# Service difficulty reports: N970SW

A list on [N970SW](https://openairdocs.org/aircraft/N970SW.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 SWIA2026072276668](https://openairdocs.org/sdr/SWIA2026072276668.md): Psu · faulted · Jul 22, 2026 · N970SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > ON MLG UP SELECTION, RECEIVED A/SKID INOP CAUTION FOLLOWED BY PARK BRAKE SOV CAUTION. NOTED AN AIRFRAME VIBRATION. MLG LEVER SELECTED IAW SOP, UP BUT FOUND MLG INDS TO BE DOWN & 3 GREEN. ON SELECTING MLG DOWN, CAUTION MESSAGES EXTINGUISHED & LANDED UNEVENTF
- [SDR SWIA2026041877227](https://openairdocs.org/sdr/SWIA2026041877227.md): Skin · cracked · Apr 18, 2026 · N970SW · Cndair CL6002B19 · Wing, Plate/Skin
  > ONE-OFF CRACK TO AFT LOWER WING PLANK, DWG 601R10046, 0300 THK AT CRACK LOCATION AFT EDGE AT WS 45 CRACK IS 0600 LONG AND STARTS FROM AFT EDGE OF AFT LOWER WING PLANK AT WS 450 FLIGHT 6080. COMPLIED WITH PERMANENT REPAIR FOR CRACK DAMAGE AT LT AFT LOWER WIN
- [SDR SWIA2026041676737](https://openairdocs.org/sdr/SWIA2026041676737.md): Skin · cracked · Apr 16, 2026 · N970SW · Cndair CL6002B19 · Wing, Plate/Skin
  > 1-OFF CRACK TO AFT LOWER WING PLANK AFT EDGE AT WS 45. CRACK IS 0.600? LONG AND STARTS FROM AFT EDGE OF AFT LOWER WING PLANK AT WS 45. COMPLIED WITH PERMANENT REPAIR FOR CRACK DAMAGE AT LHS AFT LOWER WING PLANK, AFT EDGE AT WS 45.00 IAW ALL STEPS OF REO 601R-
- [SDR SWIA2026022575724](https://openairdocs.org/sdr/SWIA2026022575724.md): Skin · dented · Feb 25, 2026 · N970SW · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > #2 ENG UPPER CORE COWL WITH EXTERNAL SKIN TOOLING MARKS AND DENTS AT ACUSTIC AREA. COMPLIED WITH CORE COWL DOORS REPAIR OF RUB DAMAGE TO OUTER SKIN NEAR FWD EDGE, REPAIR # SRS104, ON #2 ENG LOWER CORE COWL EXTERNAL SKIN AT ACUSTIC AREA, IAW CRJ200, CMM 71-12
- [SDR SWIA202604175725](https://openairdocs.org/sdr/SWIA202604175725.md): Skin · scratched · Nov 26, 2025 · N970SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA106889-601R-52-31-439 REV. -A 2025-11-20 MXCODEID118398-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 106889DUE TO SCRATCH ON THE OUTSIDE TOP OF THE CARGO DOOR, PER REO 601R-52-31-439 REV. -A 2025-11-20, PERMANENT REPAIR
- [SDR SWIA2025111975726](https://openairdocs.org/sdr/SWIA2025111975726.md): Skin · dented · Nov 19, 2025 · N970SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA84579-REO 601R-53-11-3871. COMPLY WITH PERMANENT REPAIR ON RA ID: 845792+ CM DENT RIGHT SIDE NOSE, ADJACENT TO N/W DOOR. PERMANENT REPAIR IS DUE WITHIN 5650 FLIGHT HOURS FOR THE DENT DAMAGE TO FUSELAGE SKIN BETWEEN FS
- [SDR SWIA2025111700005](https://openairdocs.org/sdr/SWIA2025111700005.md): Hydraulic Line · damaged · Nov 15, 2025 · N970SW · Cndair CL6002B19 · Hydraulic System, Main
  > HYDRAULIC 3 LO PRESS WHEN SELECTING GEAR DOWN. IMMEDIATELY FOLLOWED BY A GEAR DISAGREE. WE CHECKED THE HYDRAULICS AND NOTICED SYSTEM 3 AT 0%. WE RAN THE QRH FOR THE GEAR DISAGREE. WE HAD TO PULL THE EMERGENCY GEAR EXTENSION HANDLE. GEAR CAME DOWN AND LOCKED. L
- [SDR SWI2025F01311](https://openairdocs.org/sdr/SWI2025F01311.md): Warning Message · activated · Sep 14, 2025 · N970SW · Cndair CL6002B19 · Central Warning
  > FLAPS FAIL. ON CLIMB SEQUENCE (FLIGHT 5754 - FILED CLOSED)RESET AND OPERATED FLAPS 5 FUL CYCLES AND COMPETED AD 2009-16-12/10 COMPLIANCE FORM OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES COMPLIED WITH IN ACCORDANCE WITH FIM FMRP CHAPTER 27 RESET PROCEDURE
- [SDR SWI2025F01050](https://openairdocs.org/sdr/SWI2025F01050.md): Warning Message · illuminated · Jul 21, 2025 · N970SW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAP FAIL CAUTION MSG (RESET AND OP FLAPS 5 FULL CYCLES & COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE IN SERVICE FOR 10 FLT CYCLES. COMPLIED WITH IAW FIM FMRP 27 RESET PROCEDURES & AD 2009-06-12 MCI CREATED FOR FULL AD COMPLIANCE BY MCC. CURREN
- [SDR SWI2025F00154](https://openairdocs.org/sdr/SWI2025F00154.md): Warning Message · false activation · Feb 17, 2025 · N970SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > MOMENTARY GEAR DISAGREE WARNING MESSAGE ON GO AROUND. GEAR HANDLE WAS UP. (FLIGHT 5232 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWI202407080552](https://openairdocs.org/sdr/SWI202407080552.md): Packing · failed · Jul 5, 2024 · N970SW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > ON TAKEOFF OUT OF CHICAGO O€™HARE WHEN COMMANDED GEAR UP. GOT GEAR DISAGREE WARNING MESSAGE. NOSE DOOR OPEN WARNING.PERFORMED QRH AND TRRIED TWICE TO BING GEAR UP AND TO NO EVALUATION. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28485614 WITH THE FOLLOWIN
- [SDR SWI2024F00233](https://openairdocs.org/sdr/SWI2024F00233.md): Unknown · fumes · Mar 15, 2024 · N970SW · Cndair CL6002B19 · Air Distribution System
  > FUEL SMELL IN THE FLT DECK AND IN THE CABIN ON GROUND. IN AIR THE SMELL WAS STRONGER AFTER THE TEMPERATURE WAS INCREASED IN THE FLT DECK NOT IN THE CABIN. WENT AWAY AFTER THE TEMPERATURE WAS DECREASED (FLIGHT 5590 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED
- [SDR SWI2024F00110](https://openairdocs.org/sdr/SWI2024F00110.md): Anti-Ice Valve · faulted · Feb 4, 2024 · N970SW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > D:WING OVHT WARNING MESSAGE ON TAXI OUT. COMPLIED WITH EMER 9-2. MESSAGE CLEARED.C:DEFERRED WING ANTI-ICE MODULATING AND SOV RH SIDE PER MEL 30-12-1B. MX ACTION CW. PLACARD INSTALLED.CAT C DUE 2-12-24WING OVHT WARNING MESSAGE ON TAXI OUT. COMPLIED WITH EMER 9-
- [SDR SWIA20240202131](https://openairdocs.org/sdr/SWIA20240202131.md): Unknown · odor · Jan 31, 2024 · N970SW · Cndair CL6002B19 · Air Distribution System
  > WITH THE APU AND PACKS ON, A STRONG SMELL OF GAS BEGAN FILLING THE CABIN BEFORE BOARDING. FUEL VAPOR CAN VISIBLY BE SEEN IN THE CABIN. TURNED OFF AIRCRAFT. (FLIGHT 5278 FILED CLOSED)FEB 01, 2024 STATION: CID--VERIFIED WITH CREW NO ASSOCIATED EICAS MSG PRESENT
- [SDR SWIA2024020100031](https://openairdocs.org/sdr/SWIA2024020100031.md): Unknown · odor · Jan 31, 2024 · N970SW · Cndair CL6002B19 · Air Distribution System
  > WITH THE APU AND PACKS ON, A STRONG SMELL OF GAS BEGAN FILLING THE CABIN BEFORE BOARDING. FUEL VAPOR CAN VISIBLY BE SEEN IN THE CABIN. TURNED OFF AIRCRAFT. (FLIGHT 5278 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS.
- [SDR SWIA2024011500013](https://openairdocs.org/sdr/SWIA2024011500013.md): Unknown · warning message · Jan 13, 2024 · N970SW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > D:AFTER ROTATION ON TAKEOFF RECEIVED WING OVRHT WARNING MESSAGE. RAN QRH AND MESSAGE CLEARED. MESSAGE NEVER RETURNED USINGWING ANTI ICE STDBY.C:MEL 30-12-3BCAT C DUE 23/JAN/24AFTER ROTATION ON TAKEOFF RECEIVED WING OVRHT WARNING MESSAGE. RAN QRH AND MESSAGE CL
- [SDR SWIA2023120600005](https://openairdocs.org/sdr/SWIA2023120600005.md): Unknown · warning message · Dec 5, 2023 · N970SW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > WING OVHT WARNING MESSAGE RECEIVED AFTER TAKEOFF AROUND 2,000 FEET WITH WING AND COWL ANTI ICE SELECTED ON. COMPLETED QRH AND PLACED WING ANTI ICE IN STBY MODE. MESSAGE DID NOT RETURN FOR THE REMAINDER OF FLIGHT WITH STANDBY MODE USED. (FLIGHT 5449 FILED CLOSE
- [SDR SWIA20231020](https://openairdocs.org/sdr/SWIA20231020.md): Unknown · asymetric · Oct 20, 2023 · N970SW · Cndair CL6002B19 · Wing Structure
  > IN CRUISE, AT FL330, AIRSPEED APPROX 270 KIAS, LEFT FLAP INTERMITTENTLY DEPLOYED TO 2. RIGHT FLAP STAYED AT 0. WE COULD FEEL PITCH AND ROLL IN CONTROLS WHEN IT WOULD MOVE TO 2. WOULD CONTINUE INTERMITTENTLY THROUGH DESCENT. WHEN FLAPS SELECTED FOR LANDING,
- [SDR SWIA202305220018](https://openairdocs.org/sdr/SWIA202305220018.md): Landing Gear · warning message · May 18, 2023 · N970SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > UPON TAKEOFF, GEAR DISAGREE AND NOSEDOOR UNSAFE WARNING MESSAGES OCCURRED. NOSE GEAR DID NOT COME UP. FOLLOWED QRH PROCEDURES AND SUCCESSFULLY LOWERED ALL THREE GEAR. NO OVERWEIGHT LANDING. NO OVERSPEED OR SOPM LIMITATIONS WERE EXCEEDED. (FLT 5256 FILED CLO
- [SDR SWIA202305190016](https://openairdocs.org/sdr/SWIA202305190016.md): Unknown · warning message · May 18, 2023 · N970SW · Cndair CL6002B19 · Landing Gear System
  > UPON TAKEOFF, GEAR DISAGREE AND NOSEDOOR UNSAFE WARNING MESSAGES OCCURRED. NOSE GEAR DID NOT COME UP. FOLLOWED QRH PROCEDURES AND SUCCESSFULLY LOWERED ALL THREE GEAR. NO OVERWEIGHT LANDING. NO OVERSPEED OR SOPM LIMITATIONS WERE EXCEEDED. (FLT 5256 FILED OPE
- [SDR SWIA20230112](https://openairdocs.org/sdr/SWIA20230112.md): None · broken · Jan 12, 2023 · N970SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > REMOVE AND REINSTALL CARGO DOOR TO FOM (C-CHECK RO 2/14/2023) REMOVED AND REINSTALLED CARGO COMPARTMENT DOOR. REF. CRJ 200 AMM 52-31-00-400-801. OPERATIONAL TEST GOOD AT THIS TIME.
- [SDR SWIA20230110](https://openairdocs.org/sdr/SWIA20230110.md): None · cracked · Jan 10, 2023 · N970SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > SUPPORT ANGLE FOR RH FLOOR SILL AT FS319 IS CRACKED. (C-CHECK RO 2/14/2023) REPLACED SUPPORT ANGLE AT RH FLOOR SILL FS.319 WITH NEW SUPPORT ANGLE PN 601R31148-73 REF. CRJ 200 SRM 51-42-06 AND DWG #601R31148 REV. AC. CW SKYWEST TASK CARD 51-900-1003-SKY
- [SDR SWIA20230108](https://openairdocs.org/sdr/SWIA20230108.md): None · damaged · Jan 8, 2023 · N970SW · Cndair CL6002B19 · Stabilizer Position Indicating
  > EVALUATE KNICK ON LEFT HASTA SUPPORT DOUBLER. (MARKED) (C-CHECK RO 2/14/2023) BLENDED OUT DAMAGE AND RESTORED FINISH REF REO 601R-55-31-421 REV -- DATED 2023-01-14 C/W TASK CARD 51-900-1003-SKY.
- [SDR SWIA20230107](https://openairdocs.org/sdr/SWIA20230107.md): Hinge · corroded · Jan 7, 2023 · N970SW · Cndair CL6002B19 · Elevator Tab, Attach Fittings
  > UPON REMOVAL ON JOB 27881105 OP 107 CAMP 26030843, FOUND L/H ELEVATOR L/E HINGE FITTING ASSY P/N 600-24043-1 @ ES16.52 TO HAVE PITTING CORROSION IN BEARING BORES OF BOTH HINGE HALVES. REPLACE HINGE FITTING ASSY. (C-CHECK RO 2/14/2023) REMOVED AND REPL
- [SDR SWIA20230106](https://openairdocs.org/sdr/SWIA20230106.md): None · blew out · Jan 6, 2023 · N970SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > R/H WING - TIP FAIRING - LOWER SIDE - BOTTOM FASTENER HOLE FOR WINGTIP PANEL 671BB BLOWN OUT AND NUTPLATE IS MISSING (C-CHECK RO 2/14/2023) PERFORMED CUT OUT REPAIR ON R/H WING - TIP FAIRING - LOWER SIDE FOR WINGTOP PANEL 671BB. REF REO 601R-57-31-1412
- [SDR SWIA20230105](https://openairdocs.org/sdr/SWIA20230105.md): None · elongated · Jan 5, 2023 · N970SW · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings
  > PAX DOOR HINGE - DOOR SIDE - HOLE FOR HINGE PIN RETAINING SPRING ELONGATED (C-CHECK RO 2/14/2023) REMOVED AND INSTALLED NEW PAX DOOR HINGE - DOOR SIDE. REF CRJ-200 SRM 51-42-06 AND SRM 51-42-21. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASKCARD 51-900-100
- [SDR SWIA20230104](https://openairdocs.org/sdr/SWIA20230104.md): None · corroded · Jan 4, 2023 · N970SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD5 AFT CORRODED (C-CHECK RO 2/14/2023) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD5 AFT. REF CRJ-200 SRM 51-42-06 AND DWG 601R31702 REV N. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASKCARD 51-900-1003-SKY. SEE CONTINUATION CARD
- [SDR SWIA20230103](https://openairdocs.org/sdr/SWIA20230103.md): None · corroded · Jan 3, 2023 · N970SW · Cndair CL6002B19 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN RBL 27 - RBL 45 (C-CHECK RO 2/14/2023) REPAIRED FLOOR SUPPORT STRAP AT FS. 559.00 BETWEEN RBL 27 - RBL 45 REF. CRJ200 SRM 51-42-06 & CRJ20 SRM 51-40-11. AND DWG 601R31145 REV M. COMPLIED WITH SKYWEST
- [SDR SWIA202301003](https://openairdocs.org/sdr/SWIA202301003.md): None · corroded · Jan 3, 2023 · N970SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > RH SILL CORRODED APPROX FS319.70 / WL73.50. MARKED WITH GREASE PENCIL (C-CHECK RO 2/14/2023) REMOVED AND REPLACED RH FLOOR SILL AND DOUBLER AT APPROX. FS310 - FS319.70 CRJ200 SRM 51-42-06, REV 39, DATED MAR 10/21. AND DWG# 601R31148, REV AC SEE CONTINUA
- [SDR SWIA2023010003](https://openairdocs.org/sdr/SWIA2023010003.md): None · dented · Jan 3, 2023 · N970SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > EVALUATE DENT ON RH PRESSURE FLOOR SILL PANEL BETWEEN FS 499.00 - 513.00 (C-CHECK RO 2/14/2023) EVALUATED AND REPAIRED DENT ON RH PRESSURE FLOOR SILL PANEL BETWEEN FS 499.00 - 513.00. INSTALLED REPAIR DOUBLE ON RH PRESSURE FLOOR SILL PANEL. REF MHIRJ R
- [SDR SWIA20230102](https://openairdocs.org/sdr/SWIA20230102.md): None · corroded · Jan 2, 2023 · N970SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > AREAS OF CORROSION ON FLOOR SEAT TRACK AT RBL9 BETWEEN FS 473.00 - 589.00 (C-CHECK RO 2/14/2023) REMOVED AND REPLACED FLOOR SEAT TRACK AT RBL9 BETWEEN FS 473.00 - 589.00 WITH NEW, PER CRJ200 AMM 53-01-11-400-802. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA20230100002](https://openairdocs.org/sdr/SWIA20230100002.md): None · cracked · Jan 2, 2023 · N970SW · Cndair CL6002B19 · Fuselage Floor Panel
  > FS 484 AT LBL 36.0 AND LBL 27( CLIPS ARE CRACKED.UNDER FLOOR). (C-CHECK RO 2/14/2023) REMOVED 2EA. CLIPS, LOCATED, DRILLED AND INSTALLED 2EA.CLIPS P/N 601R31171-17 AND FABRICATED PART -1 LH ANGLE OUT OF S6144-14 ANGLE. REF REO 601R-53-41-059 REV-C DATED
- [SDR SWIA20230000102](https://openairdocs.org/sdr/SWIA20230000102.md): None · dented · Jan 2, 2023 · N970SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE AT FS283 BETWEEN STR 24R & 25R HAS TWO EACH DENTS (MARKED WITH TAPE) (C-CHECK RO 2/14/2023) REPAIRED DENT BY COMPLYING WITH REO 601R-51-00-309 REV-A DATED 2017-08-23 AND REO 601R-53-21-3595 REV -- DATE 2023-01-23..SEE CONTINUE CARD FO
- [SDR SWIA20221231](https://openairdocs.org/sdr/SWIA20221231.md): None · corroded · Dec 31, 2022 · N970SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR INTERCOSTAL DD4 MID CORRODED (C-CHECK RO 2/14/2023) REMOVED AND INSTALLED NEW DD4 INTERCOSTAL P/N 601R318081-1 ON PASSENGER DOOR. REF. DWG 601R31702, REV: N, AND CRJ 200 SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY. FOUND TO BE OUT OF LIMITS REF
- [SDR SWIA20221230](https://openairdocs.org/sdr/SWIA20221230.md): None · gouged · Dec 30, 2022 · N970SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR CUT-OUT FRAME FS349.00, REPAIR STRIIP BENT AND GOUGED ST APPROXIMATE STRINGER 12. (C-CHECK RO 2/14/2023) INSTALLED NEW REPAIR STRAP AT FRAME FS349.00 REF GREO 601R-53-22-033 REV C 2007/07/18 REPAIR TYPE 1. AND CRJ 200 SRM 51-42-06. LEAK CHECK A
- [SDR SWIA20221229](https://openairdocs.org/sdr/SWIA20221229.md): Windshield · damaged · Dec 29, 2022 · N970SW · Cndair CL6002B19 · Flight Compartment Windows
  > FO WINDSHIELD FAILS SENSOR RESISTANCE CHECK. (C-CHECK RO 2/14/2023) REMOVED AND INSTALLED COPILOT WINDSHIELD REF. CRJ200 AMM 56-11-01-400-801. COMPLIED WITH 56-220-1000-SKY.OPS CHECK LEAK CHECKS GOOD
- [SDR SWIA20221000229](https://openairdocs.org/sdr/SWIA20221000229.md): None · corroded · Dec 29, 2022 · N970SW · Cndair CL6002B19 · Fuselage Main, Structure
  > *PAX DOOR INTERCOSTAL DD3 MID CORRODED (C-CHECK RO 2/14/2023) AREMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD3 MID. REMOVED AND REINSTALLED FS329.50 FORMER. REF CRJ-200 SRM 51-42-06 AND DWG 601R31702, REV N.LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK
- [SDR SWIA20221223](https://openairdocs.org/sdr/SWIA20221223.md): None · damaged · Dec 23, 2022 · N970SW · Cndair CL6002B19 · Navigation System
  > AFTER REMOVAL OF THE ADF ANTENNA FOUND TOOLING DAMAGE ON THE AIRCRAFT MOUNTING SURFACE (C-CHECK RO 2/14/2023) PERFORMED CUT OUT REPAIR OF ADF ANTENNA MOUNTING SURFACE. REF MHIRJ REO 601R-53-31-1257 REV -- DATED 2023-01-20. COMPLIED WITH SKYWEST TASKCARD
- [SDR SWIA20221222](https://openairdocs.org/sdr/SWIA20221222.md): None · chafed · Dec 22, 2022 · N970SW · Cndair CL6002B19 · Wing Structure
  > *RH AILERON LOWER OUTBD RUB SEAL CHAFFED (C-CHECK RO 2/14/2023) REPLACED RH AILERON LOWER OUTBD RUB SEAL (PANEL) WITH NEW DUE TO BLEND OUT OF LIMITS SEE CONTINUATION CARD FOR WORK DETAILS REF. CRJ 200 SRM 51-42-21 AND DWG #CC670-13000 REV. D. CW 51-900-
- [SDR SWIA20221219](https://openairdocs.org/sdr/SWIA20221219.md): None · damaged · Dec 19, 2022 · N970SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > THERE ARE SIGNS OF DAMAGE ON THE RH NOSE OF THE AIRCRAFT BETWEEN THE ADG DOOR AND THE NLG DOOR. PLEASE PLOT, MAP AND EVALUATE DAMAGE. IF DAMAGE IS FOUND IN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICES AND PROCEDURES. (C-CHECK
- [SDR SWIA20221207](https://openairdocs.org/sdr/SWIA20221207.md): None · chafed · Dec 7, 2022 · N970SW · Cndair CL6002B19 · Ailerons
  > INSTALL LH INBD FLAP TO FACILITATE OTHER MAINTENANCE PER AMM TO FOM. (C-CHECK RO 2/14/2023) INSTALLED LH I/B FLAP REF. CRJ 200 AMM 27-54-01-400-801
- [SDR SWIA202266725](https://openairdocs.org/sdr/SWIA202266725.md): Wire Harness · failed · Nov 3, 2022 · N970SW · Cndair CL6002B19 · Landing Gear System Wiring
  > GEAR DISAGREE AFTER TAKEOFF. NOSE INDICATED DWN. MAIN GEAR HAD WHITE INDICATORS. RAN QRH, MANUAL DEPLOY HANDLE PULLED. SUCCESSFUL GEAR EXTENSION. RETURN TO FIELD (FLIGHT 4737) REF CP 25745965 FOR TROUBLESHOOTING GEAR DISAGREE. REF CP 25750887 FOR DAMAGED
- [SDR SWIA202053021](https://openairdocs.org/sdr/SWIA202053021.md): Windshield · failed · Oct 3, 2020 · N970SW · Cndair CL6002B19 · Flight Compartment Windows
  > LEFT WINDSHIELD SHATTERED AT FL 320. LT WINDSHIELD HEAT CAUTION MESSAGE AT SAME TIME. FILED CLOSED RO 10/3/2020. REMOVED AND REPLACED LT WINDSHIELD WITH SERVICEABLE UNIT, REF AMM. OPERATIONAL CHECK OF WINDSHIELD HEAT WAS FOUND TO BE GOOD, WITH NO DISCREPAN
- [SDR SWIA2019111146753](https://openairdocs.org/sdr/SWIA2019111146753.md): Sensor · out of limits · Nov 11, 2019 · N970SW · Cndair CL6002B19 · Drag Control System
  > LH OTBD GRD SPOILER ALWAYS INDICATES DEPLOYED WITH ASSOCIATED GRD SPOILER FAULT CAS MSG, RESET AND ENGAGED GLD, MESSAGE AND FAULT PERSISTS. (C-CHECK) RO: 11/9/2019 TROUBLESHOT LH OTBD GRD SPOILER ALWAYS INDICATES DEPLOYED WITH ASSOCIATED GRD SPOILER FAULT C
- [SDR SWIA2019111146752](https://openairdocs.org/sdr/SWIA2019111146752.md): Frame · corroded · Nov 11, 2019 · N970SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 574 LBL38 BETWEEN STR 20L-19LCORROSION ON FRAME. (C-CHECK) RO: 11/9/2019 --REMOVED CORROSION ON FS574 FRAME BETWEEN STR20L - 19L "OUT OF LIMITS" --REPAIRED FRAME SECTOR FS574 LBL36 BETWEEN STR20L - STR19L BY FABRICATING AND INSTALLING NEW FRAME AND SPLIC
- [SDR SWIA2019111146751](https://openairdocs.org/sdr/SWIA2019111146751.md): Frame · corroded · Nov 11, 2019 · N970SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 333 BETWEEN STR 25R - 25L CORRODED ON AFT SIDE. (C-CHECK) RO: 11/9/2019 --REMOVED CORROSION FROM THE FS333 FRAME BETWEEN STR25R - STR25L "OUT OF LIMITS"--REMOVED AND REPLACED FS333 FRAME SECTION STR25R - STR25L RESTORED ACCESS AND FINISH. LEAK CHECKS GO
- [SDR SWIA2019111146750](https://openairdocs.org/sdr/SWIA2019111146750.md): Skin · dented · Nov 11, 2019 · N970SW · Cndair CL6002B19 · Spoilers
  > LEFT WING OUTBD GROUND SPOILER HAS DENTS ON TOP SKIN MARKED. (C-CHECK) RO: 11/9/2019 LH OTBD GROUND SPOILER DAMAGE FOUND OUT OF LIMITS. REMOVED AND INSTALLED NEW GROUND SPOILER IAW AMM. CLEARANCE CHECK GOOD. OPERATIONAL TEST GOOD.
- [SDR SWIA2019111146749](https://openairdocs.org/sdr/SWIA2019111146749.md): Thrust Reverser · dented · Nov 11, 2019 · N970SW · Cndair CL6002B19 · Engine Thrust Reverser
  > UPPER TRANSLATING COWL 434AT HAS MULTIPLE EXTERIOR DENTS. (C-CHECK) RO: 11/9/2019 UPPER TRANSLATING COWL 434AT FOUND TO BE OUT OF REPAIABLE LIMITS. ORDERED AND RECEIVED SERVICABLE COWL
- [SDR SWIA2019111146748](https://openairdocs.org/sdr/SWIA2019111146748.md): Skin · dented · Nov 11, 2019 · N970SW · Cndair CL6002B19 · Spoilers
  > L/H WING FLIGHT SPOILER SMALL DENT IN THE CENTER OF THE SPOILER APPROXIMATELY 6 INCHES AFT OF THE SPOILER LEADING EDGE. IT IS AN APPROXIMATELY 1-1/8 INCH DIAMETER CIRCULAR DENT. (C-CHECK) RO: 11/9/2019 DENT WAS FOUND OUT OF LIMITS. REMOVED AND REPLACED THE
- [SDR SWIA2018073144912](https://openairdocs.org/sdr/SWIA2018073144912.md): Downlock · shorted · Jul 31, 2018 · N970SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > AFTER TAKEOFF IN PUB HAD A GEAR DISAGREE WARNING MESSAGE COME ON. (FLT 5065) CLOSED PSEU NOTED S35 NOSE GEAR DOWN LOCK NR 2 SHORTED. REPLACED AND ADJUSTED NOSE GEAR DOWN LOCK IAW AMM. GEAR SWING OPS CHECK GOOD.

Next page: https://openairdocs.org/aircraft/N970SW/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 = 'N970SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N970SW/reports

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