# Service difficulty reports: N926SW

A list on [N926SW](https://openairdocs.org/aircraft/N926SW.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 · 206 reports

- [SDR SWIA2026060876846](https://openairdocs.org/sdr/SWIA2026060876846.md): Floorbeam · cracked · Jun 8, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > DURING INSTALL, FOUND RBL 27 FLOORBEAM TO BE CRACKED ON LOWER INBOARD EDGE AT FS 615. INSTALLED A NEW FABRICATED BEAM IAW SNIEO 601R352289 S01, SRM 51-40-11, 51-42-02, 51-42-06, 51-42-21 AND 51-41-04. COMPLETED SKYCARD 51-900-1003-SKY. MAJOR REPAIR
- [SDR SWIA2026042876856](https://openairdocs.org/sdr/SWIA2026042876856.md): Web · cracked · Apr 28, 2026 · N926SW · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > INDICATION FOUND ON ENGINE BEAM UPPER WEB, UNDER LBL 31.41, ANGLE BETWEEN FWD 2 FASTNERS AT 100% FSH, FAILED NDT. REPAIRED THE ENGINE BEAM UPPER WEB UNDER LBL 31.41 ANGLE BTWN FWD TWO FASTENERS IAW REO 601R-53-61-8536, REV -, AND SKY CARD 51-900-1003-SKY.
- [SDR SWIA2026042576863](https://openairdocs.org/sdr/SWIA2026042576863.md): Frame · corroded · Apr 25, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 333 FRAME CORRODED ON THE FWD FACE AND LOWER FLANGE BTWN STR 23R & STR 22R. R & R FRAME SEGMENT AT BS 333 FROM STR 18R TO STR 23R IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026042576855](https://openairdocs.org/sdr/SWIA2026042576855.md): Frame · corroded · Apr 25, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 310 FRAME CORRODED ON THE AFT FACE BETWEEN STR 22R & 23R. R & R THE FRAME IAW SRM 51-42-06, 51-42-21, AND SKY CARD 51-900-1003-SKY.
- [SDR SWIA2026042576848](https://openairdocs.org/sdr/SWIA2026042576848.md): Frame · corroded · Apr 25, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 319 FRAME CORRODED ON THE FWD FACE BTWN STR 23R AND STR 22R. R & R FRAME SPLICE COMMON TO FRAME BS 319.00, S23R - S22R IAW SRM 51-42-06 AND SRM 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026042376865](https://openairdocs.org/sdr/SWIA2026042376865.md): Frame · cracked · Apr 23, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 235, RT UPPER FRAME SECTOR IS CRACKED WHERE IT ATTACHES TO THE RT WINDOW LOWER SILL. REPAIRED THE RT UPPER FRAME SECTOR IAW REO 601R-53-11-4073, REV - AND SKY CARD 51-900-1003-SKY.
- [SDR SWIA2026042376859](https://openairdocs.org/sdr/SWIA2026042376859.md): Frame · cracked · Apr 23, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 235 LT UPPER FRAME SECTOR IS CRACKED WHERE IT ATTACHES TO THE LT WINDOW LOWER SILL. REPAIRED THE LT UPPER FRAME SECTOR CRACK WHERE IT ATTACHED TO THE LH WINDOW LOWER SILL IAW REO 601R-53-11-4072, REV -, & SKY CARD 51-900-1003-SKY.
- [SDR SWIA2026042276864](https://openairdocs.org/sdr/SWIA2026042276864.md): Floorbeam · corroded · Apr 22, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CARGO FLOORBEAM AT RBL 27, BS 619 HAD CORROSION DAMAGE. CARGO FLOORBEAM AT LBL 27, BS 619. REPLACED IAW SRM 51-42-22, 51-41-02, 51-25-00, 51-42-21, 51-40-11, & 51-42-06, REV.39B, REO 601R-53-61-3778, REV B, COMPLETED SKYCARD 51-900-1003-SKY.
- [SDR SWIA2026042076866](https://openairdocs.org/sdr/SWIA2026042076866.md): Pressure Deck · corroded · Apr 20, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, Structure
  > LEFT CABIN, PRESSURE FLOOR SKIN CORRODED AT ONE LOCATION BTWN BS 473.15, & FS 461. REPAIRED THE LT PRESSURE FLOOR SKIN IAW REO 601R-53-41-666, REV C. COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026042076862](https://openairdocs.org/sdr/SWIA2026042076862.md): Pressure Deck · corroded · Apr 20, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, Structure
  > LEFT CABIN PRESSURE DECK CORRODED AT TWO LOCATIONS BTWN BS 449.85 & 461. REMOVED CORROSION ON LT CABIN PRESSURE DECK IAW REO 601R-53-41-666, REV-C, STEP 1.2. & 51-900-1003-SKY ORIGINAL THICKNESS 0.055" REMAINING THICKNESS OF LOWEST DEPTH 0.047" ALLOWABLE BLEN
- [SDR SWIA2026042076861](https://openairdocs.org/sdr/SWIA2026042076861.md): Pressure Deck · corroded · Apr 20, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, Structure
  > RIGHT CABIN PRESSURE DECK CORRODED AT ONE LOCATION BTWN BS 484 & 499. REMOVED CORROSION ON RT PRESSURE DECK IAW REO 601R-53-41-666, REV C. & SKYCARD 51-900-1003-SKY ORIGINAL THICKNESS 0.055" REMAINING THICKNESS OF LOWEST DEPTH 0.047" ALLOWABLE BLEND DEPTH 0.0
- [SDR SWIA2026042076853](https://openairdocs.org/sdr/SWIA2026042076853.md): Pressure Deck · corroded · Apr 20, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, Structure
  > RIGHT PRESSURE DECK CORRODED AT ONE LOCATION, BS 449.85. REPAIRED RT PRESSURE DECK IAW REO 601R-53-41-666, REV-C. COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026042076851](https://openairdocs.org/sdr/SWIA2026042076851.md): Pressure Deck · corroded · Apr 20, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, Structure
  > LEFT CABIN PRESSURE DECK CORRODED AT TWO LOCATIONS, BS 424. REPAIRED LT CABIN PRESSURE DECK AT BS 424 IAW REO 601R-53-41-666, REV C. COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026042076849](https://openairdocs.org/sdr/SWIA2026042076849.md): Pressure Deck · corroded · Apr 20, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, Structure
  > LEFT CABIN, PRESSURE DECK CORRODED AT ONE LOCATION BETWEEN BS 424 & 439. REMOVED CORROSION ON THE PRESSURE DECK IAW REO 601R-53-41-666, REV C, STEP 1.2. & TASK CARD 51-900-1003-SKY ORIGINAL THICKNESS 0.055" REMAINING THICKNESS OF LOWEST DEPTH 0.042" ALLOWABLE
- [SDR SWIA2026041776852](https://openairdocs.org/sdr/SWIA2026041776852.md): Frame · corroded · Apr 17, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 333 FRAME CORRODED BTWN STR 20L TO STR 21L. R & R BS 333 FRAME, STR 20L - 23L IAW SRM 51-42-06, AND SRM 51-42-21, COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026041776850](https://openairdocs.org/sdr/SWIA2026041776850.md): Floor Support · corroded · Apr 17, 2026 · N926SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 9 FLOOR SUPPORT HAS MULTIPLE AREA OF CORROSION FROM BS 409+128 TO 559. PERFORMED A MAJOR REPAIR BY REPLACING THE RT RBL 9 FLOOR SUPPORT FROM BS 409+128 - 559 IAW REO 601R-53-00-005 IAW 601R-53-51-3428. COMPLETED STRUCTURAL MAJOR REPAIR TASK CARD 51-900-10
- [SDR SWIA2026041776847](https://openairdocs.org/sdr/SWIA2026041776847.md): Floor Support · corroded · Apr 17, 2026 · N926SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR SUPORT HAD MULTIPLE AREAS OF CORROSION ON INBD AND OTBD FLOOR SUPPORT BS 409+128 - 559. PERFORMED A MAJOR REPAIR BY REPLACING THE UPPER CAP OF THE LBL 9 FLOOR SUPPORT BTWN BS 409+128 & 559 IAW REO 601R-53-41-3427, REV-. COMPLETED TASK CARD 51-900-
- [SDR SWIA2026041776845](https://openairdocs.org/sdr/SWIA2026041776845.md): Frame · corroded · Apr 17, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 319 FRAME CORRODED BTWN STR 20L TO STR 21L. R & R THE FRAME SECTOR AT BS 319 BTWN STR 18L & 21L IAW SRM 51-42-06, & 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026041376860](https://openairdocs.org/sdr/SWIA2026041376860.md): Skin · chafed · Apr 13, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CENTER SECTION LOWER PLANK IS CHAFED AT LBL 45 AND RBL 45 FROM CONTACT WITH FWD FUSELAGE FAIRING. REPAIRED THE LOWER PLANK, LBL 45 & RBL 45 IAW REO 601R-57-21-880, REV-D, COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026041276857](https://openairdocs.org/sdr/SWIA2026041276857.md): Cap · cracked · Apr 12, 2026 · N926SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT WING WHEEL WELL, FIRST BATT RIB IN MLG CUTOUT CRACKED AT TWO LOCATIONS. REMOVED AND INSTALLED NEW SERVICEABLE CAP ON R/H WING WHEEL WELL, FIRST BATT RIB IN L/G CUTOUT IAW CRJ 200 SRM 51-42-21.
- [SDR SWIA2026041276854](https://openairdocs.org/sdr/SWIA2026041276854.md): Channel · cracked · Apr 12, 2026 · N926SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT MLG WHEEL WELL, SECOND BATT RIB OTBD, BRACKET CRACKED ON FWD END OF RIB. PERFORMED A MAJOR REPAIR BY REPLACING 2ND BATT RIB CHANNEL, AND ATTACHING ANGLES, OTBD IN LT MLG WHEEL WELL. IAW SRM 51-40-11, 51-42-21, & 51-42-06 COMPLETED SKYWEST RII TASK CA
- [SDR SWIA2026041176858](https://openairdocs.org/sdr/SWIA2026041176858.md): Skin · chafed · Apr 11, 2026 · N926SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT LOWER WING PLANK TRAILING EDGE IS CHAFED AT APPROX. BL45. REPAIRED TRAILING EDGE OF LT LOWER WING PLANK IAW REO 601R-57-21-880, REV-D, COMPLETED SKYCARD 51-900-1003-SKY. MAJOR REPAIR.
- [SDR SWIA202504300026](https://openairdocs.org/sdr/SWIA202504300026.md): Switch · faulted · Apr 26, 2025 · N926SW · Cndair CL6002B19 · Overheat Detection
  > ANTI ICE DUCT WARNING. OVERHEAD SHOWED WING DUCT FAILED. RAN QRH MESSAGE WENT AWAY. (FLIGHT 4745 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30045347 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE CP 30045723 FOR THERMAL SWITCH HEALTH CHECK. S
- [SDR SWIA202504280026](https://openairdocs.org/sdr/SWIA202504280026.md): Warning Message · intermittent · Apr 26, 2025 · N926SW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > ANTI ICE DUCT WARNING. OVERHEAD SHOWED WING DUCT FAILED. RAN QRH MESSAGE WENT AWAY. (FLIGHT 4745 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWI2025F00153](https://openairdocs.org/sdr/SWI2025F00153.md): Smoke Warning · false activation · Feb 14, 2025 · N926SW · Cndair CL6002B19 · Smoke Detection
  > SMOKE CARGO WARNING MESSAGE DURING ROLLOUT AFTER LANDING. RAN QRC & QRH, MESSAGE DID NOT GO OUT. FIREX BOTTLES WERE BLOWN. (FLIGHT 5352 - FILED CLOSED) PLEASE REFERENCE AML 1537776 FOR REPLACEMENT OF CARGO SMOKE DETECTOR #1. PLEASE REFERENCE AML 153
- [SDR SWIA2024072300022](https://openairdocs.org/sdr/SWIA2024072300022.md): Target · out of adjust · Jul 22, 2024 · N926SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE ON CLIMB OUT. R MAIN LNG DID NOT COME UP. RAN QRH AND GEAR EXTENDED WITH THREE GREEN. RETURNED TO FIELD. (FLIGHT 4658 - FILED CLOSED) PLEASE REFERENCE AML 1394917 PER FIM 32-60-07, INTERROGATED PSEU. FOUND S18 UNREASONABLE, FAR. CHECKED RT MLG U
- [SDR SWIA2023011367099](https://openairdocs.org/sdr/SWIA2023011367099.md): Rib · cracked · Dec 23, 2022 · N926SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RH WING REAR SPAR CHANNEL/ RIB 601R10203-28 IS CRACKED AT THE TOP AND AFT END. REPAIRED RH WING REAR SPAR CHANNEL/ RIB PER REO 601R-57-51-046 REV -B DATED 2002-02-28, REPAIR 2.
- [SDR SWIA2023011367098](https://openairdocs.org/sdr/SWIA2023011367098.md): Floorbeam · damaged · Dec 18, 2022 · N926SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RIVET FOR NUTPLATE PULLED THROUGH FLOORBEAM AT OBD SIDE OF BEAM AT RBL 27.0, FS 464.00. REPAIRED NOTED NUT PLATE RIVET HOLES THAT PULLED THROUGH FLOORBEAM AT RBL 27.0, FS 464.00 REF REO 601R-53-41-3111 REV -, STEPS 1-15.
- [SDR SWIA2023011367097](https://openairdocs.org/sdr/SWIA2023011367097.md): Floorbeam · cracked · Dec 12, 2022 · N926SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FOUND BS 280 FLOORBEAM WEB TO BE CRACKED AT LBL 9. REPAIRED THE FLOORBEAM ANGLE AND FLOORBEAM BETWEEN LBL 20.75 TO RBL 20.75 IAW REO 601R-53-11-926 REV. B. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2023011367106](https://openairdocs.org/sdr/SWIA2023011367106.md): Seat Track · corroded · Dec 7, 2022 · N926SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION NOTED ON FLOOR SEAT TACK AT LBL 9 BETWEEN BS 364-394. REMOVED AND INSTALLED A NEW SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR SWIA2023011367105](https://openairdocs.org/sdr/SWIA2023011367105.md): Seat Track · corroded · Dec 7, 2022 · N926SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION NOTED ON THE FLOOR SEAT TACK AT RBL 9 BETWEEN BS 364-394. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-01-11-400-802.
- [SDR SWIA2023011367100](https://openairdocs.org/sdr/SWIA2023011367100.md): Floorbeam · cracked · Dec 7, 2022 · N926SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > SUSPECTED CRACKS AT 280 FLOORBEAM AT RBL9 AND LBL9. REPLACED NEW CLIPS AND ANGLES AT BS 280 FLOORBEAM AT RBL 9.0 AND LBL 9.0 ON CAMP 25925155, JOB 27678791, OP 330.
- [SDR SWIA2023011367102](https://openairdocs.org/sdr/SWIA2023011367102.md): Seat Track · corroded · Dec 6, 2022 · N926SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK AT RBL 9, BS 409 + 126 - 559 + 4 WAS CORRODED, DENTED, GOUGED, AND CHAFED AT MULTIPLE PLACES ALONG LENGTH OF TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-01-11-400-802.
- [SDR SWIA2023011367101](https://openairdocs.org/sdr/SWIA2023011367101.md): Seat Track · corroded · Dec 6, 2022 · N926SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK AT LBL 9, BS. 409 + 126 - 559 + 4 WAS CORRODED, DENTED, GOUGEED, AND CHAFED AT MULTIPLE PLACES ALONG LENGTH OF TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-01-11-400-802,
- [SDR SWIA2023011367096](https://openairdocs.org/sdr/SWIA2023011367096.md): Skin · corroded · Dec 6, 2022 · N926SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ADF ANTENNA CUT-OUT. CORROSION ON UPPER FUSELAGE BS 409.85-409.88, STRINGER 0 PLUS 2, LEFT DOWN TO STRINGER 0. REMOVED CORROSION ON UPPER FUSELAGE IAW SRM 51-21-06. AND REO 601R-53-31-1255 REV--.
- [SDR SWIA2023011367104](https://openairdocs.org/sdr/SWIA2023011367104.md): Seat Track · corroded · Dec 3, 2022 · N926SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > MULTIPLE SPOTS OF CORROSION, SCRATCHES AND GOUGES NOTED ON THE LT SIDE SEAT TRACK BETWEEN BS 544-559+80. REMOVED DAMAGED SEAT TRACK IAW AMM 53-01-11-000-802, INSTALLED A REPLACEMENT SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR SWIA2023011367095](https://openairdocs.org/sdr/SWIA2023011367095.md): Cleat · corroded · Dec 3, 2022 · N926SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR CLEAT COMMON TO FS320.163 FRAME AND LWR MID CHANNEL CORRODED. REMOVED AND REPLACED PAX DOOR CLEAT COMMON TO FS320.163 FORMER AND LWR MID CHANNEL IAW DWG 601R31702 REV. N AND SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY.
- [SDR SWIA2023011367094](https://openairdocs.org/sdr/SWIA2023011367094.md): Cleat · corroded · Dec 3, 2022 · N926SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR CLEAT COMMON TO BS 338.963 FORMER AND LWR MID CHANNEL CORRODED. REMOVED AND REPLACED THE PAX DOOR CLEAT IAW DWG 601R31702 REV. N, AND SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY.
- [SDR SWIA2023011367093](https://openairdocs.org/sdr/SWIA2023011367093.md): Frame · dented · Dec 3, 2022 · N926SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR BS 327.763 FRAME WAS DENTED WITH A POSSIBLE CRACK ON UPPER FLANGE. REMOVED AND INSTALLED A NEW PAX DOOR FRAME IAW DWG 601R31702 REV N, SRM 51-42-06, AND SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. OPS/LEAK CHECK FOUND GOOD
- [SDR SWIA2023011367092](https://openairdocs.org/sdr/SWIA2023011367092.md): Skin · corroded · Nov 26, 2022 · N926SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING PLANK UNDER FUEL ACCESS PANEL 510AB WAS CHAFED AND CORRODED. BLENDED DAMAGE IAW REO 601R-57-21-030 REV -L. MATERIAL LOSS IS FOUND TO BE WITHIN ALLOWABLE LIMITS. ALL CHECKED GOOD.
- [SDR SWIA2023011367091](https://openairdocs.org/sdr/SWIA2023011367091.md): Skin · corroded · Nov 26, 2022 · N926SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING PLANK UNDER FUEL ACCESS PANEL 550HB WAS CHAFED AND CORRODED. REMOVED CORROSION IAW REO 601R-57-21-030 REV-L. FOUND TO BE WITH IN LIMITS. COMPLIED WITH ALL STEPS OF REO 601R-57-21-030 REV-L. NO LEAKS NOTED. COMPLIED WITH SKY CARD 51-900-1003.
- [SDR SWIA2023011367090](https://openairdocs.org/sdr/SWIA2023011367090.md): Skin · corroded · Nov 25, 2022 · N926SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING PLANK UNDER FUEL ACCESS PANEL 650HB WAS CHAFED AND CORROSION. BLENDED DAMAGE FROM RT WING PLANK FUEL CELL ACCESS HOLE FOR PANEL 650HB IAW REO 601R-57-21-030, REV L. MATERIAL LOSS IS FOUND TO BE WITHIN ALLOWABLE LIMITS IAW REO 601R-57-21-3666 REV
- [SDR SWIA2023011367089](https://openairdocs.org/sdr/SWIA2023011367089.md): Door Sill · corroded · Nov 21, 2022 · N926SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR CUT-OUT, LOWER SILL HAS MULTIPLE AREA'S OF CORROSION. REPAIRED SERVICE DOOR CUT-OUT, LOWER SILL F CORROSION REF SRM 51-42-21 REV 39, SRM 51-42-36 REV 39, SRM 51-42-10, REV 39,, DWG 601R38303 REV AR. OPS CHECKED GOOD. C/W 51-900-1003-SKY.
- [SDR SWIA2023011367103](https://openairdocs.org/sdr/SWIA2023011367103.md): Nut · corroded · Nov 19, 2022 · N926SW · Cndair CL6002B19 · Spoilers
  > HARDWARE FOR RT FLIGHT SPOILER HINGE FITTINGS APPEARS TO BE CORRODED. INSTALLED SERVICEABLE NUTS AND WASHERS ONLY ON THE RT OTBD FLIGHT SPOILER CENTER HINGE FITTINGS IAW AMM 27-64-01-400-801, STEP 2B,(3D-3G), 2B, (4D, 4F-4H) AND 2C(3).
- [SDR SWIA2023011367088](https://openairdocs.org/sdr/SWIA2023011367088.md): Skin · dented · Nov 18, 2022 · N926SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LEFT SIDE FUSELAGE THERE IS DENT AT UPPER AFT EMPANNAGE APPROX AFT OF FS 736.0 AND JUST FWD OF FS 755.0 AT STR7. REPAIRED LEFT SIDE FUSELAGE DENT AT UPPER AFT EMPANNAGE APPROX AFT OF FS 736.0 AND JUST FWD OF FS 755.0 AT STR7 REF REO 601R-53-71-219 REV-- D
- [SDR SWIA2023011367087](https://openairdocs.org/sdr/SWIA2023011367087.md): Fitting · cracked · Nov 17, 2022 · N926SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FITTING UPPER FWD IN DOOR STOP LOCATION IS CRACKED. REMOVED AND INSTALLED NEW CARGO DOOR FITTING UPPER FWD IN DOOR STOP REF DWG # CC670-38702 REV -C, SRM 51-42-13, SRM 51-41-02. COMPLIED WITH 51-900-1003-SKY.
- [SDR SWIA2023011367086](https://openairdocs.org/sdr/SWIA2023011367086.md): Receptacle · gouged · Nov 15, 2022 · N926SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR - EXTERIOR HANDLE RECESS GOUGED SEVERAL PLACES (C-CHECK RO 1/9/2023) INSTALLED NEW CARGO DOOR HANDLE RECESS REF DWG # 601R35027 REV AY, CRJ200 SRM 51-42-21 REV 39: MAR 10-2021.LEAK CHECK GOOD C/W 51-900-1003-SKY
- [SDR SWIA202265276](https://openairdocs.org/sdr/SWIA202265276.md): None · reads low · Apr 6, 2022 · N926SW · Cndair CL6002C10 · Engine Oil Quantity
  > L ENG OIL PRESS WARNING IN FLIGHT. C/W QRH, SHUT DOWN ENGINE IN FLIGHT. RETURNED TO FIELD. (FLIGHT 5375 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24617621 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE THE FOLLOWING CAMPS FOR WORK PERFORM
- [SDR SWIA2021071959586](https://openairdocs.org/sdr/SWIA2021071959586.md): Pan · corroded · Jul 5, 2021 · N926SW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR BOTTOM PAN, INNER SPLICE ANGLE IS CORRODED. (FILED CLOSED) REMOVED AND REPLACED SERVICE DOOR BOTTOM PAN, INNER SPLICE ANGLE (P/N 601R38304-187) IN REF TO SRM 51-42-06. FABRICATED NEW PART IN REF TO DWG 601R38304, SRM 51-24-06, AND 51-24-21.
- [SDR SWIA2021071959588](https://openairdocs.org/sdr/SWIA2021071959588.md): Skin · dented · Jul 1, 2021 · N926SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR HAS A DENT ON THE OUTER SKIN, 14" FROM FWD EDGE AND 30" FROM TOP OF DOOR. (FILED CLOSED) PERFORMED PERMANENT REPAIR TO PASSENGER DOOR DENT ON OUTER SKIN, 14" FROM FWD EDGE AND 30" FROM TOP OF DOOR. REPAIR PERFORMED IN ACCORDANCE WITH REO

Next page: https://openairdocs.org/aircraft/N926SW/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 = 'N926SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N926SW/reports

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