.org/sdr/SWIA20230908628.md): Unknown · corroded · Jun 28, 2023 · N978SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL MID DD6 IS CORRODED(MARKED). (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED NEWLY DRILLED INTERCOSTAL D6 BETWEEN FS320 - FS338 CRJ200 SRM 51-42-06 CRJ200 SRM 51-42-21 AND DWG 601R31702 REV-N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE
- [SDR SWI2023F00323](https://openairdocs.org/sdr/SWI2023F00323.md): Unknown · corroded · Jun 28, 2023 · N978SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL MID DD2 IS CORRODED(MARKED). (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED NEWLY DRILLED INTERCOSTAL D2 BETWEEN FS320 - FS338 REF CRJ200 SRM 51-42-06 REF CRJ200 SRM 51-42-21 AND DWG 601R31702 REV-N. COMPLIED WITH 51-900-1003-SKY AND P
- [SDR SWIA2023090800627](https://openairdocs.org/sdr/SWIA2023090800627.md): Unknown · worn · Jun 27, 2023 · N978SW · Cndair CL6002B19 · Wing Structure
  > RH WING AILERON HAS WEAR ON LOWER LEADING EDGE SHROUDS. MARKED. (C-CHECK RO 9/6/2023) REPLACED SHROUD AT R/H WING AILERON LWR I/B L/E WITH NEW FASTENERS REF. CRJ200 SRM 51-42-21 & BOMBARDIER DWG. CC670-1300 REV. -D AND RESTORED FINISH ON FASTENERS REF.
- [SDR SWIA2023090800626](https://openairdocs.org/sdr/SWIA2023090800626.md): Unknown · dented · Jun 26, 2023 · N978SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD WING FLAP LOWER SKIN DENTED INBD SIDE MARKED. (C-CHECK RO 9/6/2023) REPAIRED LEFT INBD WING LOWER SKIN (LH INBD FLAP LOWER SKIN). REF CRJ200 SRM 57-52-00 REPAIR #3. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (STRUCTURAL MAJOR REPAIR).
- [SDR SWI2023F00314](https://openairdocs.org/sdr/SWI2023F00314.md): Unknown · gouged · Jun 26, 2023 · N978SW · Cndair CL6002B19 · Wing Structure
  > LH WING AILERON CENTER HINGE (WING SIDE) HAS GOUGES. MARKED. (C-CHECK RO 9/6/2023) REPAIRED GOUGE ON LH WING AILERON (WING SIDE) CENTER HINGE TO A SMOOTH CONTOUR REF CRJ200 SRM 51-12-00. AND REO 601R-57-51-1018 REV--, DATED 2023-07-19 ALL STEPS COMPLIED
- [SDR SWIA20230908623](https://openairdocs.org/sdr/SWIA20230908623.md): Unknown · dented · Jun 23, 2023 · N978SW · Cndair CL6002B19 · Fuselage Structure (General)
  > BETWEEN FS409+48 AND FS409+64 BETWEEN STR 23L AND 24L. BLEND PERFORMED PER REO 601R-53-00-115 REV A. LOOKS LIKE A SMALL DENT. 2 DENTS LOCATED APPROXIMATELY BETWEEN FS409+16 AND FS409+48 AND BETWEEN STRINGERS 23L AND 24L. 2EA INDICATIONS OF DENTING DETERMINED T
- [SDR SWIA202265988](https://openairdocs.org/sdr/SWIA202265988.md): None · dented · Jul 10, 2022 · N978SW · Cndair CL6002B19 · Fuselage Structure (General)
  > DENT ON FUSELAGE SKIN FWD OF FS574.00 BETWEEN STGR1L AND 2L. (HAS BEEN DETEMINED TO BE A MAJOR REPAIR.) (FILED CLOSED)PERFORMED A DOUBLER REPAIR INSTALLED ON FUSELAGE SKIN FWD OF FS574.00 BETWEEN STGR1L AND 2L IN REFERENCE TO CRJ200 SRM 53-00-31, FASTENERS I

Next page: https://openairdocs.org/aircraft/N978SW/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 = 'N978SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N978SW/reports

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