# Service difficulty reports: N964SW

A list on [N964SW](https://openairdocs.org/aircraft/N964SW.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 · 171 reports

- [SDR SWIA20251223031](https://openairdocs.org/sdr/SWIA20251223031.md): Stringer · corroded · Oct 31, 2025 · N964SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > UNDER FLOOR FROM BS 280 TO 409, S23R WAS CORRODED. REPAIRED STRINGER 23R FROM BS 280 - 349 IAW SRM 53-00-03-02, SRM 51-42-06, & 51-42-21.
- [SDR SWI2025F01867](https://openairdocs.org/sdr/SWI2025F01867.md): Frame · corroded · Oct 24, 2025 · N964SW · Cndair CL6002B19 · Fuselage Main, Frame
  > MAIN CABIN FRAME BS 333 BETWEEN S20R - 25L WAS CORRODED. REMOVED AND REPLACED THE FRAME SECTION IAW SRM 51-42-06, AND 51-42-21.
- [SDR SWI2025F01866](https://openairdocs.org/sdr/SWI2025F01866.md): Floor Support · corroded · Oct 24, 2025 · N964SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT HAS CORROSION FROM BS 409+128 TO 559, RBL 40. COMPLIED WITH REO 601R-53-41-3372 FOR THE REPAIR OF THE FLOOR SUPPORT. BS 409 - 559, RBL 40.
- [SDR SWIA202512230024](https://openairdocs.org/sdr/SWIA202512230024.md): Floor Support · corroded · Oct 24, 2025 · N964SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SILL STRUCTURE HAS CORROSION FROM FS 409.00 TO FS 559.00 LBL 40. COMPLIED WITH REO 601R-53-41-3371 FOR REPAIR OF THE FLOOR SILL STRUCTURE
- [SDR SWI2025F01865](https://openairdocs.org/sdr/SWI2025F01865.md): Frame · corroded · Oct 22, 2025 · N964SW · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 589 LOWER FLANGE WAS CORRODED AND PEELING PAINT FROM JUST UNDER CARGO DOOR SILL TO STRINGER 20R IN SEVERAL AREAS. REMOVED AND REPLACED THE FRAME BS 589, S20R - S20L IAW SRM 51-42-06, & 51-42-21.
- [SDR SWI2025F01864](https://openairdocs.org/sdr/SWI2025F01864.md): Frame · corroded · Oct 22, 2025 · N964SW · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 605 HAS CORROSION AND BARE METAL ON FWD SIDE OF FRAME & UPPER SURFACE OF LOWER FLANGE FROM JUST BELOW CARGO DOOR SILL TO S23R. R & R FRAME SECTOR BS 605, FROM S20R - 20L INSTALLED & FRAME SECTOR BS 605.00 FROM STRINGERS 17L - 20L. INSTALLED SRM 51-42-06,
- [SDR SWIA202512230022](https://openairdocs.org/sdr/SWIA202512230022.md): Frame · corroded · Oct 22, 2025 · N964SW · Cndair CL6002B19 · Fuselage Main, Frame
  > UPPER FLANGE OF BS 589 HAS CORROSION ON UPPER SURFACE FROM S25L - S26R. R & R FRAME SECTION AT BS 589 FROM S25L - S26R IAW SRM 51-42-06
- [SDR SWIA202266415](https://openairdocs.org/sdr/SWIA202266415.md): None · damaged · Jul 16, 2022 · N964SW · Cndair CL6002B19 · Ailerons
  > THE L-H WING INBD FLAP, THE MID LEADING EDGE VANE CAP, REQUIRES REPLACEMENT, PART # 601R14303-51 (C-CHECK RO 8/31/2022) / REMOVED AND REPLACED VANE CAP REF CRJ 200 SRM 51-42-13 AND DWG 601R14302, REV E, / L-H WING INBD FLAP, THE MID LEADING EDGE VANE
- [SDR SWIA202266414](https://openairdocs.org/sdr/SWIA202266414.md): None · damaged · Jul 16, 2022 · N964SW · Cndair CL6002B19 · Ailerons
  > THE L-H WING INBD FLAP, THE OUTBD LEADING EDGE VANE CAP, REQUIRES REPLACEMENT, PART # 601R14303-43 (C-CHECK RO 8/31/2022) REMOVED AND REPLACED VANE CAP REF CRJ 200 SRM 51-42-13 AND DWG 601R14302, REV E / L-H WING INBD FLAP, THE OUTBD LEADING EDGE VANE C
- [SDR SWIA202266413](https://openairdocs.org/sdr/SWIA202266413.md): None · damaged · Jul 16, 2022 · N964SW · Cndair CL6002B19 · Ailerons
  > THE L-H WING INBD FLAP, THE INBD LEADING EDGE VANE CAP, REQUIRES REPLACEMENT, PART # 601R14303-53 (C-CHECK RO 8/31/2022) / REMOVED AND REPLACED VANE CAP REF CRJ 200 SRM 51-42-13 AND DWG 601R14302, REV E / L-H WING INBD FLAP, THE INBD LEADING EDGE VAN
- [SDR SWIA202266412](https://openairdocs.org/sdr/SWIA202266412.md): None · worn · Jul 14, 2022 · N964SW · Cndair CL6002B19 · Ailerons
  > RH WING INBD FLAP VANE, MID-OUTBD LEADING EDGE SKIN WORN AREASREMOVED AND INSTALLED NEW THE RH WING INBOARD FLAP VANE MID-OUTBOARD LEADING EDGE SKIN REF CRJ 200 SRM 51-42-13 WITH DRAWING 601R14302 REV E FOR FASTENER CALL OUT. COMPLIED WITH TASK CARD 51-900-10
- [SDR SWIA202266411](https://openairdocs.org/sdr/SWIA202266411.md): None · worn · Jul 14, 2022 · N964SW · Cndair CL6002B19 · Ailerons
  > RH WING INBD FLAP VANE, INBD LEADING EDGE SKIN WORN AREAS (C-CHECK RO 8/31/2022) REMOVED AND INSTALLED NEW THE RH WING INBOARD FLAP VANE INBOARD LEADING EDGE SKIN REF CRJ 200 SRM 51-42-13 WITH DRAWING 601R14302 REV E FOR FASTENER CALL OUT. COMPLIED WITH
- [SDR SWIA202266422](https://openairdocs.org/sdr/SWIA202266422.md): None · corroded · Jul 8, 2022 · N964SW · Cndair CL6002B19 · Doors
  > CORROSION FOUND ON PAX DOOR UPPER STOP BRACKET ASSY (C-CHECK RO 8/31/2022) REMOVED AND REPLACED BRACKET IAW CRJ200 SRM 51-42-06
- [SDR SWIA202266410](https://openairdocs.org/sdr/SWIA202266410.md): None · corroded · Jul 7, 2022 · N964SW · Cndair CL6002B19 · Doors
  > CORROSION FOUND ON PAX DOOR DD4 INTERCOSTAL BETWEEN FS 339 AND FS 347.25 (C-CHECK RO 8/31/2022) PAX DOOR DD4 INTERCOSTAL BETWEEN FS 339 AND FS 347.25 HAS INTERGRANULAR CORROSION IN THE RADIUS OF PART, OUT OF LIMITS OF CRJ200 SRM 52-00-00 REMOVED PAX DOO
- [SDR SWIA202266409](https://openairdocs.org/sdr/SWIA202266409.md): None · corroded · Jul 7, 2022 · N964SW · Cndair CL6002B19 · Doors
  > CORROSION FOUND ON PAX DOOR FWD BOTTOM CORNER INSIDE FLANGE (C-CHECK RO 8/31/2022) REMOVED CORROSION ON PAX DOOR FWD BOTTOM CORNER REF CRJ200 SRM 51-21-06 EVALUATED DAMAGE / CORROSION ON MORE THAN 2 ELEMENTS ON PAX DOOR FWD BOTTOM CORNER FOUND TO BE O
- [SDR SWIA202266408](https://openairdocs.org/sdr/SWIA202266408.md): None · corroded · Jul 6, 2022 · N964SW · Cndair CL6002B19 · Doors
  > CORROSION FOUND ON PAX DOOR FWD FORMER AT FS 311.75 (C-CHECK RO 8/31/2022) REMOVED AND INSTALLED NEW PAX DOOR FWD FORMER AT FS 311.75 IAW DWG 601R31702 REV -N, CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO LEAKS N
- [SDR SWIA202266407](https://openairdocs.org/sdr/SWIA202266407.md): None · damaged · Jul 6, 2022 · N964SW · Cndair CL6002B19 · Doors
  > REPLACE THE AFT FORMER ON PAX DOOR.( FORMER HAS A PREVIOUS REPAIR AND CUT OUT.) (C-CHECK RO 8/31/2022) REMOVED AND INSTALLED NEW PAX DOOR AFT FORMER AT FS 347.25 REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG 601R31702 REV: -N. COMPLIED WITH 51-9
- [SDR SWIA202266406](https://openairdocs.org/sdr/SWIA202266406.md): None · corroded · Jul 5, 2022 · N964SW · Cndair CL6002B19 · Doors
  > CORROSION FOUND ON UPPER AND LOWER SURFACES OF PAX DOOR INTERCOSTAL DD4 BETWEEN FS 320 AND FS 338 (C-CHECK RO 8/31/2022) REMOVED AND: INSTALLED PAX DOOR DD4 INTERCOSTAL REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG 601R31207 REV -N,COMPLIED WITH
- [SDR SWIA202266405](https://openairdocs.org/sdr/SWIA202266405.md): None · corroded · Jul 1, 2022 · N964SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON INTERCOSTAL DD6 BETWEEN FS 320 AND FS 338 (C-CHECK RO 8/31/2022) BLENDED INTERCOSTAL DD6 BETWEEN FS 320 AND FS 338 REF CRJ 200 SRM 51-21-06 FOUND TO BE OUT OF LIMITS REF CRJ200 SRM 52-00-00. REMOVED AND INSTALLED FORMER AT FS 329 BET
- [SDR SWIA202266404](https://openairdocs.org/sdr/SWIA202266404.md): None · corroded · Jul 1, 2022 · N964SW · Cndair CL6002B19 · Fuselage Structure (General)
  > CORROSION FOUND ON FRAME AT FS 327.763 BETWEEN INTERCOSTALS DD4 AND DD5 (C-CHECK RO 8/31/2022) BLENDED FRAME AT FS 327.763 BETWEEN INTERCOSTALS DD4 AND DD5 REF CRJ 200 SRM 51-21-06 FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 52-00-00. REMOVED AND: INST
- [SDR SWIA202266403](https://openairdocs.org/sdr/SWIA202266403.md): None · damaged · Jul 1, 2022 · N964SW · Cndair CL6002B19 · Ice/Rain Protection System
  > LH ENGINE COWL ANTI ICE DUCT BRACKETS DAMAGED *FLAGGED (C-CHECK RO 8/31/2022) REMOVED AND REPLACED 3EA NEW BRACKETS P/N 228-50055-123 REF CRJ200 SRM 51-40-11 AND FABRICATED, LOCATED AND DRILLED, APPLIED THE FINISH AND WET INSTALLED THE REPAIR FOR THE L-
- [SDR SWIA202266402](https://openairdocs.org/sdr/SWIA202266402.md): None · worn · Jun 29, 2022 · N964SW · Cndair CL6002B19 · Elevator, Plate/Skin
  > *RH HORIZONTAL STAB ELEVATOR HINGE FITTING AT RBL 55.8865 HAS WEAR MARKS/DAMAGE (C-CHECK RO 8/31/2022) / BLENDED WITHIN LIMITS REF REO 601R-55-11-723 REV -- DATE 2022-07-09. RH HORIZONTAL STAB ELEVATOR HINGE FITTING AT RBL 55.8865. COMPLIED WITH TASK
- [SDR SWIA202266401](https://openairdocs.org/sdr/SWIA202266401.md): None · worn · Jun 29, 2022 · N964SW · Cndair CL6002B19 · Elevator, Plate/Skin
  > *RH HORIZONTAL STAB ELEVATOR HINGE FITTING AT RBL 24.4884 HAS WEAR MARKS/DAMAGE (C-CHECK RO 8/31/2022) / BLENDED WITHIN LIMITS REF REO 601R-55-11-723 REV -- DATE 2022-07-09 / RH HORIZONTAL STAB ELEVATOR HINGE FITTING AT RBL 24.4884. COMPLIED WITH 51-90
- [SDR SWIA202266400](https://openairdocs.org/sdr/SWIA202266400.md): None · worn · Jun 29, 2022 · N964SW · Cndair CL6002B19 · Elevator, Plate/Skin
  > *LH HORIZONTAL STAB ELEVATOR HINGE FITTING AT LBL 55.8865 HAS WEAR MARKS/DAMAGE (C-CHECK RO 8/31/2022) / BLENDED WITHIN LIMITS REF REO 601R-55-11-723 REV -- DATE 2022-07-09. LH HORIZONTAL STAB ELEVATOR HINGE FITTING AT LBL 55.8865. COMPLIED WITH TASK C
- [SDR SWIA202266399](https://openairdocs.org/sdr/SWIA202266399.md): None · crushed · Jun 28, 2022 · N964SW · Cndair CL6002B19 · Doors
  > *FS621.00 CARGO AFT MID DOOR TRACK APPROX. STRG 13LH CRUSHED (MARKED) (C-CHECK RO 8/31/2022) EVALUATED DENTED TRACK FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 53-61-23 AND 53-00-00. REMOVED AND INSTALLED NEW TRACK P/N 601R3066-5 REF CRJ 200 SRM 51-42-0
- [SDR SWIA202266398](https://openairdocs.org/sdr/SWIA202266398.md): None · crushed · Jun 28, 2022 · N964SW · Cndair CL6002B19 · Doors
  > *FS574.00 CARGO FWD MID DOOR TRACK APPROX. STRG 13LH CRUSHED (MARKED) (C-CHECK RO 8/31/2022) REPLACED AND INSTALLED NEW CARGO FWD MID DOOR TRACK AT FS574.00 TRACK REF DRAWING 601R35207 REV:-W, DRAWING 601R35065 REV: B AND CRJ200 SRM 51-42-06 SEE CONTI
- [SDR SWIA202266397](https://openairdocs.org/sdr/SWIA202266397.md): None · corroded · Jun 27, 2022 · N964SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *FS409.00+128 €“ FS559.00 RH PRESSURE FLOOR SILL PANEL HAS SEVERAL AREAS OF CORROSION (MARKED) (C-CHECK RO 8/31/2022) REPAIRED RH PRESSURE FLOOR SILL PANEL AT FS409.00+128 €“ FS559.00 REF. REO 601R-53-41-666 REV-C DATED: 2012-11-06 & REO 601R-53-41-3
- [SDR SWIA202266396](https://openairdocs.org/sdr/SWIA202266396.md): None · corroded · Jun 27, 2022 · N964SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *FS409.00+128 €“ FS559.00 LH PRESSURE FLOOR SILL PANEL HAS SEVERAL AREAS OF CORROSION (MARKED) (C-CHECK RO 8/31/2022) REMOVED CORROSION ON FS409.00+128 €“ FS559.00 LH PRESSURE FLOOR SILL PANEL REF REO 601R-53-41-666 REV -C DATED: 2012-11-06. REO 601
- [SDR SWIA202266395](https://openairdocs.org/sdr/SWIA202266395.md): None · corroded · Jun 27, 2022 · N964SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > *FS349.00 STRG 15LH INTERCOSTAL TIE TO THE DOOR FRAME, CORRODED (MARKED) (C-CHECK RO 8/31/2022) REMOVED AND REPLACED GUSSET WITH FABRICATED GUSSET P/N 601R38312-41 OUT OF 7075T-6 PO:T58030. REF CRJ 200 SRM 51-42-06 AND PER DWG. N0. 601R38312 REV-H. CO
- [SDR SWIA202266421](https://openairdocs.org/sdr/SWIA202266421.md): None · corroded · Jun 24, 2022 · N964SW · Cndair CL6002B19 · Doors
  > *PAX DOOR HAS CORROSION ON ATTACH SURFACE FOR TOP STEP. ARE MARKED. (C-CHECK RO 8/31/2022) REMOVED DAMAGED PAX DOOR TOP STEP LANDING AND INSTALLED NEW PART P/N 601R317075-3 REF CRJ 200 SRM 51-42-06, FOR COMPLETE DETAILS OF WORK PERFORMED SEE ATTACHED CO
- [SDR SWIA202266420](https://openairdocs.org/sdr/SWIA202266420.md): None · corroded · Jun 24, 2022 · N964SW · Cndair CL6002B19 · Doors
  > *PAX DOOR HAS CORROSION ON ATTACH ANGLE FOR BOTTOM STEP. (C-CHECK RO 8/31/2022) REMOVED DAMAGED PAX DOOR BOTTOM STEP ANGLE AND INSTALLED NEW ANGLE REF CRJ 200 SRM 51-42-06, FOR COMPLETE DETAILS OF WORK PERFORMED SEE ATTACHED CONTINUATION CARD.
- [SDR SWIA202266394](https://openairdocs.org/sdr/SWIA202266394.md): None · dented · Jun 24, 2022 · N964SW · Cndair CL6002B19 · Wing Structure
  > *DENT NOTED ON L/H INBD GRND SPOILER UPPER SKIN (MARKED) (C-CHECK RO 8/31/2022) DENT ON LH INBOARD GROUND SPOILER REPAIRED WITH REF REO 601R-57-71-586 REV --, DATED 2022-06-30. ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1003-SKY AND M-337 F
- [SDR SWIA202266424](https://openairdocs.org/sdr/SWIA202266424.md): None · corroded · Jun 22, 2022 · N964SW · Cndair CL6002B19 · Aileron Tabs
  > *LEFT WING, OUTBD FLAP, OUTBD ACTUATOR WING ATTACH HARDWARE IS CORRODED. (MARKED) (C-CHECK RO 8/31/2022) LH OUTBD FLAP, OUTBOARD FLAP ACTUATOR WING ATTATCHMENT CORRODED HARDWARE WAS REPLACED ON MX# 24916069, JOB 27868105, OP 5523
- [SDR SWIA202266423](https://openairdocs.org/sdr/SWIA202266423.md): None · corroded · Jun 22, 2022 · N964SW · Cndair CL6002B19 · Ailerons
  > *RIGHT WING, INBD FLAP, OUTBD FLAP ACTUATOR WING ATTACHMENT HARDWARE CORRODED. (MARKED) (C-CHECK RO 8/31/2022) RH INBD FLAP, OUTBOARD FLAP ACTUATOR WING ATTATCHMENT CORRODED HARDWARE WAS REPLACED ON MX# 24916071, JOB 27868105, OP 5525
- [SDR SWIA202266419](https://openairdocs.org/sdr/SWIA202266419.md): None · corroded · Jun 22, 2022 · N964SW · Cndair CL6002B19 · Aileron Tabs
  > *RIGHT WING, OUTBD FLAP ACTUATOR WING ATTACHMENT HARDWARE CORRODED. (MARKED) (C-CHECK RO 8/31/2022) RH OUTBOARD FLAP ACTUATORS WING ATTATCHMENT CORRODED HARDWARE WAS REPLACED ON MX# 24916072, JOB 27868105, OP 5526 AND MX# 24916073, JOB 27868105, OP 552
- [SDR SWIA202266393](https://openairdocs.org/sdr/SWIA202266393.md): None · bent · Jun 21, 2022 · N964SW · Cndair CL6002B19 · Air Conditioning Doors
  > *GROUND AIR CONDITIONING DOOR HAS FWD AND AFT LANDINGS BENT (C-CHECK RO 8/31/2022) REMOVED AND INSTALLED NEW ANGLE (PN: 601R35226-31) COMMON TO LOW PRESSURE AIR GROUND CONNECTION DOOR SURROUND IAW DWG 601R35226 REV -P, CRJ200 SRM 51-42-06 & CRJ200 SRM 5
- [SDR SWIA202266392](https://openairdocs.org/sdr/SWIA202266392.md): None · stuck · Jun 21, 2022 · N964SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > STUCK SCREW SHANK IN PRESSURE FLOOR SILL (RELATIVE TO FLOOR PANEL 262DRF) (C-CHECK RO 8/31/2022) REMOVED AND REPLACED 1 EA DOME NUT IN PRESSURE FLOOR SILL (RELATIVE TO FLLOR PANEL 262DRF) PER CRJ 200 SRM 51-42-06 AND PERFORM REPAIR PER REO 601R-53-41-3
- [SDR SWIA202266391](https://openairdocs.org/sdr/SWIA202266391.md): None · worn · Jun 20, 2022 · N964SW · Cndair CL6002B19 · Ailerons
  > *EVALUATE RH WING INBD FLAP VANE LEADING EDGE SKING WEAR AREAS (3EA) (C-CHECK RO 8/31/2022) REMOVED AND REPLACED RH WING INBD FLAP VANE, OUTBD LEADING EDGE SKIN P/N 601R14303-44, / REF CRJ 200 SRM 51-42-13 AND DWG 601R14302 REV E. COMPLETED TASK CA
- [SDR SWIA202266390](https://openairdocs.org/sdr/SWIA202266390.md): None · worn · Jun 20, 2022 · N964SW · Cndair CL6002B19 · Ailerons
  > *EVALUATE LH WING INBD FLAP VANE LEADING EDGE SKING WEAR AREAS (3EA) (C-CHECK RO 8/31/2022) REMOVED AND REPLACED LH WING CENTER OB FLAP VANE LEADING EDGE PN 601R14303-51 PER CRJ 200 SRM 51-42-10 AND DWG # 601R14303 REV J AND COMPLIED WITH SKYWEST CARD
- [SDR SWIA202266389](https://openairdocs.org/sdr/SWIA202266389.md): None · cracked · Jun 17, 2022 · N964SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > *FWD EQUIPMENT COMPARTMENT (TRU BAY) HAS A CRACK IN THE LWR WEB NEAR THE L/H ACCESS DOOR AFT END. (C-CHECK RO 8/31/2022) REPAIRED FWD EQUIPMENT COMPARTMENT LWR WEB NEAR THE L/H ACCESS DOOR AFT END. REF REO 601R-53-11-3787 REV -- DATE 2022-07-07 AND GRE
- [SDR SWIA202266416](https://openairdocs.org/sdr/SWIA202266416.md): None · damaged · May 31, 2022 · N964SW · Cndair CL6002B19 · Elevator Tab, Attach Fittings
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: NDT ELEV CTR/OB HING FIT RH - COMPLY WITH 55-340-603 CL600 (CRJ200) RIGHT ELEVATOR CENTER AND OUTBOARD HINGE FITTINGS - DETAILED INSPECTION (MRB 55-21-107), PART NUMBER: -, SERIAL NUMBER: 7868, POSITION: (C-CHECK
- [SDR SWIA202161619](https://openairdocs.org/sdr/SWIA202161619.md): None · damaged · Sep 28, 2021 · N964SW · Cndair CL6002B19 · Doors
  > TRANSFER FROM EAML 741809: REF AML 741587, FOUND DAMAGE TO MCD WHERE DOOR ASSIST SYSTEM CABLE AND PULLEY ATTACH TO AFT SIDE OF DOOR OUT OF LIMITS PER SRM (FLIGHT 5074 - FILED CLOSED) REPAIRED DAMAGE TO PASSENGER DOOR AFT FORMER AND INNER SKIN AT DOOR A
- [SDR SWIA202158126](https://openairdocs.org/sdr/SWIA202158126.md): Handle · malfunctioned · May 8, 2021 · N964SW · Cndair CL6002B19 · Landing Gear Selector
  > ***ACFT DOWN GRADE FROM CAT II PER GMM CHAPTER 2 SECTION 23*** / D: GEAR DISAGREE WITH NOSE WHEEL FAILING TO RETRACT. RAN QRH PROCEDURE AND SUCCESSFULLY EXTENDED GEAR. NOSE DOOR OPEN WARNING MESSAGE PERSISTED. LANDING GEAR MANUAL RELEASE HANDLE WOULD NOT STOW
- [SDR SWIA202157930](https://openairdocs.org/sdr/SWIA202157930.md): Window Frame · cracked · Apr 25, 2021 · N964SW · Cndair CL6002B19 · Passenger Compartment Windows
  > D: SIDEWALL PANEL WINDOW FRAME CRACKED AT 6DC. DAMAGE IS COSMETIC IN NATURE PART IS GOOD FOR CONTINUED SERVICE AT THIS TIME. / C: MCI (FILED CLOSED) REMOVED AND REPLACED SIDEWALL PANEL (WINDOW FRAME) REVEAL ASSEMBLY AT 6DC IN REFERENCE TO CRJ200 CMM
- [SDR SWIA202157929](https://openairdocs.org/sdr/SWIA202157929.md): Window Frame · cracked · Apr 25, 2021 · N964SW · Cndair CL6002B19 · Passenger Compartment Windows
  > D: SIDEWALL PANEL WINDOW FRAME CRACKED AT 6/AB.DAMAGE IS COSMETIC IN NATURE PART IS GOOD FOR CONTINUED SERVICE AT THIS TIME. FIX AT NEXT AVAILABLE OPPORTUNITY, NO LATER THEN NEXT C-CHECK. / C: MCI (FILED CLOSED) REMOVED AND REPLACED SIDEWALL PANEL (W
- [SDR SWIA202157928](https://openairdocs.org/sdr/SWIA202157928.md): Window Frame · cracked · Apr 25, 2021 · N964SW · Cndair CL6002B19 · Passenger Compartment Windows
  > D: SIDEWALL PANEL WINDOW FRAME CRACKED AT 9AB. DAMAGE IS COSMETIC IN NATURE PART IS GOOD FOR CONTINUED SERVICE AT THIS TIME. / C: MCI (FILED CLOSED) REMOVED AND REPLACED SIDEWALL PANEL (WINDOW FRAME) REVEAL ASSEMBLY AT 9AB IN REFERENCE TO CRJ200 CMM
- [SDR SWIA2020091452484](https://openairdocs.org/sdr/SWIA2020091452484.md): Proximity Sensor · out of rig · Sep 14, 2020 · N964SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE. FLIGHT 5812-FILED CLOSED. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 21522858 WITH THE FOLLOWING CORRECTIVE ACTION: COMPLIED WITH THE MLG AND NLG EXTENSION/RETRACTION TEST REFERENCE APPLICABLE STEPS IN AMM. FOUND NLG UPLOCK PROX SENSOR TO
- [SDR SWIA202051338](https://openairdocs.org/sdr/SWIA202051338.md): Unknown · malfunctioned · Jul 14, 2020 · N964SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > BROUGHT GEAR UP NOSE GEAR DID NOT COME UP RAN QRH CHECK LIST RETURNED TO FIELD. FLIGHT 5431 - FILED CLOSED. DEFERRED LANDING GEAR RETRACTIONS SYSTEM PER MEL. MX ACTION COMPLIED WITH, AIRCRAFT DOWNGRADED FROM CAT II. PLACARDS INSTALLED.
- [SDR SWIA2019060545956](https://openairdocs.org/sdr/SWIA2019060545956.md): Strap · corroded · Apr 30, 2019 · N964SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR SUPPORT FS559.0 BETWEEN LBL27 AND O/B FLOOR SILL STRAP HAS CORROSION. (C-CHECK) RO: 06/02/2019 REMOVED AND INSTALLED NEW STRAP P/N: 601R31225-29 IAW SRM.
- [SDR SWIA2019060545955](https://openairdocs.org/sdr/SWIA2019060545955.md): Strap · corroded · Apr 30, 2019 · N964SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR SUPPORT FS559.00 BETWEEN RBL27 AND O/B FLOOR SILL STRAP HAS CORROSION. (C-CHECK) RO: 06/02/2019 REMOVED AND INSTALLED NEW STRAP P/N: 601R31225-29 IAW SRM.

Next page: https://openairdocs.org/aircraft/N964SW/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 = 'N964SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N964SW/reports

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